c5	c10	c12	c14	c15	c16	c17	c18	c20	c25	c35	c40	c90	c100	c110	c120	c130	c140	c150	c152	c160	c170	c180	c190	c192	c200	c210	c220	c230	c240	c250	c260	c270	c280	c290	c300	c310a	c310b	c310c	c310d	c314a	c314b	c314c	c314d	c320a	c320b	c320c	c324a	c324b	c324c	c330	c332	c340	c350	c360	c370	c380	c390	c400	c410	c420	c430	c440	c450	c460	c490	c510a	c510b	c510c	c510d	c510e	c510f	c602	c604	c606	c608	c610	c612	c614	c616	c620	c640	c652	c654	c660	eof
2000032800005	20000328	00005	EU  	2000	3	28	20000328SH009    	1	19991127	G	3231	MY20248001	PIN             			AMD   	FALC20	FALCON      	2720302	EU  										LT MLG DOOR	BROKEN          	B			FE6R	O				OTHER                   				O			OTHER                     			LD	LANDING        	1			NM	11	216SA				707	016				AIRCRAFT LANDED AT BOISE, IDAHO WITH THE NOSE AND THE RIGHT MAIN LANDING GEAR EXTENDED WHILE THE LEFT MAIN LANDING GEAR 	REMAINED IN THE RETRACTED POSITION.  INSPECTION OF THE LEFT HAND LANDING GEAR REVEALED THE PIN, PN MY20248-001 WHICH IS 	PART OF THE FORWARD GEAR DOOR LOCK, PN VTS4424, TO BE CORRODED (RUSTED) AT POINT OF ROTATION, AND CRACKED FOR SOME PERIO	D.  PIN FINALLY FAILED.  SUBMITTER STATED THIS MAY HAVE BEEN PREVENTED BY A MORE DETAILED INSPECTION OF THE LANDING GEAR	 DOOR LOCKS.  (X)		2	L	7	2 	4F			 	A7EU    					 
2000032900438	20000329	00438	NM  	2000	3	29	20000328SH018    	1	19991221	G	2421	F2MA712614B1	DUCT            			AMD   	FALC50	FALCON2000  	2730170	NM  										ALTERNATOR INTAK	CRACKED         	B			UO2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	596A	1573 				28				FOUND LEFT ALTERNATOR INTAKE DUCT CRACKED DURING A ROUTINE 600-HOUR ENGINE INSPECTION.  (X)						2	K	7	3 	4F			RT	A50NM   					 
2000040400486	20000404	00486	SW  	2000	4	4	20000329SH042    	1	19991022	G	6210	206010200133	BLADE           			BELL  	206   	206B        	1181511	SW  										MAIN ROTOR	DAMAGED         	B			DFUR	A				UNSCHED LANDING         				O			OTHER                     			NR	NOT REPORTED   	1			SO	09		2769 								MAIN ROTOR BLADE FACTORY INSTALLED WEIGHT DISLODGED DURING OPERATION STRIKING MAIN ROTOR BLADE TIP CAP.  TIP CAP TRAILIN	G EDGE WAS BENT OUTBOARD APPROXIMATELY 30 DEGREES AND APPROXIMATELY ONE INCH OF WEIGHT PROTRUDED THROUGH OUTBOARD END OF	 SPAR.  UPPER AND LOWER MAIN ROTOR BLADE SKIN BALLOONED OUT FROM FORCE OF WEIGHT IMPACT.  MAIN ROTOR BLADE WAS RETURNED 	TO BELL HELICOPTER FOR INVESTIGATION.  (X)			1	G	7	1 	3U			 	H2SW    					 
2000040600063	20000406	00063	CE  	2000	4	6	20000331SH005    	1	19991213	G	2140	HL5508Z	RESISTOR        			CESSNA	402   	402C        	207590R	CE  										HEATER FAN	FAILED          	C				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			CL	CLIMB          	1			NE	01	121PB	4    			1213	402C0507				CREW TURNED ON HEATER PRIOR TO DEPARTURE FROM HYA.  ON CLIMB-OUT, PILOT NOTICED FUNNY SMELL, TURNED OFF HEATER.  PASSENG	ERS INFORMED CREW OF SMOKE IN CABIN.  RETURNED TO HYA FOR UNEVENTFUL LANDING.  MAINTENANCE FOUND HEATER FAN DROP RESISTO	R BURNED.  REMOVED AND REPLACED ASSY, HEATER FAN SYSTEM CHECKS OK.  RELEASED AIRCRAFT BACK TO SERVICE.  (X)				1	L	7	2 	3O			 	A7CE    					 
2000040600064	20000406	00064	CE  	2000	4	6	20000331SH006    	1	19990105	G	3230	99101363	ACTUATOR        			CESSNA	414   	414A        	2075907	CE  										MLG	CONTAMINATED    	D				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			NE	01	135BG					414A0419				PILOT REPORTED RT GEAR DOWN LIGHT DID NOT COME ON IMMEDIATELY AFTER FLIGHT IN SUBFREEZING TEMP.  A BANGING NOISE WAS HEA	RD BEFORE LIGHT CAME ON.  AFTER LANDING, ACFT WAS PARKED FOR SEVERAL HRS IN SUBFREEZING TEMPS AND AT PRE-FLIGHT, RT GEAR	 DOWN LIGHT WAS OUT AND GEAR WARNING LIGHT WAS ON.  ACFT WAS DELIVERED TO MAINT IN ABOVE FREEZING TEMPS AND GEAR OPERATI	ON WAS NORMAL ON JACKS WITH HYD MULE.  ACTUATOR REMOVED AND EMPTIED OF FLUID.  APPROX 1/4 TO 2/3 CUP OF WATER WAS REMOVE	D WITH MIL-H-5606 FLUID.  INVEST SHOWED HYD RESERVOIR SERVICE PORT ON OUTSIDE OF NOSE BAGGAGE BAY WAS MISSING ITS ORIG S	EAL.  SUBMITTER SUSPECTED WATER FROZE IN ACTUATOR AND FORCED INTERNAL DOWNLOCK TO DISENGAGE.  (X)	1	L	7	2 	3O			 	A7CE    					 
2000040600079	20000406	00079	CE  	2000	4	6	20000403SH004    	1	19991109	G	3233		ACTUATOR        			CESSNA	414   	414A        	2075907	CE  										NLG	INOPERATIVE     	D				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			WP	13	5614C					414A0203				NOSE GEAR COLLAPSED ON LANDING CAUSING DAMAGE TO BOTH PROPS, ENGS, AND NOSE STRUCTURE DAMAGE TO BOTTOM OF ACFT FROM RADA	R DOME TO BS 43.0.  NOSE OF THE ACFT WAS PLACED ON A JACK.  NOSE GEAR ACTUATOR WAS LOCKED DOWN.  THERE WAS NO PHYSICAL D	AMAGE TO NOSE GEAR UNLOCKING OF LOCKING SYS.  NOSE GEAR ACTUATOR P/N 9910139-3 REPLACED WITH A SERVICEABLE ACTUATOR.  TH	E SUSPECT ACTUATOR SENT FOR TEAR DOWN ANALYSIS.  FOUND HYD FLUID CONTAMINATED WITH WATER.  UNLOCKING PRESS 750 PSIG; NOR	MAL ULOCKING PRESS 250-400 PSIG.  THIS CAUSED BY LARGE AMTS OF DIRT AND GRIME ON LOCKING RAM P/N 15211906-5.  PART HAS T	O BE ABLE TO SHIFT FREELY.  ENGS AND PROPS REPLACED.  DAMAGE TO NOSE STRUCTURE REPAIRED.  ACFT RETURNED TO SERVICE.  (X)	1	L	7	2 	3O			 	A7CE    					 
2000040500024	20000405	00024	NE  	2000	4	5	20000404SH006    	1	19991104	G	2822	6550453	PUMP            			SKRSKY	S64   	CH54A       	8142501	NE  										FUEL BOOST	INOPERATIVE     	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	25	44094					6718421				UNIT WAS INOPERABLE.  RETURNED TO STOCK.  BENCH CHECKED BAD, WINDING SHORTED, LEAKING AROUND ELECTRICAL LEADS.  REPLACED	 COMPLETE UNIT WITH AN EXTERNALLY MOUNTED FUEL BOOST PUMP.  (X)					2	G	7	2 	4U			 	H16NM   					 
2000040600088	20000406	00088	NE  	2000	4	6	20000404SH014    	2	19991218	G	7250	50A096	BEARING         								PWA   	4460  	PW4460      	 	NE  					NR 4 MAIN	FAILED          	H				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CR	CRUISE         	1			SW	99	B2171	9116 					P723940			DURING CRUISE, LOUD BANG AND VIBRATION.  ENGINE SHUTDOWN.  DISASSEMBLY INSPECTION REVEALED FRACTURED NR 2 MAIN BEARING, 	EXTENSIVE HPC/HPT/LPT DAMAGE AND FIRE DAMAGE NR 2 BEARING AREA.  FAILED MATERIAL SENT TO P&W E.H. FOR ANALYSIS.   (X)										4	F			E24NE				 
2000040600089	20000406	00089	CE  	2000	4	6	20000404SH016    	1	19991216	G	3110	B904ANDB906	HOSE            			CESSNA	185   	A185F       	2072821	CE  										COCKPIT	DISINTEGRATED   	B			YUER	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03	9344N	510  				18504334				FOUND HOSE .3750 INCH AND .25 INCH (AS REQUIRED BY SUCTION SYSTEM/INSTRUMENTS) TO HAVE ITS RED INNER SLEEVE COMPONENT DI	SINTEGRATED AND HOSE BLOCKED.  SECTIONS OF BLACK OUTER SLEEVE WOULD ALSO DISINTEGRATE ON CONTACT.  ORIG CAUSE FOR INVEST	 WAS VARIOUS SUCTION DISCREPANCIES INCLUDING SUCTION INST INOP.  POSSIBLE CAUSE, HOSE IS OF POOR QUALITY THAT IT WILL NO	T STAND UP TO AGE.  TO PREVENT RECURRENCE, ALL HOSE OF THIS TYPE SHOULD BE REPLACED UNLESS HOSE CAN BE TRACED TO A BAD B	ATCH USED ON SPECIFIC S/N OR NUMBER RANGES.  FOUND NO SIGNS OF EXTERNAL IMPETUS TO SUSPECT A CAUSE OF EARLY DECAY SUCH A	S PETROLEUM PRODUCTS, HEAT OR ULTRA VIOLET RAYS (ALL HOSES UNDER INST PANEL).(X)	1	H	7	1 	3O			 	3A24    					 
2000040600090	20000406	00090	SO  	2000	4	6	20000404SH019    	1	19991208	G	7120	6711949	MOUNT           			PIPER 	PA28  	PA28R180    	7102809	SO  	LYC   	O360  	IO360B1E    	41514	EA  					ENGINE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	01	7625J	4103 				28R31020	L579651A			DURING ANNUAL INSPECTION, NOTICED A RUST COLORED AREA ON THE ENG MOUNT, LOWER CROSSTUBE, ON LT SECTION.  CLOSER INSPECTI	ON REVEALED TUBE WAS CRACKED ALMOST ALL THE WAY AROUND.  THE ENGINE WAS REMOVED AND THE CRACKED AREA WELDED.  NOTE:  SUB	MITTER STATED IN THE NEXT HANGAR ANOTHER PA 28R-180 IN FOR A 100-HR INSPECTION AND FOUND MOUNT CRACKED IN SAME AREA.  (X	)			1	L	7	1 	3O	3	O	 	2A13    	1E10				 
2000040600091	20000406	00091	SO  	2000	4	6	20000404SH020    	1	19991208	G	7120	6711949	MOUNT           			PIPER 	PA28  	PA28R180    	7102809	SO  	LYC   	O360  	IO360B1E    	41514	EA  					ENGINE	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	01	251DB	3487 				28R30426	L466551A			DURING A 100-HOUR INSPECTION, FOUND THE ENGINE MOUNT CRACKED, LOWER CROSS MEMBER, LEFT SIDE.  REMOVED ENGINE AND FOUND T	HE TUBE CRACKED ALMOST ALL THE WAY AROUND.  WELDED.  (X)					1	L	7	1 	3O	3	O	 	2A13    	1E10				 
2000040600124	20000406	00124	CE  	2000	4	6	20000405SH021    	1	19990818	G	3230	12802091	PIN             			CESSNA	182   	R182        	2072734	CE  										DOWNLOCK	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	5482T	3435 			12802403F	R18201877				WHILE PERFORMING RECURRENT INSP OF NOSE GEAR DOWNLOCK PINS LOCATED IN ACTUATOR BEARING END, FOUND DOWNLOCK PINS IN AN UN	AIRWORTY CONDITION.  LT PIN LOOSE AND ROTATING FREELY, RT PIN BROKEN WITH ITS WORKING END WIGGLING FREE, FITTED END STIL	L SEATED.  FOUND NG DRAG LINK (ACTUATOR) ATTACH BRACKET PN 2243309-4 CRACKED THRU ONE OF THE UPPER RIVET HOLES.  WHILE R	EMOVING CRACKED DRAG LINK BRACKET, INSP REVEALED CRACKS IN SHEET METAL.  NG ACT MODIFIED, SEB 95-20, BY USING CESSNA ACT	 PIN SERVICE KIT NR SK210-115.  MODIFIED NG ACT RE-INSTALLED ON ACFT USING NEW (NAS464P7-36) BOLT.  OPER CHECK, RIGGING,	 AND FINAL INSP OF NG ACT PERFORMED WITH NO FURTHER DISCOVERY OF FAILURES.  (X)	1	H	7	1 	3O			RT	3A13    					 
2000040600128	20000406	00128	SO  	2000	4	6	20000405SH026    	2	19991220	G	7414	S6RN1225	POINTS          			CESSNA	182   	182Q        	2072732	CE  	CONT  	O470  	O470U       	17026	SO  					RT MAGNETO	SHORTED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	735ZT					18265821				AFTER UNDERGOING A 500-HOUR MANDATORY AD INSPECTION, THESE MAGNETOS WERE RETURNED TO CUSTOMER RE-INSTALLED AND TIMED TO 	ENGINE PER MFG SPECS.  ACFT WENT THROUGH A NORMAL PRE-FLIGHT AND RUN-UP, THEN FLOWN FOR 1 HR AT NORMAL CRUISE.  IN THIS 	LENGTH OF TIME, THE EGT STARTED RISING ALONG WITH ENG ROUGHNESS.  AFTER RETURN TRIP AND RECHECK MADE, FOUND RT MAG SHORT	ED AND POINTS CLOSED.  THE LT MAG TIMING WAS ADVANCED BEYOND MFG''S SPECS.  DETERMINED BOTH FELT PADS HAD COME LOOSE AND	 ALLOWED POINTS TO CLOSE.  MAGS WERE RETURNED TO CUSTOMER, YELLOW TAGGED, AND TORQUE SEALED.  (X)		1	H	7	1 	3O	3	O	NT	3A13    	E273				 
2000040600129	20000406	00129	SO  	2000	4	6	20000405SH027    	2	19991220	G	7414	S6RN1225	POINTS          			CESSNA	182   	182Q        	2072732	CE  	CONT  	O470  	O470U       	17026	SO  					LT MAGNETO	OUT OF TOLERANCE	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	735ZT					18265821				AFTER UNDERGOING A 500-HOUR MANDATORY AD INSPECTION, THESE MAGNETOS WERE RETURNED TO CUSTOMER RE-INSTALLED AND TIMED TO 	ENGINE PER MFG SPECS.  ACFT WENT THROUGH A NORMAL PRE-FLIGHT AND RUN-UP, THEN FLOWN FOR 1 HR AT NORMAL CRUISE.  IN THIS 	LENGTH OF TIME, THE EGT STARTED RISING ALONG WITH ENG ROUGHNESS.  AFTER RETURN TRIP AND RECHECK MADE, FOUND RT MAG SHORT	ED AND POINTS CLOSED.  LT MAG TIMING WAS ADVANCED BEYOND MFG''S SPECS.  DETERMINED BOTH FELT PADS HAD COME LOOSE AND ALL	OWED POINTS TO CLOSE.  MAGS WERE RETURNED TO CUSTOMER, YELLOW TAGGED, AND TORQUE SEALED.  (X)		1	H	7	1 	3O	3	O	NT	3A13    	E273				 
2000040600146	20000406	00146	NE  	2000	4	6	20000406SH008    	2	19991207	G	7261	230307203	SEAL            			BOLKMS	117   	BK117A3     	5626015	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					CSD	LEAKING         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	1140H	45   				7078				OUTPUT SEAL LEAKING.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U	3	U	 	H13EU   	E5NE				 
2000040600148	20000406	00148		2000	4	6	20000406SH010    	4	19991210	G	2211	11788292	COMPUTER        																	SPAS	DAMAGED         	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05										RECEIVED DAMAGED FROM AEC.  SEVERAL BENT AND AT LEAST ONE BROKEN PIN ON J949 RECEPT.  REMOVED AND REPLACED. (X)																			 
2000040600149	20000406	00149	SW  	2000	4	6	20000406SH011    	1	19990927	G	5210	1008401	LATCH           			BELL  	230   	230         	1182149	SW  										CREW DOOR	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV					23019				WORN CAM.  REMOVED AND REPLACED. (X)						1	G	7	2 	3U			NC	H9SW    					 
2000041100103	20000411	00103		2000	4	11	20000406SH012    	4	19990907	G	3120	M8005BATT	CLOCK           			BELL  	230   	230         	1182149	SW  										COCKPIT	FAILED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	4UV					23019				CLOCK WILL NOT RETAIN MEMORY.  REMOVED AND REPLACED. (X)						1	G	7	2 	3U			NC	H9SW    					 
2000040600150	20000406	00150	SW  	2000	4	6	20000406SH013    	1	19990907	G	2432		BATTERY         			BELL  	230   	230         	1182149	SW  										BATTERY BAY	DISCHARGED      	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	4UV					23019				BATTERY DEAD.  REMOVED AND REPLACED. (X)						1	G	7	2 	3U			NC	H9SW    					 
2000040600151	20000406	00151	EU  	2000	4	6	20000406SH014    	1	19991216	G	6320	0750111091	SEAL            			UROCOP	EC135 	EC135P1     	8680990	EU  										M/R GEARBOX	LEAKING         	B			TI1R	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	05	911SV					0070				SEAL LEAKING.  REMOVED AND REPLACED. (X)						1	G	7	2 	3U			O	H88EU   					 
2000040600152	20000406	00152		2000	4	6	20000406SH015    	4	19991230	G	3423	C2300DL4B	COMPASS         			BELL  	206   	206L        	1181522	SW  										COCKPIT	LEAKING         	B			TI1R	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	05	206MH	112  				45426				MAGNETIC COMPASS LEAKED FLUID.   REMOVED AND REPLACED. (X)						1	G	7	1 	3U			 	H2SW    					 
2000040600153	20000406	00153	EU  	2000	4	6	20000406SH016    	1	19991215	G	6700	L713M2144101	BELLOWS         			UROCOP	EC135 	EC135P1     	8680990	EU  										MAIN ROTOR	DAMAGED         	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	911SV	384  				0070				BELLOWS ASSEMBLY UNSTICHED.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			O	H88EU   					 
2000040600154	20000406	00154	EU  	2000	4	6	20000406SH017    	1	19991022	G	2510	L311M1038205	PIN             			UROCOP	EC135 	EC135P1     	8680990	EU  										CYCLIC	BROKEN          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	911SV	307  				0070				PIN BROKEN.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			O	H88EU   					 
2000040600155	20000406	00155	EU  	2000	4	6	20000406SH018    	1	19991223	G	6720		BEARING         			BOLKMS	BK117 	BK117C1     	5626025	EU  										BELLCRANK	WORN            	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	317MC					7505				BEARINGS WORN.  REF:  RAM R023415.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			NC	H13EU   					 
2000040600156	20000406	00156	EU  	2000	4	6	20000406SH019    	1	19991222	G	7714	1179405303	INDICATOR       			BOLKMS	117   	BK117A1     	5626010	EU  										TRIPLE TACH	INTERMITTENT    	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	117M					S7023				ROTOR NEEDLE DROPS INTERMITTENTLY. (X)						1	G	7	2 	3U			 	H13EU   					 
2000040600158	20000406	00158	EU  	2000	4	6	20000406SH022    	1	19991222	G	7714	1179405303	INDICATOR       			BOLKMS	117   	BK117A3     	5626015	EU  										TRIPLE TACH	MALFUNCTIONED   	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	4493X					S7038				N2 ON NR 2 ENGINE SIDE DRAGS DOWN.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			 	H13EU   					 
2000040600159	20000406	00159		2000	4	6	20000406SH024    	4	19990114	G	3421	5040017926	GYRO            			BOLKMS	117   	BK117A3     	5626015	EU  										COCKPIT	FAILED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	312LS					7061				ATTITUDE GYRO WILL NOT CAGE.  VERY ERRATIC.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			 	H13EU   					 
2000040600161	20000406	00161	SW  	2000	4	6	20000406SH026    	1	19991209	G	2435		ARMATURE        			BELL  	206   	206L1       	1182107	SW  										STARTER/GEN	VIBRATES        	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	39112	71   			5885	45652				ARMATURE VIBRATES EXCESSIVELY AT OPERATING SPEED.  FAILED AFTER 71.3 TSO.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U			 	H2SW    					 
2000040600162	20000406	00162	EU  	2000	4	6	20000406SH027    	1	19991223	G	6720	741C000005	ACTUATOR        			BOLKMS	117   	BK117A3     	5626015	EU  										TAIL ROTOR	FAILED          	B			TI1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	05	117MH					7112				ACTUATOR FAILS TEST AND HUNTS (RUNAWAY TEST).  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			 	H13EU   					 
2000040600163	20000406	00163	EU  	2000	4	6	20000406SH028    	1	19991223	G	6210	10515150	BLADE           			BOLKMS	105   	BO105LSA3   	5626020	EU  										MAIN ROTOR	DAMAGED         	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	8118Y	8819 				2017				BLADE WOULD NOT BALANCE WITH OPPOSITE BLADE.  REMOVED AND REPLACED. (X)						1	G	7	2 	3U			 	H3AU    					 
2000040600164	20000406	00164	EU  	2000	4	6	20000406SH029    	1	19991223	G	6210	10515150	BLADE           			BOLKMS	105   	BO105LSA3   	5626020	EU  										MAIN ROTOR	UNBONDED        	B			TI1R	O				OTHER                   				F			FLT CONT AFFECTED         			NR	NOT REPORTED   	1			SW	05	8118Y	8819 				2017				BLADE WAS COMING UNSTACKED IN-FLIGHT.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			 	H3AU    					 
2000040600165	20000406	00165	EU  	2000	4	6	20000406SH030    	1	19991226	G	6310	4639202011	CLUTCH          			BOLKMS	117   	BK117B1     	5626012	EU  										ENGINE	FROZEN          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	117VU	2919 				7211				CLUTCH LOCKED UP AND SEVERED NR 2 ENGINE DRIVESHAFT.   REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			 	H13EU   					 
2000041100104	20000411	00104	EU  	2000	4	11	20000406SH031    	1	19991226	G	6510	1171601001	DRIVE SHAFT     			BOLKMS	117   	BK117B1     	5626012	EU  										TAIL ROTOR	SHEARED         	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	117VU					7211				DRIVESHAFT SEVERED.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			 	H13EU   					 
2000041100105	20000411	00105		2000	4	11	20000406SH033    	4	19991014	G	3422	40205773	GYRO            			BOLKMS	117   	BK117A3     	5626015	EU  										COCKPIT	INOPERATIVE     	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	118LL					7097				DIRECTIONAL GYRO UNSERVICEABLE UPON INSTALLATION.  COMPASS READS 90 PERCENT OFF.   REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			 	H13EU   					 
2000041100106	20000411	00106	EU  	2000	4	11	20000406SH034    	1	19991021	G	3340	67839	LIGHT           			BOLKMS	117   	BK117B2     	5626013	EU  										FUSELAGE	INOPERATIVE     	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	117MK					7196				SEARCH LIGHT WILL NOT EXTEND.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			NC	H13EU   					 
2000041100107	20000411	00107	SW  	2000	4	11	20000406SH035    	1	19990831	G	6330	230030535101	ROD END         			BELL  	230   	230         	1182149	SW  										TRANSMISSION	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV					23019				BEARINGS WORN.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			NC	H9SW    					 
2000041100108	20000411	00108	SW  	2000	4	11	20000406SH036    	1	19990831	G	6330	230030535103	BEARING         			BELL  	230   	230         	1182149	SW  										XMSN MOUNT	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV					23019				BEARING WORN.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			NC	H9SW    					 
2000041100109	20000411	00109	GL  	2000	4	11	20000406SH037    	2	19991130	G	7510	1092T1002W	ACTUATOR        			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					ANTI-ICE SYSTEM	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05										PRIOR TO INSTALLATION, PERFORMED OPS CHECK, BLOWN CIRCUIT BREAKER.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U	3	U	 	H3EU    	E4CE				 
2000041100120	20000411	00120	SW  	2000	4	11	20000406SH038    	1	19991209	G	3110	230375011103	LIGHT           			BELL  	230   	230         	1182149	SW  										COCKPIT	FAILED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	4UV					23019				SEGMENT ABOVE AIR DISTRIBUTION SWITCHES NOT ILLUMINATING, RADAR AND RADAR IND.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			NC	H9SW    					 
2000041100121	20000411	00121	SW  	2000	4	11	20000406SH040    	1	19990827	G	5210	222031525101	STOP            			BELL  	230   	230         	1182149	SW  										CREW DOOR	GOUGED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	4UV	2523 				23019				STOP GOUGED.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			NC	H9SW    					 
2000041100122	20000411	00122	SW  	2000	4	11	20000406SH041    	1	19990827	G	5210	222031525103	STOP            			BELL  	230   	230         	1182149	SW  										CREW DOOR	GOUGED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	4UV	2523 				23019				TOP GOUGED.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			NC	H9SW    					 
2000041100123	20000411	00123	NE  	2000	4	11	20000406SH042    	2	19991216	G	7314	9A2045	PUMP            			UROCOP	EC135 	EC135P1     	8680990	EU  	PWA   	PW206 	PW206B      	0	NE  					FUEL SYSTEM	INOPERATIVE     	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	911SV	384  				0070				MOTOR INOPERABLE.  LEAKING FUEL THROUGH (-) TERMINAL.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U	3	U	O	H88EU   	E42NE				 
2000041100124	20000411	00124	EU  	2000	4	11	20000406SH043    	1	19991223	G	2422	SS100	INVERTER        			SNIAS 	350   	AS350B2     	8680813	EU  										E/E BAY	FAILED          	B			TI1R	O				OTHER                   				H	J		ELECT. POWER LOSS-50 PC   	WARNING INDICATION        		NR	NOT REPORTED   	1			SW	05	40751	146  				3154				NO A/C OUTPUT.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U			 	H9EU    					 
2000041100125	20000411	00125	NE  	2000	4	11	20000406SH044    	2	19991014	G	7314	P94B12209	PUMP            			SNIAS 	350   	AS350B2     	8680813	EU  	TMECA 	ARRIEL	ARRIEL1D    	 	NE  					FUEL SYSTEM	FAILED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	40751	163  				3154				BOOST PUMP FAILED DURING CRUISE FLIGHT.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U	3	U	 	H9EU    	E19EU				 
2000041100126	20000411	00126	EU  	2000	4	11	20000406SH045    	1	19991228	G	3340	1179203903	POWER SUPPLY    			BOLKMS	117   	BK117B1     	5626012	EU  										STROBE	FAILED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	311LS					7144				POWER SUPLY FAILED OPS CHECK (NO CHARGE).  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			 	H13EU   					 
2000041100127	20000411	00127	SW  	2000	4	11	20000406SH047    	1	19990825	G	2430	1820300150	SHUNT           			BELL  	230   	230         	1182149	SW  										DC GEN SYSTEM	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV					23019				SHUNT WORN AND DISCOLORED.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			NC	H9SW    					 
2000041100128	20000411	00128	EU  	2000	4	11	20000406SH048    	1	19991223	G	7714	1179405303	INDICATOR       			BOLKMS	117   	BK117A3     	5626015	EU  										TRIPLE TACH	INTERMITTENT    	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	1140H		66   			7078				TACHOMETER OPERATED 65.9 HOURS SINCE REPAIR.  NR 2 N2 NEEDLE INTERMITTENT, READS 2 PERCENT LOW, WENT TO ZERO PERCENT, BA	CK UP TO 50 PERCENT, THEN UP TO 90-95 PERCENT IN-FLIGHT.  NR 1 N2 AND NR REMAINED (ALL 100 PERCENT).  (X)					1	G	7	2 	3U			 	H13EU   					 
2000041100129	20000411	00129	EU  	2000	4	11	20000406SH049    	1	19991104	G	3310	1179203903	POWER SUPPLY    			BOLKMS	BK117 	BK117C1     	5626025	EU  										LIGHTS	DISCHARGED      	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	317MC					7505				POWER SUPPLY WILL NOT HOLD CHARGE.  REF:  RMA R022695.  REMOVED AND REPLACED. (X)						1	G	7	2 	3U			NC	H13EU   					 
2000041100130	20000411	00130	EU  	2000	4	11	20000406SH050    	1	19991108	G	2435	150SG122Q	BRUSH BLOCK     			SNIAS 	350   	AS350B2     	8680813	EU  										STARTER/GEN	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	40751	234  				3154				BRUSHES WORN.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U			 	H9EU    					 
2000041100131	20000411	00131	EU  	2000	4	11	20000406SH051    	1	19991111	G	6320	4649001007	TRANSMISSION    			UROCOP	EC135 	EC135P1     	8680990	EU  										MAIN ROTOR	FAILED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	911SV					0070				MAIN TRANSMISSION FAILED.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			O	H88EU   					 
2000041100134	20000411	00134	CE  	2000	4	11	20000406SH054    	1	19991221	G	5210	051701912	PIN             			CESSNA	172   	172R        	2072401	CE  										RT CREW DOOR	SHEARED         	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	01	9522S	654  				17280432				PIN SHEARED.  FOUND RT DOOR FORWARD SKIN AT LOWER HINGE AREA IMPROPERLY TRIMMED, EXTENDED TOO FAR FORWARD, CAUSING DOOR 	TO UNDER-LAP FUSELAGE SKIN AT THE HINGE STRESSING HINGE PIN.  NOTE:  SUBMITTER STATED LOSS OF THIS LOWER HINGE INTEGRITY	 IN-FLIGHT COULD LEAD TO SEPARATION OF THE DOOR ASSY IMPACTING HORIZ TAIL SURFACES CAUSING LOSS OF CONTROL OF THE ACFT, 	INJURY AND DEATH.  TRIMMED DOOR SKIN, REPLACED PIN, OPS CHECK OK.  (X)			1	H	7	1 	3O			NT	3A12    					 
2000041300430	20000413	00430	WP  	2000	4	13	20000412SH022    	1	19990119	G	3340		LIGHT           			HUGHES	369   	369D        	4470706	WP  										HORIZONTAL STAB	CONTAMINATED    	B			EOOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	5074R					1151D				DURING INSPECTION, THE AFT TAIL LIGHT WAS FOUND INOPERABLE.  FURTHER INSPECTION REVEALED TAIL LIGHT LENS WAS HALF FILLED	 WITH WATER.  THE INSTALLATION OF THIS LIGHT ASSEMBLY LENDS ITSELF TO THIS TYPE OF DAMAGE DURING OPERATION IN RAINY WEAT	HER.  (X)				1	G	7	1 	3U			 	H3WE    					 
2000041700186	20000417	00186	SW  	2000	4	17	20000413SH019    	1	19991231	G	6220	28175018	RING            			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	LEAKING         	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV					23019				MATING RING LEAKING.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			NC	H9SW    					 
2000041700196	20000417	00196	SW  	2000	4	17	20000413SH025    	1	19991229	G	7810	230063301102	DUCT            			BELL  	230   	230         	1182149	SW  										EXHAUST	CRACKED         	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV					23019				EXHAUST DUCT CRACKED AT AFT LOWER SIDE.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			NC	H9SW    					 
2000041700206	20000417	00206		2000	4	17	20000413SH029    	4	19990816	G	3425	066304607	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT HSI	LOOSE           	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	350AZ	221  				3127				INDICATOR LOOSE IN FRAME AND PRECESSES.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U			 	H9EU    					 
2000041700207	20000417	00207	SW  	2000	4	17	20000413SH030    	1	19990801	G	7332	222375077105	TRANSDUCER      			BELL  	230   	230         	1182149	SW  										COCKPIT	FLUCTUATES      	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	4UV					23019				PRESSURE READING FLUCTUATIONS.  REMOVED AND REPLACED.   (X)						1	G	7	2 	3U			NC	H9SW    					 
2000041700210	20000417	00210		2000	4	17	20000413SH034    	4	19991102	G	2211	11788292	COMPUTER        			BOLKMS	117   	BK117B1     	5626012	EU  										SPAS	FAILED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	460H					7142				ACTUATOR NOT MOVING.  WILL NOT TEST.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			 	H13EU   					 
2000041700211	20000417	00211	SW  	2000	4	17	20000413SH035    	1	19991231	G	6320	1223328	SEAL            			BELL  	230   	230         	1182149	SW  										M/R GEARBOX	LEAKING         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	4UV					23019				SEAL LEAKING.  REMOVED AND REPLACED.  (X)						1	G	7	2 	3U			NC	H9SW    					 
2000041700234	20000417	00234	EU  	2000	4	17	20000413SH037    	1	19991229	G	6420	350A33214501	PITCH LINK      			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	350AZ	428  				3127				T/R PITCH CHANGE REMOVED PER AD 98-24-25.  WORN OUT.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U			 	H9EU    					 
2000041700235	20000417	00235	EU  	2000	4	17	20000413SH038    	1	19991229	G	6420	350A33214501	PITCH LINK      			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	350AZ	428  				3127				T/R PITCH CHANGE REMOVED PER AD 98-24-35.  WORN OUT.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U			 	H9EU    					 
2000041700243	20000417	00243	EU  	2000	4	17	20000413SH043    	1	19991007	G	7931	648180101	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										OIL PRESSURE	MISINSTALLED    	B			TI1R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	05	40751					3154				OIL PRESSURE INDICATOR - PART USED FOR TROUBLESHOOTING ONLY - WORKS OKAY.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U			 	H9EU    					 
2000041900265	20000419	00265	EA  	2000	4	19	20000413SH047    	2	19991212	G	8500		ENGINE          			BNORM 	BN2   	BN2B26      	1520350	EU  	LYC   	O540  	O540E4C5    	41532	EA  					RIGHT	FAILED          	B				A				UNSCHED LANDING         				K	E	J	FLUID LOSS                	VIBRATION/BUFFET          	WARNING INDICATION        	CR	CRUISE         	1			SO	21	663VL	7338 	598  			2110	L1881940A			ON CRUISE FLIGHT, RIGHT ENGINE STARTED TO VIBRATE AND LEAK OIL.  PILOT DECLARED EMERGENCY AND LANDED AT TORTOLA AIRPORT 	(BEEF ISLAND).  PRELIMINARY INSPECTION REVEALED RIGHT ENGINE CRANKCASE CRACKED.  ENGINE CHANGE.  (X)					1	H	7	2 	3O	3	O	RT	A17EU   	E295				 
2000051800042	20000518	00042	SW  	2000	5	18	20000424SH007    	1	19991231	G	3234	560011000	BAR             			MOONEY	M20   	M20B        	5870206	SW  										GEAR HANDLE	CRACKED         	H				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			CE	03	74777	2613 				1777				AFTER LANDING AND TAXIING ABOUT ONE-HALF MILE, NOSE GEAR COLLAPSED AFTER GOING OVER DIP IN TAXI STRIP.  UPON INSPECTION 	OF GEAR SYSTEM, FOUND JOHNSON WITH SEVERAL CRACKS, ONE AT BASE OF HANDLE, 2 EACH AT NOSE ROD ATTACH ARM.  CAUSE, UNKNOWN	.   (X)				1	L	7	1 	3O			 	2A3     					 
2000042500301	20000425	00301	EU  	2000	4	25	20000424SH015    	1	19991217	G	6410	704A33633116	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WORN            	A			R7MA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	101LN	537  				3038				ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS.  REPLACED WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	1 	3U			 	H9EU    					 
2000051800049	20000518	00049	EU  	2000	5	18	20000424SH016    	1	19991217	G	6220	117775P	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										STARFLEX	WORN            	A			R7MA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	101LN	537  				3038				TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS.  REPLACED WITH NEW UNIT, CORRECTED PROBLEM.   (X)						1	G	7	1 	3U			 	H9EU    					 
2000050500089	20000505	00089	CE  	2000	5	5	20000426SH001    	1	19990322	G	5210	1313232C15	CLEVIS PIN      			BEECH 	90    	C90         	1152913	CE  										PAX DOOR	FAILED          	G				A				UNSCHED LANDING         				O			OTHER                     			NR	NOT REPORTED   	1			NE	03	91TJ	7192 				LJ744				DURING FLIGHT INTO AQW, PASSENGERS AND CREW HEARD A LOUG BANG AND THE PRESSURIZATION BEGAN TO DESCEND QUICKLY.  LANDING 	WAS MADE WITHOUT INCIDENT.  INSPECTION REVEALED THE CLEVIS PIN THAT IS THE PIVOT FOR THE UPPER CABIN DOOR LATCH HOOK HAD	 BROKEN.  RAYTHEON HAS ADDED INSPECTION OF THESE PINS IN THE PHASE 3 AND COMPLETE INSPECTION GUIDES.  THIS AIRCRAFT IS D	UE A PHASE 3 BY AUGUST OF 2000.  (X)			1	L	7	2 	3T			 	3A20    					 
2000050800083	20000508	00083	SO  	2000	5	8	20000427SH001    	2	19990330	G	7320	J0799Z1AR	FCU             	CONT        		CESSNA	210   	210L        	2073448	CE  	CONT  	O520  	IO520L      	17032	SO  					ENGINE	LEAKING         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	15	59299	33   				21060199				FUEL LEAKING FROM DATA PLATE ATTACH RIVET/SCREW.  (X)						1	H	7	1 	3O	3	O	 	3A21    	E5CE				 
2000051000161	20000510	00161	GL  	2000	5	10	20000502SH007    	2	19991213	G	7210	6893674	GEAR            	ALLSN       		BELL  	407   	407         	       	SW  	ALLSN 	250C  	250C47B     	 	GL  					GEARBOX	DAMAGED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417AL	1197 			CAG47188	53054	CAE847188			DISASSEMBLED, CLEANED, AND INSPECTED. FOUND SPALLING AND GALLING ON GEAR TEETH.  TM GEAR HAS EXCESSIVE SPALLING AND GALL	ING ON GEAR TEETH POSSIBLY DUE TO IMPROPER MESHING OF TM AND PINION GEARS.  SECONDARY DAMAGE.  PINION GEAR, PN 6893672, 	SN 77723, TT 1,196.5, SPALLING AND GALLING ON GEAR TEETH.  (X)				1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
2000051000226	20000510	00226	CE  	2000	5	10	20000504SH003    	1	19990601	G	3220	12434262	TORQUE LINK     			CESSNA	210   	210L        	2073448	CE  										NLG	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03	50DB	8504 				21060107				DURING A ROUTINE INSPECTION, FOUND NOSE GEAR UPPER TORQUE LINK PN 1243426-2 CRACKED.  PREVIOUS NOSE WHEEL SHIMMY WAS REP	ORTED AND STEERING COLLAR SHIMS AND SHIMMY DAMPENER WERE RE-SEALED.  (X)					1	H	7	1 	3O			 	3A21    					 
2000051000282	20000510	00282		2000	5	10	20000505SH004    	4	19990121	G	2562	AK450	ELT             																	CABIN	FAILED          	D				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			NM	02										DURING ROUTINE TEST PER FAR 91-207D ON ANNUAL INSPECTION, SUBJECT ELT FAILED G-SWITCH TEST.  UNIT WAS SENT TO AMERI-KING	 FOR REPAIR.   (X)																		 
2000061400199	20000614	00199	CE  	2000	6	14	20000508SH001    	1	19990607	G	3252	C1000161A	SHIMMY DAMPENER 			BEECH 	23    	C23         	1151242	CE  										INTERNAL	LEAKING         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	02	6639D					M2223				SHIMMY DAMPENER HAS NUMEROUS DEAD SPOTS (AIR INSIDE) WHEN ACTUATED.  CAUSES NOSE WHEEL TO SHIMMY READ BAD.  (X)						1	L	7	1 	3O			 	A1CE    					 
2000061400200	20000614	00200	CE  	2000	6	14	20000508SH002    	1	19990607	G	3252	C10001618	SHIMMY DAMPENER 			BEECH 	23    	C23         	1151242	CE  										INTERNAL	FAILED          	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	02	6639D					M2223				RETRIEVED SUBJECT SHIMMY DAMPENER FROM STOCK ROOM.  ON FUNCTIONAL CHECK, DETERMINED MUCH WORSE THAN THE REMOVED UNIT.  						1	L	7	1 	3O			 	A1CE    					 
2000061400204	20000614	00204	SO  	2000	6	14	20000508SH011    	2	19991201	G	8530	CLASS70	CYLINDER        			CESSNA	182   	182Q        	2072732	CE  	CONT  	O470  	O470U       	17026	SO  					NUMBER4	CRACKED         	B			GGNR	A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			NM	13	759JH		29   			18266027	466167			THE ENGINE WAS TOPPED WITH 6 ENGINE COMPONENTS INC CERMINIL CYLINDERS.  AFTER 29 HOURS OF OPERATION, ENGINE RAN ROUGH AN	D WAS LOSING OIL. PILOT WAS ABLE TO FIND A PRIVATE STREET AND  LANDED SAFELY.  IT WAS DETERMINED THAT NR 4 CYLINDER WAS 	CRACKED .8750 INCH AROUND AND 5.4 INCHES DOWN LOOKING INTO THE BARREL.  (X)				1	H	7	1 	3O	3	O	NT	3A13    	E273				 
2000060900523	20000609	00523	NE  	2000	6	9	20000508SH032    	2	19990715	G	7230	430150601	SEAL            			BOLKMS	117   	BK117A4     	5626017	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					NR 2 BEARING	LEAKING         	A			R7MA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			NM	07	911BY	625  				7127	LE45022EA			SEAL, NR 2 BEARING, LEAKING BEYOND SERVICEABLE LIMITS.  REPLACED WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	2 	3U	3	U	 	H13EU   	E5NE				 
2000060900524	20000609	00524	NE  	2000	6	9	20000508SH033    	2	19990715	G	7250	430144801	SEAL            			BOLKMS	117   	BK117A4     	5626017	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					NR 3 BEARING	MELTED          	A			R7MA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			NM	07	911BY	625  				7127				SEAL, NR 3 BEARING, LEAKING BEYOND SERVICE LIMITS.  REPLACED WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	2 	3U	3	U	 	H13EU   	E5NE				 
2000061300369	20000613	00369	NE  	2000	6	13	20000508SH035    	2	19990715	G	7240	410106701	SEAL            			BOLKMS	117   	BK117A4     	5626017	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					TURBINE SHOUD	WORN            	A			R7MA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	911BY	625  				7127				SEAL RING WORN BEYOND SERVICEABLE LIMITS.  REPLACED WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	2 	3U	3	U	 	H13EU   	E5NE				 
2000061300371	20000613	00371	NE  	2000	6	13	20000510SH009    	2	19990929	G	7250		BLADE           			BOLKMS	117   	BK117A1     	5626010	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					GAS PRODUCER	DAMAGED         	A			R7MA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	07	128HH	2756 				7036	LE45214EA			BLADES SUBJECTED TO CARBON BALL BLASTING.  REPLACED WITH NEW UNIT, CORRECTED PROBLEM.   (X)						1	G	7	2 	3U	3	U	 	H13EU   	E5NE				 
2000061300372	20000613	00372	NE  	2000	6	13	20000510SH010    	2	19990929	G	7230	430150601	SEAL            			BOLKMS	117   	BK117A1     	5626010	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					TURBINE SHROUD	LEAKING         	A			R7MA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	07	128HH	837  				7036	LE45214EA			BEARING LEAKING BEYOND SERVICEABLE LIMITS.  REPLACED WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	2 	3U	3	U	 	H13EU   	E5NE				 
2000061300373	20000613	00373	NE  	2000	6	13	20000510SH011    	2	19990929	G	7250		SEAL            			BOLKMS	117   	BK117A1     	5626010	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					 TURBINE SHROUD	WORN            	A			R7MA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	07	128HH	837  				7036	LE45214EA			SEAL RING WORN BEYOND SERVICEABLE LIMITS.  REPLACED WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	2 	3U	3	U	 	H13EU   	E5NE				 
2000061300374	20000613	00374	NE  	2000	6	13	20000510SH012    	2	19991015	G	7250	430144801	SEAL            			BOLKMS	117   	BK117A4     	5626017	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					NR 3 BEARING	LEAKING         	A			R7MA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	07	117CW	384  				7125	LE45243EA			SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	2 	3U	3	U	 	H13EU   	E5NE				 
2000061600447	20000616	00447	NE  	2000	6	16	20000510SH013    	2	19991015	G	7250	410106701	SEAL            			BOLKMS	117   	BK117A4     	5626017	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					TURBINE SHROUD	WORN            	A			R7MA	O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	117CW	384  				7125	LE45273EA			SEAL RING WORN BEYOND SERVICEABLE LIMITS.  REPLACED WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	2 	3U	3	U	 	H13EU   	E5NE				 
2000062000044	20000620	00044	NE  	2000	6	20	20000510SH014    	2	19991015	G	7230	430150601	SEAL            			BOLKMS	117   	BK117A4     	5626017	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					NR 2 BEARING	LEAKING         	A			R7MA	O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	117CW	384  				7125	LE45273EA			SEAL LEAKING BEYOND SERVICEABLE LIMITS.  REPLACED WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	2 	3U	3	U	 	H13EU   	E5NE				 
2000062000045	20000620	00045	SW  	2000	6	20	20000510SH016    	1	19991221	G	5302	212030191001	SKIN            			BELL  	412   	412         	1182202	SW  										TAIL BOOM	CRACKED         	B			JLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01	17LA					36044				DURING DAILY INSPECTION, MECHANIC  FOUND A CRACK IN THE SKIN JUST BELOW  TAIL BOOM ATTACH FITTING ON UPPER LEFT HAND SID	E OF THE AIRFRAME.  INSP REVEALED THE MAIN BEAM CAP WAS BROKEN.  MAINT REMOVED HELICOPTER FROM SERVICE.  REMOVED RT HAND	 FITTING AND UPPER LT HAND FITTING FROM ANOTHER HELICOPTER S/N 36043, (SISTER SHIP).  LT HAND FITTING HAD EVIDENCE OF CH	IPS AND BURRS ON ALL BUT 2 HOLES.  BEAM CAP IS THE SAME.  MOST OF THE HOLES HAD NOT BEEN DEBURRED.  THIS IS ON THE BROKE	N FITING AND BEAM CAP.  AFTER REMOVING A SECTION OF THE FWD PORTION OF BEAM CAP, FOUND HOLES HAD NOT BEEN DEBURRED.  THE	 RIGHT HAND FITTING LOOKS THE SAME.  ALL BUT 3 OF THE HOLES WERE NOT DEBURRED.  (X)	1	G	7	2 	4U			 	H4SW    					 
2000062000046	20000620	00046	SW  	2000	6	20	20000510SH017    	1	19991221	G	5302	2030191001	SKIN            			BELL  	412   	412         	1182202	SW  										TAIL BOOM	LEAKING         	B			JLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01	18LA					36043				DURING DAILY INSPECTION, MECHANIC  FOUND A CRACK IN THE SKIN JUST BELOW  TAIL BOOM ATTACH FITTING ON UPPER LEFT HAND SID	E OF THE AIRFRAME.  INSP REVEALED THE MAIN BEAM CAP WAS BROKEN.  MAINT REMOVED HELICOPTER FROM SERVICE.  REMOVED RT HAND	 FITTING AND UPPER LT HAND FITTING FROM ANOTHER HELICOPTER S/N 36043, (SISTER SHIP).  LT HAND FITTING HAD EVIDENCE OF CH	IPS AND BURRS ON ALL BUT 2 HOLES.  BEAM CAP IS THE SAME.  MOST OF THE HOLES HAD NOT BEEN DEBURRED.  THIS IS ON THE BROKE	N FITING AND BEAM CAP.  AFTER REMOVING A SECTION OF THE FWD PORTION OF BEAM CAP, FOUND HOLES HAD NOT BEEN DEBURRED.  THE	 RIGHT HAND FITTING LOOKS THE SAME.  UPPER LT FITTING - ALL BUT 2 HOLES WERE NOT DEBURRED.  (X)	1	G	7	2 	4U			 	H4SW    					 
2000051600176	20000516	00176	NM  	2000	5	16	20000515AP039    	1	19990908	G	3230	10607441	BALLSCREW       			BOEING	727   	727225      	1384077	NM  										NLG WW	CORRODED        	A			MYWA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	803MA					22434				NOSE LANDING GEAR MANUAL EXTENSION JACKSCREW HAS PITTING CORROSION.  REMOVED AND REPLACED NLG MANUAL EXTENSION JACKSCREW	 IAW MM 32-34-1 PAGE 401, OPS CHECK GOOD IAW MM 32-34-0 PAGE 201.  (M)					2	L	7	3 	4F			 	A3WE    					 
2000121500005	20001215	00005	SO  	2000	12	15	20000515SH002    	2	19991122	G	7314	6467681A1	PUMP            			CESSNA	206   	TU206G      	2073357	CE  	CONT  	O520  	TSIO520M    	17040	SO  					DRIVE SHAFT SEAL	LEAKING         	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CE	07	HCBZE		231  			U20605753	291994R			ENGINE DRIVEN FUEL PUMP WAS LEAKING FUEL OUT OF THE PUMP DRAIN LINE.  (X)						1	H	7	1 	3O	3	O	 	A4CE    	E8CE				 
2000121500006	20001215	00006	SO  	2000	12	15	20000515SH003    	2	19991122	G	7314	6467681A1	PUMP            			CESSNA	206   	TU206G      	2073357	CE  	CONT  	O520  	TSIO520M    	17040	SO  					DRIVESHAFT SEAL	LEAKING         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	07	HCBMO		18   			U20605349	818044R			ENGINE DRIVEN FUEL PUMP WAS LEAKING FUEL FROM THE PUMP DRAIN LINE.  (X)						1	H	7	1 	3O	3	O	 	A4CE    	E8CE				 
2000051600141	20000516	00141	EA  	2000	5	16	20000515SH012    	2	19991028	G	8530	75068	EXHAUST VALVE   			CESSNA	172   	172M        	2072418	CE  	LYC   	O320  	O320E2D     	41508	EA  					KEEPER	DAMAGED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01	13818	537  				17263013	L4831027A			ENGINE HAD ERRATIC IDLE AND WAS GETTING WORSE.  W.O.T. POWER NORMAL.  STARTED ENGINE COLD AND FOUND NR 4 EXHAUST COLD.  	CHECKED LIFTER DROP CLEARANCE, FOUND IT WAS ZERO AND EXHAUST VALVE SUNK IN SEAT.  REMOVED CYLINDER, FOUND BROKEN KEEPERS	, WORN KEEPERS GROOVE AND RETAINERS.    REMOVED REMAINING CYLINDERS AND FOUND WORN KEEPER GROOVES AND SUNK VALVES AND VA	LVE SEATING ON OUTER EDGE OF VALVE. (X)			1	H	7	1 	3O	3	O	NT	3A12    	E274				 
2001030200001	20010302	00001	NE  	2001	3	2	20000518SH016    	1	19991104	G	2822		PUMP            	NASH        		SKRSKY	S64   	S64*        	8142502	NE  										FUEL SYSTEM	LEAKING         	G				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	25	18428				FB74132	6718428				UNIT WAS RETURNED TO STOCK FOR REPAIR.  TAG READS LOW PUMP OUTPUT OR INTERMITTENTLY INOPERATIVE.  BENCH CHECKED UNIT, FO	UND TO BE LEAKING INTERNALLY DOWN WIRE HARNESS AND TO BE INTERMITTENTLY SHORTED.  REPAIR IS TO REPLACE WITH AN EXTERNAL 	MOUNTED TYPE FUEL PUMP.  (X)				2	G	7	2 	4U			 	        					 
2001030200002	20010302	00002	NE  	2001	3	2	20000518SH017    	1	19991104	G	2822	640250	PUMP            	NASH        		SKRSKY	S64   	S64*        	8142502	NE  										FUEL SYSTEM	SHORTED         	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	25	18428				FB64972	6718428				UNIT WAS RETURNED FROM A/C AS LEAKING AND INOPERATIVE.  BENCH CHECKED UNIT, FOUND TO BE SHORTED INTERNALLY.  REPLACED WI	TH AN EXTERNALLY MOUNTED FUEL BOOST PUMP.  (X)					2	G	7	2 	4U			 	        					 
2000091800010	20000918	00010	EA  	2000	9	18	20000523SH002    	2	19991121	G	8520	LW102075	PISTON          			CONAER	LA4   	LA4200      	5110310	NE  	LYC   	O360  	IO360A1C    	41514	EA  					ENGINE	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	5006L					463	L773851A			ENGINE PISTON ON NR 4 CYLINDER HEAD SEPARATED FROM BASE BELOW THE OIL RING LAND.  TWISTED ROD AND CAUSED ENGINE TO FAIL.	  ENGINE FAILURE ON CLIMB-OUT AT ABOUT 700 FEET AGL AT CLIMB POWER.   ENGINE TT SN, 1,445 HOURS. (X)					1	H	7	1 	3O	3	O	 	1A13    	1E10				 
2000102400272	20001024	00272	GL  	2000	10	24	20000523SH006    	2	19990615	G	7250	23038136	SHAFT           								ALLSN 	250C  	250C30      	03013	GL  					OUTER PWR TUR	DEFECTIVE       	B			QT2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17					CAT95545		CAE900074			THE REFERENCED OUTER POWER TURBINE SHAFT WAS INSPECTED9.  THIS PART WAS DETERMINED TO BE UNSERVICEABLE AND UNREPAIRABLE 	DUE TO CURVIC COUPLING ROOT DAMAGE (REF: FORM ESPD NR 08-070-301500; ALLISON GAS TUBRINE 250-C30 SERIES OVERHAUL MANUAL,	 SECTION 72-50-00, PAGES 349-350, ITEM 42, AND PAGES 316-317, FIGURE 303).  THE CUSTOMER REQUESTED REJECTED PARTS BE  RE	TURNED TO HIM (REF:   FORM ESPD NR 99-999-001028. REF:  DAI JOB NR NR0017.  (X)								3	U			E1GL				 
2000102400127	20001024	00127	GL  	2000	10	24	20000523SH007    	2	19990617	G	7230	23056634	SPUR GEAR       								ALLSN 	250C  	250C30      	03013	GL  					ASSEMBLY	SPALLED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17					23056634		CAE900074			THE REFERENCED SPUR ADAPTER GEARSHAFT ASSEMBLY WAS INSPECTED AT DALLAS AIRMOTIVE-MILLVILLE ON 6-17-99.  THIS PART WAS DE	TERMINED TO BE UNSERVICEABLE AND UNREPAIRABLE DUE TO SPALLED GEAR TEETH (REFERENCE DALLAS AIRMOTIVE FORM ESPD NR 08-070-	300100; ALLSION ENGINE COMPANY 250-C30 SERIES OVERHAUL MANUAL, SECTION 72-30-00, PAGE 331, ITEM 18; PAGE 332, FIGURE 314	; AND SECTION 72-60-00, PAGE 308, TABLE 302, ITEM 2).  THE CUSTOMER REQUESTED REJECTED PARTS BE RETURNED TO HIM (REFEREN	CE ATTACHED DAI FORM ESPD NR 99-999-001-028).  REF:  DAI JOB NR NR0017.  (X)							3	U			E1GL				 
2000091800011	20000918	00011	SO  	2000	9	18	20000523SH017    	1	19991216	G	2560	2063691	CONNECTOR       			PIPER 	PA42  	PA42        	7104202	SO  										BS 57.0	DAMAGED         	B			JGVR	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			CE	09	811DA	5755 				428001029				CREW REPORTED SMOKE SMELL IN THE COCKPIT AND THEN NUMEROUS CIRCUIT BREAKERS STARTED TRIPPING.  AFTER AIRCRAFT SHUT DOWN 	AFTER LANDING, THE BATTERY POWER COULD NOT BE SHUT OFF.  THE BATTERY WAS DISCONNECTED AND AN INVESTIGATION REVEALED THE 	ELECTRICAL CONNECTOR FOR THE PRESSURE BULKHEAD FEED THROUGH LABELED 'E433' WAS FOUND OVERHEATED AND DAMAGED.  FWD PLUG C	OULD NOT BE REMOVED NORMALLY.  HAD TO BE DAMAGED TO BE DISCONNECTED.  AFTER PLUG DISCONNECTED, IT WAS FOUND BURNT THROUG	H TO AFT SIDE CONNECTOR.  LANDINGS:  5,823.  (X)		1	L	7	2 	4T			 	A23SO   					 
2001013000034	20010130	00034	SO  	2001	1	30	20000531SH011    	2	19990929	G	8520	642507	CRANKCASE       			CESSNA	340   	340A        	2076405	CE  	CONT  	O520  	TSIO520NB   	17040	SO  					ENGINE	CRACKED         	B			JZRR	K				NONE                    				O			OTHER                     			NR	NOT REPORTED   	1			WP	07	5343J		600  			340A0416	519354			BROKEN CYLINDER BASE STUDS AND 7TH STUD WERE FOUND AT NR 3 CYLINDER LOCATION.  CRANKCASE STRESS WAS CAUSE OF CRANKSCASE 	TO CRACK (4 INCH CRACK)  AT NR 3 CYLINDER.  HIGH MANIFOLD PRESSURE MAY HAVE CONTRIBUTED TO THE CAUSE.  ENGINE IS RATED T	O 41 INCHES M/P FOR 325 HP RAM SERIES IV ENGINES.  (X)				1	L	7	2 	3O	3	O	 	3A25    	E8CE				 
2001020200001	20010202	00001	SW  	2001	2	2	20000601SH011    	1	19991222	G	3212	7MA10603	FLOAT           			BELL  	212   	212         	1181420	SW  										FUSELAGE	HUNG UP         	B			QS7D	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	09	16973					30882				DURING EMERGENCY INFLATION TEST, LEFT FORWARD BAG HUNG ON LANDING GEAR STEP.  (X)						1	G	7	1 	4U			 	H4SW    					 
2001012900075	20010129	00075	NE  	2001	1	29	20000605SH008    	2	19991217	G	7412	9580113800	GENERATOR       			BOLKMS	BK117 	BK117C1     	5626025	EU  	TMECA 	ARRIEL	ARRIEL1C    	60030	NE  					ENGINE	INOPERATIVE     	A			R7MA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	117SU	2277 				7527				HE GENERATOR INOPERATIVE.  REPLACED WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	2 	3U	3	U	NC	H13EU   	E19EU				 
2001012900092	20010129	00092	EU  	2001	1	29	20000605SH027    	1	19991112	G	7931	1130021089	PRESSURE SWITCH 			SNIAS 	350   	AS350B2     	8680813	EU  										GEARBOX OIL	INOPERATIVE     	A			R7MA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	911LR	9    				2404				PRESSURE SWITCH INOPERATIVE.  WARNING LIGHT COMES ON WITH NORMAL MGB OIL PRESSURE.  REPLACED WITH NEW UNIT, CORRECTED PR	OBLEM.  (X)					1	G	7	1 	3U			 	H9EU    					 
2001012900093	20010129	00093	EU  	2001	1	29	20000605SH028    	1	19991103	G	7931	1130021089	PRESSURE SWITCH 			SNIAS 	350   	AS350B2     	8680813	EU  										GEARBOX OIL	INOPERATIVE     	A			R7MA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	911LR	25   				2404				PRESSURE SWITCH INOPERATIVE.  OIL WARNING LIGHT COMES ON AT IDLE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	1 	3U			 	H9EU    					 
2001012900094	20010129	00094	EU  	2001	1	29	20000605SH029    	1	19991010	G	7931	1130021089	PRESSURE SWITCH 			SNIAS 	350   	AS350B2     	8680813	EU  										GEARBOX OIL	INOPERATIVE     	A			R7MA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	911LR	351  				2404				PRESSURE SWITCH INOPERATIVE.  LOW PRESSURE LIGHT COMES ON AT IDLE.  REPLACED WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	1 	3U			 	H9EU    					 
2000072600085	20000726	00085	CE  	2000	7	26	20000621SH010    	1	19991007	G	7921	626189	COOLER          			CESSNA	206   	206CESSNA   	2073302	CE  	CONT  	O520  	IO520A      	17032	SO  					CORE MATRIX	LEAKING         	B			RF3R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	23										PART BEGAN LEAKING DURING NORMAL SERVICE DUE TO EPOXY FAILURE.  EPOXY WAS USED OVER A CRACK IN THE OIL COOLER WHICH WORK	ED ITS WAY TO THE SURFACE OF THE HARDENED EPOXY.  SUBMITTER RECOMMENDED ELIMINATING THE USE OF EPOXY IN OIL COOLERS.  (X	)				1	H	7	1 	3O	3	O	 	A4CE    	E5CE				 
2000072600086	20000726	00086	CE  	2000	7	26	20000621SH011    	1	19991006	G	7921	1E1104	COOLER          			CESSNA	310   	310         	2074202	CE  	CONT  	O470  	O470B       	17026	SO  					CORE	LEAKING         	B			RF3R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	23										OIL COOLER RUPTURED AT POINT OF PREVIOUS EPOXY REPAIR CAUSING SEVERE LEAK.  EPOXY FAILURE IS COMMON AND SHOULD BE ELIMIN	ATED FROM BEING USED IN OIL COOLERS.  (X)					1	L	7	2 	3O	3	O	RT	3A10    	E273				 
2000072600166	20000726	00166	SO  	2000	7	26	20000621SH012    	2	19991111	G	7414	M3081	SPRING          	SLICK       		CESSNA	172   	172C        	2072408	CE  	CONT  	O300  	O300D       	17022	SO  						BROKEN          	B			KC2R	O				OTHER                   				W	R		INADEQUATE Q C            	PARTIAL RPM/PWR LOSS      		CR	CRUISE         	1			GL	03		8    			99092113					MAGNETO FAILED IN-FLIGHT. INSPECTION REVEALED BROKEN CONTACT SPRING.  SPRING BROKE NEAR TRANSITION FROM FLAT SECTION TO 	RADIUSED EDGE.  SUBMITTER SUSPECTED IMPROPER TEMPER OF SPRING OR OTHER MANUFACTURING DEFECT.  MAG HAS ONLY 8 HOURS SINCE	 NEW.  (X)				1	H	7	1 	3O	3	O	NT	3A12    	E253				 
2000072600188	20000726	00188	NE  	2000	7	26	20000621SH015    	2	19991217	G	7250	2A0851	BEARING         								IAE   	V2500 	V2500A1     	 	NE  					NR 4 BEARING	CRACKED         	B			KB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03										PART RECEIVED FOR FLUORESCENT PENETRANT INSPECTION PER SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501, OF 	THE IAE V2500 PROPULSION SYSTEM ENGINE MANUAL, REV 41.  PART REJECTED AT FPI DUE TO CRACKS 2 PLACES ON TOP SURFACE 0.10 	INCH AND 0.125 INCH.  (X)									4	F			E311NE				 
2000073100008	20000731	00008	NE  	2000	7	31	20000621SH016    	2	19991207	G	7250	2A0851	SEAL            								IAE   	V2500 	V2500A1     	 	NE  					NR 4 BEARING	CRACKED         	B			KB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03										PART RECEIVED FOR FLUORESCENT PENETRANT INSPECTION PER IAE V2500 PROPULSION SYSTEM ENGINE MANUAL, REV 38, SECTION 70-23-	01, INSPECTION CHECK-01, TASK 70-23-01-230-501.  PART REJECTED AT FPI DUE TO A CRACK 0.200 INCH LONG ON TOP SURFACE.  (X	)									4	F			E311NE				 
2000072600009	20000726	00009	SO  	2000	7	26	20000621SH018    	1	19990930	G	7120	6711957	MOUNT           			PIPER 	PA28  	PA28R201    	7102816	SO  										AFT DRAG STRUT	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99		7476 				28R7737139				DURING SCHEDULED INSPECTION, FOUND MOUNT BROKEN AT DRAG STRUT ATTACH POINT ON RIGHT SIDE.  PILOT HAD NOTED THE GEAR UNSA	FE LIGHT WAS COMING ON ONLY DURING DESCENT.  THE MICROSWITCH FOR THE UNSAFE LIGHT IS MOUNTED ABOVE THE BROKEN AREA.  WHE	N POWER WAS REDUCED AND TORQUE WENT DOWN, THE MOUNT SEPARATED AND THE SWITCH WAS NOT CONTACTING.  THIS BROKEN AREA IS TH	E WEAKEST PART OF THE MOUNT AND MAY HAVE BEEN BROKEN FROM A HARD LANDING ON NOSE.  (X)			1	L	7	1 	3O			 	2A13    					 
2000072600191	20000726	00191	CE  	2000	7	26	20000622SH001    	1	19990831	G	5541		SPAR            			CESSNA	150   	152         	2071835	CE  										LIGHTENING HOLE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	49194	10988				15281186				DURING SCHEDULED INSPECTION, FOUND RUDDER SPAR CRACKED AT UPPER LIGHTENING HOLE NEAR THE UPPER HINGE BRACKET.  AFTER EXA	MINATION OF 6 OTHER 152''S IN THE FLEET, FOUND 2 OTHERS WITH SIMILAR CRACKS, CESSNA SEB 94-3 PERTAINS TO THIS SUBJECT.  	REPLACED SPAR WITH STRENGTHENED DESIGN.  (X)				1	H	7	1 	3O			NT	3A19    					 
2000072600192	20000726	00192	CE  	2000	7	26	20000622SH003    	1	19991105	G	2841	S32812	INDICATOR       			CESSNA	172   	172R        	2072401	CE  										FUEL	INACCURATE      	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	99	174GF	243  				17280532				FUEL INDICATOR MANUFACTURED DATE 12-31-97.  AIRCRAFT AND INDICATOR TOTAL TIME SINCE NEW 243.3 HOURS, NEW 5-19-98.  PER C	ESSNA MM 28-20-00, WOULD NOT CALIBRATE TO ''FULL'' READING ON RIGHT TANK.  WOULD NOT READ OVER 24 GALLONS AT 26 GALLONS 	FULL.  NO TOLERANCES CALLED OUT IN MM.  SUBMITTER SUSPECTED FUEL QUANTITY SYSTEM MAY HAVE BEEN OUT OF TOLERANCE SINCE FA	CTORY NEW.  (X)			1	H	7	1 	3O			NT	3A12    					 
2000072600179	20000726	00179	CE  	2000	7	26	20000622SH004    	1	19991108	G	7110	J744436	MOUNT           			CESSNA	172   	172R        	2072401	CE  										COWL/FIREWALL	TORN            	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	99	174GF	243  				17280532				FOUND, OF ELEVEN SHOCK MOUNTS ON THE AIRCRAFT, THREE TO BE DETERIORATED, ONE TORN 50 PERCENT THROUGH.  SUBMITTER HAS WIT	NESSED AT LEAST 20 OF THESE J7444-36 MOUNTS TORN, ALL WITH LESS THAN 500 HOURS TT.  ON THE NEW SERIES 172R AIRCRAFT, THE	 DASH 36 MOUNT IS MADE MUCH THINNER THAN THE SAME DASH 14 PART USED (WITH BETTER RELIABILITY) ON THE OLDER 172P MODELS. 	 SUBMITTER SUGGESTED CESSNA RE-ENGINEER THIS J7444-36 PART TO CORRECT THE UNSATISFACTORY FAILURE RATE.  (X)			1	H	7	1 	3O			NT	3A12    					 
2000100200243	20001002	00243	GL  	2000	10	2	20000622SH005    	2	19991122	G	7323		LINE            			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					GOVERNOR	LOOSE           	D				A				UNSCHED LANDING         				O			OTHER                     			CR	CRUISE         	1			EA	23	105MH					S419	CAE833360			NR 2 ENGINE DECELERATED DURING FLIGHT.  ENGINE WAS SHUT DOWN AND A SINGLE ENGINE LANDING WAS MADE.  UPON INVESTIGATION B	Y MAINTENANCE, THE PR LINE AT THE GOVERNOR WAS EXTREMELY LOOSE. TIGHTENED B-NUT AND ENGINE PERFORMED SATISFACTORY DURING	 POST RUN-UP.  GOVERNOR AND CONTROL HAD RECENTLY BEEN REPLACED.  NO TORQUE STRIPE WAS FOUND ON FITTING TO INDICATE ANY S	LIPPAGE OF NUT.  POSSIBLE CAUSE:  LINE NOT TORQUED PROPERLY.  ALL OTHER B-NUTS WERE CHECKED FOR PROPER TORQUE.  (X)			1	G	7	2 	3U	3	U	 	H3EU    	E4CE				 
2000072600180	20000726	00180	CE  	2000	7	26	20000622SH006    	1	19991013	G	7110	0024100143	PAN             			BEECH 	36    	A36         	1151604	CE  	CONT  	O550  	IO550B      	 	SO  					FWD ENG COWLING	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	1089E	155  				E3030	682262			DURING AN ANNUAL INSPECTION, THE PN 002-410014-3 ''PAN'', LOCATED AT THE FORWARD NOSE COWLING AREA, BELOW THE ENGINE CRA	NKSHAFT FLANGE, AND ABOVE THE AIR FILTER, HAD LARGE CRACKS WITH A PIECE MISSING APPROXIMATELY 2 INCH BY 4 INCH.  SUBMITT	ER SUSPECTED SOME TYPE VIBRATION PROBLEM.  LEFT, AFT BAFFLE AT OIL COOLER ALSO CRACKED.  (X)				1	L	7	1 	3O	3	O	 	3A15    	E3SO				 
2000072600181	20000726	00181	CE  	2000	7	26	20000622SH007    	1	19990903	G	3213	07410018	STRUT           			CESSNA	185   	A185F       	2072821	CE  										RT UPPER AXLE AT	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	185FK	3257 				18502513				RIGHT MAIN LANDING GEAR LEG FOUND CRACKED IN UPPER AXLE ATTACH BOLT HOLE TO LEADING EDGE.  AIRCRAFT OPERATED ON C4000 WH	EEL SKIS.  1,032 HRS SINCE LAST INSPECTION (MAGNAFLUX) OF GEAR LEG.  (X)					1	H	7	1 	3O			 	3A24    					 
2000100200244	20001002	00244	EA  	2000	10	2	20000622SH008    	2	19991005	G	7414	LW15416	BEARING CAGE    	SLICK       		HUGHES	269   	269C1       	8059504	SW  	LYC   	O360  	HO360C1A    	41514	EA  					MANETO	CRACKED         	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	03	2063X	598  			98081720	0091	L3639536A			BEARING CAGE CRACKED AND CAME APART DURING OPERATION.  RIVETING MARKS SEEMS TO HAVE BEEN THE ORIGIN OF CRACKS FOUND IN S	IMILAR FAILURES IN THE PAST.  (X)					1	G	7	1 	3O	3	O	O	4H12    	E286				 
2000071800518	20000718	00518	EU  	2000	7	18	20000622SH009    	1	19991006	G	3240	F1K21700	HOSE            			SOCATA	TB20  	TB21        	8680697	EU  										COPILOT BRAKE	RESTRICTED      	H				O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			WP	11	20LV					686				FOUND COPILOT BRAKE FLEX HOSES RESTRICTED DUE TO INTERNAL SWELLING OF THE RUBBER.  UNKNOWN IF IMPROPER FLUID EVER USED. 	 BRAKE WOULD LOCK UP WHEN RIGHT BRAKE APPLIED.  NEW HOSES INSTALLED, SYSTEM BLED.  OPS NORMAL.  (X)					1	L	7	1 	3O			RT	A51EU   					 
2000071800519	20000718	00519	SO  	2000	7	18	20000622SH013    	2	19990929	G	7322	30766	FLOAT           	FACET       		AMTR  	VAREZE	VARIEZE     	       	GL  	CONT  	O200  	O200*       	17020	SO  					CARBURETOR	LEAKING         	H				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			GL	13	3798X	1150 				175				ON DEPARTURE, THE ENGINE LOST POWER CAUSING AN INCIDENT.  INSPECTION FOUND A CRACK IN THE FLOAT SIDE AND PARTIALY FILLED	.  NO PREVIOUS INDICATION.  POSSIBLE DUE TO CARBURETOR POSITION.   COMPONENT S/N 104894A1BE1410418.   (X)					1	M	7	1 	3O	3	O	 	EXPA1M71	E252				 
2000071800520	20000718	00520	CE  	2000	7	18	20000622SH014    	1	19990802	G	3250	25430121	BELLCRANK       			CESSNA	303   	T303        	2073820	CE  										NOSE GEAR	CRACKED         	D				O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	3241V					T30300272				CRACKS FOUND IN RADIUS.  (X)						1	L	7	2 	3O			 	A34CE   					 
2000101200169	20001012	00169		2000	10	12	20000622SH017    	4	19991220	G	3416	206070263101	ALTIMETER       			BELL  	407   	407         	       	SW  											FAULTY          	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	491PH	8    				53386				REPLACED WITH NEW ALTIMETER FROM BELL HELICOPTER.  (X)						1	G	7	1 	3U			O	H2SW    					 
2001020200005	20010202	00005	SW  	2001	2	2	20000622SH020    	1	19990826	G	6310	406340102101	SEAL            			BELL  	407   	407         	       	SW  										FREEWHEEL UNIT	DAMAGED         	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	407WH	339  				532027				REPLACED WITH NEW SEAL FROM BELL HELICOPTER.  (X)						1	G	7	1 	3U			O	H2SW    					 
2001020200008	20010202	00008	GL  	2001	2	2	20000622SH023    	2	19991105	G	7320	23069251	FUEL CONTROL    			BELL  	407   	407         	       	SW  	ALLSN 	250C  	250C47B     	 	GL  					HMU	LEAKING         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	99	407CR	407  				53254				FUEL CONTROL (HMU) FOUND LEAKING AT AMBIENT AIR PASSAGE.  LEAK AMOUNT (MOIST TO 1 OR 2 DROPS) AFTER LEAK CHECK, INTERNAL	 LEAKAGE.  (X)					1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
2001020200009	20010202	00009	SW  	2001	2	2	20000622SH024    	1	19991104	G	2435	23081018	STARTER GEN     			BELL  	407   	407         	       	SW  										ENGINE	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	13	407CR	406  				53254				STARTER/GENERATOR FAILED WITH 405.6 TT.  BRUSH LENGTH FAIR TO GOOD.  NOT OIL OR FUEL SOAKED.  BEARINGS OK.  POSSIBLE INT	ERNAL SHORTING.  (X)					1	G	7	1 	3U			O	H2SW    					 
2000062700141	20000627	00141	EU  	2000	6	27	20000622SH032    	1	19991018	G	7931	204A37L62043	TRANSMITTER     			SNIAS 	350   	AS350B      	8680801	EU  											FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	61CU	1    				1636				PRESSURE TRANSMITTER FAILED WITHIN 1.2 HOURS. (X)						1	G	7	1 	3U			 	H9EU    					 
2001020200012	20010202	00012	SW  	2001	2	2	20000622SH033    	1	19991013	G	2425	209070263003	INDICATOR       			BELL  	412   	412EP       	1182205	SW  										DUAL VOLTAGE	INOPERATIVE     	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	414PD	26   				36233				REPLACED WITH NEW INDICATOR FROM BELL HELICOPTER.  (X)						1	G	7	2 	4U			 	H4SW    					 
2001020200013	20010202	00013		2001	2	2	20000622SH037    	4	19991113	G	2200	8241631	POTENTIOMETER   	HAMSTD      		SKRSKY	S76   	S76A        	8143006	NE  										AFSC ACTUATOR	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	72649	8543 	553  		80091184	760292				FEEDBACK POTENTIOMETER PREMATURE FAILURE, CAUSES ACTUATOR TO KICK IN-FLIGHT.  (X)						1	G	7	2 	3U			 	H1NE    					 
2000062700146	20000627	00146	EA  	2000	6	27	20000623SH001    	2	19991102	G	8520		BEARING         			PIPER 	PA32  	PA32300     	7103212	SO  	LYC   	O540  	IO540K1A5   	41532	EA  					ROD	SPUN            	B			YYBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03	4058R	2709 	648  			3240363	L518248			NR 6 ROD BEARING SPUN MANGLED BEARING SHELL..  REMNANTS FOUND IN SUMP.  NR 4 ROD BEARING SPUN, BUT WAS STILL INTACT.  AL	L OTHER ROD BEARINGS SHOWED DISTRESS AS FROM BEING HAMMERED.  IT WAS DETERMINED THE ROD BEARING DISTRESS/FAILURE WAS THE	 RESULT OF STANDARD SIZE ROD BEARINGS BEING INSTALLED IN PLUS .010 INCH CONNECTINGROD BORE.  THE RODS WERE NOT IDENTIFIE	D AS P10 AS INSTRUCTED BY LYC SB 439A.  SUBMITTER STATED THIS PROBLEM WOULD ALSO BE PREVENTED BY BOLTING RODS TOGETHER A	ND MEASURING DIAMETER TO FIND CLEARANCE IS WITHIN MANUFACTURER''S REQUIREMENTS.  (X)		1	L	7	1 	3O	3	O	 	A3SO    	1E4				 
2000062700149	20000627	00149	CE  	2000	6	27	20000623SH004    	1	19990901	G	2430	363800481	DRIVE SHAFT     			BEECH 	36    	A36         	1151604	CE  										STANBY GENERATOR	SHEARED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	23	922CW	537  				E2886				WHILE C/W 500-HOUR STANDBY GENERATOR BRUSH INSPECTION, FOUND DRIVESHAFT IN GENERATOR SHEARED.  (X)						1	L	7	1 	3O			 	3A15    					 
2000062700150	20000627	00150	CE  	2000	6	27	20000623SH005    	1	19991122	G	2720	04117785	RUDDER PEDAL    			CESSNA	182   	182S        	2072701	CE  										LT RUDDER PEDAL	WRONG PART      	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	95260	187  				18280182				THE PILOT''S LEFT RUDDER PEDAL HAS THE WRONG PART NUMBER FORWARD SHAFT INSTALLED FROM FACTORY AND IN THE PARTS BREAKDOWN	.  PN 0411778-5 IS TOO SHORT AND WILL SHEAR THE COTTER PIN ALLOWING SHAFT TO COME OUT.  THIS WOULD CAUSE POTENTIAL LOSS 	OF RUDDER CONTROL.  SUBMITTER STATED:  TO FIX THIS PROBLEM, THE PROPER LENGTH SHAFT SHOULD BE INSTALLED:  PN 0411778-6. 	 (X)			1	H	7	1 	3O			NT	3A13    					 
2000082800018	20000828	00018	GL  	2000	8	28	20000626SH024    	3	19991113	G	6110	OPTIBELT8803M30	BELT            			AMTR  	AVIA  	CHRISTAVIAMK	05602MJ	GL  						AMTR	C8289	C8289       	GL  	PROPELLER ASSY	FAILED          	G				O				OTHER                   				F			FLT CONT AFFECTED         			TO	TAKEOFF        	1			WP	25	62199	220  				999				DURING TAKEOFF, BOTH PROP DRIVE BELTS BROKE CAUSING LOSS OF THRUST.  ACFT DESCENDED RAPIDLY AND IMPACTED THE TERRAIN.  B	ELTS HAD CONSUMED 220 HRS OF 300-HOUR REPLACEMENT TIME.  FAILURE NOT SPECIFICALLY DETERMINED, BUT COULD INCLUDE CAUSAL F	ACTORS SUCH AS UNEVEN WEAR OR TENSION, OR FAILURE OF ONE BELT CAUSING FAILURE OF SECOND DUE TO ENTANGLEMENT.  A SINGLE W	IDE BELT IS ONLY CONFIG NOW AVAILABLE FROM ENG MFG.  SUBMITTER RECOMMENDED ALL 2 BELT CONFIGS STILL IN USE BE CLOSELY IN	SPECTED AND ADJUSTMENT VERIFIED.  (X)		1	H	7	1 	3O			NC	EXPA    		5	N	EXPP5N	 
2001020200015	20010202	00015	NE  	2001	2	2	20000710SH007    	1	19990219	G	5510	7620305001123	SKIN            			SKRSKY	S76   	S76A        	8143006	NE  										STABILIZER	CORRODED        	B			EGRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	764LF	3816 				760264				CORROSION OF VERTICAL STBILIZER SKIN.  (X)						1	G	7	2 	3U			 	H1NE    					 
2001020200021	20010202	00021	EU  	2001	2	2	20000710SH013    	1	19991119	G	5311	1053025152	FRAME           			BOLKMS	117   	BK117A3     	5626015	EU  										FUSELAGE	CRACKED         	B			EGRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	271	6538 				7059				FRAME WAS FOUND CRACKED.  REPAIRED PER AMERICAN EUROCOPTER REPAIR PROCEDURE.  (X)						1	G	7	2 	3U			 	H13EU   					 
2000101600310	20001016	00310	CE  	2000	10	16	20000711SH005    	1	19990526	G	3230	A18MX296	SWITCH          	EATON       		BEECH 	200   	200BEECH    	1152920	CE  										L/G CONTROL	INOPERATIVE     	B			MV1R	O				OTHER                   				J			WARNING INDICATION        			LD	LANDING        	1			EA	17	35				3871	BB88				DURING A FLIGHT TO MGW, PILOT TRIED TO LOWER THE LANDING GEAR FOR LANDING.  THE SYSTEM DID NOT RESPOND.  THE PILOT DECLA	RED AN EMERGENCY THEN PUMPED THE GEAR DOWN MANUALLY.  THE GEAR CAME DOWN AND LOCKED.  THE PILOT LANDED WITHOUT FURTHER I	NCIDENT.  MAINTENANCE FOUND THAT MICROSWITCH NR 1 IN THE LANDING GEAR CONTROL WAS BROKEN INTERNALLY.  REPLACED LANDING G	EAR CONTROL.  OPERATED SYSTEM UP AND DOWN SEVERAL TIMES IAW BE200.2 MM.  OPS CHECKED OK. (X)			1	L	7	2 	4T			 	A24CE   					 
2001020200035	20010202	00035	SW  	2001	2	2	20000712SH006    	1	19991119	G	5302	206020113129	STRUCTURE       			BELL  	206   	206L3       	1182108	SW  										VERTICAL FIN	CRACKED         	C			EGRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	33PP	8270 				51051				CRACK ON UPPER PORTION OF LEFT SIDE.  CRACK TRAVELED ALMOST THE ENTIRE LENGTH OF FIN.  THE FIN WAS REMOVED FROM SERVICE.	  A REPLACEMENT FIN WAS ORDERED.  (X)					1	G	7	1 	3U			 	H2SW    					 
2001020200038	20010202	00038	EU  	2001	2	2	20000712SH010    	1	19991220	G	7120	1176272101	MOUNT           			BOLKMS	117   	BK117A3     	5626015	EU  										ENGINE	CRACKED         	B			EGRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	532KH	4852 				7069				MOUNT CRACKED AT THE INNER MOUNT LUG.  REPLACED WITH NEW PART IAW THE MFG MM.  (X)						1	G	7	2 	3U			 	H13EU   					 
2001020200041	20010202	00041	NE  	2001	2	2	20000712SH016    	1	19990728	G	5320	MJLH2577010	NUT             			SKRSKY	S76   	S76B        	8143007	NE  										FUSELAGE	CRACKED         	B			EGRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	9NJ	4635 				760345				TWO EACH BARREL NUTS WERE REMOVED DUE TO CRACKS.  INSTALLED 2 NEW BARREL NUTS.  (X)						1	G	7	2 	4U			 	H1NE    					 
2001020200042	20010202	00042	EU  	2001	2	2	20000712SH017    	1	19990219	G	5320	1172230320	STIFFENER       			BOLKMS	117   	BK117B1     	5626012	EU  										FUSELAGE	CRACKED         	B			EGRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	911CH	3602 				7223				STIFFENER CRACKED,  A REPAIR WAS MADE.  (X)						1	G	7	2 	3U			 	H13EU   					 
2001020200043	20010202	00043	EU  	2001	2	2	20000712SH018    	1	19990219	G	5320	1172230331	STIFFENER       			BOLKMS	117   	BK117B1     	5626012	EU  										FUSELAGE	CRACKED         	B			EGRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	911CH	3602 				7223				STIFFENER CRACKED.  A REPAIR WAS MADE.  (X)						1	G	7	2 	3U			 	H13EU   					 
2001020200044	20010202	00044	EU  	2001	2	2	20000712SH019    	1	19990219	G	5311	1053025151001	FRAME           			BOLKMS	117   	BK117B1     	5626012	EU  										FUSELAGE	CRACKED         	B			EGRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	911CH	3602 				7223				FRAME 10L IS CRACKED.						1	G	7	2 	3U			 	H13EU   					 
2000101800113	20001018	00113	NE  	2000	10	18	20000712SH021    	2	19990721	G	7250	2A0851	SEAL            								IAE   	V2500 	V2500A1     	 	NE  					NR 4 TOP SURFACE	CRACKED         	B			KB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03										PART RECEIVED FOR FLUORESCENT PENETRANT INSPECTION PER SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501, IAW	 INTERNATIONAL AERO ENGINE V2500 PROPULSION SYSTEM ENGINE MANUAL, REV. 38.  PART REJECTED AT F.P.I. DUE TO CRACK 0.3580 	INCH LONG ON TOP SURFACE.  (X)									4	F			E311NE				 
2000101800116	20001018	00116	GL  	2000	10	18	20000712SH025    	3	19990712	G	6111	V8433N7R	BLADE           	HARTZL      												HARTZL	HCA2X	HCA2XK1     	GL  		CRACKED         	B			NWOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05								J1119		TRAILING EDGE OF BLADE CRACKED APPROXIMATELY 2.50 INCHES LONG.  (X)																5	C	P908	 
2001011103990	20010111	03990		2001	1	11	20000712SH026    	1	19990119	G	7920	CH48110	OIL FILTER      																	INNER SEAL RING	CRACKED         	B			DY1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13										DURING ROUTINE OIL CHANGE, FILTER WAS VISUALLY EXAMINED BEFORE INSTALLATION.  METAL RING INSIDE OF O-RING SEAL SURFACE W	AS FOUND CRACKED AND CUT.  (OIL FILTER LOT NR IS F06J02-1).  SUBMITTER STATED ALL FILTERS NEED A VISUAL INSPECTION FOR D	EFECTS BEFORE INSTALLATION TO DETECT SUCH PROBLEMS.  (X)																	 
2000101800072	20001018	00072	CE  	2000	10	18	20000712SH027    	1	19991101	G	6100		PROPELLER       			CESSNA	210   	P210N       	2073454	CE  						MCAULY	D3A34	D3A34C402   	GL  		MALFUNCTIONED   	H				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			WP	21	4706A	22   				P21000817		980891		PROPELLER IS UNCONTROLLABLE, TO LOWER PITCH, AT HIGH ALTITUDE (COLD TEMPERATURE).  NEW PROPELLER FROM MANUFACTURER.  INS	TALLED SERVICEABLE PROPELLER.  ALL SYSTEMS WORK NORMALLY.  INSTALLED ANOTHER NEW PROPELLER, ALL SYSTEMS WORK NORMALLY.  	POSSIBLE WRONG GREASE IN HUB OR TOLERANCE TOO TIGHT.  (X)				1	H	7	1 	3O			 	3A21    		5	C	P47GL	 
2000101800117	20001018	00117		2000	10	18	20000712SH028    	4	19990326	G	3416	A30	ENCODER         			CESSNA	150   	152         	2071835	CE  											FAILED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	10	94299	698  				15285646				REPORTING INVALID ALTITUDE SEVERAL DIFERENT DATES.  REPLACED WITH NEW ENCODER OF DIFFERENT MFG.  (X)						1	H	7	1 	3O			NT	3A19    					 
2000101800138	20001018	00138	NE  	2000	10	18	20000712SH030    	2	19990330	G	7250	2A0851	SEAL            								IAE   	V2500 	V2500A1     	 	NE  					NR 4 TOP SURFACE	CRACKED         	B			KB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03							V0185			PART REJECTED AT F.P.I. DUE TO A CRACK 0.180 INCH ON TOP SURFACE.  (X)											4	F			E311NE				 
2001020200045	20010202	00045	GL  	2001	2	2	20000712SH031    	2	19990405	G	7313	47086	FILTER          	ALLSN       		BOLKMS	105   	BO105CBS    	5626008	EU  	ALLSN 	250C  	250C20B     	03013	GL  					FUEL NOZZLE	CONTAMINATED    	B			HEFR	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			WP	21	10VH		924  		AG27444	S619	CAE834779			UNIT WAS IN FOR FUNCTIONAL TEST ONLY.  DISASSEMBLED UNIT FOR POSSIBLE FILTER CONTAMINATION AND FOUND 50 PERCENT OF FILTE	R COVERED WITH BLACK PARTICLES AND CHIPS OF METAL.  (X)					1	G	7	2 	3U	3	U	NC	H3EU    	E4CE				 
2000102400269	20001024	00269	NE  	2000	10	24	20000712SH032    	2	19990330	G	7250	2A0851	BEARING         								IAE   	V2500 	V2500A1     	 	NE  					TOP SURFACE NR 4	CRACKED         	B			KB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03							0213			PART REJECTED AT F.P.I. DUE TO A CRACK ON TOP SURFACE, .0175 INCH.  (X)											4	F			E311NE				 
2001011100928	20010111	00928		2001	1	11	20000712SH034    	1	19990622	G	7920	47086	FILTER          	ALLSN       							ALLSN 	250C  	250C20B     	03013	GL  					FUEL NOZZLE	TORN            	B			HEFR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	21					AG32550					UNIT WAS IN FOR OVERHAUL.  DISASSEMBLED UNIT FOR INSPECTION AND FOUND FILTER SCREEN TORN AT BRAZE.  (X)											3	U			E4CE				 
2000101800075	20001018	00075	GL  	2000	10	18	20000712SH035    	3	19990614	G	6114	D4883C55	HUB             													MCAULY	2AF34C	2AF34C55    	GL  	NR 1 BLADE SOCKT	CRACKED         	B			DJFR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	23			141  					687339		PROPELLER LEAKING RED OIL.  DISASSEMBLED AND FOUND CRACK IN THREADS, NR 1 BLADE SOCKET.  (X)																5	C	P5EA	 
2000101800076	20001018	00076	CE  	2000	10	18	20000712SH036    	1	19990609	G	7921	1E1326	COOLER          			CESSNA	310   	310         	2074202	CE  	CONT  	O520  	IO520*      	17032	SO  					CORE	LEAKING         	B			RF3R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	23										PART BEGAN LEAKING DURING NORMAL SERVICE DUE TO EPOXY REPAIR FAILURE.  SUBMITTER RECOMMENDED ELIMINATING USE OF EPOXY RE	PAIR ON AND IN OIL COOLERS AS EPOXY REPAIR FAILURE IS VERY COMMON WHEN USED ON OIL COOLERS.  (X)					1	L	7	2 	3O	3	O	RT	3A10    	E5CE				 
2000102400075	20001024	00075	WP  	2000	10	24	20000712SH038    	2	19990726	G	7250	30740962	TURBINE WHEEL   								GARRTT	TFE731	TFE7313R    	01518	WP  					3RD STAGE	CHAFED          	B			XB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09		355  					84412			SECOND OCCURRENCE OF 3RD STAGE LP TURBINE RUBBING FORWARD SIDE OF 3RD STAGE LPT SEAL.  (X)											4	F			E6WE				 
2000102400044	20001024	00044	NE  	2000	10	24	20000712SH040    	2	19990510	G	7250	2A0847	BEARING         								IAE   	V2500 	V2500A1     	 	NE  					OD WALL & ID FLG	CRACKED         	B			KB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	Q6						0260			PART REJECTED FOR CRACKS IN 2 PLACES.  2 CRACKS ON OUTSIDE DIAMETER WALL IN CLOSE LINEAR ALIGNMENT - 0.060 INCH THICK.  	CRATER TYPE CRACK IN INSIDE DIAMETER FLANGE, 0.125 INCH DIAMETER.  (X)										4	F			E311NE				 
2000102400046	20001024	00046	NE  	2000	10	24	20000712SH041    	2	19990208	G	7250	2A0851	BEARING         								IAE   	V2500 	V2500A1     	 	NE  					TOP SURFACENR 4	CRACKED         	B			KB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03							V0201			PART REJECTED FOR CRACKS 2 PLACES ON TOP SURFACE:  CRACK NR 1, THROUGH CRACK .400 INCH LONG.  CRACK NR 2, CRACK 0.500 IN	CH LONG.  (X)										4	F			E311NE				 
2001011103991	20010111	03991		2001	1	11	20000712SH042    	2	19990113	G	7414	ES103825881	COIL            	BENDIX      																OUTPUT TAB	CRACKED         	B			KC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03					8012814					***NO ENGINE SUBMITTED WITH THIS SDR***THIS MAGNETO WAS OVERHAULED, S/N 5080123.  IT WAS REMOVED FOR A ROUTINE 500-HOUR 	INSPECTION.  THE LEFT COIL MANUFACTURED BY ELECTOSYSTEMS, WITH A DATE CODE OF 4 95, WAS FOUND WITH A CRACK EXTENDING THE	 LENGTH OF THE COIL BY THE HIGH TENSION OUTPUT TAB.  (X)																	 
2000101800046	20001018	00046	SW  	2000	10	18	20000713SH002    	1	19990507	G	3230	5630923	CLUTCH          	PLESSEY     		MOONEY	M20   	M20J        	5870219	SW  										INTERNAL/MTR DR	BROKEN          	B			DY1R	A				UNSCHED LANDING         				O			OTHER                     			CL	CLIMB          	1			EA	13	10848	763  			911003	243266				AIRCRAFT OWNER REPORTED GEAR WILL NOT RETRACT, TRIPS CIRCUIT BREAKER. REMOVED JAMMED GEAR MOTOR ASSY, AND FOUND CLUTCH S	PRING TAB BROKEN.  SPRING WAS REPLACED 763 HOURS AGO IAW MOONEY SI M20-92 PER RECOMMENED REPLACEMENT SCHEDULE OF EVERY 1	,000 HRS TIS.  CAUSE OF FAILURE UNKNOWN.  THIS IS A CLUB AIRCRAFT WHICH ACCUMULATES AN AVERAGE OF 350 HRS - 400 HRS ANNU	ALLY, BUT IS KEPT IN GOOD MECHANICAL CONDITION.  POSSIBLE HIGHER THAN NORMAL GEAR CYCLING USE, OR DEFECTIVE SPRINGS.  SU	BMITTER SUGGESTED LOWERING HOURS OF TIME IN SERVICE BETWEEN SPRING CHANGES IF THIS IS A RECURRING PROBLEM IN THE FLEET. 	 (X)	1	L	7	1 	3O			 	2A3     					 
2001020200046	20010202	00046	WP  	2001	2	2	20000713SH003    	1	19990404	G	6310	369D25351	SPRAG CLUTCH    			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					M/R CLUTCH	BROKEN          	B			GHHR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	1109P	294  			6779	1100849D	CAE833681			NO INDICATION OF SPRAG FAILURE, NORMAL ENGINE AND ROTOR COAST DOWN ON SHUT DOWN.  BROKEN SPRAG FOUND WHEN CLUTCH WAS DIS	ASSEMBLED FOR 300-HOUR INSPECTION.  (X)					1	G	7	1 	3U	3	U	 	H3WE    	E4CE				 
2000102400188	20001024	00188	CE  	2000	10	24	20000713SH007    	1	19990602	G	7603	C289505050	THROTTLE CABLE  			CESSNA	185   	A185F       	2072821	CE  										ENGINE COMPT	BROKEN          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	23	1743R	700  				18502463				THROTTLE CABLE OUTER HOUSING SEPARATED AT THE THROTTLE HORN END CAUSING SLOPPY OPERATION OF THROTTLE CONTROL.  (X)						1	H	7	1 	3O			 	3A24    					 
2001020200047	20010202	00047	SW  	2001	2	2	20000713SH008    	1	19990803	G	6510	406040340101	DISC PACK       			BELL  	407   	407         	       	SW  										T/R DRIVESHAFT	NICKED          	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	175P	9    				53316				REJECTED DISK PACK REPLACED WITH NEW FROM BELL HELICOPTER.  (X)						1	G	7	1 	3U			O	H2SW    					 
2000102400124	20001024	00124	EA  	2000	10	24	20000713SH011    	2	19990512	G	8520	3227	CASE            			GULSTM	500   	500S        	0141107	SW  	LYC   	O540  	IO540E1B5   	41532	EA  					UNDER CYL NR 2	CRACKED         	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			GL	03	2BZ	6673 	782  			3227	L1253948			CRACKS IN CASE HALF AROUND NR 2 CYLINDER.  FOUND DURING INSPECTION FOR OIL LEAK.  (X)						1	H	7	2 	3O	3	O	 	6A1     	1E4				 
2000102400125	20001024	00125	SO  	2000	10	24	20000713SH012    	1	19990517	G	3234	688131	SWITCH          			PIPER 	PA34  	PA34200T    	7103406	SO  										INSTRUMENT PANEL	BROKEN          	C				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	11	224BD	20   				348133186				LANDING GEAR SELECTOR SWITCH BROKE OFF UPON SELECTING GEAR UP.  THE SHAFT ON THE SWITCH SNAPPED AND APPEARS TO HAVE BEEN	 OVERSTRESSED OR WEAK MATERIAL.  (X)					1	L	7	2 	3O			 	A7SO    					 
2000102400131	20001024	00131	SO  	2000	10	24	20000713SH016    	1	19990609	G	2821		STRAINER        			PIPER 	PA28  	PA28R201    	7102816	SO  										THREADS	DEFECTIVE       	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	36282					28R7837271				COULD NOT TIGHTEN FUEL BOWL.  FOUND THREADS STRIPPED.  SUBMITTER RECOMMENDED CHANGING DESIGN TO A THREADED FUEL FILTER B	OWL ASSY.  FOUND DURING 100-HOUR INSPECTION.  (X)					1	L	7	1 	3O			 	2A13    					 
2000102400132	20001024	00132	SO  	2000	10	24	20000713SH017    	1	19990408	G	3230	AN551	BOLT            			PIPER 	PA28  	PA28RT201   	7102818	SO  										NOSE GEAR	WORN            	C				O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			NE	01	3059Z	3000 				28R918123				THE AN5-51 BOLT THAT ATTACHES THE SPRING ARM AND DRAG LINK TO THE TRUNNION WAS REMOVED FOR INSPECTION AFTER NOSE GEAR FA	ILED TO EXTEND.  THE WEAR PATTERN APPEARED NORMAL, BUT WAS DEEP ENOUGH TO REQUIRE REPLACEMENT.  SUBMITTER RECOMMENDED IN	SPECTION OF THIS BOLT WITHIN THE NEXT 25 HOURS TIS FOR WEAR.  IF WORN, REPLACE BEFORE FURTHER FLIGHT.  THEREAFTER, INSPE	CT EVERY 500 HOURS TIS IF AIRCRAFT USED FOR PILOT TRAINING, OR EVERY 5 YEARS FOR NON-TRAINING AIRCRAFT.  (X)			1	L	7	1 	3O			 	2A13    					 
2001020200048	20010202	00048	EU  	2001	2	2	20000713SH018    	1	19990730	G	6520	350A33215300	BEARING         			SNIAS 	350   	AS350BA     	8680817	EU  										TAIL ROTOR	FAILED          	E				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	11	318SA	611  				3046				THIS HAS BEEN THE SECOND OCCURRENCE IN WHICH THE T/R SPHERICAL BEARINGS HAVE FAILED.  THE FIRST OCCURRED AT ACTT:  138.2	 HOURS IN WHICH THE MECHANIC FOUND THE BEARING ELASTOMERS TORN BEYOND LIMITS.  THE SECOND FAILURE OCCURRED AT 748.7 HOUR	S ACTT, PART TT, 610.5 HOURS .  PILOT NOTED A VIBRATION IN THE AIRFRAME.  UPON INSPECTION, THE MECHANIC NOTED THE SPHERI	CAL BEARING ELASTOMERS WERE COMPLETELY WORN THROUGH.  BOTH THESE FAILURES OCCURRED ON AN AIRCRAFT WITH A TT OF 748.7 HOU	RS.  (X)		1	G	7	1 	3U			NC	H9EU    					 
2000102400133	20001024	00133	SO  	2000	10	24	20000713SH019    	1	19990722	G	3233	SFA2325	ACTUATOR        			PIPER 	PA32  	PA32R301T   	7103220	SO  										ACTUATOR SHAFT	LEAKING         	B			AMYR	O				OTHER                   				K			FLUID LOSS                			CR	CRUISE         	1			CE	05	4134D	143  				3257070				MALFUNCTION OCCURRED IN-FLIGHT.  PILOT REPORTED HYDRAULIC PUMP FAILURE IN-FLIGHT.   TROUBLESHOT PROBLEM, DETERMINED THAT	 LT MAIN GEAR ACTUATOR WAS LEAKING AT ACTUATOR SHAFT, AS WELL AS NOSE GEAR ACTUATOR LEAKING INTERNALLY AND SUCKING IN AI	R, ALL CONTRIBUTING TO CAUSE HYDRAULIC PUMP TO CYCLE CONTINUOUSLY AND FAIL.  (X)				1	L	7	1 	3O			 	A3SO    					 
2000102400134	20001024	00134	SO  	2000	10	24	20000713SH020    	1	19990722	G	5280	67090010	BRACKET         			PIPER 	PA32  	PA32R301T   	7103220	SO  										LT MAIN DOOR	CRACKED         	B			AMYR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	05	4134D	143  				3257070				AIRCRAFT WAS IN FOR OTHER MAINTENANCE AND FOUND LT MAIN GEAR DOOR CRACKED AT GEAR DOOR ATTACH BRACKET.  (X)						1	L	7	1 	3O			 	A3SO    					 
2000102700001	20001027	00001	SO  	2000	10	27	20000713SH021    	1	19990722	G	2913	636029	PUMP            			PIPER 	PA32  	PA32301T    	7103209	SO  										INTERNAL SEAL	INOPERATIVE     	B			AMYR	O				OTHER                   				K			FLUID LOSS                			CR	CRUISE         	1			CE	05	41340	143  				3257070				MALFUNCTION OCCURRED IN-FLIGHT.  PUMP SEAL WENT BAD.  ALL FLUID LEAKED OUT AND GEAR FREE FELL TO DOWN AND LOCKED POSITIO	N.  TROUBLESHOT PROBLEM, DETERMINED LT MAIN GEAR ACTUATOR WAS LEAKING AND NOSE GEAR ACTUATOAR WAS SUCKING AIR CAUSING PU	MP TO CYCLE. THIS CYCLING CAUSED PUMP TO FAIL AND FLUID TO ALL LEAK OUT WHICH IS WHEN THE PILOT NOTICED A PROBLEM WHEN H	IS GEAR FELL DOWN AND LOCKED IN CRUISE FLIGHT.  (X)			1	L	7	1 	3O			 	A3SO    					 
2000102400135	20001024	00135	SO  	2000	10	24	20000713SH022    	1	19990722	G	2913	6326029	PUMP            			PIPER 	PA32  	PA32R301T   	7103220	SO  										FLUID LEAKS/PUMP	INOPERATIVE     	B			AMYR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CE	05	4134D					3257070				RECEIVED NEW PUMP FROM PIPER AND INSTALLED ON AIRCRAFT THEN FOUND THROUGH BLEEDING AND OPS CHECK OPERATIONS THAT NEW PUM	P WAS BLEEDING OFF PRESSURE BACK THROUGH THE PUMP.  (X)					1	L	7	1 	3O			 	A3SO    					 
2000102400136	20001024	00136	EA  	2000	10	24	20000713SH026    	2	19990521	G	8520	351385015	STUD            			GULSTM	500   	500B        	0141106	SW  	LYC   	O540  	IO540E1A5   	41532	EA  						BROKEN          	E				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	411PT		1430 			500B120799	RL298248			NR 6 CYLINDER HOLD-DOWN STUDS, 4 EACH P/N 38-13, 2 EACH P/N 38-13, WERE BROKEN CAUSING OIL LEAKS AND VIBRATION.  OIL LEA	K WAS DETECTED ON POST-FLIGHT.  (X)					1	H	7	2 	3O	3	O	 	6A1     	1E4				 
2000102400080	20001024	00080	CE  	2000	10	24	20000714SH001    	1	19990106	G	2842	S33311	SENSOR          			CESSNA	172   	172R        	2072401	CE  										RT WING FUEL TAN	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	445ER	340  				17280662				DURING A POST INSPECTION RUN-UP, THE RIGHT FUEL GAUGE NEEDLE WAS READING ERRATIC (FULL TO ZERO).  INSPECTION OF THE FUEL	 INDICATION SYSTEM FOUND THE RT FUEL TANK SENDER BAD.  REPLACEMENT OF THE SENDER UNIT HAS CORRECTED THIS PROBLEM FOR A S	HORT TIME.  THERE HAS BEEN A HIGH NUMBER OF SENDERS; BOTH LEFT AND RIGHT, REPLACED IN FLEET OF 53 CESSNA 172R''S SINCE T	HEIR ARRIVAL.  (X)			1	H	7	1 	3O			NT	3A12    					 
2000102400085	20001024	00085	SO  	2000	10	24	20000714SH004    	1	19990127	G	2121	554901	CLAMP           			PIPER 	PA31T 	PA31T       	7103124	SO  										NOSE	LOOSE           	D				I				CABIN DEPRESSURIZATION  				O			OTHER                     			CR	CRUISE         	1			SW	07	53AM					31T7920037				ENVIRONMENTAL SYSTEM INTERCONNECT HOSE, P/N 49990-07, PULLED FREE FROM UNDER CLAMP, P/N 554-901, AND STRAP, P/N 49989-05	, FOR A LENGTH FROM 10 TO 2 O''CLOCK POSITION.  THE STRAP AND CLAMP WERE STILL IN PLACE.  AIRCRAFT WAS AT 27,000 FEET WH	ICH CAUSED IMMEDIATE DECOMPRESSION.  CORRECTIVE ACTION WAS TO RETURN INTERCONNECT HOSE TO PROPER LOCATION UNDER CLAMP AN	D STRAP AND RE-TORQUE CLAMP.   THERE ARE SIMILAR CLAMPING ARRANGEMENTS ON THE NOSE SECTION ENVIRONMENTAL DUCT WORK.  SUG	GEST TORQUE CHECK OF CLAMPS AT EACH EVENT INSPECTION.  (X)		1	L	7	2 	3T			 	A8EA    					 
2000102600004	20001026	00004	NE  	2000	10	26	20000714SH005    	2	19990808	G	8530	399354	CYLINDER        			DHAV  	DHC2  	DHC2*       	2800108	EA  	PWA   	R985  	R985SB3     	52008	NE  					CYL HEAD, NR 2	SEPARATED       	E				A				UNSCHED LANDING         				Y			ENGINE STOPPAGE           			CR	CRUISE         	1			AL	03	2740X		1381 			579	21389			NR 2 CYLINDER HEAD SEPARATED FROM BARREL.  AIRCRAFT IN CRUISE, PRECAUTIONARY LANDING MADE WITHOUT INCIDENT.  SUBMITTER R	ECOMMENDED UNTHREADING OF CYLINDER HEAD/BARREL AT OVERHAUL OR MANUFACTURE OF NEW CYLINDER ASSY.  (X)					1	H	7	1 	3R	3	R	 	A806    	5E1				 
2000102400086	20001024	00086	EA  	2000	10	24	20000714SH006    	2	19990222	G	8520	72877	TAPPET          			PIPER 	PA32  	PA32300     	7103212	SO  	LYC   	O540  	IO540K1A5   	41532	EA  						DEFECTIVE       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03	5481T					327240107	L992948			ALL POSITIONS EXCEPT REARMOSTFOLLOWING EMERG LANDING, ENG TEARDOWN REVEALED ALL BUT ONE OF THE TAPPET FACES BROKEN.  ENG	 STILL FUNCTIONING, BUT OIL PRESS WAS VERY LOW AT SHUTDOWN SINCE THE COURSE OIL SCREEN WAS 2/3 FULL OF PEA-SIZED AND SMA	LLER PIECES OF TAPPET BODY FACES WHICH HAD BEEN BROKEN OFF LIKE WEDGES OF A PIE.  ENG TIME SMOH:  995 HRS.  TT:  4,968 H	RS.  POSSIBLE CAUSE WAS ONE BROKEN TAPPET BODY FACE WHICH WAS KICKED BY SPINNING CRANK AND WEDGED BEHIND ANOTHER RECEDIN	G TAPPET BODY AND SOON THROUGH THE ENGINE.  CASE BROKEN OUTWARD IN 3 PLACES WHERE PRESS WOULD HAVE BEEN APPLIED BY SOMET	HING WEDGED BEHIND A TAPPED BODYFACE.  MAGNAFLUX INSP OF REWORKED TAPPETS SHOULD PREVENT THIS.	1	L	7	1 	3O	3	O	 	A3SO    	1E4				 
2001011103992	20010111	03992	GL  	2001	1	11	20000714SH007    	3	19990623	G	6110		CLAMP           			PIPER 	PA24  	PA24250     	7102404	SO  						HARTZL	HC82V	HC82VK2     	GL  	PITCH CHANGE BLO	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	11	5441P		87   			24495		959G		EXCESS PLAY NR 1 BLADE.  REMOVED SPINNER, FOUND BOLT, P/N A295, THAT SECURES PITCH CHANGE BLOCK BROKEN.  (X)						1	L	7	1 	3O			 	1A15    		5	C	P23EA	 
2000102600006	20001026	00006	EA  	2000	10	26	20000714SH009    	1	19990415	G	5541		RUDDER          			SCWZER	G164  	G164A       	3952704	EA  										SPAR	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	5304	7555 				593				AN INTERNAL INSPECTION OF THE RUDDER SPAR RECEIVED CORROSION.  AD 78-08-09 REQUIRES AN EXTERNAL VISUAL INSPECTION EACH 3	00 HRS.  SUBMITTER RECOMMENDED AN INTERNAL INSPECTION AT EACH ANNUAL AND FOR ALL G-164 SERIES AIRCRAFT.  (X)					1	Q	7	1 	3R			 	1A16    					 
2000102600007	20001026	00007	CE  	2000	10	26	20000714SH012    	1	19990814	G	2701	9652402915	ADAPTER         			BEECH 	56    	56TC        	1152736	CE  										CONTROL COLUMN	BROKEN          	D				A				UNSCHED LANDING         				F			FLT CONT AFFECTED         			CR	CRUISE         	1			NM	02	6252V					TG49				PILOT MADE AN ABRUPT CONTROL MOVEMENT AND THE ADAPTER ASSY BROKE AT THE WELD.  THE CONTROL YOKE CAME OFF, PILOT LANDED T	HE AIRCRAFT WITHOUT INCIDENT.  AD 71-24-10 RELATES TO THIS SPECIFIC PART.  SUBMITTER RECOMMENDED ALL ADAPTERS BE REPLACE	D WITH P/N 96-524029-31.  THIS AIRFRAME ONLY HAD 1.981 HOURS TOTAL TIME.  (X)				1	L	7	2 	3O			 	3A16    					 
2000102600008	20001026	00008	CE  	2000	10	26	20000714SH013    	1	19990811	G	3222	07410094	SPRING          			CESSNA	182   	182         	2072702	CE  										RT MAIN L/G	BROKEN          	H				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			GL	23	6284A					33084				AIRCRAFT TT 7,577 HOURS.  RIGHT SIDE MAIN SPRING LANDING GEAR BROKE ON LANDING.  SPRING LANDING GEAR BROKE APPROXIMATELY	 3 INCHES FROM FUSELAGE ON A LINE THROUGH THE DIMPLES IN THE SPRING GEAR THAT HOLDS THE BRAKE LINE RETAINER BRACKET.  (X	)				1	H	7	1 	3O			NT	3A13    					 
2000102400039	20001024	00039	CE  	2000	10	24	20000714SH014    	1	19990201	G	3230	08411062	BELLCRANK       			CESSNA	310   	310K        	2074228	CE  										RT INBD GEAR DOO	BROKEN          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	21	6942L	8000 				310K0042				RIGHT INBOARD GEAR DOOR FAILED TO CLOSE AFTER GEAR EXTENSION.  (X)						1	L	7	2 	3O			 	3A10    					 
2000102400040	20001024	00040	CE  	2000	10	24	20000714SH015    	1	19990305	G	5751	122005217	BRACKET         			CESSNA	206   	TU206G      	2073357	CE  										LT OUTBOARD	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	682RC	2169 				U20605537				THIS AIRCRAFT IS EQUIPPED WITH A ROBERTSON STOL KIT.  BOTH OUTBOARD AILERON ATTACH BRACKETS WERE FOUND CRACKED AND BROKE	N.  THE ADDITIONAL STRESSES RELATED TO THE ROTATION CAUSED THIS CONDITION.  THESE PARTS SHOULD BE INSPECTED ON ALL ROBER	TSON EQUPPED AIRCRAFT.  (X)				1	H	7	1 	3O			 	A4CE    					 
2000102400041	20001024	00041	CE  	2000	10	24	20000714SH016    	1	19990305	G	5751	122005218	BRACKET         			CESSNA	206   	TU206G      	2073357	CE  										RT OUTBOARD	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	682RC	2169 				U20605537				THIS AIRCRAFT IS EQUIPPED WITH A ROBERTSON STOL KIT.  BOTH OUTBOARD AILERON ATTACH BRACKETS WERE FOUND CRACKED AND BROKE	N.  THE ADDITIONAL STRESSES RELATED TO THE ROBERTSON CAUSED THIS CONDITON.  ALL ROBERTSON STOL EQUIPPED AIRCRAFT SHOULD 	HAVE THIS BRACKET INSPECTED.  (X)				1	H	7	1 	3O			 	A4CE    					 
2000102400043	20001024	00043	EA  	2000	10	24	20000714SH018    	2	19990616	G	7414	M3114C	COIL            	SLICK       		CESSNA	172   	172N        	2072434	CE  	LYC   	O360  	O360A4M     	41514	EA  					INTERNAL/OPEN	DEFECTIVE       	D				O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	7382T	1900 			90060206	17270372	L3255636A			HAVE FOUND FOUR OCCURRENCES OF FAULTY COILS IN SLICK MAGNETOS WITH HOURS FROM 400 - 1,900.  SOME COILS ARE OLDER, P/N M3	114C.  REPLACEMENT P/N, K3975.  (X)					1	H	7	1 	3O	3	O	NT	3A12    	E286				 
2000071800105	20000718	00105	SO  	2000	7	18	20000714SH021    	2	19990816	G	8530	25117	PLUG            			PIPER 	J3    	J3C65       	7100510	SO  	CONT  	A65   	A651        	17003	SO  					PISTON PIN	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03	88366	85   				15984	31143			FOLLOWING MAJOR OVERHAUL, ALUM PARTICLES WERE FOUND IN THE OIL SCREEN AT 30, 55, AND 75 HOURS.  CYLINDERS WERE REMOVED A	ND THE PISTON PIN PLUGS WERE FOUND WORN ON THE SHANK IN THE FORM OF A TAPER.  THE PINS AND PLUGS WERE NEW AND CAME FROM 	A SET.  THE OVERHAUL MANUAL CALLS FOR THESE TO BE A .0005 INCH TO .0025 INCH TIGHT FIT, BUT THE SERVICE LIMIT IS .003 IN	CH LOOSE AND PLUGS HAVE ALWAYS SLID IN AND OUT.  SUBMITTER STATED THEIR FIX WAS TO GET PLUGS WITH A .0025 INCH FIT.  (X)			1	H	7	1 	3O	3	O	 	A691    	E205				 
2001020200049	20010202	00049	GL  	2001	2	2	20000714SH022    	1	19990609	G	6400	28172011	GUARD           			ENSTRM	F28   	F28F        	3300412	GL  										TAIL ROTOR	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	86243					724				TAIL ROTOR GUARD CRACKED DUE TO VIBRATION.						1	G	7	1 	3O			 	H1CE    					 
2000071800126	20000718	00126	EA  	2000	7	18	20000714SH025    	2	19990623	G	7322	229164	ACCELL PUMP     	PRECISION   		PIPER 	PA28  	PA28161     	7102803	SO  	LYC   	O320  	O320D3G     	41508	EA  					DISCHGNOZZLETUBE	BROKEN          	D				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			EA	07			1080 		CK35988	288816017				AIRCRAFT RAN ROUGH AND DAMAGED MUFFLER.  FOUND ACCELERATOR PUMP DISCHARGE TUBE BROKEN OFF LETTING UNMETERED FUEL ENTER I	NTAKE SYSTEM CAUSING EXCESSIVELY RICH MIXTURE.  SUBMITTER SUGGESTED INSPECTING INSIDE CARBURETOR THROAT WITH MIRROR AT I	NSPECTIONS.  (X)				1	L	7	1 	3O	3	O	 	2A13    	E274				 
2000071800127	20000718	00127	CE  	2000	7	18	20000714SH026    	1	19990416	G	5210		DOOR SEAL       			CESSNA	500   	550         	2076604	CE  											DEFLATED        	H				O				OTHER                   				O			OTHER                     			DE	DESCENT        	1			SO	16	926RM					5500567				WHILE IN DESCENT TO GNV, CABIN LOST PRESSURIZATION.  FOUND MOISTURE IN DOOR SEAL LINE.  FACTORY SAYS LINE SHOULD BE PURG	ED MONTHLY OR AFTER HEAVY RAIN.  MOISTURE FROZE AND CUT OFF AIR SUPPLY TO DOOR SEAL DEFLATING SEAL AND LOOSING CABIN PRE	SSURE.  (X)				1	L	7	2 	4F			 	A22CE   					 
2000071800128	20000718	00128	NM  	2000	7	18	20000714SH027    	1	19990624	G	3211	20002102	FITTING         			PIPER 	PA60  	PA60601P    	7106012	NM  										INBD GEAR SIDE	CORRODED        	B			DY1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	9807Q	2065 				61P0448171				DURING ANNUAL INSPECTION, FOUND SEVERAL AREAS THROUGHOUT AIRFRAME HAVE SURFACE CORROSION STARTING.  RIGHT WING GEAR AFT 	SIDE BRACE SUPPORT FITTING HAS INTERGRANULAR CORROSION VISIBLE.  REMOVED FITTING FOR REPLACEMENT.  OTHER AREAS THROUGHOU	T AIRFRAME CAN BE REPAIRED USING STANDARD REMOVAL, AND REPRIMER TECHNIQUES.  AIRCRAFT WILL BE TREATED WITH ''CORROSION X	'' AFTER ALL PAINTING IS COMPLETED.  AIRCRAFT SPENDS TIME NEAR ''SALT AIR'' ENVIRONMENT ON OUTSIDE RAMP AROUND ONE-THIRD	 OF THE YEAR; OTHERWISE, IS KEPT IN HANGAR AT HOME BASE.  AS THE AEROSTAR FLEET CONTINUES TO AGE, INCREASED VIGILANCE IS	 REQUIRED FOR SUCH CONDITIONS.  (X)	1	M	7	2 	3O			RT	A17WE   					 
2000071800129	20000718	00129	SW  	2000	7	18	20000714SH028    	1	19990323	G	3230	560244501	ROD END         			MOONEY	M20   	M20R        	5870225	SW  	CONT  	O550  	IO550G      	17042	SO  					AFT SECT OF ROD	LOOSE           	B			DY1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	995K	535  				290040	679116			DURING ROUTINE ANNUAL INSP, FOUND EXCESSIVE PLAY AT ROLL PINS USED TO HOLD ROD ENDS IN PLACE FOR GEAR DOWN RETRACT/EXTEN	SION ROD ASSY AT LEAST .1250 INCH PLAY NOTED AT AFT END ALLOWING INNER TUBE INSERT FORE/AFT MOVEMENT WHERE ROLL PINS SEC	URE FWD END OF TUBE TO START WEARING WHERE ROLL PINS SECURE TO ROD END.  ROD ASSY REPLACED WITH NEW.				1	L	7	1 	3O	3	O	RT	2A3     	E3SO				 
2000110700019	20001107	00019	CE  	2000	11	7	20000802SH026    	1	19991201	G	5742	252200656	RIB             			CESSNA	303   	T303        	2073820	CE  										WING/ENG MOUNT	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	01	212HR	8660 				T3030239				RIB FOUND CRACKED AT INBOARD RIGHT WING AT INBOARD ENGINE MOUNT SUPPORT.  ADDED A DOUBLER SUPPORT AND STOP DRILLED CRACK	.  THIS IS THE THIRD AIRCRAFT OF THIS TYPE WITH THIS PROBLEM FOUND DURING AN ANNUAL  INSPECTION, ONE AIRCRAFT WAS FOUND 	WITH BOTH ENGINES'' MOUNTS CRACKED AT THE SAME INBD AREAS.  SUBMITTER SUSPECTED FATIGUE FROM TIME CAUSING CRACKS.  (X)				1	L	7	2 	3O			 	A34CE   					 
2001020600079	20010206	00079	NE  	2001	2	6	20000804SH002    	1	19991014	G	6510	MKB16B	BEARING         			SKRSKY	S76   	S76A        	8143006	NE  										TAIL ROTOR	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31211					760225				PILOT REPORTED THAT T/R PEDALS WERE DRIVING THE COLLECTIVE.  TROUBLESHOOTING FOUND BEARING WORN AND ROUGH.  REPLACED BEA	RING AND OPS CHECK C/W.  SUBMITTER RECOMMENDED BEARINGS BE REPLACED WHEN T/R CABLES ARE REPLACED.  THIS IS THE 3RD SET O	F BEARINGS REPLACED ON S76 FLEET.  (X)				1	G	7	2 	3U			 	H1NE    					 
2001020600081	20010206	00081	SW  	2001	2	6	20000807SH004    	1	19991219	G	6730		SLEEVE          	TEXTRON     	COLLECTIVE  	BELL  	407   	407         	       	SW  										BYPASS SPOOL	CONTAMINATED    	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	557AL	917  			HR788	53243				SERVO ACTUATOR REMOVED FROM AIRCRAFT DUE TO BINDING IN COLLECTIVE LEVER.  CIRCUMSTANCES UNKNOWN.  SHOP INSPECTION REVEAL	ED SERVO BYPASS SPOOL WAS BINDING IN BYPASS SPOOL SLEEVE.  SPOOLS AND SLEEVE CONTAMINATED WITH SOME FORM OF COATING.  TH	IS COATING COULD NOT BE SEEN, BUT WAS WASHED OFF.  NORMAL SPOOLS AND SLEEVE OPERATION RESTORED.  CAUSE UNKNOWN.   (X)				1	G	7	1 	3U			O	H2SW    					 
2000091400127	20000914	00127	CE  	2000	9	14	20000808SH012    	1	19990329	G	8120	4067958	PLATE           	CONT        		CESSNA	414   	414A        	2075907	CE  	CONT  	O520  	TSIO520N    	17040	SO  					THRUST BEARING	WORN            	F				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	23	222PL				BIO17759	414A0521				PILOT REPORTED FLUCTUATING MAP.  TROUBLESHOOTING FOUND TOO MUCH AXIAL PLAY IN TURBOSHAFT.  TIME ON TURBO 64.4 HRS.						1	L	7	2 	3O	3	O	 	A7CE    	E8CE				 
2000112900018	20001129	00018	NE  	2000	11	29	20000814SH009    	2	19991214	G	7230	500002102	FAN BLADE       								PWA   	JT8   	JT8D217A    	52053	NE  						IMPROPER PART   	B			SCS4	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	33							717421			PWA ENGINE JT8D-217A ESN 717421 REMOVED FROM ACFT NR 839 12-14-99, DUE TO FUEL NOZZLE AIR SCOOP ROTATION.  ENGINE SENT F	OR REPAIR.  UPON INSP OF FRONT COMPRESSOR 1ST STAGE ASSY (FAN ROTOR) NOTED THE FAN BLADES HAD BEEN MIXED.  TWO OF THE FA	N BLADES, (180 DEGRESS APART) HAD 67 DEGREE MIDSPAN SHROUD CONFIG.  PRE PW SB 6193, REST OF BLADES (32 EACH) HAD 55 DEGR	EE MIDSPAN SHROUD CONFIG, POST PW SB 6193.  BLADES ONLY INTERCHANGEABLE IN COMPLETE SETS AND NOT TO BE INTERMIXED.  P/N 	OF 2 BLADES PRE SB 6193 IS 500021-02 AND S/N''S, BCAUAB0646 AND BCAUAB0705.  REF:  IPM PROCEDURES Q 07-110.  (X)							4	F			E9NE				 
2001020700113	20010207	00113	EU  	2001	2	7	20000817SH001    	1	19990818	G	7720	430150102	THERMOCOUPLE    			BOLKMS	117   	BK117A3     	5626015	EU  										ENGINE	SHORTED         	B			R7MR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	424MB					7082				INTERNAL SHORT.  REPLACED THERMOCOUPLE WITH NEW UNIT, CORRECTED PROBLEM.  (X)						1	G	7	2 	3U			 	H13EU   					 
2000082800185	20000828	00185	CE  	2000	8	28	20000817SH030    	1	19991018	G	7820	045033818	MUFFLER         			CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A102	1A102OCM    	GL  	AFT END PLATE	ERODED          	H				B				EMER. DESCENT           				D			INFLIGHT SEPARATION       			CR	CRUISE         	1			SO	19	3240V	3781 	37   			15076436	252433A48	G15581		DURING CRUISE FLIGHT, SMOKE FROM UNDER INSTRUMENT PANEL NOTED.  PILOT SECURED ELECTRICAL AND MAGNETO SWITCH AND EXECUTED	 A FORCED LANDING.  HEAT DAMAGE TO ELECTRICAL WIRES NEAR THE BATTERY BOX.   EXAMINATION OF THE RIGHT MUFFLER P/N 0450400	-26, REVEALED THE AFT END PLATE P/N 0450338-18, WAS NOT IN PLACE AND NOT RECOVERED.  NO RECORD OF REPAIR OR REPLACEMENT 	OF THE RIGHT MUFFLER.  THE AIRPLANE HAD BEEN INSPECTED LAST 8 MONTHS EARLIER IN ACCORDANCE WITH AN ANNUAL INSPECTION.  E	ROSION OF THE REMAINING FLANGE OF END PLATE WAS NOTED AND PERFORATION OF THE TUBE WAS ALSO NOTED.  (X)		1	H	7	1 	3O	3	O	 	3A19    	E252	5	N	P918	 
2000120700045	20001207	00045	GL  	2000	12	7	20000828SH036    	1	19991113	G	6100	8808M30	BELT            			AMTR  	AVIA  	CHRISTAVIAMK	05602MJ	GL  						AMTR	C8289	C8289       	GL  	PROPELLER ASSY	FAILED          	G				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			WP	25	62199	220  				999				DURING TAKEOFF, BOTH PROPELLER DRIVE BELTS BROKE CAUSING LOSS OF THRUST.  ACFT DESCENDED RAPIDLY AND IMPACTED THE TERRAI	N.  BELTS HAD CONSUMED 220 HOURS OF THE 300 HOUR REPLACEMENT TIME.  FAILURE NOT SPECIFICALLY DETERMINED, BUT COULD INCLU	DE CAUSAL FACTORS OF ONE BELT CAUSING FAILURE OF THE SECOND BELT DUE TO ENTANGLEMENT.  A SINGLE WIDE BELT IS THE ONLY CO	NFIGURATION NOW AVAILABLE FROM THE CURRENT ENGINE MFG.  SUBMITTER RECOMMENDED ALL TWO-BELT CONFIGURATIONS STILL IN USE B	E CLOSELY INSPECTED AND ADJUSTMENT VERIFIED.  (X)		1	H	7	1 	3O			NC	EXPA    		5	N	EXPP5N	 
2000120600007	20001206	00007	SO  	2000	12	6	20000911SH023    	2	19990831	G	8530	641370	CYLINDER        			PIPER 	PA34  	PA34200T    	7103406	SO  	CONT  	O360  	TSIO360C    	17025	SO  					NR 3	SEPARATED       	D				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			SW	99	328RG					347570061	303065			CYLINDER HEAD SEPARATED COMPLETELY FROM BARREL IN-FLIGHT.  FAILURE POSSIBLE DUE TO FATIGUE.  TOTAL CYLINDER TIME IS UNKN	OWN.  TOTAL TIME SINCE CERMICHROME:  259.0 HOURS.  (X)					1	L	7	2 	3O	3	O	 	A7SO    	E9CE				 
2000102400277	20001024	00277	CE  	2000	10	24	20000925SH010    	1	19990607	G	3230	08411004DN	BRACE           			CESSNA	310   	310L        	2074230	CE  										ATTACH LOBE	FAILED          	G				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			WP	07	3210					310L0136				AFTER LANDING, DURING ROLL-OUT, RIGHT MAIN LANDING GEAR SIDE BRACE EXPERIENCED CATASTROPHIC FAILURE RESULTING IN THE COL	LAPSE OF THE RIGHT MAIN GEAR.  THE ATTACHMENT LOBE ON THE SIDE BRACE FRACTURED.  (X)					1	L	7	2 	3O			 	3A10    					 
2001022200171	20010222	00171	NE  	2001	2	22	20000925SH022    	2	19990808	G	7322	P13773	SCREW           			WTHRLY	620   	620B        	9630605	CE  	PWA   	R985  	R985AN1     	52008	NE  					CARBURETOR	LOOSE           	D				A				UNSCHED LANDING         				Y			ENGINE STOPPAGE           			NR	NOT REPORTED   	1			CE	07	197SK	849  				1645				CARBURETOR FLOAT FULCRUM SCREW SAFETY WIRE VIBRATED THROUGH BACKING OUT FULCRUM SCREW FOR FLOAT.  ENGINE QUIT RUNNING CA	USING FORCED LANDING.  AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE.  FULCRUM SHOWED CHATTER MARKS INDICATING FULCRUM SCREW WAS	 NOT PROPERLY SEATED.  RECORDS DID NOT INDICATE ANY CARBURETOR WORK SINCE NEW.  AIRCRAFT WAS NEW 2-17-97 AND HAD 849 TSN	 HOURS.  SUBMITTER RECOMMENDED AN AD OR SA1B BE ISSUED TO INSPECT FLOAT SCREW FOR PROPER INSTALLATION.  (X)			1	L	7	1 	3R	3	R	NC	A26WE   	5E1				 
2001022200172	20010222	00172	NE  	2001	2	22	20000925SH023    	2	19990901	G	7322	P13773	SCREW           	BENDIX      		WTHRLY	620   	620B        	9630605	CE  	PWA   	R985  	R985AN1     	52008	NE  					CARBURETOR	LOOSE           	D				A				UNSCHED LANDING         				O			OTHER                     			NR	NOT REPORTED   	1			CE	07	9025D					1618				CARBURETOR FLOAT FULCRUM SCREW VIBRATED LOOSE CAUSING FLOAT TO STICK.  AIRCRAFT ENGINE BEGAN RUNNING ROUGH.  AIRCRAFT SU	CCESSFULLY RETURNED TO FIELD.  FULCRUM SCREW BRASS THREADS WERE FOUND WORN CAUSING SCREW3 TO COME LOOSE.  AIRCRAFT WAS N	EW ON 12-6-96 AND NO RECORD OF PREVIOUS MAINTENANCE WAS FOUND IN RECORDS.  SUBMITTER SUSPECTED SCREW WAS NOT PROPERLY IN	STALLED AT MANUFACTURER, SUGGESTED AN AD OR SA1B BE ISSUED TO INSPECT FULCRUM SCREW FOR A PROPER INSTALLATION.  (X)			1	L	7	1 	3R	3	R	NC	A26WE   	5E1				 
2001030200013	20010302	00013		2001	3	2	20001024SH016    	4	19991223	G	2562	P3030029010	ELT             	BFGOODRICH  																LIFE RAFT	FAILED          	B			VW3R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			WP	09					10R213					ELT FAILED, UNABLE TO TRANSMIT SIGNALS.  ELT PACKED IAW OEM MANUAL INSTRUCTIONS.  ELT MODEL SRB-10.  (X)																			 
2001030200014	20010302	00014		2001	3	2	20001024SH017    	4	19991220	G	2562	P3030029010	ELT             	BFGOODRICH  																LIFE RAFT	FAILED          	B			VW3R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			WP	09					10R271					ELT FAILED, UNABLE TO TRANSMIT SIGNALS.  ELT PACKED IAW OEM MANUAL INSTRUCTIONS.  ELT MODEL SRB-10.  (X)																			 
2001030200015	20010302	00015		2001	3	2	20001024SH018    	4	19991216	G	2562	P3030029010	ELT             	BFGOODRICH  																LIFE RAFT	FAILED          	B			VW3R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			WP	09					10R212					ELT FAILED, UNABLE TO TRANSMIT SIGNALS.  ELT PACKED IAW OEM MANUAL INSTRUCTIONS.  ELT MODEL SRB-10.  (X)																			 
2001030200016	20010302	00016		2001	3	2	20001024SH019    	4	19991213	G	2562	P3030029010	ELT             	BFGOODRICH  																LIFE RAFT	FAILED          	B			VW3R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			WP	09					10R215					ELT FAILED, UNABLE TO TRANSMIT SIGNALS.  ELT PACKED IAW OEM MANUAL INSTRUCTIONS.  ELT MODEL SRB-10. (X)																			 
2001030200017	20010302	00017		2001	3	2	20001024SH020    	4	19991208	G	2562	P3030029010	ELT             	BFGOODRICH  																LIFE RAFT	FAILED          	B			VW3R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			WP	09					10R279					ELT FAILED, UNABLE TO TRANSMIT SIGNALS.  ELT PACKED IAW OEM MANUAL INSTRUCTIONS.  ELT MODEL SRB-10. (X)																			 
2001030200018	20010302	00018		2001	3	2	20001024SH021    	4	19991018	G	2562	SRB10	ELT             	BFGOODRICH  																LIFE RAFT	FAILED          	B			VW3R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			WP	09					10R209					DURING THE FUNCTIONAL TESTING OF THE ELT, IT DID NOT TRANSMIT ANY SIGNALS.  THE BATTERY WAS REPLACED WITH A BATTERY THAT	 TESTED OKAY ON OTHER ELT''S, BUT ELT WOULD STILL NOT TRANSMIT.  (X)																		 
2001030200019	20010302	00019		2001	3	2	20001024SH022    	4	19991018	G	2562	SRB10	ELT             	BFGOODRICH  																LIFE RAFT	FAILED          	B			VW3R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			WP	09					10R216					DURING THE FUNCTIONAL TESTING OF THE ELT, IT DID NOT TRANSMIT ANY SIGNALS.  THE BATTERY WAS REPLACED WITH A BATTERY THAT	 TESTED OKAY ON OTHER ELT''S, BUT THE ELT WOULD STILL NOT TRANSMIT.  (X)																		 
2001022600022	20010226	00022	CE  	2001	2	26	20001031SH001    	1	19990914	G	5712	1051000101	RIB             			BEECH 	76    	76          	1153005	CE  										LT WING	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	6003Y	3747 				ME129				DURING A 100-HOUR INSPECTION INTERVAL, CRACKS WERE FOUND IN THE WING RIBS ADJACENT TO THE LEFT INBOARD AND OUTBOARD AILE	RON HINGE BEARING ATTACHMENT BRACKETS P/N 105-100011-51.  BOTH CRACKS BEGAN AT THE AFT EDGE OF EACH RIB AND PROCEEDED FO	RWARD TO THE BOTTOM ATTACHING RIVET.  REPAIRS MADE BY FABRICATING DOUBLERS FOR EACH RIB.  (X)				1	L	7	2 	3O			 	A29CE   					 
2001022600023	20010226	00023	CE  	2001	2	26	20001031SH002    	1	19990914	G	5712	1051000102	RIB             			BEECH 	76    	76          	1153005	CE  										LT WING	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	6003Y	3747 								DURING A 100-HOUR INSPECTION INTERVAL, CRACKS WERE FOUND IN THE WING RIBS ADJACENT TO THE LEFT INBOARD AND OUTBOARD AILE	RON HINGE BEARING ATTACHMENT BRACKETS P/N 105-100011-51.  BOTH CRACKS BEGAN AT THE AFT EDGE OF EACH RIB AND PROCEEDED FO	RWARD TO THE BOTTOM ATTACHING RIVET.  REPAIRS MADE BY FABRICATING DOUBLERS FOR EACH RIB. (X)				1	L	7	2 	3O			 	A29CE   					 
2000121800236	20001218	00236	CE  	2000	12	18	20001205SH003    	1	19990405	G	7602	S12203AAR3797	CONTROL CABLE   			CESSNA	210   	210D        	2073414	CE  										MIXTURE	BROKEN          	G				A				UNSCHED LANDING         				Y			ENGINE STOPPAGE           			CR	CRUISE         	1			WP	23	2340F	99   				21058540				AIRCRAFT LOST POWER AND COLLIDED WITH GROUND OBSTRUCTIONS FOLLOWING A FORCED LANDING OFF-FIELD.  SUBSEQUENT INVESTIGATIO	N REVEALED A BROKEN MIXTURE CABLE.  AD-85-03-01 IS A ONE-TIME AD WHICH APPLIES TO THIS AIRCRAFT.  THE AD INCORPORATED SE	69-16.  THE AIRCRAFT RECORDS REVEALED THE ONE-TIME AD HAD BEEN C/W.  THE PART HAD BEEN INSTALLED 99 HRS PRIOR AT THE LAS	T ANNUAL INSPECTION.  SUBSEQUENT INVESTIGATION REVEALED THIS CABLE WAS INSTALLED INCORRECTLY AND NOT IAW WITH SE69-16 CA	USING EXCESS FLEXING OF THE INNER CONTROL CABLE.  (X)		1	H	7	1 	3O			 	3A21    					 
2000121900205	20001219	00205	SW  	2000	12	19	20001205SH011    	1	19991115	G	2435	230790001	STARTER GEN     			GULSTM	690TP 	690A        	0141722	SW  											FAILED          	H				O				OTHER                   				H			ELECT. POWER LOSS-50 PC   			NR	NOT REPORTED   	1			GL	25	121JW					11299				STARTER/GENERATOR FAILED AFTER 207 HOURS OF OPERATION.  FAILED FIRST TIME AFTER 14 HOURS.  FAILURE OCCURRED INTERNALLY. 	 (X)					1	H	7	2 	3T			 	2A4     					 
2000010800094	20000108	00094	NE  	2000	1	8	2000ZZZX1        	2	19991024	G	7314	P94B12209	PUMP            			SNIAS 	350   	AS350B2     	8680813	EU  	TMECA 	ARRIEL	ARRIEL1     	60030	NE  					FUEL SYSTEM	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	40751	39   			20443	3154				PUMP WILL NOT PRODUCE SUFFICIENT PRESSURE.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H9EU    	E19EU				 
2000011500628	20000115	00628		2000	1	15	2000ZZZX100      	1	19991228	G	3240	7010FS9545708	SEAL            		50105201    															BRAKE	LEAKING         	B			XC4R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	19		632  			JUN981385					BRAKE ASSEMBLY, P/N 5010520-1, FAILED PREMATURELY.  ONE EACH PISTON LEAKING FROM INSULATOR AREA.  PISTON INTERNALLY FILL	ED WITH FLUID. EVIDENCE OF T-SEAL FAILURE.  THIS IS A CONTINUAL DISCREPANCY.  NOTE:  OEM PARTS INSTALLED IN BRAKE ASSEMB	LY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 5010520-1.																	 
2000011500629	20000115	00629		2000	1	15	2000ZZZX101      	1	19991230	G	3240	7010FS9545708	SEAL            		50105201    															BRAKE	LEAKING         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	17		2103 			MAR981249					BRAKE ASSEMBLY, P/N 5010520-1, FAILED PREMATURELY.  THREE EACH PISTONS LEAKING FROM INSULATOR AREA.  PISTONS INTERNALLY 	FILLED WITH FLUID.  EVIDENCE OF T-SEAL FAILURE.  THIS IS A CONTINUAL DISCREPANCY.  NOTE:  OEM PARTS INSTALLED IN BRAKE A	SSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 5010520-1.																	 
2000011500630	20000115	00630	SO  	2000	1	15	2000ZZZX102      	1	19991229	G	3240	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE	BROKE           	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		1056 			0419					BRAKE ASSEMBLY, P/N 2-1585, FAILED  PREMATURELY.  NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE TUBE KEY SLOTS.  THIS	 IS A CONTINUAL DISCREPANCY.  BRAKE ASSEMBLY SHOULD LAST 2,500 CYCLES.  NOTE:  OEM PARTS INSTALLED IN BRAKE ASSEMBLY AND	 THE MOST RECENT BRAKE CONFIGURATION, P/N 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
2000011500631	20000115	00631	SO  	2000	1	15	2000ZZZX103      	1	19991230	G	3240	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE	BROKEN          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		2931 			0877A					BRAKE ASSEMBLY, P/N 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE TUBE KEY SLOTS. THIS I	S A CONTINUAL DISCREPANCY.  NOTE:  OEM PARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 2-	1585.				2	L	7	2 	4T			RT	A31SO   					 
2000011500632	20000115	00632	EA  	2000	1	15	2000ZZZX104      	1	19991210	G	7110	22850072101	COVER           	VOUGHT      	22050020109 	CNDAIR	CL600 	CL6002B16   	1900305	EA  										LT COWL	CRACKED         	B			SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	304FX	3630 			056	5063				THE LEFT AND RIGHT NOSE INLET COWL AIRLINE COVER (POCKET) FOR THE 14TH STAGE T/R PDV LINE SHOW SIGNS OF EXCESSIVE HEAT D	AMAGE AND IS BUCKLED AND CRACKED.					2	L	7	2 	4F			RT	A21EA   					 
2000011500633	20000115	00633	EA  	2000	1	15	2000ZZZX105      	1	19991210	G	7110	22B50072101	COVER           	VOUGHT      	22050020109 	CNDAIR	CL600 	CL6002B16   	1900305	EA  										RT COWL	CRACKED         	B			SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	304FX	3630 			050	5063				THE LEFT AND RIGHT NOSE INLET COWL AIRLINE COVER (POCKET) FOR THE 14TH STAGE T/R PDV LINE SHOW SIGNS OF EXCESSIVE HEAT D	AMAGE AND IS BUCKLED AND CRACKED.					2	L	7	2 	4F			RT	A21EA   					 
2000011500634	20000115	00634	CE  	2000	1	15	2000ZZZX106      	1	19991216	G	3010		DEICE ELEMENT   		9914217207  	CESSNA	650   	650         	2076802	CE  										HORIZ STABILIZER	MISMANUFACTURED 	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NE	03	40N				CSO191	6507031				HORIZONTAL STABILIZER ANTI-ICE LEADING EDGE.  NEW FROM CESSNA KS HAD ONE TEMP SWITCH LOOSE IN MOUNTING, AND ONE TEMP SWI	TCH BROKEN OUT OF MOUNTING POINT. LEADING EDGE IS ELECTRICALLY HEATED.  LOSS OF TEMPERATURE CONTROL WILL RESULT AND ALSO	 LOSS OF ANTI-ICE PROTECTION.  DEFECTS FOUND DURING RECEIVING INSPECTION.				2	L	7	2 	4F				A9NM    					 
2000011500635	20000115	00635	CE  	2000	1	15	2000ZZZX107      	1	19991217	G	3010		DEICE ELEMENT   		9914217207  	CESSNA	650   	650         	2076802	CE  										HORIZ STABILIZER	MISMANUFACTURED 	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NE	03	40N				CSO236	6507031				HORIZONTAL STABILIZER ANTI-ICE LEADING EDGE.  THIRD NEW LEADING EDGE RECEIVED FROM CESSNA KS.  HAS ONE TEMPERATURE SWITC	H BROKEN LOOSE FROM MOUNTING POINT.  DEFECT FOUND DURING RECEIVING INSPECTION.  SUBMITTER RECOMMENDED NEW TYPE OF BONDIN	G OF TEMPERATURE SWITCHES.  THIS PART NUMBER IS THE NEW IMPROVED L/E BECAUSE OF A HIGH FAILURE RATE.				2	L	7	2 	4F				A9NM    					 
2000011500636	20000115	00636	CE  	2000	1	15	2000ZZZX108      	1	19991216	G	3010		DEICE ELEMENT   		9914217207  	CESSNA	650   	650         	2076802	CE  										HORIZ STABILIZER	MISMANUFACTURED 	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NE	03	40N				CSO180	6507031				HORIZONTAL STABILIZER ANTI-ICE LEADING EDGE.  SECOND NEW L/E RECEIVED FROM CESSNA KS.  HAS TWO HEATING ELEMENT DEFECTS, 	ONE 26 INCHES FROM OUTBOARD EDGE AND ONE 15 INCHES FROM OUTBOARD EDGE.  DEFECTS FOUND DURING RECEIVING INSPECTION.					2	L	7	2 	4F				A9NM    					 
2000011500637	20000115	00637	EA  	2000	1	15	2000ZZZX109      	1	19991210	G	7110	22850072101	COVER           	VOUGHT      	22850020109 	CNDAIR	CL600 	CL6002A12   	1900304	EA  										LT NACELLE	CRACKED         	B			SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	998JR	4941 			005	3045				THE LEFT NOSE COWL AIRLINE COVER (POCKET) FOR THE 14TH STAGE T/R PDU LINE SHOWS SIGNS OF HEAT DAMAGE AND IS BUCKLED AND 	CRACKED.					2	L	7	2 	4F			RT	A21EA   					 
2000011500638	20000115	00638	CE  	2000	1	15	2000ZZZX110      	1	19991214	G	5510		STRUCTURE       		55320002    	CESSNA	500   	550         	2076604	CE  										HORIZ STABILIZER	MISDRILLED      	B			QFYR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NE	03	87SF	9856 				5500096				DURING COURSE OF 10,000-HOUR INSPECTION, THE HORIZONTAL STABILIZER WAS FOUND TO HAVE NUMEROUS DOUBLE HOLES, HOLES DRILLE	D OFF-CENTER, HOLES DRILLED ON AN ANGLE AFTER REMOVAL OF THE HYLOCKS IN THE CENTER SECTION THROUGH ALL SPARS AND FITTING	S.  SUBMITTER STATED IT IS VERY OBVIOUS A MANUFACTURING PROBLEM.				1	L	7	2 	4F				A22CE   					 
2000011500639	20000115	00639	CE  	2000	1	15	2000ZZZX111      	1	19991223	G	2140	57D27	CAPACITOR       	ELECTROSYS  	FR88D812EL  	CESSNA	421   	421C        	2076016	CE  										HEATER	FAILED          	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	02	81RD				A97100031	421C0291				UPON INITIAL INSTALLATION OF FACTORY REBUILT COMBUSTION HEATER ASSEMBLY, ATTEMPTED OPERATIONAL CHECK OF HEATER.  ATTEMPT	ED TO ENERGIZE HEATER IGNITION CIRCUIT RESULTED IN IMMEDIATE TRIP OF HEATER CIRCUIT BREAKER.  FOUND CAPACITOR SHORTED. P	ART TOTAL TIME UNKNOWN.  TIME SINCE FACTORY REBUILD:  ZERO.				1	L	7	2 	3O				A7CE    					 
2000011500640	20000115	00640	CE  	2000	1	15	2000ZZZX112      	1	19991202	G	7500	57153064	BLEED TUBE      			CESSNA	441   	441         	2076020	CE  										BS 130	BURNED          	C	L	A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	544AL	16447				4410120				ELECTRIC POWER WIRES CHAFED INTO BLEED AIR TUBE CAUSING BLEED AIR LEAK.  BREAKERS DID NOT POP.  WIRE NR'S P10616, LT FEE	DER; P105A6 RT FEEDER; P96F6, LT AVIONICS; P95G6 RT AVIONICS.  ALL 4 WIRES WELDED THEMSELVES TO BLEED TUBE AT STA 130. C	HECKED ANOTHER C-441; WIRES WERE ROUTED DIFFERENTLY.  SUBMITTER SUSPECTED OTHER C-441'S WILL HAVE SOME PROBLEM.				1	L	7	2 	3T			RT	A28CE   					 
2000011500641	20000115	00641	EU  	2000	1	15	2000ZZZX113      	1	19991216	G	3231	AIR400390	GLAND SEAL      		AIR864141   	SAAB  	SF340 	340B        	7860101	EU  										NLG	WORN            	B			FW1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	433XJ	5006 			LK9701062	433				INSIDE DIAMETER OF SEAL WORN ON THE SIDE FACING OUT.						2	L	7	2 	4T			RT	A52EU   					 
2000011500643	20000115	00643	SO  	2000	1	15	2000ZZZX115      	1	19991202	G	5410	12003852001	FRAME           			EMB   	120   	EMB120RT    		SO  										RT NACELLE	CRACKED         	B			WVER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	09	263AS					120157				RIGHT NACELLE UPPER FRAME NR 1 WAS FOUND CRACKED AT THE ENGINE TORQUE TUBE MOUNTING AREA.  EMB SB 120-54-0036 IS BEING I	NCORPORATED WHICH PROVIDES A NEW FRAME WITH A BEEFED UP WEB AREA AT THE TORQUE TUBE MOUNTING AREA.					2	L	7	2 	4T			RT	A31SO   					 
2000011500644	20000115	00644	SO  	2000	1	15	2000ZZZX116      	1	19991202	G	5410	12003852001	FRAME           			EMB   	120   	EMB120RT    		SO  										LT NACELLE	CRACKED         	B			WVER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	09	263AS					120157				LEFT NACELLE UPPER FRAME NR 1 WAS FOUND CRACKED AT THE ENGINE TORQUE TUBE MOUNTING AREA.  EMB SB 120-54-0036 IS BEING IN	CORPORATED WHICH PROVIDES A NEW FRAME WITH A BEEFED UP WEB AREA AT THE TORQUE TUBE MOUNTING AREA.					2	L	7	2 	4T			RT	A31SO   					 
2000011500647	20000115	00647	SO  	2000	1	15	2000ZZZX118      	1	19991223	G	3244	600X68PLY	TIRE            			PIPER 	PA31  	PA31P       	7103120	SO  										NLG	FAILED          	H				O				OTHER                   				E			VIBRATION/BUFFET          			LD	LANDING        	1			SW	99	57BT					31P7400175				DURING LANDING, A 'THUMPING' NOISE WAS NOTICED WHEN THE NOSE WHEEL TOUCHED DOWN.  INSPECTION REVEALED A BULGE IN THE NOS	E TIRE SIDE WALL THAT WAS CONTACTING THE NOSE FORK DURING ROTATION OF THE TIRE.  THE TIRE, OTHERWISE, APPEARED TO BE IN 	GOOD CONDITION.				1	L	7	2 	3O				A8EA    					 
2000010800118	20000108	00118	SW  	2000	1	8	2000ZZZX12       	1	19991201	G	6322	206061432121	HOUSING         		407040303105	BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	477AL	124  			A263	53203				DURING DAILY INSPECTION, FOUND CRACKED BLOWER HOUSING.						1	G	7	1 	3U			O	H2SW    					 
2000011500649	20000115	00649	CE  	2000	1	15	2000ZZZX120      	1	19991022	G	3240	0500118126	LINE            			CESSNA	172   	172R        	2072401	CE  										BRAKE	LEAKING         	B				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	05	9522Q					17280426				HYDRAULIC FLUID WAS NOTED COMING FROM BOTH MAIN GEAR STRUT BRAKE LINES.  PIN HOLES WERE FOUND IN BOTH LINES AT THE LOWES	T POINT, JUST INBOARD OF THE BRAKE CALIBER.  THERE IS A PLASTIC SLEEVE ON THE LINE THAT IS INSTALLED AT THE FACTORY.  IT	 APPEARS THAT BOTH LINES WERE CORRODED, AND THAT WAS THE REASON FOR THE PIN HOLES.  IT IS SUGGESTED THAT SMALL HOLES BE 	CUT INTO THE PLASTIC SLEEVING AT THE LOWEST POINT OF THE BRAKE LINE INSTALLATION TO DRAIN ANY WATER THAT MIGHT COLLECT.			1	H	7	1 	3O			NT	3A12    					 
2000011500651	20000115	00651	GL  	2000	1	15	2000ZZZX122      	2	19991109	G	7250	6898977	COUPLING SPLINE 								ALLSN 	250C  	250C28B     	03013	GL  					N1	WORN            	B			YKER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17										WORN SPLINES WERE NOTED IN ONE END OF THE COUPLING AFTER THE ENGINE WAS DISASSEMBLED FOR MAINTENANCE.  THE SPLINES WERE 	CHECKED FOR WEAR WITH THE MANUFACTURER'S RECOMMENDED TOOL.  NOT ONLY DID THE TOOL (A NO-GO GAUGE) ENTER THE WORN AREA, B	UT IT FIT INTO THE SPLINES THE ENTIRE LENGTH OF THE PART.  THIS WOULD INDICATE THE SPLINES WERE NOT TO PRINT AT THE TIME	 OF MANUFACTURE SINCE WEAR CAN TAKE SPLACE ONLY AT THE ENDS OF THE COUPLING WHERE THE SPLINES OF THE MATING PARTS ENGAGE	.							3	U			E1GL				 
2000011500652	20000115	00652	GL  	2000	1	15	2000ZZZX123      	2	19991110	G	7230	23056634	GEARSHAFT       								ALLSN 	250C  	250C28B     	03013	GL  					SPUR ADAPTER	WORN            	B			YKER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17					CG114995					SEVERE SPLINE WEAR WAS NOTED ON THE AFT END OF THE GEARSHAFT AFTER THE ENGINE WAS DISASSEMBLED FOR MAINTENANCE.  NO APPR	ECIABLE WEAR WAS NOTED ON THE SPLINES OF THE MATING PART.										3	U			E1GL				 
2000011500653	20000115	00653	NE  	2000	1	15	2000ZZZX124      	2	19991216	G	7250	1347M95G02	SHROUD          								GE    	CF6   	CF650*      	30018	NE  					EDNGINE	DISBONDED       	H			T9LR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15										2 EACH CF6-50 STAGE 1 HPT SHROUDS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF THE WEARCOAT MATERIAL FROM THE SUBS	TRATE.  PW ENGINEERING STATED THIS IS NOT A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE IS UNDER INVESTIGATION.										4	F			E23EA				 
2000011500654	20000115	00654	GL  	2000	1	15	2000ZZZX125      	2	19991216	G	7250	1646M45P11	SHROUD          								GE    	CF6   	CF680C      		GL  					ENGINE	DISBONDED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15			2000 							25 EACH CF-6-80C2 STAGE 1 HPT SHROUDS WITH 400 CYCLES AND 2,000 HOURS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF	 THE WEARCOAT MATERIAL FROM SUBSTRATE.  PW ENGINEERING STATED THIS IS NOT A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE IS UNDER	 INVESTIGATION.									4	F			E23EA				 
2000011500655	20000115	00655	GL  	2000	1	15	2000ZZZX126      	2	19991216	G	7250	9392M86G08	SHROUD          								GE    	CF6   	CF680C      		GL  					ENGINE	DISBONDED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15			1433 							6 EACH CF6-80C2 STAGE 2 HPT SHROUDS WITH 1,274 CYCLES AND 1,433 HOURS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF	 THE WEARCOAT MATERIAL FROM THE SUBSTRATE.  PW ENGINEERING STATED THIS IS NOT A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE IS U	NDER INVESTIGATION.									4	F			E23EA				 
2000011500656	20000115	00656	GL  	2000	1	15	2000ZZZX127      	2	19991216	G	7250	9392M86G08	SHROUD          								GE    	CF6   	CF680C      		GL  					ENGINE	DISBONDED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15			1123 							5 EACH CF6-80C2 STAGE 2 HPT SHROUDS WITH 347 CYCLES AND 1,123 HOURS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF T	HE WEARCOAT MATERIAL FROM THE SUBSTRATE.  PW ENGINEERING STATED THIS IS NOT A SAFETY OF FLIGHT ISSUE. ROOT CAUSE IS UNDE	R INVESTIGATION.									4	F			E23EA				 
2000011500657	20000115	00657	GL  	2000	1	15	2000ZZZX128      	2	19991216	G	7250	9392M86G08	SHROUD          								GE    	CF6   	CF680C      		GL  					ENGINE	DISBONDED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15			10361							3 EACH CF6-80C2 STG 2 HPT SHROUDS WITH 1,352 CYCLES AND 10,361 HOURS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF 	THE WEARCOAT MATERIAL FROM THE SUBSTRATE.  PW ENGINEERING STATED THIS IS NOT A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE IS UN	DER INVESTIGATION.									4	F			E23EA				 
2000011500658	20000115	00658	GL  	2000	1	15	2000ZZZX129      	2	19991216	G	7250	9392M86G08	SHROUD          								GE    	CF6   	CF680C      		GL  					ENGINE	DISBONDED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15										6 EACH CF6-80C2 STAGE 2 HPT SHROUDS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF THE WEARCOAT MATERIAL FROM THE SU	BSTRATE.  PW ENGINEERING STATED THIS IS NOT A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE IS UNDER INVESTIGATION.										4	F			E23EA				 
2000011500659	20000115	00659	GL  	2000	1	15	2000ZZZX130      	2	19991216	G	7250	9392M86G08	SHROUD          								GE    	CF6   	CF680C      		GL  					ENGINE	DISBONDED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15			347  							3 EACH CF6-80C2 STG 2 HPT SHROUDS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF THE WEARCOAT MATERIAL FROM THE SUBS	TRATE.  PW ENGINEERING STATED THIS IS NOT A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE IS UNDER INVESTIGATION.										4	F			E23EA				 
2000011500662	20000115	00662	CE  	2000	1	15	2000ZZZX133      	1	19991228	G	5320	6619282124	WELD ASSY       			CESSNA	500   	560CESSNA   	2076750	CE  										FUSELAGE	WRONG PART      	B	P		JSNR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	09	207PC	573  				5605008				RIGHT FORWARD 8 INCH CLOSET WAS REMOVED FOR ACCESS TO WIRING AND INSPECTION UNDER FLOOR.  IT WAS DISCOVERED THE SIX SCRE	WS ATTACHING THE P/N 6619282-124 WELD ASSEMBLY FOR THE CM2-80AST SHOCK MOUNT WERE TOO SHORT, IN THAT ONLY A THREAD OR TW	O OF EACH SCREW WAS ENGAGED IN THE NUTPLATE.  IPC CALLS OUT AN MS 24694S53 SCREW.  S52 AND S51 LENGTH SCREWS WERE INSTAL	LED.  THIS WAS ORIGINAL FROM THE CESSNA FACTORY.			2	L	7	2 	4F			RT	A22CE   					 
2000011500663	20000115	00663	CE  	2000	1	15	2000ZZZX134      	1	19991228	G	3397		WIRE            	RAPCO       		CESSNA	500   	560CESSNA   	2076750	CE  										COCKPIT	DAMAGED         	B			JSNR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	207PC	573  				5605008				CABIN READING LIGHT CIRCUIT BREAKER, RIGHT, LOCATED IN AFT CLOST J-BOX, WOULD INTERMITTENTLY TRIP.  CABIN LOWER TRIM PAN	ELS AND RIGHT FORWARD CLOSET WERE REMOVED TO CHECK WIRING.  A PINCHED AND BARE WIRE WAS FOUND OUTBOARD OF THE FORWARD RI	GHT CLOSET ASSOCIATED WITH THIS CIRCUIT BREAKER.  IT WAS NOTED VERY FEW OF THE WIRE BUNDLES WERE TIED UP PROPERLY EVEN T	HOUGH THERE WERE EXISTING CABLE TIE ANCHORS IN THE VICINITY.  CESSNA ALSO USED VARIOUS ELECTRICAL BULKHEAD CONNECTORS IN	 THE WIRE BUNDLES AND FAILED TO TIE THEM UP.  WHEN TOILET ASSEMBLY WAS REMOVED, NONE OF THE WIRE BUNDLES WERE FASTENED. 	 THE WIRE BUNDLES WERE RUBBING ON THE METAL FRAME OF THE TOILET ASSEMBLY.	2	L	7	2 	4F			RT	A22CE   					 
2000011500664	20000115	00664	CE  	2000	1	15	2000ZZZX135      	1	19991011	G	3260	66416352	SUPPORT         			CESSNA	500   	560CESSNA   	2076750	CE  										MLG	DAMAGED         	B	P		JSNR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	207PC	480  				5605008				DAMAGE WAS NOTED TO THREADS OF P/N 65430087 UPLOCK SWITCH ON RT MAIN GEAR.  THE EARS FROM THE LANDING GEAR UPLOCK ROLLER	 WERE CONTACTING THE THREADED PORTION OF THE SWITCH AS THE ROLLER CAME UP INTO THE P/N 6641634-2 UPLOCK LATCH.  THIS WAS	 CAUSED BY IMPROPER LOCATION OF P/N 6641635-2 SUPPORT FITTING AT THE CESSNA FACTORY.  CESSNA SACRAMENTO SERVICE CENTER C	HANGED OUT THE SUPPORT FITTING.  SUBMITTER STATED THIS IS THE SECOND AIRCRAFT IN THE OPERATOR'S FLEET TO HAVE THE SAME P	ROBLEM WITH THE 6641635-2 SUPPORT FITTING BEING INCORRECTLY LOCATED.		2	L	7	2 	4F			RT	A22CE   					 
2000011500665	20000115	00665	CE  	2000	1	15	2000ZZZX136      	1	19991216	G	5510	07326155	FAIRING         			CESSNA	182   	182S        	2072701	CE  										STABILIZER	MISMANUFACTURED 	B			DPOR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	07	213CM	150  				18280046				PART INDICATED CAME FROM FACTORY INSTALLATION ON BRAND NEW AIRCRAFT WITHOUT 2 FORWARD HOLES DRILLED AND FITTED.						1	H	7	1 	3O			NT	3A13    					 
2000010800121	20000108	00121	SW  	2000	1	8	2000ZZZX15       	1	19991113	G	5302	407023800118	SUPPORT         		407030801101	BELL  	407   	407         		SW  										TAILBOOM	MISINSTALLED    	B			ALGR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	607AL	1606 			53264	53264				DURING DAILY INSPECTION, FOUND PART INSTALLED IN PRELOADED CONDITION.						1	G	7	1 	3U			O	H2SW    					 
2000010800123	20000108	00123	SW  	2000	1	8	2000ZZZX17       	1	19991111	G	6322	206061432121	HOUSING         		407040303105	BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437AL				A302	53141				DURING DAILY INSPECTION, FOUND BLOWER HOUSING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
2000012200353	20000122	00353	CE  	2000	1	22	2000ZZZX170      	1	19991227	G	2434	AC2101	CONTROL UNIT    	LAMAR       	MC012A      	CESSNA	172   	172R        	2072401	CE  										ALTERNATOR	FAILED          	H				O				OTHER                   				H			ELECT. POWER LOSS-50 PC   			NR	NOT REPORTED   	1			GL	03	718EH	686  			80059601	17280061				PILOT DETECTED ALTERNATOR OUT LIGHT IN-FLIGHT AND NO OUTPUT ON METER.  CYCLED ALT SWITCH AND ALTERNATOR OUT LIGHT STAYED	 OFF, BUT METER WENT TO FULL CHARGE DEFLECTION.  PILOT LANDED WITH NO PROBLEMS.  UPON INVESTIGATION, FOUND ALT CONTROL U	NIT MELTED INTO AREA OF CONNECTOR.  ALL WIRES IN CONNECTOR WERE SEVERELY BURNED AND ARCED.  REGULATOR WAS SHORTED TO MAX	IMUM OUTPUT OF ALTERNATOR.  POWER JUNCTION BOX SHOWS SIGNS OF EXTREME HEAT AND SMOKE.  REPLACED ALTERNATOR OUT SENSOR AN	D POWER JUNCTION BOX.  OPS CHECKED OK.  THIS AIRCRAFT HAS HAD SB 99-24-01 C/W.  ACFT TT:  1,683.5 HRS.		1	H	7	1 	3O			NT	3A12    					 
2000012200354	20000122	00354	EA  	2000	1	22	2000ZZZX171      	2	19991228	G	8530		CYLINDER        			PIPER 	PA28  	PA28180     	7102808	SO  	LYC   	O360  	O360A4A     	41514	EA  					ENGINE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	8315W	250  			633484	282488	L936836A			CYLINDER CRACKED AND SEPARATED CAUSING CATASTROPHIC ENGINE FAILURE.  P/N CCST 12 CA AEL65102-12.						1	L	7	1 	3O	3	O		2A13    	E286				 
2000012200356	20000122	00356	NE  	2000	1	22	2000ZZZX173      	2	19991124	G	7412	103815501	EXCITER BOX     			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A42      	52043	NE  					LEFT ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	430MC					BB904	PCE93097			DURING ROUTINE START-UP, THE LEFT ENGINE FAILED TO LIGHT OFF.  THE IGNITION SYSTEM WAS IMMEDIATELY SUSPECT DUE TO LACK O	F 'POPPING' THAT ACCOMPANIES THE FIRING OF THE IGNITERS.  THE EXCITER BOX WAS REPLACED AND THE ENGINE STARTED NORMALLY.					1	L	7	2 	4T	4	T		A24CE   	E4EA				 
2000012200357	20000122	00357	CE  	2000	1	22	2000ZZZX174      	1	19991213	G	3610		P3 AIR LINE     			BEECH 	200   	200BEECH    	1152920	CE  										LEFT ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	430MC					BB904				DURING GROUND RUN-UP, THE LEFT ENGINE WOULD ONLY DEVELOP 89 PERCENT N1 (COMPRESSOR RPM).  INSPECTION OF THE FUEL CONTROL	 P3 AIR LINES REVEALED A LOOSE B-NUT AT THE PROP GOVERNOR.  LEAKAGE IN THIS LINE LIMITS THE FUEL CONTROL TO 80 PERCENT (	MAXIMUM REVERSE N1).  THE SAFETY WIRE FOR THE B-NUT HAD BROKEN AND ALLOW THE B-NUT TO LOOSEN.  THERE IS NO REASON EVIDEN	T AS TO WHY THE SAFETY WIRE BROKE.			1	L	7	2 	4T				A24CE   					 
2000012200358	20000122	00358	NM  	2000	1	22	2000ZZZX175      	1	19990612	G	3230	161A11462	TORSION LINK    			BOEING	737   	7377K9      	138447E	NM  										LT MLG	BROKEN          	H				O				OTHER                   				E			VIBRATION/BUFFET          			LD	LANDING        	1			EA	33	101UN					28089				SVO/ALA - FLT UN 205 - TRX FLIGHT CREW HAS REPORTED THE OCCURRENCE OF MLG SHIMMY VIBRATION DURING LANDING AT ALMA-ATA AI	RPORT.  DURING GROUND VISUAL INSP, FOUND FOLLOWING DAMAGES TO LEFT MAIN LANDING GEAR COMPONENTS:  UPPER TORSION LINK ATT	ACH PIN, FRACTURED.  UPPER TORSION LINKS BUSHING, WORN, FRACTURED, AND DAMAGED.  TORSION LINK ATTACH LUGS COMMON TO OUTE	R CYLINDER, DAMAGED.			2	L	7	2 	4F			RT	A16WE   					 
2000012200359	20000122	00359	CE  	2000	1	22	2000ZZZX176      	1	19991210	G	3230	66416341	ROD ASSY        			CESSNA	500   	560CESSNA   	2076750	CE  										MLG	MISINSTALLED    	B			JSNR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	09	207PC	558  				5605008				PILOT COMPLAINED RT LANDING GEAR WOULD NOT FULLY RETRACT INTO WHEELWELL ON LAST FLIGHT.  HYD PRESSURE ANNUNCIATOR REMAIN	ED ON.  GEAR EXTENSION NORMAL.  ACFT PLACED ON JACKS AND INSPECTED.  FOUND RT GEAR DOOR RIGGED TOO TIGHT AND RT 66641634	-2 UPLOCK LATCH RUBBING ON LANDING GEAR TRAILING LINK AND ADEL CLAMP.  DOOR ROD P/N 6641634-1 ADJUSTED AND UPLOCK LATCH 	DRESSED TO PROVIDE .25 INCH CLEARANCE FROM TRAILING LINK.  ADEL CLAMP REPOSITIONED.  LANDING GEAR RETRACTED USING SLOW C	YCLE AND NORMAL TEST PROCEDURES.  THIS LANDING GEAR RECENTLY HAD P/N 6641635-2 SUPPORT BRACKET REPLACED WHICH RELOCATED 	P/N 661634-2 UPLOCK LATCH AND CESSNA SB 560XL-32-03, MLG DOOR AND TRUNNION IMPROVEMENT.	2	L	7	2 	4F			RT	A22CE   					 
2000012200360	20000122	00360	CE  	2000	1	22	2000ZZZX177      	1	19991228	G	3520	83357802	FITTING         	SCOTT       		CESSNA	500   	560CESSNA   	2076750	CE  										BS 358	LOOSE           	B	P		JSNR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	09	207PC	573  				5605008				DURING A SCHEDULED INSPECTION TO FUNCTIONALLY CHECK THE PASSENGER OXYGEN MASKS, NOTICED OXYGEN WAS FLOWING BEFORE ANY OF	 THE PINTLE PINS WERE REMOVED.  IT WAS DISCOVERED THE FITTING ON THE AFT OXYGEN DROP-OUT BOX ASSY WAS NOT EVEN FINGER TI	GHT.  THE SEALING O-RING WAS VISIBLE AND THE FITTING LEAKING OXYGEN.  CABIN CEILING REMOVED TO GAIN ACCESS TO FITTING. F	ITTING WAS TIGHTENED AND LEAK STOPPED.  THE MAGNITUDE OF THE LEAK WOULD HAVE SERIOUSLY SHORTENED THE OPERATIONAL TIME OF	 THE SYSTEM HAD IT BEEN DEPLOYED.		2	L	7	2 	4F			RT	A22CE   					 
2000012200361	20000122	00361	CE  	2000	1	22	2000ZZZX178      	1	19991228	G	2540	99190091	TOILET          			CESSNA	500   	560CESSNA   	2076750	CE  										LAVATORY	MISMANUFACTURED 	B			JSNR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	09	207PC	573  				5605008				EXTERNALLLY SERVICEABLE TOILET ASSY P/N 9919009-1 WAS BEING CHANGED OUT.  DURING PROCESS, DISCOVERED THERE WAS A RATCHET	ING SCREWDRIVER STUCK IN THE P/N 9914632-2 WASTE PIPE ADAPTER, AND A .3750 INCH SOCKET BETWEEN THE FLOOR AND TANK BOTTOM	 THAT POSSIBLY COULD HAVE BEEN USED TO LEVEL THE TOILET ASSY.  NOTED THE NEW TOILET ASSY WOULD NOT FIT CORRECTLY ON THE 	FLOOR LOCATOR SHEAR PINS P/N 4611026-3 (3 EACH).  THE ORIGINAL TOILET MOUNT HOLES WERE AUGURED OUT AT THE FACTORY.  CESS	NA ENG WOULD NOT ALLOW NEW TOILET ASSY TO BE 'MODIFIED' IN THE SAME WAY.  AN ENGINEERING ORDER ALLOWED FLOOR RAIL TO BE 	REPAIRED WITH A DOUBLER AND THE SHEAR PINS HAD TO BE CORRECTLY LOCATED IN ORDER FOR THE NEW TOILET TO FIT PROPERLY.	2	L	7	2 	4F			RT	A22CE   					 
2000012200363	20000122	00363	NE  	2000	1	22	2000ZZZX179      	2	19991222	G	7314	105476	DRIVESHAFT      		MFP45       	BAG   	BAE146	BAE146100A  	1500260	EU  	LYC   	ALF502	ALF502R3    	41580	NE  					FUEL PUMP	WORN            	H				E				ENGINE SHUTDOWN         				O			OTHER                     			NR	NOT REPORTED   	1			WP	05		16255			AFR0692					ENGINE SHUTDOWN IN-FLIGHT.  DRIVE SPLINES ON FUEL PUMP SEVERELY WORN.  PUMP TO BE OVERHAULED.  HIGH OPERATING TIME LED T	O FAILIURE.					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
2000010800125	20000108	00125	SO  	2000	1	8	2000ZZZX18       	1	19991219	G	2842	486467	TRANSMITTER     			PIPER 	PA32  	PA32R301T   	7103220	SO  										FUEL QUANTITY	ERRATIC         	B	S		SO5R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	03	75AU				1170	3257079				RIGHT FUEL QUANTITY ERRATIC.  DEFUELED AIRCRAFT AND REPLACED INBOARD AND OUTBOARD SENDERS WITH NEW.  ATTEMPTED FUEL QUAN	TITY CALIBRATION.  RIGHT WING WOULD INDICATE 10 U.S. GAL WHEN EMPTY.  UNABLE TO CALIBRATE.  INVESTIGATED PROBLEM, UPON R	EMOVAL OF SIGHT GAUGE ON TOP OF RIGHT WING, FOUND FLOAT ARM ON INBD SENDER RESTING ON CUT-OUT IN RIB PRIOR TO CONTACT RO	LL PIN STOP ON SENDER.  REPOSITIONED ARM AND COMPLETED FUEL CALIBRATION SUCCESSFULLY.  SUBMITTER STATED THIS IS SECOND A	CFT FOUND WHERE FLOAT ARM WHERE IT PASSES THROUGH THE RIB RESTS ON THE RIB PRIOR TO LIFTING STOP.  RECOMMEND ONE-TIME IN	SP OF ALL NEW SARATOGAS FOR PROPER CLEARANCE, AND A FUEL CALIBRATION IF INTERFERENCE IS FOUND.	1	L	7	1 	3O				A3SO    					 
2000012200364	20000122	00364	WP  	2000	1	22	2000ZZZX180      	1	19991209	G	3210	NAS63839	BOLT            			DOUG  	DC8   	DC871F      	302199D	WP  										RT MLG	MISMANUFACTURED 	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	19	CTEXT	81575	33434			45945				DURING REPLACEMENT OF RT MLG ATTACH FITTING (TRUNNION) WHILE INSTALLING LOWER REAR AUXILIARY SPAR CAP TO TRUNNION, 'NEW 	CONDITION' BOLT, P/N NAS-638-39, CRACKED WHILE TURNING INTO POSITION.  THIS BOLT WAS ONLY BEING RUN IN AT TIME OF FAILUR	E, NOT TORQUED.  ACFT N NR HK-4176X.				2	L	7	4 	4F			RT	4A25    					 
2000012200365	20000122	00365		2000	1	22	2000ZZZX181      	4	19991222	G	3416		INDICATOR       	BENDIX      	0660306200  	BEECH 	1900  	1900D       	1154162	CE  										COCKPIT	MALFUNCTIONED   	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01	154GL		759  		4446	UE154				MILIBAR AND INCHES OF  MERCURY SCALES DO NOT MATCH (I.E., 29.92 IN HG SHOWS 0993 MB INSTEAD OF 1013 MB).						2	L	7	2 	4T			RT	A24CE   					 
2000012200366	20000122	00366	EU  	2000	1	22	2000ZZZX182      	1	19991208	G	6710	1174120101	CYCLIC JACKSHAFT			BOLKMS	117   	BK117A3     	5626015	EU  										MAIN ROTOR	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	312LS	6173 			761	7061				TECHNICIAN PULLED LARGE AMOUNT OF RUST OUT OF INSIDE OF CYCLIC JACKSHAFT WHILE USING MAGNET TO RETRIEVE LOST SCREW.  REM	OVED JACKSHAFT AND INSPECTED.  LARGE AMOUNT OF RUST RESIDUE AND PITTING OF JACKSHAFT ESPECIALLY ON PILOT SIDE.  MFG ALLO	WS .4 MM CORROSION DAMAGE.  ALMOST IMPOSSIBLE TO MEASURE DEPTH WITH CONVENTIONAL MEANS.  WILL SEND TO BE ULTRASONICALLY 	TESTED.  SUBMITTER SUSPECTED THIS ONE BEYOND LIMITS.  REMOVED SAME P/N SHAFT OUT OF ANOTHER ACFT.  IT HAD SMALL AMOUNT O	F SURFACE RUST.  APPEARS THERE IS INSUFFICIENT PAINT TO PROTECT INTERIOR.  DESIGN OF SHAFT HAS CASTING ON EACH END THAT 	ANGLES UP 45 DEGREES WHICH WOULD MAKE CAPTURING FLUIDS EASY.  SUBMITTER STATED THERE ARE NO PROVISIONS FOR DRAINAGE.	1	G	7	2 	3U				H13EU   					 
2000012200367	20000122	00367	WP  	2000	1	22	2000ZZZX183      	1	19991206	G	3230	5771407501	BRACE           		57146965529 	DOUG  	DC8   	DC871       	302199A	WP  										NLG	DAMAGED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19	CTEXT				350	45849				UPON GEAR EXTENSION INTO MIAMI, HEARD STRANGE NOISE FROM NOSE WHEELWELL AREA.  GEAR EXTENDED NORMALLY WITH 3 GREEN INDIC	ATIONS.  POST-FLIGHT SIDE BRACE ATTACH LUG FOR RETRACT CYLINDER ATTACHMENT CRACKED.  ACFT N NR HK-3785X.					2	L	7	4 	4F				4A25    					 
2000012200368	20000122	00368	GL  	2000	1	22	2000ZZZX184      	2	19991228	G	7250	9392M86G08	SHROUD          								GE    	CF6   	CF680C      		GL  					TURBINE	DISBONDED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15			400  							3 EACH CF6-80C2 STG 2 HPT SHROUDS WITH 40 CYCLES AND 2,000 HOURS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF WEAR	COAT MATERIAL FROM SUBSTRATE.  PW ENGINEERING STATED THIS IS NOT A FLIGHT SAFETY ISSUE.  ROOT CAUSE IS STILL UNDER INVES	TIGATION.									4	F			E23EA				 
2000012200369	20000122	00369	NM  	2000	1	22	2000ZZZX185      	1	19991215	G	3233	65446921	HOUSING         		65446913    	BOEING	737   	737*        		NM  										MLG ACTUATOR	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					193					HOUSING IS CRACKED IN THE 'U' AND 'D' REGULATOR PORTS.  FATIGUE, OVERSTRESSED OR FLAW/DEFECT IN CASTING OF THE HOUSING.						2	L	7	2 	4F			RT	A16WE   					 
2000012200370	20000122	00370	NM  	2000	1	22	2000ZZZX186      	1	19991215	G	3233	65446921	HOUSING         		65446913    	BOEING	737   	737*        		NM  										MLG ACTUATOR	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					349					HOUSING IS CRACKED AT THE BOTTOM OF THE 'D' PRIORITY PORT.  FATIGUE, OVESTRESSED OR FLAW/DEFECT IN CASTING OF THE HOUSIN	G.					2	L	7	2 	4F			RT	A16WE   					 
2000012200371	20000122	00371	NM  	2000	1	22	2000ZZZX187      	1	19991220	G	2730	654484511	MANIFOLD        		654476118   	BOEING	737   	737*        		NM  										ELEVATOR PCU	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					3107					MANIFOLD IS CRACKED AT AND AROUND THE FILTER BOWL.  FATIGUE, OVERTORQUING OF THE RETAINER AND/OR MISHANDLED.						2	L	7	2 	4F			RT	A16WE   					 
2000012200372	20000122	00372	NM  	2000	1	22	2000ZZZX188      	1	19991213	G	2761	654494710	HOUSING         		65448517    	BOEING	737   	737*        		NM  										SPOILER ACTUATOR	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		45036	32336		1224					HOUSING IS CRACKED ON SIDE OPPOSITE OF PORTS.  OVERSTRESSED, FATIGUE, AND/OR POSSIBLE FLAW IN HOUSING DESIGN.						2	L	7	2 	4F			RT	A16WE   					 
2000012200373	20000122	00373	NM  	2000	1	22	2000ZZZX189      	1	19991215	G	2750	5068801	BODY            		506875      	BOEING	707   	707*        		NM  										CONTROL VALVE	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					RC31					HOUSING IS CRACKED IN THE FILTER BOWL.  FATIGUE, OVERSTRESSED AND/OR POSSIBLE HIGH HOURS.						2	L	7	4 	4J			RT	4A21    					 
2000010800167	20000108	00167	EA  	2000	1	8	2000ZZZX19       	1	19991213	G	2597		WIRE            		14501       	CNDAIR	CL600 	CL6002B16   	1900305	EA  										WATER HEATER	CHAFED          	B	P		RO3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03	607RP				951221406	5184				AFTER BEING REPORTED BY THE OWNER/OPERATOR THAT THE WATER HEATER OVER-HEATED AND CAUSED DAMAGE TO THE WATER HEATER AND A	T LAVATORY SURROUNDING CABINETRY.  UPON ACCOMPLISHMENT OF A VISUAL INSPECTION OF THE LAVATORY AREA AND WATER HEATER/ELEC	TRICAL SYSTEM, IT WAS DETERMINED THE HEATER ELEMENT CONTROL WIRING HAD SHORTED TO GROUND AT THE THERMOSTAT (WIRE CHAFING	).  THIS CAUSED THE HEATER TO REMAIN IN THE 'ON' POSITION AT ALL TIMES.  FURTHER INSPECTION REVEALED BURNED WIRING AND D	AMAGE TO LAV WALL LINERS AND SHELVING.  REPLACED WATER HEATER AND RE-ROUTED CONTROL WIRE TO PREVENT CHAFING ON THE THERM	OSTAT.  LAV WALL LINERS AND ASSOCIATED ITEMS REPLACED DUE TO HEAT.  NO DAMAGE TO THE AIRFRAME WAS NOTED.	2	L	7	2 	4F			RT	A21EA   					 
2000012200374	20000122	00374	NM  	2000	1	22	2000ZZZX190      	1	19991209	G	2782	71001297	BODY            	ROTOL       	26002913    	BOEING	727   	727         	UTILSYS	NM  										SLAT ACTUATOR	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					A153					BODY ASSEMBLY IS CRACKED ON THE RETRACT PORT AT THE CROSS HOLE INTERSECTION IN TRUNNION BORE.  BODY HAS SHARP CORNERS AT	 THE CROSS HOLE INTERSECTION IN THE TRUNNION BORE.  INCORPORATE A RADIUS ON THE SHARP CORNERS OF THE INTERSECTION IN THE	 TRUNNION BORE IAW SB 2-690029-27-112.				2	L	7	3 	4J			RT	A3WE    					 
2000012200375	20000122	00375	NM  	2000	1	22	2000ZZZX191      	1	19991214	G	3230	6F230925	BODY            	CRISSAIR    	6F23925     	BOEING	737   	737*        		NM  										MLG	BROKEN          	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01										VALVE BODY IS BROKEN INTO TWO PIECES.  FATIGUE, OVERSTRESSED AND/OR WEAK POINT IN BODY.						2	L	7	2 	4F			RT	A16WE   					 
2000012200376	20000122	00376	NM  	2000	1	22	2000ZZZX192      	1	19991207	G	2742	69778551	SPRING          		654997025   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		18876			KEO1710					SPRINGS P/N 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE AND INCREAS	ED SPRING OIL STRESSES.  SPRINGS P/N 69-77855-1 ARE TO BE REPLACED WITH P/N 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLIES MA	NUFACTURED PRIOR TO S/N KEO1730 PER BOEING SL 737-SL-27-090-B.				2	L	7	2 	4F			RT	A16WE   					 
2000012200377	20000122	00377	NM  	2000	1	22	2000ZZZX193      	1	19991215	G	2742	69778551	SPRINGS         		654997025   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		19123			KEO1721					SPRINGS P/N 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT-TREATING, AUSTENTITE, FATIGUE AND INCREA	SED SPRING COIL STRESSES.  SPRINGS P/N 69-77855-1 ARE TO BE REPLACED WITH P/N 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLIES 	MANUFACTURED PRIOR TO S/N KEO1730 PER BOEING SL 737-SL-27-090-B.				2	L	7	2 	4F			RT	A16WE   					 
2000012200378	20000122	00378	NM  	2000	1	22	2000ZZZX194      	1	19991220	G	2761	654494710	HOUSING         		65448517    	BOEING	737   	737277      	1384570	NM  										SPOILER	LEAKING         	B	P		IU6R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NM	01	178AW	56185			3233	22645				HOUSING HAS A PINHOLE NEXT TO THE PORT.  OVERSTRESSED, FATIGUE, AND/OR POSSIBLE FLAW IN HOUSING DEESIGN.						2	L	7	2 	4F			RT	A16WE   					 
2000012200379	20000122	00379	NM  	2000	1	22	2000ZZZX195      	1	19991214	G	2910	106611F	ARM             	ITT         	AV24E1144   	BOEING	727   	727         	UTILSYS	NM  										HYD ACTUATOR	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		51201	12415		J88377					SWITCH ACTUATING ARM IS CRACKED.  WEAKENED AREA FROM CONTINUOUS CONTACT WITH SWITCH.						2	L	7	3 	4J			RT	A3WE    					 
2000012200380	20000122	00380	NM  	2000	1	22	2000ZZZX196      	1	19991214	G	3233	65446922	HOUSING         		65446914    	BOEING	737   	737*        		NM  										MLG MODULE	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					45					HOUSING IS CRACKED IN THE 'D' PRIORITY PORT.  FATIGUE, OVERSTRESSED OR FLAW/DEFECT IN CASTING OF THE HOUSING.						2	L	7	2 	4F			RT	A16WE   					 
2000012200381	20000122	00381	NM  	2000	1	22	2000ZZZX197      	1	19991220	G	5311		FRAME           			BOEING	727   	727227      	1384078	NM  										BS 1015 - 1115	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED ON L2 DOOR CUSP FRAME STA 1015 - STA 1115.						2	L	7	3 	4F				A3WE    					 
2000012200382	20000122	00382		2000	1	22	2000ZZZX198      	4	19991220	G	3454	DMN15021	MODE S ANTENNA  			BOEING	727   	727227      	1384078	NM  										FUSELAGE	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755				60787	21366				DURING A C-CHECK, COROSION NOTED ON UPPER MODE 'S' ANTENNA.						2	L	7	3 	4F				A3WE    					 
2000012200383	20000122	00383	NM  	2000	1	22	2000ZZZX199      	1	19991220	G	5347		SEAT TRACK      			BOEING	727   	727227      	1384078	NM  										BS 1070	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK BS 1070 RBL 24.75 AND LBL 24.75.						2	L	7	3 	4F				A3WE    					 
2000010800095	20000108	00095	EU  	2000	1	8	2000ZZZX2        	1	19991022	G	7931	S1120021090	SWITCH          			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	40751	194  			6621	3154				SWITCH CONTACTS DO NOT OPEN WHEN FUEL PRESSURE IS APPLIED TO SWITCH RMA R022541.  REMOVED AND REPLACED.						1	G	7	1 	3U				H9EU    					 
2000010800168	20000108	00168	EA  	2000	1	8	2000ZZZX20       	2	19990909	G	8530	05K21114K4	CYLINDER        			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  					ENGINE	CRACKED         	D	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	25	89629	506  				15282807	L2006315			MASSIVE OIL LEAK REVEALED CRACKED CYLINDER BARREL ON LYCOMING P/N LW16703, 506.2 TTSN.  DISCOVERED 9-9-99.						1	H	7	1 	3O	3	O	NT	3A19    	E223				 
2000012200386	20000122	00386	NM  	2000	1	22	2000ZZZX202      	1	19991220	G	5315		FLOORBEAM       			BOEING	727   	7272M7      	138407S	NM  										BS 400	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	725RW					21502				DURING A C-CHECK, CORROSION NOTED ON FLOORBEAM'S (AT BS 400) CHORD.  UPPER AND LOWER SURFACES LBL 24 - RBL 44.						2	L	7	3 	4F				A3WE    					 
2000012200387	20000122	00387	NM  	2000	1	22	2000ZZZX203      	1	19991220	G	5315		FLOORBEAM       			BOEING	727   	7272M7      	138407S	NM  										BS 1110	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	725RW					21502				DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM AT BS 1110 ON LOWER CHORD'S UPPER AND LOWER SURFACES.						2	L	7	3 	4F				A3WE    					 
2000012200388	20000122	00388	NM  	2000	1	22	2000ZZZX204      	1	19991220	G	5315		FLOORBEAM       			BOEING	727   	7272M7      	138407S	NM  										BS 1050	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	725RW					21502				DURING A C-CHECK, CORROSION NOTED AT BS 1050 FLOORBEAM'S LOWER CHORD, UPPER AND LOWER SURFACE APPROXIMATELY LBL 10.						2	L	7	3 	4F				A3WE    					 
2000012200389	20000122	00389	NM  	2000	1	22	2000ZZZX205      	1	19991220	G	5320		WEB             			BOEING	727   	7272M7      	138407S	NM  										FUSELAGE	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	725RW					21502				DURING A C-CHECK, CORROSION NOTED IN RT AFT LAVATORY AREA ON UPPER SURFACE OF SHEAR WEB.						2	L	7	3 	4F				A3WE    					 
2000012200390	20000122	00390	NM  	2000	1	22	2000ZZZX206      	1	19991220	G	5311		FRAME           			BOEING	727   	7272M7      	138407S	NM  										BS 740-760	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	725RW					21502				DURING A C-CHECK, CORROSION NOTED IN DELTA BEAM AREA ENTIRE FRAME UPPER AND LOWER SURFACES FOR ADF LOOP ANTENNA, BS 740 	- BS 760 BL ZERO.					2	L	7	3 	4F				A3WE    					 
2000012200391	20000122	00391	NM  	2000	1	22	2000ZZZX207      	1	19991220	G	5314		KEEL BEAM       			BOEING	737   	737236      	1384476	NM  										FUSELAGE	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	920WA					21791				DURING A C-CHECK, CORROSION NOTED ON LEFT KEEL BEAM AT AIRCRAFT DOOR HINGE ATTACH POINTS.						2	L	7	2 	4F			RT	A16WE   					 
2000012200392	20000122	00392	NM  	2000	1	22	2000ZZZX208      	1	19991220	G	5280		ANGLE           			BOEING	737   	737236      	1384476	NM  										NLG DOOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	920WA					21791				DURING A C-CHECK, CORROSION NOTED ON NOSE COMPARTMENT DOOR (1103) ANGLE, INTERCOSTAL AND PLATE.						2	L	7	2 	4F			RT	A16WE   					 
2000012200393	20000122	00393	NM  	2000	1	22	2000ZZZX209      	1	19991220	G	5311	69157683	FRAME           			BOEING	727   	727231      	1384079	NM  										BS 228	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	64319					20052				DURING A C-CHECK, CORROSION NOTED ON FRAME AT STA 228.5, BL ZERO.						2	L	7	3 	4F				A3WE    					 
2000010800169	20000108	00169	CE  	2000	1	8	2000ZZZX21       	1	19991216	G	7110	J744436	MOUNT           			CESSNA	172   	172S        	2072439	CE  										COWL	TORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	949SP	388  				172S8145				DURING PHASE 2 INSPECTION, FOUND 4 LOWER COWL ATTACH SHOCK MOUNTS TORN AT THE BASE.  LOCATED AT THE 2, 3, AND 4 O'CLOCK 	POSITIONS AND THE LOWER L.  REPLACED SHOCK MOUNTS.					1	H	7	1 	3O			NT	3A12    					 
2000012900230	20000129	00230	NM  	2000	1	29	2000ZZZX216      	1	19991220	G	5315		FLOORBEAM       			BOEING	727   	7272M7      	138407S	NM  										BS 1030	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	725RW					21502				DURING A C-CHECK, CORROSION WAS NOTED ON UPPER CHORD UPPER AND LOWER SURFACES OF FLOORBEAM STA 1030 RBL 12 TO LBL 24.						2	L	7	3 	4F				A3WE    					 
2000012900231	20000129	00231	SW  	2000	1	29	2000ZZZX217      	1	19990616	G	2820	222366621101	FUEL FILTER     			BELL  	206   	206B        	1181511	SW  										FUEL SYSTEM	BROKE           	H		A		O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			NM	11	5754K	6518 				3126				REASON FOR REMOVAL, FILTER BODY CENTER THREADED PORTION, CRACKED AND SEPARATED FROM BODY ALLOWING FILTER CAN TO SEPARATE	 FROM FILTER BODY.  MACHINE WORK TO INSIDE OF THIS BODY LOOKS TO HAVE BEEN OUT OF CENTER; THUS, CAUSED THE MOUNTING SUPP	ORT WEB TO BE VERY THIN ON ONE SIDE.  SUBMITTER SUSPECTED NORMAL TIGHTENING OF FILTER CAN WILL EVENTUALLY CAUSE THREADED	 WEB TO SEPARATE FROM HOUSING ALLOWING FILTER CAN TO SEPARATE FROM FILTER.  SUGGEST A ONE-TIME INSPECTION OF SUSPECTED F	ILTER HOUSING BE CONDUCTED TO DETERMINE IF THREADED WEB HAS ENOUGH THICKNESS AND NO CRACKS EXIST WHERE WEB AND HOUSING C	OME TOGETHER.	1	G	7	1 	3U				H2SW    					 
2000012900232	20000129	00232	CE  	2000	1	29	2000ZZZX218      	1	19991229	G	3710	211CC	PUMP            	RAPCO       		CESSNA	150   	152         	2071835	CE  										VACUUM SYSTEM	FAILED          	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	03	47446		1169 		69515	15283227				FOUND PUMP BODY SEPARATED FROM PUMP BASE.  SECURING BOLTS WERE MISSING.						1	H	7	1 	3O			NT	3A19    					 
2000010800170	20000108	00170	CE  	2000	1	8	2000ZZZX22       	1	19991216	G	7111	04530032	BRACKET         			CESSNA	172   	172S        	2072439	CE  										COWL	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	949SP					172S8145				DURING PHASE 2 INSPECTION, FOUND LOWER COWL SHOCK MOUNT BRACKET CRACKED AT THE 4 O'CLOCK POSITION.  THE OTHER HALF OF TH	E SHOCK MOUNT BRACKET WAS ALSO CRACKED, P/N 045303-3.  REPLACED BOTH BRACKETS.					1	H	7	1 	3O			NT	3A12    					 
2000012900234	20000129	00234	CE  	2000	1	29	2000ZZZX220      	1	19991230	G	3243		HOSE            			CESSNA	180   	180A        	2072604	CE  										BRAKE ASSY	DETERIORATED    	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	13	1044Y	7675 				32833				DURING AN ANNUAL INSPECTION BOTH MASTER CYLINDER FLEXIBLE HOSES WERE FOUND SEVERELY DETERIORATED.						1	H	7	1 	3O				5A6     					 
2000012900236	20000129	00236	CE  	2000	1	29	2000ZZZX222      	1	19991129	G	7810	085071123	TAIL PIPE       			CESSNA	310   	T310R       	2074246	CE  										LT ENGINE	BUCKLED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	5038J	12136				310R0158				UPON COMPLETION OF AD 75-23-08-R5 NOTED TAIL PIPE SEVERELY BUCKLED.  TOTAL TIME 1,436.0 HOURS.  INSTALLED KNISLEY STC SA	 00040LB.  OPS CHECKED SYSTEM, NO DEFECTS FOUND.					1	L	7	2 	3O				3A10    					 
2000012900238	20000129	00238	CE  	2000	1	29	2000ZZZX224      	1	19991129	G	3010		DEICE SYSTEM    			CESSNA	310   	T310Q       	2074244	CE  										VERTICAL STAB	INOPERATIVE     	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	767RR					3101P455				NOTED THAT DE-ICE FOR VERTICAL STABILIZER INOPERATIVE.  FURTHER INVESTIGATION REVEALS HOSES TIED OFF.  REPLACED HOSES, P	ATCHED BOOT.  OPS CHECKED, WORKS FINE.  TOATL TIME AT INSTALLATION UNKNOWN.					1	L	7	2 	3O				3A10    					 
2000012900239	20000129	00239	CE  	2000	1	29	2000ZZZX225      	1	19991129	G	5720		FITTING         			CESSNA	310   	T310Q       	2074244	CE  										RT WING	UNAPPROVED PART 	H	S			K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	01	767RR					310Q0455				NOTE:  FITTING WAS STEEL  SUBMITTER STATED FITTING LOOKED HOMEMADE.  INSTALLED FORGED NEW CORRECT CESSNA PART MADE FORM 	ALUMINUM.  PART TOTAL TIME UNKNOWN.					1	L	7	2 	3O				3A10    					 
2000012900240	20000129	00240	SO  	2000	1	29	2000ZZZX226      	1	19991207	G	3230	6703704	FORK            			PIPER 	PA44  	PA44180     	7104402	SO  										MLG	SEPARATED       	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	15	8322S				OPJ80	448195014				WHEEL FORK SEPARATED ABOVE STRUT ATTACH POINT UPON LANDING.  SUBMITTER STATED IT APPEARED TO BE A STRESS FATIGUE FAILURE	 AND RECOMMENDED REMOVING WHEEL FORK AND AN INSPECTION ABOVE THE STRUT TUB.					1	L	7	2 	3O				A19S0   					 
2000012900241	20000129	00241	CE  	2000	1	29	2000ZZZX227      	1	19991129	G	7810	085071144	TAIL PIPE       			CESSNA	340   	340CESSNA   	2076404	CE  										RT ENGINE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	771TC					3400249				UPON COMPLETION OF AD 75-23-O8-5R, NOTED TAIL PIPE CRACKED WHERE IT GOES THROUGH NACELLE AND METAL VERY FATIGUED.  COULD	 PUSH FINGER THROUGH PIPE.  TOTAL TIME UNKNOWN.					1	L	7	2 	3O				3A25    					 
2000012900243	20000129	00243	EA  	2000	1	29	2000ZZZX229      	2	19991224	G	7414	S6LN204	SCREW           	BENDIX      	101630599   	PIPER 	PA23  	PA23250     	7102308	SO  	LYC   	O540  	IO540C4B5   	41532	EA  					MAGNETO	LOOSE           	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	05	331FC		80   		9023095	277554024	L1251148A			MAGNETO CASE SCREW CAME LOOSE CAUSING MAGNETO TO COME APART IN-FLIGHT.  UPON INSPECTION, FOUND BACK HALF OF MAG CASE LYI	NG LOOSE HANGING FROM WIRES.  SCREWS COULD NOT BE FOUND.					1	L	7	2 	3O	3	O		1A10    	1E4				 
2000010800171	20000108	00171	CE  	2000	1	8	2000ZZZX23       	1	19991216	G	7111	04530033	BRACKET         			CESSNA	172   	172S        	2072439	CE  										COWL	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	949SP					172S8145				DURING PHASE 2 INSPECTION, FOUND LOWER COWL SHOCK MOUNT BRACKET CRACKED AT THE 4 O'CLOCK POSITION.  THE OTHER HALF OF TH	E SHOCK MOUNT BRACKET WAS ALSO CRACKED, P/N 045303-3.  REPLACED BOTH BRACKETS.					1	H	7	1 	3O			NT	3A12    					 
2000012900246	20000129	00246	SO  	2000	1	29	2000ZZZX232      	2	19991118	G	7200	652541	NUT             			CESSNA	421   	421B        	2076014	CE  	CONT  	O520  	GTSIO520H   	17032	SO  					LT ENGINE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	17	500AB					4210369	218176R			FOUND LOWER FORWARD ENGINE CASE THROUGH-BOLT NUT (LEFT) CRACKED ENTIRELY THROUGH.  THIS IS THE NEW TWELVE POINT FLANGED 	NUT REQUIRED BY TELEDYNE CONT M92-9.					1	L	7	2 	3O	3	O		A7CE    	E7CE				 
2000012900247	20000129	00247	CE  	2000	1	29	2000ZZZX233      	1	19991213	G	2752	EZ7RWT8C	SWITCH          		51523710    	CESSNA	402   	402B        	207590P	CE  										FLAP ACTUATOR	BROKEN          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	19	773EA	12116				402B0544				CAM, PN 5115253-1, SLIPPED MISSING ARM ON SWITCH.  COCKPIT SWITCH BROKE AND THIS WAS THE BACK-UP CAUSING FAILURE OF FLAP	 SYSTEM.					1	L	7	2 	3O				A7CE    					 
2000012900248	20000129	00248	EA  	2000	1	29	2000ZZZX234      	2	19991101	G	7314	R69080J1	PUMP            			GULSTM	500   	500S        	0141107	SW  	LYC   	O540  	IO540E1B5   	41532	EA  					LT ENGINE	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	09	8536				C6082019	3267				PUMP WAS OVERHAULED OFF THE SHELF.  UPON INSTALLATION AND OPS CHECK, WAS FOUND TO BE PUMPING FUEL OUT OF DRAIN HOLE.						1	H	7	2 	3O	3	O		6A1     	1E4				 
2000012900249	20000129	00249	SO  	2000	1	29	2000ZZZX235      	1	19991229	G	2810	531001	FUEL CAP        			PIPER 	PA31  	PA31350     	7103110	SO  										FUEL CELL	SEPARATED       	H				O				OTHER                   				K	Y	J	FLUID LOSS                	ENGINE STOPPAGE           	WARNING INDICATION        	NR	NOT REPORTED   	1			GL	25	225TM					318152165				FTW- RIGHT INBOARD FUEL CAP POPPED OFF AND SUCKED ALL FUEL OUT WHICH SHUT ENGINE DOWN ON APPROACH INTO FT WAYNE.  REPLAC	ED FUEL CAP.					1	L	7	2 	3O				A20SO   					 
2000012900255	20000129	00255	SO  	2000	1	29	2000ZZZX241      	1	19991102	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE	BROKEN          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		998  			1562A					BRAKE ASSEMBLY, P/N 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN BINDING IN TORQUE TUBE KEY SLOTS.  SUBMITTER STATED 	THIS IS A CONTINUAL DISCREPANCY.  BRAKE ASSEMBLY SHOULD LAST 2,500 CYCLES.  NOTE:  OEM PARTS INSTALLED IN BRAKE ASSEMBLY	 AND THE MOST RECENT BRAKE CONFIGURATION, P/N 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
2000012900256	20000129	00256		2000	1	29	2000ZZZX242      	1	19991219	G	2432	G6381E	BATTERY         																	E/E BAY	DAMAGED         	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09					G01806043					BATTERY HANDLE HOLD-DOWN BOLTS ARE BEING DETERIORATED BY THE ELECTROLYTE.  SEVERAL BOLTS DISSOLVED TO NOTHING BUT POWDER	.  GILL, P/N 1407.  SUBMITTER STATED HAS SEEN PROBLEM ON THREE BATTERIES, GILL P/N G-6381E, SN'S G01806043, G01806051, A	ND G01806060.  CONTACTED MANUFACTURER AND THEY WERE AWARE OF PROBLEM.																	 
2000012900257	20000129	00257		2000	1	29	2000ZZZX243      	1	19991219	G	2432	G6381E	BATTERY         																	E/E BAY	DAMAGED         	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09					G01806051					BATTERY HANDLE HOLD-DOWN BOLTS ARE BEING DETERIORATED BY THE ELECTROLYTE.  SEVERAL BOLTS DISSOLVED TO NOTHING BUT POWDER	.  GILL, P/N 1407.  SUBMITTER STATED HAS SEEN PROBLEM ON THREE BATTERIES, GILL P/N G-6381E, SN'S G01806043, G01806051, A	ND G01806060.  CONTACTED MANUFACTURER AND THEY WERE AWARE OF PROBLEM.																	 
2000012900258	20000129	00258		2000	1	29	2000ZZZX244      	1	19991219	G	2432	G6381E	BATTERY         																	E/E BAY	DAMAGED         	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09					G01806060					BATTERY HANDLE HOLD-DOWN BOLTS ARE BEING DETERIORATED BY THE ELECTROLYTE.  SEVERAL BOLTS DISSOLVED TO NOTHING BUT POWDER	.  GILL, P/N 1407.  SUBMITTER STATED HAS SEEN PROBLEM ON THREE BATTERIES, GILL P/N G-6381E, SN'S G01806043, G01806051, A	ND G01806060.  CONTACTED MANUFACTURER AND THEY WERE AWARE OF PROBLEM.																	 
2000020500920	20000205	00920	CE  	2000	2	5	2000ZZZX255      	1	19991224	G	7603	5038901223	THROTTLE CABLE  			BEECH 	58    	58          	1152740	CE  										THROTTLE	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	95BB					TH333				CMH - LEFT THROTTLE STUCK AT FULL THROTTLE.  REMOVED AND REPLACED BROKEN THROTTLE CABLE.  OPS GOOD.						1	L	7	2 	3O			 	3A16    					 
2000020500921	20000205	00921	CE  	2000	2	5	2000ZZZX256      	1	19991215	G	3230		SWITCH          			BEECH 	58    	58          	1152740	CE  										MLG	FROZEN          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	07	95BB					TH333				SYR - LANDING GEAR WOULD NOT GO UP COMING OUT OF ROCHESTER NY.  LANDED IN SYRACUSE, NO PROBLEMS.  MAINTENANCE HEATED GEA	R THAWING SQUAT SWITCHES. SWUNG GEAR, OPS CHECKED GOOD.					1	L	7	2 	3O				3A16    					 
2000020500922	20000205	00922	CE  	2000	2	5	2000ZZZX257      	1	19991220	G	2822	476411	PUMP            			CESSNA	310   	T310R       	2074246	CE  										FUEL PUMP	FAILED          	D		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	25	5255C	16   				310R1528				OWNER NOTIFIED THAT LEFT LANDING LIGHT/TIP TANK TRANSFER PUMP CIRCUIT BREAKER OPENED.  FOUND TIP TANK TRANSFER PUMP FAIL	ED ELECTRICALLY.  UNIT SHOWS SIGNS OF ARCING AND OVERHEATING AT POWER WIRE INLET AREA.  UNIT HAD BEEN REPLACED 15.7 HOUR	S PREVIOUSLY.  THIS P/N PUMP HAS BEEN HAVING A HIGH FAILURE RATE WITH IDENTICAL FAILURE MODES.  THIS IS 6TH FAILED UNIT 	IN A 2 MONTH PERIOD ON VARIOUS ACFT.  ALL FAILED PUMPS WITH RECENT MANUFACTURE (12 TO 18 MONTHS) TIME FRAME AND ALL WITH	 IDENTICAL PROBLEM.		1	L	7	2 	3O				3A10    					 
2000010800174	20000108	00174	SO  	2000	1	8	2000ZZZX26       	1	19991108	G	7921	20006A	OIL COOLER      	NIAGARA     	E9729099    	PIPER 	PA32  	PA32R300    	7103213	SO  										LEFT	CRACKKED        	H	S			O				OTHER                   				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	19	7951C	463  				32R76800700				AFTER LANDING FROM A FLIGHT OF 4 HOURS OVER OPEN WATER, FOUND THE LEFT WING ELEVATOR AND NOSE GEAR DOORS DRIPPING WITH O	IL.  UPON FURTHER INSPECTION, FOUND THE LEFT OIL COOLER CRACKED ON BASE OF TOP COOLING FIN UNDER THE FITTING BASE.  ABOU	T 4 QUARTS OF OIL WERE LEFT IN THE ENGINE.  DURING INSPECTION, CAN ONLY COME UP WITH THAT MAYBE DUE TO NORMAL ENGINE VIB	RATION, THE HOSES AND FITTING LENGTH MAY BE CONTRIBUTING TO A LOAD ON THIS AREA CAUSING THE OIL COOLER, IN TIME, TO CRAC	K.  REPLACED OIL COOLER AND RETURNED TO SERVICE.  NO DAMAGE WAS CAUSED TO THE AIRCRAFT.		1	L	7	1 	3O				A3SO    					 
2000020500925	20000205	00925	CE  	2000	2	5	2000ZZZX260      	1	19991122	G	2810	58380036	BLADDER         			BEECH 	58    	58P         	1152744	CE  										RT WING	LEAKING         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	15					1574R	TJ252				RIGHT WING BOX SECTION FUEL CELL (BLADDER) P/N 58-380003-6, LEAKING FUEL.  ONCE OLD BLADDER WAS REMOVED, FOUND FUEL STAI	NS AT 2 INTERCONNECT HOSES.  THE CLAMPS THAT ARE ACCESSED FROM INSIDE THE TANK WERE FINGER TIGHT.  THERE IS NO MEANS FOR	 SAFETY WIRE OR INTERFERENCE FIT OF SAFETY ON THESE CLAMPS.  NEW BLADDER WAS INSTALLED AS A PRECAUTION.  SUBMITTER STATE	D THESE HOSE CLAMPS SHOULD HAVE SOME MEANS OF MAINTAINING TORQUE VIA SAFETY CLIPS OR INTERFERENCE FIT ON CLAMP TIGHTENIN	G SCREW.		1	L	7	2 	3O				A23CE   					 
2000020500926	20000205	00926	CE  	2000	2	5	2000ZZZX261      	1	19991202	G	5312		BULKHEAD        			CESSNA	340   	340A        	2076405	CE  										ENGINE BAY	CORRODED        	B			OH8R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	11	330MR					340A0721				IN C/W CESSNA SI MEB 99-10, ULTRASONIC NDT INSPECTION, FOUND ENGINE BEAMS AND CANTED BULKHEAD CORRODED BEYOND THE MATERI	ALS ACCEPTABLE THICKNESS.  CAUSE OF CORROSION WAS FROM LEAKING EXHAUST AND HIGH TURBO TEMPERATURE.  TO COVER ENGINE BEAM	S AFTER NDT INSPECTION, RECOMMEND REPLACEMENT OF CANTED BULKHEAD OR STAINLESS STEEL DOUBLERS AROUND EXHAUST AUGMENTER TU	BES RUNNING THROUGH THE CANTED BULKHEAD.			1	L	7	2 	3O				3A25    					 
2000020500928	20000205	00928		2000	2	5	2000ZZZX263      	4	19991014	G	2562	AK450	ELT             			CESSNA	340   	340A        	2076405	CE  										CABIN	INOPERATIVE     	D				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			GL	25	340BW				455167	340A0267				DURING ANNUAL TEST PER FAR 91.207 FOUND ELT UNIT INOPERATIVE. UNIT G SWITCH ACTIVATES AND TEST LIGHT ILLUMINATES BUT WIL	L NOT TRANSMIT ANY RF SIGNAL ON ANY FREQUENCY. SUBMITTER STATED THIS UNIT IS THE FOURTH UNIT IN A ROW OF THIS MAKE AND M	ODEL WITH THE SAME PROBLEM.  ALL UNITS INSTALLED IN THE LAST 2 OR 3 YEARS.  AS A SIDE NOTE THIS PARTICULAR ELT INSTALLAT	ION WAS NOT COMPLETED IN THIS ACFT IN AN AIRWORTHY FASHION.  NO LOG ENTRIES NOR 337 FORMS, EQUIP LISTS CHANGES FILED.  U	NIT TYE WRAPPED TO STRUCTURE.  NOT INSTALLED IN MFG RACK AND DID NOT MEET INSTALL REQUIREMENTS.  NO REMOTE SWITCHING OR 	INDICATOR LIGHT WAS INSTALLED PER NEW INSTALLATION REQUIREMENTS.	1	L	7	2 	3O				3A25    					 
2000020500929	20000205	00929	CE  	2000	2	5	2000ZZZX264      	1	19991202	G	5320		BEAM            			CESSNA	320   	320F        	2074516	CE  										ENGINE BAY	CORRODED        	B			OH8R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	11	999BS					320F0041				IN C/W CESSNA SI MEB 99-10, ULTRASONIC NDT INSPECTION FOUND ENGINE BEAMS AND CANTED BULKHEAD CORRODED BEYOND THE MATERIA	LS ACCEPTABLE THICKNESS.  CAUSE OF CORROSION WAS FROM LEAKING EXHAUST AND HIGH TURBO TEMPERATURE.  RECOMMEND A STAINLESS	 STEEL CHANNEL.  TO COVER ENGINE BEAMS AFTER NDT INSPECTION, RECOMMEND REPLACEMENT OF CANTED BULKHEAD OR STAINLESS STEEL	 DOUBLERS AROUND EXHAUST AUGMENTER TUBES RUNNING THROUGH THE CANTED BULKHEAD.			1	L	7	2 	3O				3A25    					 
2000020500942	20000205	00942		2000	2	5	2000ZZZX273      	4	19991222	G	3416	066306200	ALTIMETER       	BENDIX      		BEECH 	1900  	1900D       	1154162	CE  										COCKPIT	MALFUNCTIONED   	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01	253GL		1749 		1649	UE253				ALTIMETER FLAG IN VIEW.  BENCH TEST CONFIRMED PROBLEM.  ALTIMETER STAYS FLAGGED AT 1,000 FEET ABOVE THE PRESSURE ALTITUD	E.					2	L	7	2 	4T			RT	A24CE   					 
2000020500945	20000205	00945	EU  	2000	2	5	2000ZZZX276      	1	19991208	G	6710	1174120101	JACKSHAFT       			BOLKMS	117   	BK117A3     	5626015	EU  										MAIN ROTOR	CORRODED        	B		A	TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	312LS	6173 			761	7061				TECHNICIAN PULLED LARGE AMOUNT OF RUST OUT OF INSIDE OF CYCLIC JACKSHAFT WHILE USING MAGNET TO RETRIEVE LOST SCREW.  REM	OVED JACKSHAFT AND INSPECTED.  LARGE AMOUNT OF RUST RESIDUE AND PITTING OF JACKSHAFT, ESPECIALLY ON PILOT SIDE.  MFG ALL	OWS .4 MM CORROSION DAMAGE.  ALMOST IMPOSSIBLE TO MEASURE DEPTH WITH CONVENTIONAL MEANS.  WILL SEND TO BE ULTRASONICALLY	 TESTED.  SUBMITTER SUSPECTED THIS ONE BEYOND LIMITS.  REMOVED SAME P/N SHAFT OUT OF ANOTHER ACFT AND IT HAD SMALL AMOUN	T OF SURFACE RUST.  IT APPEARS THERE IS NO (OR INSUFFICIENT) PAINT TO PROTECT THE INTERIOR.  DESIGN OF SHAFT HAS A CASTI	NG ON EACH END THAT ANGLES UP 45 DEGREES WHICH WOULD MAKE CAPTURING FLUIDS EASY.  THERE IS NO PROVISIONS FOR DRAINAGE.	1	G	7	2 	3U				H13EU   					 
2000010800176	20000108	00176		2000	1	8	2000ZZZX28       	1	19991221	G	3242	7010FS9545708	SEAL            		50105201    															BRAKE	FAILED          	B			XC4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19		1845 			JUN981358					BRAKE ASSEMBLY, PN 5010520-1, FAILED PREMATURELY.  ONE EACH PISTON LEAKING FROM INSULATOR AREA.  PISTON INTERNALLY FILLE	D WITH FLUID.  EVIDENCE OF T-SEAL FAILURE.  THIS IS A CONTINUAL DISCREPANCY.  FACTORY NEW BRAKE ASSEMBLY.  NOTE:  OEM PA	RTS INSTALLED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 5010520-1.																	 
2000022300005	20000223	00005		2000	2	23	2000ZZZX29       	1	19991029	G	3242	244667	CARRIER         	BFGOODRICH  	21585       															BRAKE	FAILED          	B			XC4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19					1578A					BRAKE ASSEMBLY, PN 2-1585, FAILED PREMATURELY.  NR 3 CARRIER AND LINING ASSEMBLY BROKEN IN HALF.  THIS IS A CONTINUAL DI	SREPANCY.  NOTE:  OEM PARTS INTALLED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 2-1585.																		 
2000010800096	20000108	00096	EU  	2000	1	8	2000ZZZX3        	1	19991007	G	7930	642790041	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										OIL PRESSURE	FAILED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	40751	156  			129	3154				INDICATOR WENT TO ZERO IN-FLIGHT.  REMOVED AND REPLACED.						1	G	7	1 	3U				H9EU    					 
2000010800179	20000108	00179	CE  	2000	1	8	2000ZZZX32       	1	19991216	G	8011		SHAFT           	PRESTOLITE  	MHJ4004ECH  	BEECH 	80    	65A80       	1152808	CE  										STARTER	FAILED          	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	15	95LL		1231 		3T000043	LD235				STARTER DRIVE SHAFT TWISTED OFF ABOUT .1250 INCH FORWARD OF KEY SLOT - EVEN WITH FORWARD EDGE OF DRIVEN GEAR ON SHAFT/BE	NDIX.					1	L	7	2 	3O				3A20    					 
2000010800181	20000108	00181		2000	1	8	2000ZZZX34       	1	19990729	G	2750	69157511	SHAFT           		65219458    															GEARBOX	MISINSTALLED    	B			A2TR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	01					DRG114382					INSTALLED SHAFT AND SPROCKET INCORRECTLY (NOT PER FIGURE 1101 OF OHM 27-55-01, PAGE 1102) DURING OH.																			 
2000010800182	20000108	00182		2000	1	8	2000ZZZX35       	1	19990729	G	2750	638358	SPROCKET        		65219458    															GEARBOX	MISINSTALLED    	B			A2TR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	01					DL85					APPLIED DRY FILM LUBRICANT TO EXTERNAL SHAFT SPLINES AND INSTALLED SPROCKET INCORRECTLY (NOT PER FIGURE 1101 OF OHM 27-5	5-01, PAGE 1102) DURING OH.																		 
2000010800183	20000108	00183		2000	1	8	2000ZZZX36       	1	19990729	G	2750	638358	SPROCKET        		65219458    															GEARBOX	MISINSTALLED    	B			A2TR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	01					148385					APPLIED DRY FILM LUBRICANT TO EXTERNAL SHAFT SPLINES AND INSTALLED SPROCKET INCORRECTLY (NOT PER FIGURE 1101 OF OHM 27-5	5-01, PAGE 1102) DURING OH.																		 
2000021900081	20000219	00081	SO  	2000	2	19	2000ZZZX364      	2	19990701	G	8520		CRANKSHAFT      			CESSNA	337   	T337G       	2075726	CE  	CONT  	O360  	TSIO360CB   	17025	SO  					FLANGE	CRACKED         	B	S		EA6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	01	2QJ	48   			A445M1	P3370282	236249R			FOUND CRANKSHAFT FLANGE CRACKED (APPROXIMATELY 2.5 INCHES) ON BACK SIDE.  ENGINE IS A FACTORY REBUILT WITH 48 HOURS AND 	NO RECORDED DAMAGE HISTORY.  ENGINE INSTALLED IN REAR POSTION.					1	H	7	2 	3O	3	O		A6CE    	E9CE				 
2000021900082	20000219	00082	SO  	2000	2	19	2000ZZZX365      	1	19991217	G	7120	3570402	MOUNT           			PIPER 	PA28  	PA28R201T   	7102813	SO  										ENGINE	MISOVERHAULED   	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	17	9874K				L1832	28R7803072				AN EXHANGE ENGINE  MOUNT HAD A TUBE MISALIGNED ON THE LOWER INBOARD, RIGHT SIDE, WHICH CAUSED THE NOSE GEAR DOWNLOCK MEC	HANISM TO BIND AND FALL IN THE GEAR DOWN POSITION.  THE ENGINE MOUNT HAD BEEN IMPROPERLY ALIGNED AND/OR SECURED DURING T	HE ENGINE MOUNT OVERHAUL PROCESS.  SUBMITTER STATED CAREFUL INSPECTION OF ANY WELDED STRUCTURE AFTER AN OVERHAUL/REPAIR 	FOR ALIGNMENT AND PROPER FIT IS REQUIRED.			1	L	7	1 	3O				2A13    					 
2000022300006	20000223	00006		2000	2	23	2000ZZZX37       	1	19991214	G	3246	152058	WHEEL           	BENDIX      	1542511     															MLG	CRACKED         	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19					B1463H2922					FOUND CRACK ON TUBE WELL IN OUTBOARD WHEEL HALF.  DATE OF MANUFACTURE:  8-28-60.																			 
2000021900095	20000219	00095	CE  	2000	2	19	2000ZZZX376      	1	19991214	G	2820		SWITCH          			BEECH 	58    	58          	1152740	CE  										FUEL SYSTEM	OFF             	H				O				OTHER                   				W	R		INADEQUATE Q C            	PARTIAL RPM/PWR LOSS      		NR	NOT REPORTED   	1			GL	07	9044V					TH216				CLE - RT ENGINE LOST POWER ON TAKEOFF.  FOUND FUEL SELECTOR BETWEEN OFF AND ON.						1	L	7	2 	3O				3A16    					 
2000021900097	20000219	00097	CE  	2000	2	19	2000ZZZX378      	1	19991230	G	5530		RUDDER OPENING  			CESSNA	421   	421         	2076010	CE  										VERTICAL STAB	CONTAMINATED    	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	5AY					421033				A LARGE AND VERY WELL HIDDEN BIRD'S NEST WAS FOUND IN RUDDER OPENING.  FORWARD MIDWAY WHERE RUDDER TRIM COMES IN.  EVERY	THING HAD SCREENS, BUT THE BIRDS FOUND A PLACE.					1	L	7	2 	3O			RT	A7CE    					 
2000010800184	20000108	00184		2000	1	8	2000ZZZX38       	1	19991217	G	3246	2606347	WHEEL           	BENDIX      	26035617    															MLG	BROKEN          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19					B3901					FOUND BROKEN SPOKES IN INBOARD WHEEL HALF.																			 
2000021900099	20000219	00099	SO  	2000	2	19	2000ZZZX380      	1	19991206	G	5510		RIVET           			GULSTM	G1159 	G1159B      	3953535	SO  										HORIZ STABILIZER	MISSING         	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	24YS	11734				016				DURING AN EXTERNAL VISUAL INSPECTION OF THE HORIZONTAL STABILIZER, FOUND TWO RIVET HEADS FROM LOWER RT SKIN TO BE MISSIN	G.  REMAINING RIVET STEMS/SHANKS FOUND, ALSO PREVIOUSLY PAINTED OVER WHEN AIRCRAFT WAS PAINTED.  UPON REPLACING THESE RI	VETS WITH NEW SOLID RIVETS, THREE ADDITIONAL RIVET HEADS POPPED OFF IN NEARBY AREA.  ALL BROKEN RIVETS WERE IN SECOND ST	IFFENER FORWARD OF AFT SPAR; THREE BETWEEN STA 91.179 AND STA 102.278 AND TWO BETWEEN STA 134.761 AND STA 145.589.  AIRC	RAFT LANDINGS:   7,199; TT:  11,734.2 HOURS.		2	L	7	2 	4F			RT	A12EA   					 
2000021900100	20000219	00100	EA  	2000	2	19	2000ZZZX381      	2	19991212	G	8530		CYLINDER        			PIPER 	PA60  	PA60600     	7106001	NM  	LYC   	O540  	IO540K1J5   	41532	EA  					NR 2	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	3645T					600852816124	L1646648A			ALB - LEFT ENGINE OIL PRESSURE, DROPPED TO REDLINE IN CRUISE AND OIL TEMP WENT TO REDLINE.  REMOVED AND REPLACED NR 2 CY	LINDER ASSY FOR BLOW-BYE AND LOW COMPRESSION.					1	M	7	2 	3O	3	O	RT	A17WE   	1E4				 
2000021900101	20000219	00101	CE  	2000	2	19	2000ZZZX382      	1	19991221	G	3260		WARNING SYSTEM  			CESSNA	310   	310R        	2074245	CE  										MLG	ACTIVATED       	H				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			GL	07	37223					310R0963				DSM - GEAR HORN BLOWS WHEN ALL THREE GEAR SHOWED DOWN AND LOCK AND THROTTLES PULLED BACK OR FLAPS DOWN.  JACKED AIRCRAFT	, SWUNG GEAR SEVERAL TIMES.  COULD NOT DUPLICATE.  OK FOR CONTINUED SERVICE.					1	L	7	2 	3O				3A10    					 
2000010800185	20000108	00185	EU  	2000	1	8	2000ZZZX39       	1	19991012	G	2721	D25W58205003	ACTUATOR        		D25W58205005	ISRAEL	1125  	ASTRASPX    	4500205	EU  										RUDDER	FROZEN          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	07	398AG	140  			063	088				BOTH THE TOP AND BOTTOM ROLLER TRIM ACTUATORS BECAME INOPERATIVE AT ALT DUE TO FREEZING.  SUBMITTER STATED THIS IS THE S	ECOND OCCURRENCE OF THIS PROBLEM ON THEIR AIRCRAFT.					2	L	7	2 	4F			RT	A16NM   					 
2000021900112	20000219	00112	CE  	2000	2	19	2000ZZZX393      	1	19990429	G	5512	16962000159	SPAR            		SIERRAC24   	BEECH 	23    	C24R        	1151254	CE  										HORIZ STABILIZER	CRACKED         	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	01	18860				MC512	MC512				FRONT SPAR WAS REMOVED FROM HORIZONTAL STABILATOR RECAUSE OF CRACKS IN SPAR P/N 169-620001-59 AT THE UPPER RADIUS IN THE	 CUT-OUT SLOT FOR HINGE, P/N 169-620000-107, TO FIT.  A NEW FACTORY SPAR WAS PURCHASED.  INCOMING INSPECTION FOUND A .37	50 INCH CRACK WAS FOUND IN THE NEW PART, SAME  LOCATION.  THESE CRACKS MAY EXIST IN ALL MODELS USING THIS BEECH SPAR.  T	HIS IS A MANUFACTURER DEFECT CAUSED WHEN MAKING THE SLOT, THEN BENDING THE EDGE AFTER.  SUBMITTER STATED PART MANUFACTUR	ERS SHOULD IMPROVE THEIR CONFORMITY INSPECTIONS AND MEET REQUIREMENTS IN FAR PART 21.		1	L	7	1 	3O				A1CE    					 
2000021900116	20000219	00116	EU  	2000	2	19	2000ZZZX397      	1	19991208	G	7922	9696	BLOWER MOTOR    		1094        	SNIAS 	350   	AS350B2     	8680813	EU  										OIL COOLER	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	21	5204X	400  				3099				DURING A 100-HOUR/200-HOUR INSPECTION, DISCOVERED THE OIL COOLER BLOWER MOTOR HOUSING SEVERLY CORRODED.  PART WAS REMOVE	D AND REPLACED.  BLOWER MOTOR REMOVED WAS BEYOND ECONOMICAL TO REPAIR.  THE  MOTOR'S POSITION WHEN INSTALLED ON THE AIRC	RAFT IS EXPOSED TO THE ELEMENTS, SNOW, RAIN, SLAT SPRAY, ETC.				1	G	7	1 	3U				H9EU    					 
2000021900117	20000219	00117		2000	2	19	2000ZZZX398      	4	19991228	G	3454	IN385AC	VOR             	ARC         		CESSNA	172   	172RG       	2072438	CE  										COCKPIT	FAILED          	D				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			NM	09	6290V	5237 			12286	172RG0610				PILOT REPORTED SMOKE IN CABIN.  MECHANIC CHECKED ALL SYSTEMS AND COULD NOT DUPLICATE ANY SMOKE.  FOUND NR 2 VOR NAVIGATI	ON HEAD INOPERABLE.  REMOVED.  INSTRUMENT HAS STRONG ELECTRICAL SMELL.  REPLACED UNIT AND OPERATIONAL CHECKED NORMAL.					1	H	7	1 	3O				3A17    					 
2000010800097	20000108	00097	EU  	2000	1	8	2000ZZZX4        	1	19991015	G	2432	16061	BATTERY         			SNIAS 	350   	AS350B2     	8680813	EU  										E/E BAY	FAILED          	B			TI1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	05	40751	155  			G02005	3154				BATTERY FAILED 3-MONTH INSPECTION.  REPLACED WITH LEAD ACID BATTERY PER CUSTOMER'S REQUEST.						1	G	7	1 	3U				H9EU    					 
2000010800186	20000108	00186	CE  	2000	1	8	2000ZZZX40       	1	19991027	G	3230	358251722	ARM             			BEECH 	58    	58P         	1152744	CE  										NLG	BROKEN          	B			QELR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	52HC					TJ274				INSPECTION OF THE LANDING GEAR SYSTEM ON THE SUBJECT AIRCRAFT REVEALED THE FOLLOWING.  THE LANDING GEAR GEARBOX IS IN TH	E FULL DOWN POSITION.  THE NOSE GEAR RETRACT ARM P/N 35-825172-2 IS BROKEN.  THIS RELEASED THE OVERCENTER TENSION ON THE	 NOSE GEAR DOWNLOCK ALLOWING THE NOSE GEAR TO RETRACT.  FAILURE OF THE NOSE GEAR APPARENTLY CAUSED EXCESSIVE SIDE LOADIN	G ON THE RIGHT MAIN GEAR BENDING THE RETRACT ROD ASSY P/N 35-815125-31 AND ALLOWING THE GEAR TO COLLAPSE OUTSIDE THE INN	ER GEAR DOOR.		1	L	7	2 	3O				A23CE   					 
2000021900120	20000219	00120		2000	2	19	2000ZZZX402      	4	19990805	G	3160	7003430901	DISPLAY         	HONEYWELL   		GULSTM	560   	560         	0141402	SW  										COCKPIT	DAMAGED         	B			GJQR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	40WP				86110790	5600155				EFIS HSI DISPLAY TUBE HAS SEVERELY ETCHED SCREEN CAUSING GHOSE IMAGES.  REMOVED AND REPLACED DISPLAY UNIT.						1	H	7	2 	3O				6A1     					 
2000021900121	20000219	00121	SW  	2000	2	19	2000ZZZX403      	1	19991228	G	6230	406040090103	NUT             			BELL  	407   	407         		SW  										MAST BEARING	LEAKING         	B	L	A	IIFR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	407PR	1460 				53232				MAST SEAL, P/N 28905-3499, WORE GROOVE IN MAST BEARING NUT, P/N 406-040-090-103.  UPON REMOVAL, FOUND TORQUE ON NUT BELO	W RECOMMENDED TORQUE OF 450 FEET/POUNDS (HAND TIGHT).					1	G	7	1 	3U			O	H2SW    					 
2000021900122	20000219	00122	SO  	2000	2	19	2000ZZZX404      	2	19991224	G	8520		ROD BEARING     			BEECH 	23    	A23A        	1151208	CE  	CONT  	O346  	IO346A      	17033	SO  					ENGINE	WORN            	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	07	4708T	3153 	1593 			M10104	1005807A			IN-FLIGHT, NR 3 CONNECTING ROD BEARING FAILED POSSIBLY DUE TO WEAR.  EXCESSIVE HEAT AND EXPANSION BUILD-UP AROUND THE NR	 3 CONNECTING ROD CRANKPIN AND CAUSING THE ROD BOLTS TO BREAK APART AT THE SHANK.  THE NR 3 CONNECTING ROD IS CONNECTED 	FROM THE CRANKSHAFT CAUSING COMPLETE ENGINE FAILURE.  SUBMITTER STATED THE ENGINE WAS OPERATING 93 HOURS OVER THE MANUFA	CTURER'S RECOMMENDED OVERHAUL TIME.			1	L	7	1 	3O	3	O		A1CE    	E3CE				 
2000021900127	20000219	00127	SW  	2000	2	19	2000ZZZX409      	1	19991206	G	3230	AN364720C	NUT             	DUKES       	4196001C    	MOONEY	M20   	M20F        	5870214	SW  										MFG ACTUATOR	LOOSE           	D	L			O				OTHER                   				O			OTHER                     			LD	LANDING        	1			WP	17	3272F				981	670365				LANDING GEAR COLLAPSED ON LANDING.  AFTER AIRCRAFT WAS TOWED TO HANGAR AND PLACED ON JACKS, FOUND THE GEAR ACTUATOR JACK	SCREW HAD BECOME SEPARATED FROM THE MOTOR/GEAR PORTION OF THE GEAR ACTUATOR.  AFTER REMOVAL OF THE ACTUATOR FROM AIRCRAF	T AND DISASSEMBLY, DISCOVERED THE DRIVE GEAR/JACKSCREW RETAINING NUT, P/N AN364-720C, HAD BACKED OFF THE THREADED SHAFT 	OF THE JACKSCREW ALLOWING THE JACKSCREW TO SEPARATE FROM THE DRIVE MECHANISM.			1	L	7	1 	3O				2A3     					 
2000010800187	20000108	00187	SO  	2000	1	8	2000ZZZX41       	1	19991209	G	3222		STRUT           		3946103     	PIPER 	PA34  	PA34220T    	7103420	SO  										NLG	CRACKED         	H	P			O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			WP	07	4162K	1346 				3449097				NOSE GEAR FORK ASSEMBLY FAILED.  STRUT TUBE APPEARED TO BE CRACKED AS IT SEPARATED UNDER THE LOAD OF THE AIRCRAFT DURING	 TOW.					1	L	7	2 	3O				A7SO    					 
2000021900133	20000219	00133	CE  	2000	2	19	2000ZZZX415      	1	19991201	G	5320	50420013950	TIE STRAP       			BEECH 	200   	B200        	1152922	CE  										BS 227.125	BROKEN          	D	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	63791	7240 				BB1100				DURING ROUTINE INSPECTION, THIS TIE STRAP WAS FOUND BROKEN.  THE AIRPLANE AT ALL OTHER LIKE LOCATIONS WAS INSPECTED FOR 	MORE CRACKS OR BREAKS.  NONE WERE FOUND OTHER THAN THE ONE AT STA 227.125, RIGHT SIDE.  THE POSSIBLE CAUSE WAS THAT THE 	PARTS WERE NOT PROPERLY DRILLED AND FITTED BEFORE RIVETS WERE INSTALLED WHICH CAUSED GAPS BETWEEN THE INDIVIDUAL PARTS. 	 THIS CAUSED ALSO THE HEADS OF SOME RIVETS TO BREAK OFF ALONG WITH THE BREAK IN THE TIE STRAP.			1	L	7	2 	4T				A24CE   					 
2000021900134	20000219	00134	SO  	2000	2	19	2000ZZZX416      	1	19990117	G	7331		FFR             	LUCAS       	CASC504     	GULSTM	G1159 	GIV         	3980115	SO  										ENGINE	FAILED          	B			EC3R	O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			WP	05	71RP		520  		L1498	1222				IN-FLIGHT, ENGINE ACCELERATION/DECELERATION FL 45,000.  RIGHT ENGINE COMPRESSOR STALLED AND FLAMED OUT DURING ACCELERATI	ON.  REMOVED AND REPLACED FFR PER GULFSTREAM CMP 732032.					2	L	7	2 	4F			RT	A12EA   					 
2000010800188	20000108	00188		2000	1	8	2000ZZZX42       	4	19991221	G	2565	4A31924	RESERVOIR       	BFGOODRICH  	7A1298001   															ESCAPE SLIDE	WRONG PART      	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	19					TTC218028					EVACUATION SLIDE RECEIVED IN FOR REPAIR.  INSPECTION REVEALED THE RESERVOIR INSTALLED IS NOT PER THE MFG (BFG) DRAWING, 	P/N 4A3192.  THE RESERVOIR DOES NOT HAVE THE BF GOODRICH P/N 4A3192-4 IDENTIFIED ON THE RESERVOIR IDENTIFICATION LABEL. 	 THIS RESERVOIR IS BEING TREATED AS ANY UNAPPROVED BF GOODRICH PART.																	 
2000021900138	20000219	00138	SW  	2000	2	19	2000ZZZX420      	1	19991022	G	6210	206010200133	BLADE           			BELL  	206   	206B        	1181511	SW  										MAIN ROTOR	DAMAGED         	B			DFUR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	09		2769 			A1946					MAIN ROTOR BLADE FACTORY INSTALLED WEIGHT DISLODGED DURING OPERATION STRIKING MAIN ROTOR BLADE TIP CAP.  TIP CAP TRAILIN	G EDGE WAS BENT OUTBOARD APPROXIMATELY 30 DEGREES AND APPROXIMATELY ONE INCH OF WEIGHT PROTRUDED THROUGH OUTBOARD END OF	 SPAR.  UPPER AND  LOWER MAIN ROTOR BLADE SKIN BALLOONED OUT FROM FORCE OF WEIGHT IMPACT.  MAIN ROTOR BLADE WAS RETURNED	 TO BELL HELICOPTER FOR INVESTIGATION.			1	G	7	1 	3U				H2SW    					 
2000022600020	20000226	00020	SW  	2000	2	26	2000ZZZX435      	1	19991227	G	6210	407310102101	BEARING         		407010100115	BELL  	407   	407         		SW  										MAIN ROTOR	DEBONDED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	607AL	2899 	408  		LK3502	53264				FOUND ON POST-FLIGHT, ELASTOMERIC BEARING DEBONDED COMPLETELY.						1	G	7	1 	3U			O	H2SW    					 
2000010800190	20000108	00190	CE  	2000	1	8	2000ZZZX44       	1	19991123	G	3000	EM2112	TIMER           	ELECTROMECH 		CESSNA	340   	340A        	2076405	CE  										DEICE SYSTEM	FAILED          	B			Q2AR	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			SW	17	133PC				1779	340A0093				PILOT REPORTED SMOKE EMITTING FROM LT ELECTRICAL PANEL.  INSPECTION FOUND SURFACE DEICE TIMER POTTING COMPOUND OVERHEATE	D CAUSING LARGE QUANTITY OF SMOKE.  NO DAMAGE TO ANY ASSOCIATED COMPONENTS FOUND.					1	L	7	2 	3O				3A25    					 
2000010800191	20000108	00191		2000	1	8	2000ZZZX45       	1	19991221	G	3242	7010FS9545708	SEAL            		50105201    															BRAKE	FAILED          	B			XC4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19		1749 			OCT981513					BRAKE ASSEMBLY, P/N 5010520-1, FAILED PREMATURELY.  TWO EACH PISTONS LEAKING FROM INSULATOR AREA.  PISTONS INTERNALLY FI	LLED WITH FLUID.  EVIDENCE OF T-SEAL FAILURE. THIS IS A CONTINUAL DISCREPANCY.  FACTORY NEW BRAKE ASSEMBLY.  NOTE:  OEM 	PARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 5010520-1.																	 
2000010800192	20000108	00192	SO  	2000	1	8	2000ZZZX46       	1	19991222	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE	FAILED          	B			XC4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19					0250					BRAKE ASSEMBLY, P/N 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE TUBE KEY SLOTS.  HEAT 	STACK WARPED WITH UNEVEN WEAR.  THIS IS A CONTINUAL DISCREPANCY.  BRAKE ASSEMBLY SHOULD LAST 2,500 CYCLES.  NOTE:  OEM P	ARTS INSTALLED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
2000010800502	20000108	00502	SW  	2000	1	8	2000ZZZX47       	1	19991209	G	2560	01081441	HARNESS         	PACIFICSCIEN		BELL  	47    	47G5        	1181032	SW  										COCKPIT	SEPARATING      	H			ZIFG	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	05	7861S					7865				EXPOSURE TO SUNLIGHT HAS RESULTED IN PREMATURE FAILURE OF STITCHING IN WEBBING ON SHOULDER HARNESS.						1	G	7	1 	3O				2H3     					 
2000010800503	20000108	00503	EA  	2000	1	8	2000ZZZX48       	2	19991217	G	7322		SCREW           		MR4SPA105009	AMRGEN	AA5   	AA5A        	3960106	SO  	LYC   	O320  	O320E2G     	41508	EA  					CARBURETOR	LOOSE           	D				D				RETURN TO BLOCK         				R			PARTIAL RPM/PWR LOSS      			TX	TAXI/GRND HDL  	1			CE	01	26411				BL2214999	AA5A0571				AIRCRAFT WAS REPORTED TO BE RUNNING ROUGH AND WOULD NEARLY 'DIE' ON ROLL-OUT.  FOUND CARBURETOR THROTTLE BODY TO BOWL SC	REW LOOSE.  REMOVED FROM ENGINE.  INSPECTED FOR FURTHER DAMAGE, GASKET AND LOCKING TAB WASHERS REPLACED.  ADJUSTMENTS CH	ECKED AND RETURNED TO SERVICE.  CAUSE:  POSSIBLE GASKET SHRINKAGE OR UNDERTORQUING OF SCREWS.				1	L	7	1 	3O	3	O		A16EA   	E274				 
2000010800504	20000108	00504	EA  	2000	1	8	2000ZZZX49       	2	19991217	G	7322		SCREW           	FACET       	MA4SPA105217	CESSNA	172   	172M        	2072418	CE  	LYC   	O320  	O320E2D     	41508	EA  					CARBURETOR	LOOSE           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01	20345		1320 		DC2612	17261208	L3281127A			DURING SCHEDULED INSPECTION, CARBURETOR THROTTLE BODY TO BOWL SCREWS WERE FOUND LOOSE.  REMOVED FROM ENGINE, INSPECTION 	REVEALED NO FURTHER DEFECTS.  NEW GASKET AND LOCKING TABS INSTALLED.  CAUSE: POSSIBLE GASKET SHRINKAGE OR UNDERTORQUE OF	 SCREWS.  SUSPECT GASKET SHRINKAGE AS LOCK TABS WERE BENT TO LOCK SCREWS.				1	H	7	1 	3O	3	O	NT	3A12    	E274				 
2000030200001	20000302	00001	NE  	2000	3	2	2000ZZZX494      	3	19991230	G	6111	D5133	SHIELD          													HARTZL	HCE4A	HCE4A3A     	NE  	BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			3637 					HJ593		EROSION SHIELD DEBONDED, BLADE NR 3 CRACKS, DEBOND AND ONE-HALF IN PIECE MISSING UNDER DEICE BOOT.  REPLACED EROSION SHI	ELD.  STATIC BALANCED PROPELLER IAW HARTZELL CMM AND PROCEDURE 001.															5	C	P10NE	 
2000010800505	20000108	00505	CE  	2000	1	8	2000ZZZX50       	1	19991215	G	2140	S189140	CLAMP           			CESSNA	500   	560CESSNA   	2076750	CE  										RIGHT	FAILED          	D	P	A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	09	208PC	590  				5605005				INITIAL PILOT COMPLAINT OF COLD COCKPIT AT ALTITUDE (41,000 FEET) AND LOW FLOW OF CONDITIONED AIR.  NEXT FLIGHT HAD COLD	 COCKPIT AND CABIN AND LOW FLOW OF CONDITIONED AIR AFTER CLIMBING PAST 20,000 FEET.  ACFT COULD NOT MAINTAIN CABIN PRESS	 AT 41,000 FEET WHEN PILOTS SELECTED SINGLE SOURCE BLEED AIR.  MAINT INSP PRESS DUCTS AND FOUND HOSE CLAMP HAD SLIPPED O	FF COUPLING SLEEVE WHICH WAS ATTACHED TO WARM AIR TAIL CONE TUBE EXITING FUSELAGE SKIN DOWN STREAM OF RT MIXING MUFF.  I	T APPEARED CLAMP WAS INSTALLED ON BEAD OF THE WARM AIR TUBE, AS NOT ENOUGH OF SLEEVE CAME PAST THE BEAD.  CLAMP EVENTUAL	LY SLIPPED OFF THE PRESS AND HEATING CYCLES ALLOWING TUBE AND SLEEVE TO LEAK WHEN CABIN DIFFERENTIAL PRESS INCREASED.	2	L	7	2 	4F			RT	A22CE   					 
2000010800506	20000108	00506		2000	1	8	2000ZZZX51       	1	19991221	G	3242	7010FS9545708	SEAL            		50105201    															BRAKE	FAILED          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		1898 			MAR981251					BRAKE ASSEMBLY PN 5010520-1 FAILED PREMATURELY.  ONE EACH PISTON LEAKING FROM INSULATOR AREA.  PISTON INTERNALLY FILLED 	WITH FLUID.  EVIDENCE OF T-SEAL FAILURE.  NOTE:  OEM PARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGU	RATION.																	 
2000010800507	20000108	00507		2000	1	8	2000ZZZX52       	1	19991223	G	3242	1331096	STATOR          	BFGOODRICH  	21585       															MLG	FAILED          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		763  			1525A					BRAKE ASSEMBLY PN 2-1585 FAILED PREMATURELY.  NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE TUBE KEY SLOTS.  NOTE:  O	EM PARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION PN 2-1585.																		 
2000010800508	20000108	00508	EA  	2000	1	8	2000ZZZX53       	2	19991222	G	8550	48110	OIL FILTER      	CHAMPION    	77852       	PIPER 	PA28  	PA28140     	7102802	SO  	LYC   	O320  	O320E2A     	41508	EA  					ENGINE	MISMANUFACTURED 	B	L		MF2R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CE	05	6782J					2824507	L22232627A			OIL FILTER REPLACED AT ANNUAL, 6, 1998.  FILTER LEAKED AT START-UP.  SECOND FILTER INSTALLED AND LEAKED.  OIL AND FILTER	 CHANGED 8-20-98, ACFT FLEW 24 HOURS.  ANNUALED IN 6, 1999, OIL AND FILTER CHANGED.  MEASURED DEPTH OF OIL FILTER BASE A	DAPTER AND MALE THREADED PORTION OF OIL FILTER SHOWED NEW OIL FILTER BOTTOMING OUT BEFORE SEALING.  MEASURED OLDER CH481	11 AND FOUND THREADED PORTION SHORTER ALLOWING IT TO SEAL.  FOUND THE MFG HAD BEGUN TO PRODUCE THE FILTERS WITH THE STUD	 LENGTH AT THE 'OUTER LIMITS' OF THE DRAWING.  THIS CHANGE WAS TO AID IN THE MFG PROCESS.		1	L	7	1 	3O	3	O		2A13    	E274				 
2000010800509	20000108	00509	CE  	2000	1	8	2000ZZZX54       	1	19991206	G	7810	085073218	HEADER          			CESSNA	310   	T310R       	2074246	CE  										EXHAUST	DAMAGED         	B			AZNR	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			GL	13	376J					310R0668				COUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK.  AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQU	ENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT.  THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATE	RIAL, AND IS LOCATED UNDER THE METAL SEGMENTED 'V' BAND CLAMPS THAT ARE REQUIRED TO BE REPLACED EACH 400 HOURS BY AD 75-	23-08 R5 (11-17-75) SECT II A...TOTAL TIME ON CLAMPS COULD NOT BE DETERMINED, HOWEVER, THIS AD WAS 'GENERALLY' SIGNED OF	F.  BY THE CONDITION OF THE EXHAUST COMPONENTS, IT IS OBVIOUS THE CLAMPS HAD NOT BEEN REMOVED FOR AN EXCESSIVE AMOUNT OF	 TIME AND DEFINITELY NOT NINE MONTHS AGO.	1	L	7	2 	3O				3A10    					 
2000010800510	20000108	00510	CE  	2000	1	8	2000ZZZX55       	1	19991206	G	7120	085112121	ENGINE BEAM     			CESSNA	310   	T310R       	2074246	CE  										ENGINE BAY	CORRODED        	B			AZNR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	13	376J					310R0668				ENGINE BEAM FOUND SEVERELY CORRODED FROM EXPOSURE TO HOT EXHAUST GASSES DUE TO LEAKING EXHAUST PIPE FLANGES AND CLAMPS. 	 OTHER DAMAGE FOUND INVOLVED THE FIREWALL ACCESS PANEL WHICH COVERS THE FUEL CROSSFEED LINE IN WHICH MOSTLY ALL OF THE A	TTACHING SCREW HEADS WERE EITHER BURNT OR CORRODED AWAY.				1	L	7	2 	3O				3A10    					 
2000010800511	20000108	00511	CE  	2000	1	8	2000ZZZX56       	1	19991206	G	7810	085071239	STACK           			CESSNA	310   	T310R       	2074246	CE  										EXHAUST	DAMAGED         	B			AZNR	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			GL	13	376J					310R0668				COUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK.  AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQU	ENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT.  THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATE	RIAL AND IS LOCATED UNDER THE METAL SEGMENTED V-BAND CLAMPS THAT ARE REQUIRED TO BE REPLACED EACH 400 HOURS BY AD 75-23-	08 R5 (11-17-75) SECT II A...TOTAL TIME ON CLAMPS COULD NOT BE DETERMINED, HOWEVER, THIS AD WAS 'GENERALLY' SIGNED OFF. 	 BY THE CONDITION OF THE EXHAUST COMPONENTS, IT IS OBVIOUS THE CLAMPS HAD NOT BEEN REMOVED FOR AN EXCESSIVE AMOUNT OF TI	ME AND DEFINITELY NOT NINE MONTHS AGO.	1	L	7	2 	3O				3A10    					 
2000010800512	20000108	00512	CE  	2000	1	8	2000ZZZX57       	1	19991206	G	7810	08507323	HEADER          			CESSNA	310   	T310R       	2074246	CE  										EXHAUST	DAMAGED         	B			AZNR	D				RETURN TO BLOCK         				K			FLUID LOSS                			NR	NOT REPORTED   	1			GL	13	376J					310R0668				COUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK.  AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQU	ENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT. THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATER	IAL AND IS LOCATED UNDER THE METAL SEGMENTED 'V' BAND CLAMPS THAT ARE REQUIRED TO BE REPLACED EACH 400 HOURS BY AD 75-23	-08 R5 (11-17-75) SECT II A....TOTAL TIME ON CLAMPS COULD NOT BE DETERMINED, HOWEVER, THIS AD WAS 'GENERALLY' SIGNED OFF	.  BY THE CONDITION OF THE EXHAUST COMPONENTS, IT IS OBVIOUS THE CLAMPS HAD NOT BEEN REMOVED FOR AN EXCESSIVE AMOUNT OF 	TIME AND DEFINITELY NOT NINE MONTHS AGO.	1	L	7	2 	3O				3A10    					 
2000030900072	20000309	00072	SO  	2000	3	9	2000ZZZX571      	1	19990112	G	3233	452729	BEARING         			PIPER 	PA32  	PA32R300    	7103213	SO  										NLG	FAILED          	H				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			NM	01	5969V					32R7780384				DURING FLIGHT, A SHARP POP WAS HEARD AND NOSE WHEEL INDICATED DOWN AND LOCKED.  UPON LANDING, PILOT FOUND THE ROD END BE	ARING ON THE NOSE GEAR ACTUATOR HAD PULLED APART  IN THE THREADED PORTION NEXT TO THE BEARING PORTION OF THE PART.  MATE	RIAL ANALYSIS INDICATED A SOFT PART.   NEW PIPER CO FELT THE TARGETED MAT'L STRENGTH OF THE PART IS PROPRIETARY INFO AND	 WILL NOT SUPPLY THE INFO  TO TEST THE REPLACEMENT PART.  WHEN REPLACING DAMAGED HDWE, DISCOVERED FWD ATTACHING BOLT, AN	 23-19A, AND AFT , 405869V OR NAS464-P3-A13, REF SB747, WERE BENT.  AFT BOLT HAD BEEN REPLACED WITHIN 80 HOUR OR 2 YEARS	.  WITH NEW HDWE INSTALLED, RIGGING WAS CHECKED PER SM AND HYD CUT-OFF PRESS VERIFIED.	1	L	7	1 	3O				A3SO    					 
2000030900078	20000309	00078	SO  	2000	3	9	2000ZZZX577      	2	19990909	G	7314	TF1900	PUMP            	TRW         		TMPSON	NAVION	NAVIONA     	6150104	SW  	CONT  	E225  	E2254       	17015	SO  					FUEL SYSTEM	FAILED          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	09	4527K					NAV41527	35456D64			PIN ON FULL PUMP DRIVE SHAFT SHEARED CAUSING LOSS OF FUEL PRESSURE TO CARBURETOR AND ENGINE STOPPAGE.  SUBMITTER RECOMME	NDED TIMELY INSPECTIONS OF FUEL PUMP (THOMPSON'S) FOR DRIVE PIN WEAR.					1	L	7	1 	3O	3	O		A782    	E267				 
2000010800513	20000108	00513	CE  	2000	1	8	2000ZZZX58       	1	19991206	G	7810	085071241	STACK           			CESSNA	310   	T310R       	2074246	CE  										EXHAUST	MISINSTALLED    	B			AZNR	O				OTHER                   				W	K		INADEQUATE Q C            	FLUID LOSS                		NR	NOT REPORTED   	1			GL	13	376J					310R0668				COUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK.  AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQU	ENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT.  THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATE	RIAL AND IS LOCATED UNDER THE METAL SEGMENTED 'V' BAND CLAMPS THAT ARE REQUIRED TO BE REPLACED EACH 400 HOURS BY AD 75-2	3-08 R5 (11-17-75) SECT II 1..TOTAL TIME ON CLAMPS COULD NOT BE DETERMINED, HOWEVER, THIS AD WAS 'GENERALLY' SIGNED OFF.	  BY THE CONDITION OF THE EXHAUST COMPONENTS IT IS OBVIOUS THE CLAMPS HAD NOT BEEN REMOVED FOR AN EXCESSIVE AMOUNT OF TI	ME AND DEFINITELY NOT NINE MONTHS AGO.	1	L	7	2 	3O				3A10    					 
2000010800514	20000108	00514	CE  	2000	1	8	2000ZZZX59       	1	19991206	G	7810	085071240	STACK           			CESSNA	310   	T310R       	2074246	CE  										EXHAUST	MISINSTALLED    	B			AZNR	O				OTHER                   				W	K		INADEQUATE Q C            	FLUID LOSS                		NR	NOT REPORTED   	1			GL	13	376J					310R0668				COUPLING FLANGE BURNT AND CORRODED CAUSING EXHAUST LEAK.  AIRCRAFT UNDERWENT ANNUAL INSPECTION AND IMPORT C OF A SUBSEQU	ENTLY ISSUED BY SO-FSDO-05 NINE MONTHS PRIOR TO THIS SHOP VISIT.  THE ERODED, BURNT END OF THE COUPLING WAS MISSING MATE	RIAL AND IS LOCATED UNDER THE METAL SEGMENTED 'V' BAND CLAMPS THAT ARE REQUIRED TO BE REPLACED EACH 400 HOURS BY AD 75-2	3-08 R5 (11-17-75) SECT II A...TOTAL TIME ON CLAMPS COULD NOT BE DETERMINED, HOWEVER, THIS AD WAS 'GENERALLY' SIGNED OFF	.  BY THE CONDITION OF THE EXHAUST COMPONENTS, IT IS OBVIOUS THE CLAMPS HAD NOT BEEN REMOVED FOR AN EXCESSIVE AMOUNT OF 	TIME AND DEFINITELY NOT NINE MONTHS AGO.	1	L	7	2 	3O				3A10    					 
2000010800099	20000108	00099	SW  	2000	1	8	2000ZZZX6        	1	19991102	G	6322	206061432121	HOUSING         		407040303105	BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	687AL	206  				53366				DURING DAILY INSPECTION, FOUND CRACKED BLOWER HOUSING.						1	G	7	1 	3U			O	H2SW    					 
2000010800515	20000108	00515	CE  	2000	1	8	2000ZZZX60       	1	19991206	G	7110	99102962	SLIP JOINT      			CESSNA	310   	T310R       	2074246	CE  										COWL	CRACKED         	B			AZNR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	376J					310R0668				PART WAS FOUND CRACKED 330 DEGREES AROUND WELD AND WAS VISIBLE BY OPENING THE OUTBOARD COWLING DOOR.						1	L	7	2 	3O				3A10    					 
2000010800516	20000108	00516	CE  	2000	1	8	2000ZZZX61       	1	19991206	G	7810	K991030132INC	STACK           		C402        	CESSNA	310   	T310R       	2074246	CE  										EXHAUST	MISMANUFACTURED 	B			AZNR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	13	376J				72010	310R0668				THIS NEW FAA-PMA PART WAS NOT FORMED PROPERLY AND COULD NOT BE INSTALLED WITHOUT CAUSING UNDUE STRESS ON MATING PARTS. T	HE PART WAS TAGGED AND RETURNED TO DISTRIBUTOR AND ANOTHER NEW PART ORDERED FOR THE AIRCRAFT.  (THE ANGLE OF THE BEND IN	 THE PIPE WAS NOT CORRECT).				1	L	7	2 	3O				3A10    					 
2000010800521	20000108	00521	SO  	2000	1	8	2000ZZZX63       	1	19991211	G	3240	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE	BROKEN          	B			XC4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19					1324A					BRAKE ASSEMBLY, PN 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE TUBE KEY SLOTS.  HEAT S	TACK WARPED WITH UNEVEN WEAR.  THIS IS A CONTINUAL DISCREPANCY.  NOTE:  OEM PARTS INSTALLED IN BRAKE ASSEMBLY AND THE MO	ST RECENT BRAKE CONFIGURATION, PN 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
2000031700098	20000317	00098	CE  	2000	3	17	2000ZZZX636      	1	19991208	G	2910	631700350	TUBE            			CESSNA	525   	525         	2076601	CE  										HYDRAULIC SYSTEM	FAILED          	H				O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		NR	NOT REPORTED   	1			EA	21	49CJ	2413 				5250049				IN-FLIGHT, MAIN SYSTEM HYDRAULIC FAILURE.  LOW FLOW CAUTION INDICATION BOTH ENGINES.  MAIN LANDING GEAR DOWN AND LOCKED 	WITH EMERGENCY EXTENSION SYSTEM, ZERO DEGREES FLAP, NO SPEED BRAKES, AND THRUST ATTENUATORS LANDING WITH NO INCIDENT.  M	AIN HYDRAULIC PRESSURE TUBE FROM HIGH PRESSURE FILTERS TO BYPASS VALVE FOUND CRACKED IN 30 DEGREE BEND RADIUS LOCATION O	UTBOARD OF J-BOX/TAIL CONE.  TUBE FOUND TO BE SECURED PROPERLY WITH NO ABNORMAL STRESS POINTS.  POSSIBLE CAUSE, MATERIAL	 DEFECT.		1	L	7	2 	4F			RT	A1WI    					 
2000010800522	20000108	00522	SO  	2000	1	8	2000ZZZX64       	1	19991214	G	3240	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE	BROKEN          	B			XC4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19		656  			0683A					BRAKE ASSEMBLY, PN 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE TUBE KEY SLOTS.  THIS I	S A CONTINUAL DISCREPANCY.  BRAKE ASSEMBLY SHOULD LAST 2,500 CYCLES. NOTE:  OEM PARTS INSTALLED IN BRAKE ASSEMBLY AND TH	E MOST RECENT BRAKE CONFIGURATION, P/N 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
2000031700121	20000317	00121	SO  	2000	3	17	2000ZZZX646      	2	19990119	G	8500		CASE            			BEECH 	58    	58          	1152740	CE  	CONT  	O520  	IO520C      	17032	SO  					NR 1 ENGINE	FRACTURED       	E	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	7353R		1333 			TH486	561360			DURING ANNUAL INSPECTION, FOUND ABOVE MENTIONED HOSE LEAKING PROFUSELY.  THE HOSE APPEARED TO BE SUPPORTED PROPERLY.  WH	EN FUEL PRESSURE WAS APPLIED WITH AIRCRAFT ELECTRIC BOOST PUMP, FUEL BEGAN COMING OUT OF BRAIDED, CRIMPED AREA NEAR THE 	END OF THE HOSE.  AD 71-24-04 DOES NOT APPLY TO THIS MODEL NUMBER AND SERIAL NUMBER OF AIRCRAFT.  SE 71-7, SUPPLEMENT 1,	 DATED 11-3-71, ENCOMPASSES ALL CESSNA SINGLE ENGINE AIRCRAFT. (X)			1	L	7	2 	3O	3	O		3A16    	E5CE				 
2000010800523	20000108	00523	SO  	2000	1	8	2000ZZZX65       	1	19991209	G	3240	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE	BROKEN          	B			XC4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19		1141 			0876A					BRAKE ASSEMBLY, P/N 2-1585, FAILED PREMATURELY. NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE TUBE KEY SLOTS.  HEAT S	TACK WARPED WITH UNEVEN WEAR.  THIS IS A CONTINUAL DISCREPANCY.  BRAKE ASSEMBLY SHOULD LAST 2,500 CYCLES.  NOTE:  OEM PA	RTS INSTALLED IN BRAKE ASSEMBLY AND THE  MOST RECENT BRAKE CONFIGURATION, P/N 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
2000031700132	20000317	00132	SO  	2000	3	17	2000ZZZX657      	1	19991022	G	2740	62701097	CONTROL CABLE   			PIPER 	PA34  	PA34200     	7103405	SO  										HORIZ STABILIZER	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	19	1351T	4837 				347250295				LEFT STABILATOR TRIM CABLE, P/N 62701-097, BROKE IN-FLIGHT CAUSING AIRCRAFT TO PORPOISE (PITCH UP AND DOWN).  A NORMAL L	ANDING WAS MADE WITHOUT INCIDENT.  FURTHER INSPECTION REVEALED THE CABLE HAD BROKEN AT BS 187.84 WHERE THE CABLE PASSES 	THROUGH THE BULKHEAD.  EVIDENCE OF CABLE CHAFING WAS FOUND AT THE HOLE IN BULKHEAD WHERE CABLE PASSES THROUGH.  THE HOLE	 IN BULKHEAD WAS SLIGHTLY ENLARGED TO PROVIDE ADEQUATE CLEARANCE FOR CABLE TO PASS AND NEW TRIM CABLE WAS INSTALLED.  (X	)		1	L	7	2 	3O			 	A7SO    					 
2000031700133	20000317	00133	WP  	2000	3	17	2000ZZZX658      	2	19991115	G	7260	8968061	GEAR            			CASA  	C212  	C212CD      	2410209	EU  	GARRTT	TPE331	TPE33110    	01514	WP  					GEARBOX	FAILED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	23	204PA	9079 	2945 			309	P37600C			THE NUT SECURING BEARING TO IDLER GEAR, P/N 896806-1, LOOSENED CAUSING GEAR TO BIND IN GEARCASE.  THIS BINDING CAUSED TN	E NR 1 IDLER IN THE TORQUE SENSOR TO SHEER WHICH RESULTED IN ENGINE SHUT-DOWN.					2	H	7	2 	4T	4	T	RT	A43EU   	E4WE				 
2000010800524	20000108	00524		2000	1	8	2000ZZZX66       	1	19991209	G	3240	7010FS9545708	SEAL            		50105201    															BRAKE	LEAKING         	B			XC4R	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SO	19		998  			FEB91605					BRAKE ASSEMBLY, P/N 5010520-1, FAILED PREMATURELY.  ONE EACH PISTON LEAKING FROM INSULATOR AREA.  PISTON INTERNALLY FILL	ED WITH FLUID.  EVIDENCE OF T-SEAL FAILURE.  THIS IS A CONTINUAL DISCREPANCY.  FACTORY NEW BRAKE ASSEMBLY.  NOTE:  OEM P	ARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 5010520-1.																	 
2000031700136	20000317	00136	GL  	2000	3	17	2000ZZZX661      	2	19991209	G	7323	23057869	GOVERNOR        			HUGHES	500N  	500N        	3027374	SW  	ALLSN 	25OC  	250C20R     		GL  					ENGINE	FAILED          	D				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			WP	07	525FB		1286 			LN005	295365			GOVERNOR FAILURE, UNIT BECOMES ERRATIC IN OPERATION.  WILL NOT HOLD ENGINE RPM.  SUBMITTER STATED EXPERIENCED THREE SUCH	 FAILURES THIS YEAR ON FLEET.  (X)					1	G	7	1 	3U	3	U	NC	H3WE    	E4CE				 
2000031700139	20000317	00139	CE  	2000	3	17	2000ZZZX664      	1	19990610	G	2823	1013840403	SWITCH          	AVIONIC     		BEECH 	200   	A200C       		CE  										FUEL CUT OFF	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NE	05	CTEXT					BP038				THIS PART, NR 1 FIREWALL SHUT-OFF VALVE PULL SWITCH, HAD AT SOME POINT BEEN DISMOUNTED AND THEN REMOUNTED USING A SCREW 	THAT WAS LONGER THAN THE REQUIRED NAS387-1032-10.  THE REQUIRED SCREW LEAVES ALMOST NO CLEARANCE BETWEEN THE END OF THE 	SCREW AND THE HOUSING OF A MICROSWITCH IN THE ASSEMBLY.  THE LONGER THAN ALLOWED SCREW BROKE THE HOUSING AND THE RESULTI	NG DEBRIS CAUSED THE MICROSWITCH TO ACTUATE ERRATICALLY GIVING FALSE READINGS ON THE ANNUNCIATORS.  (X)			1	L	7	2 	4T			RT	A24CE   					 
2000010800525	20000108	00525		2000	1	8	2000ZZZX67       	1	19991208	G	3240	7010FS9545708	SEAL            		50105201    															BRAKE	LEAKING         	B			XC4R	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SO	19		2345 			SEP971094					BRAKE ASSEMBLY, P/N 5010520-1, FAILED PREMATURELY.  ONE EACH PISTON LEAKING FROM INSULATOR AREA. PISTON INTERNALLY FILLE	D WITH FLUID.  EVIDENCE OF T-SEAL FAILURE.  THIS IS A CONTINUAL DISCREPANCY.  FACTORY NEW BRAKE ASSEMBLY.  NOTE: OEM PAR	TS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 5010520-1.																	 
2000010800526	20000108	00526		2000	1	8	2000ZZZX68       	1	19991206	G	3240	7010FS9545708	SEAL            		501050201   															BRAKE	LEAKING         	B			XC4R	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SO	19		1281 			FEB991639					BRAKE ASSEMBLY, P/N 5010520-1, FAILED PREMATURELY.  TWO EACH, PISTONS LEAKING FROM INSULATOR AREA.  PISTONS INTERNALLY F	ILLED WITH FLUID.  EVIDENCE OF T-SEAL FAILURE.  THIS IS A CONTINUAL DISCREPANCY.  FACTORY NEW BRAKE ASSEMBLY.  NOTE:  OE	M PARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 5010520-1.																	 
2000010800527	20000108	00527		2000	1	8	2000ZZZX69       	1	19991211	G	3240	7010FS9545708	SEAL            		50105201    															BRAKE	LEAKING         	B			XC4R	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SO	19		1606 			FEB91636					BRAKE ASSEMBLY, P/N 5010520-1, FAILED PREMATURELY.  TWO EACH PISTONS LEAKING FROM INSULATOR AREA.  PISTONS INTERNALLY FI	LLED WITH FLUID.  EVIDENCE OF T-SEAL FAILURE.  THIS IS A CONTINUAL DISCREPANCY.  FACTORY NEW BRAKE ASSEMBLY.  NOTE:  OEM	 PARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 5010520-1.																	 
2000010800100	20000108	00100	SW  	2000	1	8	2000ZZZX7        	1	19991030	G	6510	407340340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	FAILED          	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	917AL	24   				53381				FOUR OF THE DISC PACKS ON THE TAILBOOM WERE FOUND SPREAD WHEN TURNING THE DRIVESHAFT.  THE LIMIT IS GIVEN IN THE MM AS B	EING .015 INCH OF GAP, AND ALL BUT ONE DISC PACK WAS WITHIN LIMITS AND WAS REPLACED.  PREVIOUS EXPERIENCE WITH THE BELL 	206 SHOWS THE DISC PACKS EXHIBIT NO GAPS UNLESS DRIVESHAFT HAS HAD EXCESSIVE LOADS OR DAMAGE.  SUBMITTER STATED  RECEIVE	D A NEW 407 AND THIS AIRCRAFT HAS DISC PACKS SPREAD ALREADY WITH ONLY 22 HOURS.			1	G	7	1 	3U			O	H2SW    					 
2000010800528	20000108	00528	CE  	2000	1	8	2000ZZZX70       	1	19990110	G	2910	4529102084005	LINE            			LEAR  	45    	45LEAR      	5170805	CE  										HYDRAULIC SYSTEM	CHAFED          	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	25	4FE	456  				032				CLAMPED WIRE BUNDLE ROTATES AROUND HYDRAULIC LINE ALLOWING ADEL CLAMP SCREWS TO CONTACT LT ENGINE HYDRAULIC PUMP CASE DR	AIN LINE.  OVER TIME DUE TO LINE VIBRATION, THE SCREW CHAFES THROUGH LINE.					2	L	7	2 	4F			RT	T00008WI					 
2000010800532	20000108	00532	CE  	2000	1	8	2000ZZZX72       	1	19991216	G	7120	J744436	SHOCK MOUNT     			CESSNA	172   	172S        	2072439	CE  										FIREWALL	TORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP	93   				172S8035				DURING PHASE 3 INSPECTION, FOUND 4 LOWER COWL ATTACH SHOCK MOUNTS TORN AT THE BASE.  REPLACED SHOCK MOUNTS.						1	H	7	1 	3O			NT	3A12    					 
2000032300582	20000323	00582	CE  	2000	3	23	2000ZZZX723      	1	19990818	G	7810	1099500001	STACK           			BEECH 	90    	C90A        	1152911	CE  										EXHAUST	CRACKED         	B			BQVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	01	600FL	385  				LJ1540				CRACKED EXHAUST STACK.  SUBMITTER STATED THREE OTHER M OR D REPORTS SUBMITTED FOR SAME PROBLEM.  A RAYTHEON REP HAS BEEN	 CONTACTED AND A FUTURE SERVICE BULLETIN IS PENDING RELEASE.					1	L	7	2 	3T			RT	3A20    					 
2000032300583	20000323	00583	CE  	2000	3	23	2000ZZZX724      	1	19991229	G	7810	1099500001	STACK           			BEECH 	90    	C90A        	1152911	CE  										EXHAUST	CRACKED         	B			BQVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	01	600FL	406  				LJ1540				CRACKED EXHAUST STACK.  SUBMITTER STATED 3 OTHER M OR D REPORTS SUBMITTED FOR SAME PROBLEM.  A RAYTHEON REP HAS BEEN CON	TACTED AND A FUTURE SERVICE BULLETIN IS PENDING RELEASE.					1	L	7	2 	3T			RT	3A20    					 
2000010800533	20000108	00533	CE  	2000	1	8	2000ZZZX73       	1	19991216	G	5753	052390138	SKIN            			CESSNA	172   	172S        	2072439	CE  										RT TE FLAP	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP	93   				172S8035				DURING PHASE 3 INSPECTION, FOUND RT FLAP LOWER SKIN TRAILING EDGE CRACKED IN TWO LOCATIONS, THE 13TH AND 16TH RIVETS FRO	M THE INBD END HAD CRACKS OF .25 INCH AND .50 INCH.  REPLACED FLAP ASSEMBLY WITH FACTORY NEW ASSY AND PAINTED.					1	H	7	1 	3O			NT	3A12    					 
2000010800534	20000108	00534	CE  	2000	1	8	2000ZZZX74       	1	19991216	G	5730	052301153	SKIN            			CESSNA	172   	172S        	2072439	CE  										LT WING	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP	93   				172S8035				DURING PHASE 3 INSPECTION, FOUND LT UPPER WING TRAILING EDGE SKIN ABOVE FLAP WELL HAD A 1 INCH CRACK IN THE TRAILING EDG	E SKIN AT THE 3RD RIVET FROM INBD TRAILING EDGE.  REPLACED SKIN P/N 0523011-53, RELEASED FUEL CELL, PAINTED SKIN AND LEA	K CHECKED.				1	H	7	1 	3O			NT	3A12    					 
2000010800535	20000108	00535	CE  	2000	1	8	2000ZZZX75       	1	19991216	G	5730	052301153	SKIN            			CESSNA	172   	172S        	2072439	CE  										RT WING	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP	93   				172S8035				DURING PHASE 3 INSPECTION, FOUND RT UPPER WING TRAILING EDGE SKIN ABOVE FLAP WELL HAD A 1 INCH CRACK IN THE TRAILING EDG	E SKIN AT THE3RD RIVET FROM INBD TRAILING EDGE.  REPLACED SKIN P/N 0523011-53, RESEALED FUEL CELL, PAINTED SKIN AND LEAK	 CHECKED.				1	H	7	1 	3O			NT	3A12    					 
2000010800536	20000108	00536	CE  	2000	1	8	2000ZZZX76       	1	19991216	G	5320	051507558	PANEL           			CESSNA	172   	172S        	2072439	CE  										FUSELAGE	MISINSTALLED    	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP	93   				172S8035				DURING PHASE 3 INSPECTION, REMOVED RT AFT TRIM PANEL AND FOUND 1 ATTACH SCREW WAS DRILLED THROUGH DOORPOST STRUCTURAL RI	VET.  REPLACED RIVET AND RELOCATED PANEL ATTACH SCREW WITH NEW TRIM PANEL.					1	H	7	1 	3O			NT	3A12    					 
2000010800537	20000108	00537	CE  	2000	1	8	2000ZZZX77       	1	19991216	G	7722	TE4099802	THERMOCOUPLE    			CESSNA	172   	172S        	2072439	CE  										ENGINE	INOPERATIVE     	D				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			NM	03	494SP	93   				172S8035				PILOT DISCREPANCY, EGT INOPERATIVE.  DURING PHASE 3 INSPECTION, FOUND THERMOCOUPLE LEADS SEPARATED FROM THERMOCOUPLE.  R	EPLACED EGT THERMOCOUPLE, OPERATIONAL CHECK SATISFACTORY.  SUBMITTER STATED ON A FLEET OF 5 NEW C-172S AIRCRAFT, THIS IS	 THE 10TH FAILURE IN THE PAST YEAR.				1	H	7	1 	3O			NT	3A12    					 
2000010800539	20000108	00539	SO  	2000	1	8	2000ZZZX78       	1	19991201	G	5410	12003852001	FRAME           			EMB   	120   	EMB120RT    		SO  										NACELLE	CRACKED         	B			WVER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	09	284UE					120145				C-CHECK INSPECTION REVEALED RIGHT NACELLE FRAME NR 1 CRACKED AT OUTBOARD TORQUE TUBE BOLT HOLE RISERS.						2	L	7	2 	4T			RT	A31SO   					 
2000010800542	20000108	00542	NM  	2000	1	8	2000ZZZX79       	1	19991223	G	5410		LUG             			BOEING	747   	747212B     	1384886	NM  										PYLON SPAR	CRACKED         	B	P		XYJY	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	33	816FF					21939				A THOROUGH CRACK WAS FOUND AT AFT ENGINE MOUNT LOWER SPAR LUG OF THE NR 3 PYLON.						2	L	7	4 	4F				A20WE   					 
2000010800101	20000108	00101	SW  	2000	1	8	2000ZZZX8        	1	19991029	G	6510	407340340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	FAILED          	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	937AL	23   				53383				DURING GULF COAST PREP, FOUND TAIL ROTOR DRIVESHAFT DISC PACKS SPREAD DURING ROUTINE VISUAL INSPECTION ON A NEW AIRCRAFT	.  SUBMITTER STATED THIS IS THE 5TH OCCURRENCE OBSERVED WITH THE 407 AT THIS FACILITY.					1	G	7	1 	3U			O	H2SW    					 
2000010800543	20000108	00543	NM  	2000	1	8	2000ZZZX80       	1	19991223	G	5314		KEEL BEAM       			BOEING	747   	747212B     	1384886	NM  										BS 1265	CORRODED        	B	P		XYJY	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	33	616FF					21939				SEVERE CORROSION WAS FOUND ON ANGLE IN KEEL BEAM BOX AT STA 1265 DURING MAINTENANCE D-CHECK.						2	L	7	4 	4F				A20WE   					 
2000010800544	20000108	00544	GL  	2000	1	8	2000ZZZX81       	2	19991216	G	7250	9392M86G08	SHROUD          								GE    	CF6   	CF680C      		GL  					ENGINE	DISBONDED       	B			T9LR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15			1123 							FIVE CF6-80C STAGE 2 HPT SHROUDS WITH 347 CYCLES AND 1,123 HOURS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF THE 	WEARCOAT MATERIAL FROM THE SUBSTRATE.  PW ENGINEERING STATED THIS IS NOT A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE IS UNDER 	INVESTIGATION.									4	F			E23EA				 
2000041300299	20000413	00299	GL  	2000	4	13	2000ZZZX812      	2	19991227	G	7230	23061928	HOUSING         		23065593    	BELL  	407   	407         	       	SW  	ALLSN 	250C  	250C47B     	 	GL  					COMPRESSOR	MISMANUFACTURED 	B			ALGR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	547AL	1785 			24411	53240	CAE847064			DEFECT FOUND WHEN OLD COATING WAS REMOVED.  FOUND THICKNESS OF PARENT METAL BELOW SPECS (PART WAS MANUFACTURED BELOW  MI	NIMUM SPECS).					1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
2000010800545	20000108	00545	GL  	2000	1	8	2000ZZZX82       	2	19991216	G	7250	9392M86G08	SHROUD          								GE    	CF6   	CF680C      		GL  					ENGINE	DISBONDED       	B			T9LR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15			1433 							SIX CF6-80C, STAGE 2, HPT SHROUDS WITH 1,274 CYCLES AND 1,433 HOURS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF T	HE WEARCOAT MATERIAL FROM THE SUBSTRATE.  PW ENGINEERING STATED THAT THIS IS NOT A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE I	S UNDER INVESTIGATION.									4	F			E23EA				 
2000010800546	20000108	00546	GL  	2000	1	8	2000ZZZX83       	2	19991216	G	7250	1646M45P11	SHROUD          								GE    	CF6   	CF680C      		GL  					ENGINE	DISBONDED       	B			T9LR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15			2000 							TWENTY-FIVE CF6-80C STAGE 1 HPT SHROUDS WITH 400 CYCLES AND 2,000 HOURS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT 	OF THE WEARCOAT MATERIAL FROM SUBSTRATE.  PW ENGINEERING STATED THIS IS NOT A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE IS UND	ER INVESTIGATION.									4	F			E23EA				 
2000010800547	20000108	00547	NE  	2000	1	8	2000ZZZX84       	2	19991216	G	7250	1347M95G02	SHROUD          								GE    	CF6   	CF650*      	30018	NE  					ENGINE	DISBONDED       	B			T9LR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15										TWO CF6-50 STAGE 1 HPT SHROUDS WERE RECEIVED AND EXHIBITED PARTIAL FROM THE SUBSTRATE.  PW ENGINEERING STATED THIS IS NO	T A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE IS UNDER INVESTIGATION.										4	F			E23EA				 
2000010800548	20000108	00548	GL  	2000	1	8	2000ZZZX85       	2	19991216	G	7250	9392M86G08	SHROUD          								GE    	CF6   	CF680C      		GL  					ENGINE	DISBONDED       	B			T9LR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15			641  							SIX CF6-80C STAGE 2 HPT SHROUDS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF THE WEARCOAT MATERIAL FROM THE SUBSTR	ATE.  PW ENGINEERING STATED THIS IS NOT A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE IS UNDER INVESTIGATION.										4	F			E23EA				 
2000010800549	20000108	00549	GL  	2000	1	8	2000ZZZX86       	2	19991216	G	7250	9392M86G08	SHROUD          								GE    	CF6   	CF680C      		GL  					ENGINE	DISBONDED       	B			T9LR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15			347  							THREE CF6-80C STAGE 2 HPT SHROUDS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF THE WEARCOAT MATERIAL FROM THE SUBS	TRATE.  PW ENGINEERING STATED THIS IS NOT A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE IS UNDER INVESTIGATION.										4	F			E23EA				 
2000010800550	20000108	00550	GL  	2000	1	8	2000ZZZX87       	2	19991216	G	7250	9392M86G08	SHROUD          								GE    	CF6   	CF680C      		GL  					ENGINE	DISBONDED       	B			T9LR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15			10361							THREE CF6-80C STG 2 HPT SHROUDS WITH 1,352 CYCLES AND 10,361 HOURS WERE RECEIVED AND EXHIBITED PARTIAL DISBONDMENT OF TH	E WEARCOAT MATERIAL FROM THE SUBSTRATE.  PW ENGINEERING STATED THIS IS NOT A SAFETY OF FLIGHT ISSUE.  ROOT CAUSE IS UNDE	R INVESTIGATION.									4	F			E23EA				 
2000010800102	20000108	00102	EU  	2000	1	8	2000ZZZX9        	1	19991013	G	2822	1176415103	PUMP            			BOLKMS	117   	BK117B2     	5626013	EU  										FUEL BOOST	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	912SM				159592	7150				REPLACEMENT FOR PUMP FROM A/C 7505.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
2000011500623	20000115	00623	CE  	2000	1	15	2000ZZZX95       	1	19991217	G	5520		BRACKET         			CESSNA	172   	172H        	2072424	CE  										ELEVATOR	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	05	1772F	3409 				17255167				ELEVATOR BELLCRANK SUPPORT BRACKET P/N 0513063-3 CRACKED IN 3 OF 4 BEND RADIUS.  THIS AIRCRAFT HAS BEEN STORED INSIDE.						1	H	7	1 	3O			NT	3A12    					 
2000011500624	20000115	00624		2000	1	15	2000ZZZX96       	1	19991230	G	3240	7010FS9545708	SEAL            		50105201    															BRAKE	LEAKING         	B			XC4R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	19					FEB991603					BRAKE ASSEMBLY, P/N 5010520-1, FAILED PREMATURELY.  ONE EACH PISTON LEAKING FROM INSULATOR AREA.  PISTON INTERNALLY FILL	ED WITH FLUID.  EVIDENCE OF T-SEAL FAILURE.  THIS IS A CONTINUAL DISCREPANCY.  FACTORY NEW BRAKE ASSEMBLY.  NOTE:  OEM P	ARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 5010520-1.																	 
2000011500625	20000115	00625		2000	1	15	2000ZZZX97       	1	19991227	G	3240	7010FS9545708	SEAL            		50105201    															BRAKE	LEAKING         	B			XC4R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	19		1647 			JUL971019					BRAKE ASSEMBLY, P/N 5010520-1 FAILED  PREMATURELY.  TWO EACH PISTONS LEAKING FROM INSULATOR AREA.  PISTONS INTERNALLY FI	LLED WITH FLUID.  EVIDENCE OF T-SEAL FAILURE.  THIS IS A CONTINUAL DISCREPANCY.  FACTORY NEW BRAKE ASSEMBLY.  NOTE:  OEM	 PARTS INSTALLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 5010520-1.																	 
2000011500626	20000115	00626		2000	1	15	2000ZZZX98       	1	19991228	G	3240	7010FS9545708	SEAL            		50105201    															BRAKE	LEAKING         	B			XC4R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	19		1103 			JUN981359					BRAKE ASSEMBLY, P/N 5010520-1, FAILED PREMATURELY.  TWO EACH PISTONS LEAKING FROM INSULATOR AREA.  PISTONS INTERNALLY FI	LLED WITH FLUID.  EVIDENCE OF T-SEAL FAILURE.  THIS IS A CONTINUAL DISCREPANCY.  NOTE:  OEM PARTS INSTALLED IN BRAKE ASS	EMBLY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 5010520-1.																	 
2000011500627	20000115	00627	EU  	2000	1	15	2000ZZZX99       	1	19991220	G	2435	410964	BEARING         	AUXILEC     	8060300     	AMD   	FALC50	FALCON50MYST	2730106	EU  										STARTER/GEN	FAILED          	B			XC4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19		267  			716					STARTER/GENERATOR ANTI-DRIVE END BEARING FAILED PREMATURELY UNDER NORMAL OPERATING CONDITIONS CAUSING DAMAGE TO (ANTI-DR	IVE END) END BELL.					2	L	7	3 	4F				A46EU   					 
2002012800016	20020128	00016	EU  	2002	1	28	2002FA0000057    	1	19990116	G	3010	B03AA1031	VALVE           			AEROSP	ATR42 	ATR42300    	8680920	EU  										DUAL DISTRIBUTOR	FAILED          	B			QY2R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	25										THE DUAL DISTRIBUTOR VALVE WAS SENT IN FOR FUNCTIONAL TEST.  IT WAS REMOVED FROM A DAMAGED AIRCRAFT.   FUNCTIONALLY TEST	ED THE VALVE, IT WOULD NOT HOLD PRESSURE AND THE SIGNALING SYSTEM IS INTERMITTENT.  THE VALVE WAS DISASSEMBLED AND REPAI	RED.				2	H	7	2 	4T			RT	A53EU   					 
2000041300311	20000413	00311	WP  	2000	4	13	99T64R241AR      	1	19990615	G	5411	9753263527	FRAME           		            	DOUG  	DC8   	DC862       	3021970	WP  										NR 3 PYLONG	CRACKED         	B			T64R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03	1808E	65019				46105				NR 0762 - 6 INCH CRACK IN NR 3 PYLON CAP FORMER (HORSE COLLAR) FORWARD SECTION STA YN161.  FABRICATED REPLACMENT PART PE	R EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99.  INSTALLED IAW DC-8 SRM 51-1-21.  REF:  ARROW AIR - ARWA.  (X)					2	L	7	4 	4F			 	4A25    					 
2000022600601	20000226	00601	WP  	2000	2	26	99T64R334AR      	1	19990708	G	2611	SA106350	TUBE            			DOUG  	DC8   	DC862       	3021970	WP  										CABIN	MISSING         	B			T64R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	03	1808E	65019				46105				FLT 2823 - CABIN SMOKE DETECTOR LINES AND END FITTINGS NOT INSTALLED.  FABRICATED AND INSTALLED SMOKE DETECTOR TUBES AND	 FITTINGS IAW AS ELEVEN DWG AS 11045 WITH APPROVED FAA FORM 8110-3 DATED APRIL 27, 1999 APPROVED BY FAA ATLANTA CERTIFIC	ATION OFFICE LETTER DATED JUNE 23, 1999.  REF:  ARROW AIR - ARWA.  (X)				2	L	7	4 	4F				4A25    					 
2000022600600	20000226	00600	WP  	2000	2	26	99T64R335AR      	1	19990519	G	5320		FASTENER        			DOUG  	DC8   	DC862       	3021970	WP  										DOOR JAMB	MISSING         	B			T64R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03	1808E	65019				46105				FLT 2923 - MAIN CARGO DOOR, JAMB, FORWARD JAMB AFT BEAM SPLICE PLATE NOT IAW DWG AS11036.  REMOVED DOOR JAMB SHROUD, ADD	ED FASTENERS TO BRING SPLICE PLATE IAW AS 11036, INSTALLED DOOR JAMB SHROUD IAW DC-8 SRM 51-3-0.  WITH FAA FORM 8110-3 A	PPROVED BY FAA ATLANTA CERTIFICATION OFFICE LETTER DATED JUNE 23, 1999.  REF:  ARROW AIR - ARWA.   (X)				2	L	7	4 	4F				4A25    					 
2000022600599	20000226	00599	WP  	2000	2	26	99T64R336AR      	1	19990607	G	5320	SA106350	BEAM            			DOUG  	DC8   	DC862       	3021970	WP  										DOOR JAMB	SHORT           	B			T64R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	03	1808E	65019				46105				FLT 2851 - MAIN CARGO DOOR FORWARD JAMB - FORWARD BEAM INBOARD LEG TOO SHORT.  FABRICATED DOUBLER SHIMS IAW EO DWG AS110	42, TREATED AND PRIMED IAW DC-8 SRM 51-1-8 AND INSTALLED IAW EO DWG AS11042 AND DC-8 SRM 51-1-21.  WITH APPROVED FAA FOR	M 8110-3 DATED MAY 12, 1999 APPROVED BY FAA ATLANTA CERTIFICATION OFFICE LETTER DATED JUNE 23, 1999.  REF:  ARROW AIR - 	ARWA.  (X)			2	L	7	4 	4F				4A25    					 
1999073000633	19990730	00633	EA  	1999	7	30	99ZZZM418        	1	19990623	G	7830	22850071102	BRACKETS        			CNDAIR	CL601 	CL6012A12   	1900303	EA  										TR UNIT	ELONGATED       	B			SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	17CN					3027				THE BRACKETS ARE ATTACHED TO THE INLET RIB BY HL18PB5 HI-LOCKS, MEASURED ALL 48 HOLES AND FOUND SIZES FROM .164 INCH TO 	.175 INCH, AND SHOULD BE .159 INCH TO .162 INCH.  (M)					1	L	7	2 	4F			RT	A21AE   					 
1999073000634	19990730	00634	EA  	1999	7	30	99ZZZM419        	1	19990623	G	7830	22850071101	BRACKETS        			CNDAIR	CL601 	CL6012A12   	1900303	EA  										TR UNIT	ELONGATED       	B			SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	17CN					3027				THE BRACKETS ARE ATTACHED TO THE INLET RIB BY HL18PB5 HI-LOCKS, MEASURED ALL 48 HOLES AND FOUND SIZES FROM .164 INCH TO 	.175 INCH, AND SHOULD BE .159 INCH TO .162 INCH.  (M)					1	L	7	2 	4F			RT	A21AE   					 
1999100100439	19991001	00439	NM  	1999	10	1	99ZZZM668        	1	19990913	G	5754		SKIN            			BOEING	727   	727225      	1384077	NM  										LE FLAP	GOUGED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				RIGHT WING OUTBOARD FLAP FOREFLAP HAS GOUGE IN LEADING EDGE.  FABRICATED REPAIR IAW SRM 57-50-4.  INSTALLED REPAIR IAW S	RM 57-50-4.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100440	19991001	00440	NM  	1999	10	1	99ZZZM669        	1	19990913	G	5754		SKIN            			BOEING	727   	727225      	1384077	NM  										LE FLAP	GOUGED          	B				H				DEACTIVATE SYST/CIRCUITS				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				RT WING INBOARD FLAP FOREFLAP LEADING EDGE GOUGED INBOARD OF INBOARD TRACK.  FABRICATED REPAIR DOUBLER IAW SRM 57-50-4. 	 INSTALLED REPAIR DOUBLER IAW SRM 57-50-4.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100441	19991001	00441	NM  	1999	10	1	99ZZZM670        	1	19990913	G	5753		SKIN            			BOEING	727   	727225      	1384077	NM  										LE FLAP	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				LEFT WING INBOARD FLAP AFT FLAP AT MIDDLE OUTBOARD ATTACHMENT POINT CRACKED THROUGH STOP DRILL HOLE IN SKIN.  FABRICATED	 REPAIR DOUBLER IAW SRM 57-50-4.  INSTALLED REPAIR DOUBLER IAW SRM 57-50-4.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100442	19991001	00442	NM  	1999	10	1	99ZZZM671        	1	19990913	G	5320		CROSSMEMBER     			BOEING	727   	727225      	1384077	NM  										BS 1030	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				STATION 1030 LEFT BETWEEN BL 45.50 AND 24.75 EXHIBITS CORROSION ON CROSSMEMBER.  CORROSION OUT OF LIMITS IAW SRM 51-10-6	.  REMOVED CROSSMEMBER IAW SRM 51-30-2.  FABRICATED REPAIR PARTS IAW SRM 53-10-8.  INSTALLED CROSSMEMBER IAW SRM 51-30-2	.  (M)				2	L	7	3 	4F				A3WE    					 
1999100100443	19991001	00443	NM  	1999	10	1	99ZZZM672        	1	19990913	G	5315		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 460	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				FUSELAGE INTERIOR STATION 460 LBL 62 TO RBL 62 FLOORBEAM HAS CORROSION CORROSION OUT OF LIMITS IAW SRM 53-10-1.  FABRICA	TED REPAIR PARTS IAW SRM 53-10-8.  INSTALLED REPAIR PARTS T-CHORD, NR 2 AND NR 3 SUPPORT ANGLES, NR 4 AND NR 5.  REINFOR	CEMENT STRAPS AND DOUBLER SPACER IAW SRM 53-10-8.  (M)				2	L	7	3 	4F				A3WE    					 
1999100100444	19991001	00444	NM  	1999	10	1	99ZZZM673        	1	19990913	G	5315		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 360	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				FUSELAGE INTERIOR STATION 360 LBL 62 TO RBL 62 FLOORBEAM HAS CORROSION.  CORROSION OUT OF LIMITS IAW SRM 51-10-6.  REMOV	ED FLOORBEAM CAP IAW SRM 51-30-2.  FABRICATED REPAIR IAW SRM 53-10-8.  INSTALLED FLOORBEAM REPAIR IAW SRM 51-30-2.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100445	19991001	00445	NM  	1999	10	1	99ZZZM674        	1	19990913	G	5320		SUPPORT         			BOEING	727   	727225      	1384077	NM  										BS 420-460	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				FUSELAGE INTERIOR STATION 420 TO 460 RBL 62 HAS CORROSION.  CORROSION OUT OF LIMITS IAW SRM 51-10-6.  FABRICATED SUPPORT	 IAW SRM 53-10-2 AND SRM 53-10-8.  INSTALLED FASTENERS AND SUPPORT IAW SRM 51-30-2.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100446	19991001	00446	NM  	1999	10	1	99ZZZM675        	1	19990913	G	5320		SUPPORT         			BOEING	727   	727225      	1384077	NM  										BS 303-350	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				FUSELAGE INTERIOR STATION 303 TO 350 LBL 45 FLOOR SUPPORT HAS CORROSION.  CORROSION OUT OF LIMITS IAW SRM 53-10-1.  FABR	ICATED REPAIR ANGLES IAW SRM 51-40-4.  INSTALLED REPAIR ANGLES IAW SRM 51-30-2.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100447	19991001	00447	NM  	1999	10	1	99ZZZM676        	1	19990913	G	7110		RIB             			BOEING	727   	727225      	1384077	NM  										COWL	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				NR 1 ENGINE COWL TOP HALF AFT RIB DOUBLER BY BAYONET LATCH IS BENT AND CRACKED.  FABRICATED BRACKET AND DOUBLER IAW SRM 	54-10-3.  INSTALLED REPAIR BRACKET AND DOUBLER IAW SRM 51-30-2.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100448	19991001	00448	NM  	1999	10	1	99ZZZM677        	1	19990913	G	7110		SKIN            			BOEING	727   	727225      	1384077	NM  										COWL	DAMAGED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				NR 1 ENGINE COWL HALF OUTBOARD BY NR 2 LATCH RECEPTICAL EDGE IS DAMAGED.  REMOVED DAMAGED ANGLE FROM COWL IAW SRM 54-10-	3.  FABRICATED REPAIR DOUBLER IAW SRM 54-10-3.  INSTALLED DOUBLER IAW SRM 54-10-3.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100449	19991001	00449	NM  	1999	10	1	99ZZZM678        	1	19990913	G	7110		SKIN            			BOEING	727   	727225      	1384077	NM  										COWL	SEPARATED       	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				NR 1 ENGNE COWL LOWER HALF NR 3 LATCH RECEPTICAL EDGE SEPARATING.  FABRICATED DOUBLERS IAW SRM 54-10-3.  INSTALLED DOUBL	ERS IAW SRM 54-10-3.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100450	19991001	00450	NM  	1999	10	1	99ZZZM679        	1	19990913	G	5510	652938916	TRACK           			BOEING	727   	727225      	1384077	NM  										STABILIZER	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				STABILIZER RIGHT SIDE OUT OF TRAK AND IS CRACKED.  RECEIVED NEW TRACK P/N 65-29389-16.  INSTALLED NEW TRACK IAW SRM 51-3	0-2.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100451	19991001	00451	NM  	1999	10	1	99ZZZM680        	1	19990913	G	7110		SKIN            			BOEING	727   	727225      	1384077	NM  										COWL	DAMAGED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				NR 3 ENGINE COWL UPPER HALF INBOARD SECTION ALONG EDGE EXHIBITED DAMAGE TO INNER SKIN FROM FORWARD TO AFT IN MANY AREA. 	 REMOVED DAMAGE IAW SRM 51-40-2.  FABRICATED REPAIRS IAW SRM 51-40-2.  INSTALLED REPAIRS IAW SRM 51-40-2.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100452	19991001	00452	NM  	1999	10	1	99ZZZM681        	1	19990913	G	7110		SKIN            			BOEING	727   	727225      	1384077	NM  										COWL	DAMAGED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				NR 3 ENGINE COWL UPPER HALF INBOARD SECTION BY NR 1, NR 2, AND NR 3 LATCH RECEPTICALS DAMGED SKIN.  REPAIRED DAMAGED SKI	N IAW SRM 51-10-1.  FABRICATED DOUBLER IAW RM 53-10-4.  INSTALLED DOUBLER IAW SRM 53-10-4.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100453	19991001	00453	NM  	1999	10	1	99ZZZM682        	1	19990913	G	5330		SKIN            			BOEING	727   	727225      	1384077	NM  										FUSELAGE	DENTED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				RIGHT SIDE EXTERIOR FUSELAGE BELOW FORWARD JACK POINT HAS A DENT DAMAGE OUT OF LIMITS IAW SRM 53-30-3.  REMOVED DAMAGED 	AREA IAW SRM 53-30-3.  FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3.  INSTALLED REPAIR DOUBLER AND FILLER IAW RM	 53-30-3.  (M)				2	L	7	3 	4F				A3WE    					 
1999100100454	19991001	00454	NM  	1999	10	1	99ZZZM683        	1	19990913	G	5315		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 294	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				FUSELAGE LOWER LOBE INTERIOR RIGHT HORIZONTAL WALKWAY BEAM CHORD STATION 294 HAS CORROSION.  CORROSION OUT OF LIMITS IAW	 SRM 53-10-1.  REMOVED DAMAGED CHORD AND FRAME IAW SRM 53-10-4.  FABRICATED BELT FRAME AND T-CHORD IAW SRM 53-10-4.  INS	TALLED BELT FRAME AND T-CHORD IAW SRM 53-10-4.  (M)				2	L	7	3 	4F				A3WE    					 
1999100100455	19991001	00455	NM  	1999	10	1	99ZZZM684        	1	19990913	G	5313		STRINGER        			BOEING	727   	727225      	1384077	NM  										BS 1070	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				EXTERNAL FUSELAGE BULGE IN SKIN AT FS 1070R, STRINER 27R CORROSION OUT OF LIMITS.  REMOVED STRINGER IAW SRM 53-10-1.  FA	BRICATED NEW STRINGER, SPLICES, SHIMS, AND FILLERS IAW SRM 53-10-3.  INSTALLED REPAIR PARTS IAW SRM 53-10-3.  INSTALLED 	INTERCOSTAL AND SHEAR TIES IAW SRM 51-30-2.  (M)				2	L	7	3 	4F				A3WE    					 
1999100100456	19991001	00456	NM  	1999	10	1	99ZZZM685        	1	19990913	G	5311		FRAME           			BOEING	727   	727225      	1384077	NM  										BS 440	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				FUSELAGE INTERIOR STATION 440 LBL 62 TO RBL 62 HAS CORROSION.  CORROSION OUT OF LIMITS IAW SRM 51-10-6.  FABRICATED REPA	IR PARTS IAW SRM 51-10-8.  INSTALLED REPAIR PARTS, T-CHORD NR 2 AND NR 3 SUPPORT ANGLE, NR 4 AND NR 5.  REINFORCEMENT ST	RAPS IAW SRM 53-10-8.  (M)				2	L	7	3 	4F				A3WE    					 
1999100100457	19991001	00457	NM  	1999	10	1	99ZZZM686        	1	19990913	G	5414		SKIN            			BOEING	727   	727225      	1384077	NM  										NR 3 PYLON	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				NR 3 ENGINE PYLON APRON UPPER SURFACE HAS SEVERAL CRACKS.  DAMAGED AREAS REMOVED IAW SRM 51-40-2.  FABRICATED REPAIRS IA	W SRM 51-40-2.  INSTALLED REPAIRS IAW SRM 51-40-2.  (M)					2	L	7	3 	4F				A3WE    					 
1999100100458	19991001	00458	NM  	1999	10	1	99ZZZM687        	1	19990913	G	5315		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 380	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				FUSELAGE INTERIOR STATION 380 RBL 62 TO LBL 62 FLOORBEAM HAS CORROSION.  CORROSION OUT OF LIMITS IAW SRM 53-10-8.  CUT O	UT DAMAGED AREA IAW SRM 53-10-8.  FABRICATED REPAIR PARTS IAW SRM 53-10-8.  INSTALLED REPAIR PARTS, UPPER CHORD, 2 SUPPO	RT ANGLES, AND 2 REINFORCEMENT STRAPS IAW SRM 53-10-8.  (M)				2	L	7	3 	4F				A3WE    					 
1999031901001	19990319	01001	EA  	1999	3	19	99ZZZX1000       	2	19990219	G	7311	20002A	OIL COOLER      			PIPER 	PA28  	PA28181     	7102807	SO  	LYC   	O360  	O360A4M     	41514	EA  					ENGINE OIL	CRACKED         	B			UC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	41487	216  			G98313141	2843179				ON PRE-FLIGHT INSPECTION, PILOT REPORTED THE AIRPLANE ENGINE WAS LEAKING OIL.  THE AIRPLANE WAS BROUGHT INTO THE MAINTEN	ANCE SHOP FOR FURTHER INSPECTION AND IT WAS DISCOVERED THE OIL COOLER HAD CRACKED AT THE LOWER OIL COOLER HOSE ATTACH FI	TTING.  CAUSE UNKNOWN.  PIPER HAS A SB 1019 THAT ADDRESSES OIL COOLERS OF THIS TYPE CRACKING.  BUT, IT DOES NOT APPLY BY	 S/N OR LOCATION OF CRACK.			1	L	7	1 	3O	3	O		2A13    	E286				 
1999031901002	19990319	01002	CE  	1999	3	19	99ZZZX1001       	1	19990224	G	8011	31M22045	SUPPORT         			CESSNA	172   	172S        	2072439	CE  										STARTER	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP				V68671198	172S8035				NEW CESSNA WITH 50.0 HOURS, WHILE ACCOMPLISHING A PHASE 1 INSPECTION, FOUND THE STARTER RING GEAR SUPPORT ASSY HAD A 1.5	0 INCH CRACK ON THE OUTER FACE .25 INCH AFT OF THE FRONT FACE.  REMOVAL OF THE PROPELLER AND SUPPORT ASSY REVEALED A CAS	TING DEFECT ON THE AFT SIDE OPPOSITE TO THE CRACK.				1	H	7	1 	3O			NT	3A12    					 
1999031901003	19990319	01003	CE  	1999	3	19	99ZZZX1002       	1	19990224	G	5347	05142102	SEAT TRACK      			CESSNA	172   	172S        	2072439	CE  										COCKPIT	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	172S					172S8035				NEW CESSNA WITH 50.0 HOURS, WHILE ACCOMPLISHING A PHASE 1 INSPECTION, THE COPILOT'S INBOARD SEAT RAIL HAD ONE OF THE EIG	HT BOLTS MOUNTING THE SEAT RAIL TO THE FLOOR CROSS THREADED INTO ITS NUTPLATE AND THE BOLT HEAD LACKED .1250 INCH FROM B	EING SEATED.				1	H	7	1 	3O			NT	3A12    					 
1999031901004	19990319	01004		1999	3	19	99ZZZX1003       	4	19990224	G	6113	055032110	BULKHEAD        			CESSNA	172   	172S        	2072439	CE  										PROP SPINNER	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP					172S8035				NEW CESSNA WITH 50.0 HOURS, AFTER LAST FLIGHT PRIOR TO PHASE 1 INSPECTION, FOUND AFT PROPELLER SPINNER BULKHEAD BROKEN A	T THE FIRST NUTPLATE FROM ONE BLADE CUT-OUT, APPROXIMATELY A 1 INCH PIECE BROKE OUT WITH NUTPLATE.  THE BROKEN PIECE STI	LL ATTACHED TO PROPELLER SPINNER WAS BENT OUTWARD 2 INCHES.				1	H	7	1 	3O			NT	3A12    					 
1999031901005	19990319	01005	CE  	1999	3	19	99ZZZX1004       	1	19990302	G	2400	MS2742Z4	TERMINAL STRIP  			CESSNA	421   	421C        	2076016	CE  										ELECTRICAL SYS	FAILED          	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	421SR	2232 				421C1215				CONNECTOR LUGS ON CABLES FROM ALTERNATORS TO TERMINAL STRIP CORRODED CAUSING HIGH RESISTANCE AND OVERHEATING UNDER FULL 	ALTERNATOR LOAD, NR 1 TERMINAL POST MELTED AWAY FROM TERMINAL STRIP ALLOWING PRIMARY DC WIRING TO CONTACT AIRFRAME STRUC	TURE.  RESULT:  DUAL ALTERNATOR FAILURE, VERY RAPID BATTERY DISCHARGE.  SUBMITTER STATED TOTAL ELECTRICAL FAILURE RISK O	F FIRE.			1	L	7	2 	3O				A7CE    					 
1999031901007	19990319	01007	CE  	1999	3	19	99ZZZX1006       	1	19990201	G	5540	506300000200	RIVETS          			BEECH 	65    	65          	1152802	CE  										TORQUE TUBE	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	01	5079E					LF52				ALL RIVETS HOLDING TORQUE TUBE, PN 50-630000-126, TO FITTING, PN 50-600016, AND FITTING, PN 50-600017, HAVE SHEARED OFF.	  UNKNOWN REASONS.  UNDER NORMAL USE CONDITIONS.					1	L	7	2 	3O				3A20    					 
1999031901009	19990319	01009	EA  	1999	3	19	99ZZZX1008       	2	19990203	G	8530	LW13536CP	CYLINDER        			GULSTM	500   	500S        	0141107	SW  	LYC   	O540  	IO540E1A5   	41532	EA  					ENGINE	MISOVERHAULED   	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	25	51RF					3298	RL123148			UPON INSTALLING AN OVERHAULED CYLINDER, NOTED THE CYLINDER WAS NOT ALIGNED WITH THE ONE NEXT TO IT AT THE ROCKER BOX ARE	A.  THE SHORTEST PUSH ROD WOULD NOT GO IN.  IT WAS FOUND OUT THAT THE CYLINDER WAS TOO SHORT AFTER OVERHAUL.  ANOTHER CY	LINDER WAS PUT ON AND IT WORKED OK.  THE CYLINDER THAT WAS TOO SHORT HAD A SERVICEABLE TAG.				1	H	7	2 	3O	3	O		6A1     	1E4				 
1999032600144	19990326	00144	CE  	1999	3	26	99ZZZX1009       	1	19990108	G	2140		BOLT            			CESSNA	172   	172S        	2072439	CE  										CABIN HEAT	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	25	494SP					172S8035				ACCEPTANCE INSPECTION ON NEW CESSNA WITH 8.0 HOURS SINCE MANUFACTURE REVEALED THE CABIN HEAT VALVE CABLE RETAINER BOLT W	AS PROTRUDING THROUGH THE ACTUATOR ARM AND CHAFING ON THE HOUSING.  THE BOLT WASHER CONFIGURATION WAS INCORRECT LOCKING 	THE ACTUATOR CABLE TO THE HEAT VALVE ARM.  RE-CONFIGURED WASHERS CORRECTLY, ELIMINATED CHAFING.				1	H	7	1 	3O			NT	3A12    					 
1999032600145	19990326	00145	CE  	1999	3	26	99ZZZX1010       	1	19990125	G	2710	922AB1YA4NL	SWITCH          			CESSNA	750   	750         	2076810	CE  										AILERON	FAILED          	B	P		GMCR	C				ABORTED TAKEOFF         				N			FALSE WARNING             			TO	TAKEOFF        	1			GL	23	5112	1027 				7500010				DUE TO A NO TAKEOFF WARNING ILLUMINATING AT 90 KNOTS, THE CREW REJECTED TAKEOFF.  MAINTENANCE DISCOVERED A LOOSE PROXIMI	TY SWITCH AT THE AILERON/SPOILER DISCONNECT HANDLE.  ADJUSTED PROXIMITY SWITCH AND PERFORMED OPS CHECK.  MAINTENANCE RET	URNED AIRCRAFT TO SERVICE.				2	L	7	2 	4J			RT	T00007WI					 
1999032600147	19990326	00147	CE  	1999	3	26	99ZZZX1012       	1	19990217	G	3221	2043000202	BEARING         			CESSNA	177   	177RG       	2073709	CE  										NLG	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	52596	4243 				177RG1212				FOUND UPPER TRUNNION BEARING PN S1997-40G12 COMPLETELY RUSTED AND THE BARREL ASSY PN 2043003-4 UPPER BEARING SURFACE WOR	N WITH .1250 INCH GROOVE.  FOUND DURING INSPECTION FOR NOSE WHEEL SHIMMY PROBLEM.					1	H	7	1 	3O				A20CE   					 
1999032600148	19990326	00148	CE  	1999	3	26	99ZZZX1013       	1	19990217	G	5320		RIVETS          	KING        		CESSNA	177   	177RG       	2073709	CE  										SUPPORT	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	52596	4243 				177RG1212				FOUND ALL 4 AFT HIGH SHEAR RIVETS LOOSE, PN NAS1054-8-7 AND NAS1054-6-8 IN THE SUPPORT ASSY.  REPLACED WITH OVERSIZED HI	GH LOC RIVETS.  FOUND DURING ANNUAL INSPECTION.					1	H	7	1 	3O				A20CE   					 
1999032600149	19990326	00149	EA  	1999	3	26	99ZZZX1014       	2	19990205	G	7314	41271	PUMP            			PIPER 	PA23  	PA23250     	7102308	SO  	LYC   	O540  	O540A1D5    	41532	EA  					FUEL SYSTEM	FAILED          	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	09	5374Y				AA8142	272447	L1457940			ARM ON FUEL PUMP FAILED IN LESS THAN 2 MINUTES OF OPERATION.  'BROKE THROUGH PIVOT HOLE IN ARM DROPPED INTO ACCESSORY CA	SE'.  INFO LETTER FROM REPAIR STATION STATED THEY FELT PUMP WAS IMPROPERLY INSTALLED BASED ON SEVERITY OF FRACTURE AND M	ARKS ON ARM.  STATED INSTALLED WITH LEVER BESIDE ENGINE PLUNGER PIN AS OPPOSED TO UNDER THE PIN.				1	L	7	2 	3O	3	O		1A10    	E295				 
1999032600150	19990326	00150	CE  	1999	3	26	99ZZZX1015       	1	19990125	G	5210	24130265	BULKHEAD        			CESSNA	172   	172P        	2072436	CE  										PASSENGER DOOR	CRACKED         	D	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	52872	9760 				17274625				DURING ROUTINE 100-HOUR INSPECTION, LEFT HAND FORWARD DOOR POST BULKHEAD WAS FOUND CRACKED.  CRACK IS APPROXIMATELY .50 	INCH IN LENGTH AROUND AFT ATTACH BOLT FOR LOWER DOOR HINGE.  SUBMITTER STATED 5 FOUND IN LAST 3 MONTHS.  ALL AIRCRAFT AR	E USED IN TRAINING/RENTAL ENVIRONMENT.				1	H	7	1 	3O			NT	3A12    					 
1999032600151	19990326	00151	CE  	1999	3	26	99ZZZX1016       	1	19990219	G	8011	MZ4214	STARTER         			CESSNA	150   	150M        	2071830	CE  										ENGINE	FAILED          	B			QC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	590AM				5J000314	15076540				STARTER OVERHAULED IN APRIL, 1996.  NO LOG BOOK ENTRIES FOUND.  ENGINE WAS OVERHAULED 12-6-98.  STARTER HOUSING FELL OFF	 THE ARMATURE.  ESTIMATED TIME:  700 HOURS ON STARTER.					1	H	7	1 	3O				3A19    					 
1999032600152	19990326	00152	SO  	1999	3	26	99ZZZX1017       	1	19990215	G	3710	441CC7	VACUUM PUMP     			PIPER 	PA31  	PA31310     	7103103	SO  										VACUUM SYSTEM	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	01	59984		584  		10AG674	317512042				AIR INTAKE FOR LEFT PUMP IS ON BOTTOM OF NACELLE, AFT OF FIREWALL, OUTBOARD OF NACELLE CENTERING.  THIS LOCATION IS DIRE	CTLY AFT OF THE ENGINE CRANKCASE BREATHER.  OIL VAPOR IS PRONE TO ACCUMULATE ON B3-5-1 GARTER FILTER.  COMBINED WITH ANY	 ENGINE OIL LEAK, ENOUGH OIL MAY BE PRESENT TO REACH THE PUMP ITSELF AND CAUSE A FAILURE.  SUBMITTER STATED THE GARTER F	ILTER MUST BE CHANGED OR INSPECTED OFTEN ESPECIALLY WHEN OIL LEAKS FROM THE ENGINE ARE NOTED.  ALSO, THE H-6000 HOSE TO 	THE PUMP INLET SHOULD OCCASIONALLY BE CHECKED FOR CONTAMINATION.		1	L	7	1 	3O			RT	A20SO   					 
1999032600153	19990326	00153	CE  	1999	3	26	99ZZZX1018       	1	19990223	G	2434		BRACKET         			BEECH 	35    	K35         	1151524	CE  										ALTERNATOR	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	13	6099E					D5986				ALTERNATOR LOWER ATTACH BOLT PULLED FROM BRACKET CAUSING LOSS OF BELT TENSION AND SUBSEQUENT BATTERY DRAIN AND INTERRUPT	ION OF RADIO CONTACT.  BOLT HAD ONLY ENGAGED TWO OR THREE THREADS IN MOUNTING BRACKET BECAUSE OF TOO  MANY WASHERS UNDER	 BOLT HEAD.   WITHOUT WASHERS, THE BOLT WOULD NOT THREAD ALL THE WAY INTO THE BRACKET UNTIL DIRT WAS REMOVED.  WHEN DIRT	 IN BRACKET WAS REMOVED AND STACK OF WASHERS REMOVED, ALTERNATOR COULD THEN BE MOUNTED SECURELY WITH ADEQUATE ENGAGEMENT	 OF BOLT.		1	L	7	1 	3O				3A15    					 
1999032600154	19990326	00154	GL  	1999	3	26	99ZZZX1019       	3	19990209	G	6111	A14B	BEARING         			PIPER 	PA24  	PA24250     	7102404	SO  						HARTZL	HC82X	HC82XK1     	GL  	PROPELLER	CRACKED         	B			W59R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	5686P	6893 				24758		831G		PROPELLER SUBMITTED FOR 'OVERHAUL' IN CONJUNCTION WITH AD 97-18-02 COMPLIANCE.  OPEN DISASSEMBLY, PROPELLER BLADE CLAMP,	 SN D776, WAS FOUND TO HAVE LOOSE A321 SOCKET SCREWS (SCREWS WERE ONLY HAND TIGHT).  UPON FURTHER DISASSEMBLY, THE A14B 	BEARING WAS FOUND CRACKED RADIALLY, APPROXIMATELY 2 INCHES LONG.  BLADE FAILURE WAS IMMINENT.  PROPELLER HAD ATTAINED 6,	893.2 HRS WITHOUT EVER BEING 'OVERHAULED' AND THE LATEST AD INSPECTION WAS 3-24-95 C/W 68-19-04.  SUBMITTER SUSPECTED TH	AT FAILED A14B OVERSTRESSED THE A321 SOCKET SCREWS.  THE A14B IS NOT REQUIRED TO BE INSPECTED PER 68-19-04, HOWEVER, IS 	REQUIRED TO BE INSPECTED AT O/H OR AD 97-18-02 COMPLIANCE.	1	L	7	1 	3O				1A15    		5	C	P878	 
1999032600156	19990326	00156		1999	3	26	99ZZZX1021       	4	19990201	G	3444	066103403	TRANSPONDER     			BEECH 	23    	B24R        	1151253	CE  										COCKPIT	FAILED          	H				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			NM	11	6565R				18976	MC302				MODE C FAILURE.  TESTED UNIT IN A/C.  FOUND TRANSPONDER OUT OF LIMITS.  RETURNED UNIT TO SHOP.  PERFORMED MANUFACTURER'S	 ALIGNMENT PROCEDURES AND FUNCTION TESTED GOOD.  RE-INSTALLED UNIT TO A/C AND FUNCTION TESTED GOOD.					1	L	7	1 	3O				A1CE    					 
1999032600157	19990326	00157	CE  	1999	3	26	99ZZZX1022       	1	19990210	G	2701	05133602	BRACKET         			CESSNA	172   	172P        	2072436	CE  										CONTROL YOKE	ELONGATED       	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	07	63952	6193 				17275500				CONTROL YOKE PIVOT BOLT HAS ELONGATED BOLT HOLES IN RT BRACKET ASSY CAUSING EXCESSIVE FORE AND AFT PLAY IN CONTROL YOKE 	1 INCH OF TRAVEL.  PROBLEM FOUND DURING ANNUAL INSPECTION.  TACHOMETER TIME:  4,326.0 HOURS.  HOBBS:  6,193.0.  1982 CES	SNA 172-P.				1	H	7	1 	3O			NT	3A12    					 
1999032600158	19990326	00158	CE  	1999	3	26	99ZZZX1023       	1	19990115	G	2434	DOFF103008	ALTERNATOR      	POINTER     		CESSNA	210   	210N        	2073453	CE  										ENGINE	MALFUNCTIONED   	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	09	6585A		769  		R132290	21063554				ALTERNATOR KICKS OFF-LINE UNDER A LOAD OF MID TO HIGH INTENSITY AND WILL NOT COME ON-LINE UNTIL 1,500 RPM'S OR HIGHER.						1	H	7	1 	3O				3A21    					 
1999032600160	19990326	00160	SO  	1999	3	26	99ZZZX1025       	1	19990208	G	5310	63452004	DOUBLER         			PIPER 	PA28  	PA28140     	7102802	SO  										ENTRY STEP	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	33	6459R					2821645				ON TWO SEPARATE AIRCRAFT ON ANNUAL INSPECTIONS, THIS DOUBLER HAS BEEN FOUND RUSTED AND CRACKED.  THIS IS CAUSED BY WATER	 AND DIRT ACCUMULATION AND DRAIN HOLES BEING PLUGGED.  THIS CAUSES RUST AND THIS IS A STEEL PART.  THIS SETS UP DISSIMIL	AR METAL CORROSION WHICH WEAKENS THE DOUBLER AND CAUSES CRACKS.  THIS WEAKENS AIRCRAFT STRUCTURE.  SUBMITTER SUGGESTED T	HIS AREA NEEDS CLOSER INSPECTION, CLEANING AND MONITORING FOR CORROSION.			1	L	7	1 	3O				2A13    					 
1999032600162	19990326	00162	CE  	1999	3	26	99ZZZX1027       	1	19990205	G	2720		TORQUE TUBE     			CESSNA	172   	172RG       	2072438	CE  										RUDDER	CRACKED         	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	6529V					172RG0755				IN-FLIGHT, RUDDER BECAME INOPERATIVE.  PUSHING ON LT OR RT RUDDER PEDAL, IN BOTH PILOT OR COPILOT POSITION, RESULTED IN 	MINOR YAWING OF ACFT.  AFTER LANDING AND DISASSY, TECH FOUND RUDDER TORQUE TUBE CRACKED ALMOST ALL THE WAY AROUND THE TU	BE NEXT TO THE 5-TOOTH GEAR, 6 INCHES FROM END OF THE TUBE.  THIS RESULTED IN LOSS OF TORQUE TUBE FUNCTION AND RUDDER. A	NY RUDDER PEDAL MOTION ONLY SERVED TO OPEN CRACK AND WAS NOT TRANSFERRED TO THE GEAR AND RUDDER CABLES.  BENDING OF THE 	TORQUE TUBE, BECAUSE OF THE CRACK, ALLOWED GEAR TO DISENGAGE AND RESULTED IN LOSS OF RUDDER ACTION.  DUE TO LOCATION, IN	SP OF TORQUE TUBE WAS IMPOSSIBLE, UNLESS A PROBLEM WAS SUSPECT AND FLOORING PULLED BACK TO CHECK.	1	H	7	1 	3O				3A17    					 
1999032600164	19990326	00164	CE  	1999	3	26	99ZZZX1029       	1	19990125	G	5210		BUSHING         		45A301591   	BEECH 	MU300 	400A        	1155402	CE  										CABIN DOOR	LOOSE           	B			AKGR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	05	710TA	773  				RK183				CABIN DOOR HANDLE LOCKING PIN WOULD NOT ENGAGE THE HANDLE.  FOUND THE BUSHING IN THE BEARING PLATE, PN 45A30159-1, HAD B	ACKED OUT.  THIS KEPT THE LOCKING PIN, PN 45A30181-9, FROM MOVING IN FAR ENOUGH TO LOCK THE HANDLE.  THE BUSHING WAS RE-	SEATED BACK INTO THE PLATE AND THEN STAKED; IT HAD NOT BEEN STAKED BEFORE.				2	H	7	2 	4F			RT	A16SW   					 
1999032600165	19990326	00165	SO  	1999	3	26	99ZZZX1030       	1	19990129	G	5751	5202035516	SKIN            			GULSTM	AA5   	AA5B        	3960105	SO  										AILERON	DELAMINATED     	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	09	74304	1675 				AA5B0192				AIRCRAFT WAS BEING ANNUALED AND AD 79-22-04 PARA (A)(2) WAS BEING PERFORMED.  FOUND THE UPPER SKIN DELAMINATED FROM THE 	LEADING EDGE AFT FROM 1 INCH TO 4 INCHES AT THE BONDED RIBS.					1	L	7	1 	3O				A16EA   					 
1999032600166	19990326	00166	CE  	1999	3	26	99ZZZX1031       	1	19990127	G	3411	072110518	PITOT           			CESSNA	182   	182S        	2072701	CE  										LT WING	LEAKING         	B	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	784AC	128  				18280096				PERFORMED STATIC LEAK CHECK PER SIB 98-22-02R1 AND SB KC 140-2.  FOUND PITOT TUBE TO HAVE INTERNAL LEAK INSIDE OF PITOT 	TUBE ASSY AND HEATER ELEMENT WAS CRACKED.  REPLACED PITOT TUBE ASSY.  OPS CHECK NORMAL.  (IPC 34-11-00, ITEM 30).					1	H	7	1 	3O			NT	3A13    					 
1999032600167	19990326	00167	CE  	1999	3	26	99ZZZX1032       	1	19990211	G	5540	NAS428H36	STOP            			CESSNA	182   	182M        	2072728	CE  										RUDDER	BENT            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	71886					18259793				FOUND RUDDER STOP BENT AND NO LONGER LIMITING RUDDER TRAVEL.  FOUND IMPROPER HARDWARE INSTALLED.  TRUSS HEAD SCREW INSTE	AD OF BOLT DID NOT ALLOW FOR PROPER CONTACT AREA.  COULD NOT TELL FROM LOGS WHEN THIS WAS INSTALLED.					1	H	7	1 	3O			NT	3A13    					 
1999032600169	19990326	00169	CE  	1999	3	26	99ZZZX1034       	1	19990201	G	7714		TACHOMETER      			CESSNA	172   	172N        	2072434	CE  										COCKPIT	UNAPPROVED PART 	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01	739TD	338  				17270785				OWNER COMPLAINED OF ENGINE RPM BEING LOW.  CHECKED TACHOMETER WITH TACH-CHECK, FOUND TACH 400 RPM LOW.  SUBMITTER STATED	 THIS IS THE SECOND TACH LIKE THIS FOUND IN LAST 3 YEARS.  THE ONLY MARKING ON THE TACHOMETER IS 'MADE IN CHINA'.					1	H	7	1 	3O			NT	3A12    					 
1999032600170	19990326	00170	EA  	1999	3	26	99ZZZX1035       	2	19990204	G	8520	SL15628	SEAL            			PIPER 	PA32  	PA32300     	7103212	SO  	LYC   	O540  	IO540K1A5   	41532	EA  					CRANKSHAFT	FAILED          	D				A				UNSCHED LANDING         				K			FLUID LOSS                			NR	NOT REPORTED   	1			AL	03	76RL	1641 				327540024	L1023B48			PILOT NOTICED OIL LEAK, LANDED SAFELY AND SECURED AIRCRAFT.  AFTER FURTHER INSPECTION, FOUND THE FRONT CRANKSHAFT SEAL P	USHED OUT OF ITS SEAT CAUSING THE OIL LEAK.					1	L	7	1 	3O	3	O		A3SO    	1E4				 
1999032600171	19990326	00171	CE  	1999	3	26	99ZZZX1036       	1	19990201	G	3230	05412024	BUSHING         			CESSNA	172   	172R        	2072401	CE  										RT MLG	DAMAGED         	B			WIWR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	782WW	1088 				17280295				DURING A ROUTINE INSPECTION OF THE AIRFRAME, THE RT MAIN LANDING GEAR BUSHING WAS FOUND DEFORMED.  THE INSIDE BUSHING MA	TERIAL WAS PROTRUDING FROM THE EDGE OF THE BUSHING.  THE BUSHING WAS FURTHER INSPECTED AFTER REMOVAL FOR THE AIRCRAFT AN	D CONTAINED STRESS CRACKS ALONG THE INSIDE OF THE BUSHING.				1	H	7	1 	3O			NT	3A12    					 
1999032600172	19990326	00172	CE  	1999	3	26	99ZZZX1037       	1	19990117	G	2750	BZ3AT	SWITCH          			BEECH 	36    	A36         	1151604	CE  										FLAPS	INOPERATIVE     	B			O16R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	705MB	506  				E2836				THE 14 DEGREE APPROACH LIMIT SWITCH FAILED ALLOWING THE MOTOR TO BE OVERWORKED, RUINING THE CABLES AND BURNING THE CIRCU	ITRY ON THE PCB RELAY ASSEMBLY.  THE REPLACEMENT MOTOR WAS DEFECTIVE AND FRIED THE NEW PCB BOARD.  THIS OCCURS WITHOUT B	LOWING THE MOTOR BREAKER.  SUBMITTER RECOMMENDED A WIRING MODIFICATION BE PURSUED THAT WILL NOT ALLOW FAILURE OF THE 14 	DEGREE LIMIT SWITCH TO BYPASS THE DOWN LIMIT SWITCH AND DAMAGE THE SYSTEM AND/OR A TAG THAT COMES WITH A NEW FLAP MOTOR 	THAT GIVES ELEC CAPABILITY OF MOTOR AND WARNS OF A MOTOR PULLING TOO MUCH AMPERAGE MAY WEAKEN OR BURN THE MOTOR CIRCUITR	Y ON THE PCB.  FAILURE OF THESE COMPONENTS MAY NOT ALLOW PILOT TO RETRACT FLAPS IN-FLIGHT, ETC.	1	L	7	1 	3O				3A15    					 
1999032600173	19990326	00173	CE  	1999	3	26	99ZZZX1038       	1	19990117	G	2750	P160003	MOTOR ASSY      			BEECH 	36    	A36         	1151604	CE  										FLAPS	INOPERATIVE     	B			O16R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	705MB	506  			8047	E2836				THE 14 DEGREE APPROACH LIMIT SWITCH FAILED ALLOWING THE MOTOR TO BE OVERWORKED, RUINING THE CABLES AND BURNING THE CIRCU	ITRY ON THE PCB RELAY ASSEMBLY.  THE REPLACEMENT MOTOR WAS DEFECTIVE AND FRIED THE NEW PCB BOARD.  THIS OCCURS WITHOUT B	LOWING THE MOTOR BREAKER.  SUBMITTER RECOMMENDED A WIRING MODIFICATION BE PURSUED THAT WILL NOT ALLOW FAILURE OF THE 14 	DEGREE LIMIT SWITCH TO BYPASS THE DOWN LIMIT SWITCH AND DAMAGE THE SYSTEM AND/OR A TAG THAT COMES WITH A NEW FLAP MOTOR 	THAT GIVES ELEC CAPABILITY OF MOTOR AND WARNS OF A MOTOR PULLING TOO MUCH AMPERAGE MAY WEAKEN OR BURN THE MOTOR CIRCUITR	Y ON THE PCB.  FAILURE OF THESE COMPONENTS MAY NOT ALLOW PILOT TO RETRACT FLAPS IN-FLIGHT, ETC.	1	L	7	1 	3O				3A15    					 
1999032600174	19990326	00174	CE  	1999	3	26	99ZZZX1039       	1	19990117	G	2750	P160003	MOTOR ASSY      			BEECH 	36    	A36         	1151604	CE  										FLAPS	INOPERATIVE     	B			O16R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	705MB				9299	E2836				THE 14 DEGREE APPROACH LIMIT SWITCH FAILED ALLOWING THE MOTOR TO BE OVERWORKED, RUINING THE CABLES AND BURNING THE CIRCU	ITRY ON THE PCB RELAY ASSEMBLY.  THE REPLACEMENT MOTOR WAS DEFECTIVE AND FRIED THE NEW PCB BOARD.  THIS OCCURS WITHOUT B	LOWING THE MOTOR BREAKER.  SUBMITTER RECOMMENDED A WIRING MODIFICATION BE PURSUED THAT WILL NOT ALLOW FAILURE OF THE 14 	DEGREE LIMIT SWITCH TO BYPASS THE DOWN LIMIT SWITCH AND DAMAGE THE SYSTEM AND/OR A TAG THAT COMES WITH A NEW FLAP MOTOR 	THAT GIVES ELEC CAPABILITY OF MOTOR AND WARNS OF A MOTOR PULLING TOO MUCH AMPERAGE MAY WEAKEN OR BURN THE MOTOR CIRCUITR	Y ON THE PCB.  FAILURE OF THESE COMPONENTS MAY NOT ALLOW PILOT TO RETRACT FLAPS IN-FLIGHT, ETC.	1	L	7	1 	3O				3A15    					 
1999032600176	19990326	00176	CE  	1999	3	26	99ZZZX1041       	1	19990125	G	7810	25540084	CROSSOVER       			CESSNA	182   	TR182       	2072735	CE  										EXHAUST	CRACKED         	B			QC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	7090S	1762 				R18201696				TURBOCHARGED EXHAUST 'Y' HAS CRACK ONE INCH LONG IN THE 'Y' ASSY.  SUBMITTER SUGGESTED THIS AIRCRAFT NEEDS AN AD SIMILAR	 TO THE ONE ON TURBO 210 (CESSNA).					1	H	7	1 	3O				3A13    					 
1999032600177	19990326	00177	CE  	1999	3	26	99ZZZX1042       	1	19990125	G	2140	22540151	HEATER          			CESSNA	182   	TR182       	2072735	CE  										HEAT SYSTEM	CRACKED         	B			QC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	7090S	1762 				R18201696				DURING PRESSURE CHECK OF EXHAUST SYSTEM, FOUND MUFFLER/HEAT TUB TO HAVE 2 CRACKS AROUND THE FINS.  CESSNA RECOMMENDS PRE	SSURE CHECKING THE EXHAUST SYSTEM EVERY 50 HOURS.					1	H	7	1 	3O				3A13    					 
1999032600178	19990326	00178	CE  	1999	3	26	99ZZZX1043       	1	19990203	G	2434	318	ALTERNATOR      	DELTAPROD   		CESSNA	210   	210L        	2073448	CE  										ENGINE	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	777BK	135  			8101874	21060560				FOUND ALTERNATOR CASE HALF BOLTS LOOSE CAUSING AIRCRAFT TO LOSE ELECTRICAL POWER.  SUBMITTER SUSPECTED IMPROPER ASSY AT 	FACTORY.					1	H	7	1 	3O				3A21    					 
1999032600181	19990326	00181	CE  	1999	3	26	99ZZZX1047       	1	19990201	G	2820		LINE            			CESSNA	172   	172N        	2072434	CE  										FUEL SYSTEM	LEAKING         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	23	738EW					17269929				PURCHASED 7-26-96.  FLEW AIRCRAFT TO HOME BASE.  AFER REMOVING ALL INSPECTION PLATES AND COWLING, FOUND ALL THE HOSES ON	 FUEL LINES, OIL LINES, HYDRAULIC LINES NEVER REPLACED.  THEY WERE STILL THE SAME HOSES THAT WERE INSTALLED AT THE FACTO	RY.  THE HOSES ATTACHED TO THE WING FUEL LINES STARTED TO SEEP AND SWEAT FUEL (ORIGINAL).				1	H	7	1 	3O			NT	3A12    					 
1999032600182	19990326	00182	CE  	1999	3	26	99ZZZX1048       	1	19990226	G	5620	51116052	WINDOW          			CESSNA	421   	421C        	2076016	CE  										COCKPIT	CRACKED         	B			UE3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	13	81RD	3437 				421C0291				DURING DISASSEMBLY FOR AIRFRAME REFURBISHMENT, WINDOWS AT LT PILOT SIDE (PN 511160503) AND AT CABIN DOOR, LT MOST AFT, R	T EMERGECY EXIT, RT IMMEDIATELY AFT OF EMERG EXIT, RT TWO MOST AFT WERE FOUND TO HAVE COMPRESSION TYPE 'FLAKING AND CHIP	PING' DAMAGE AND/OR CRACKS RADIATING FROM SCREW HOLES TO EDGE.  ALL HAD BACK-UP RING IN PLACE (EXCEPT PILOT SIDE WINDOW)	.  PRESENCE OF SEALANT IN SOME DAMAGED AREAS SEEMS TO INDICATE SOME DAMAGE DURING INSTALLATION.  SUBMITTER STATED EXTREM	E CARE MUST BE EXERCISED IN THIS INSTALL TO ASSURE HOLES ARE ALIGNED, SIZED, AND SCREWS ARE TORQUED SLOWLY AND EVENLY IN	 SMALL INCREMENTS.	1	L	7	2 	3O				A7CE    					 
1999032600183	19990326	00183	CE  	1999	3	26	99ZZZX1049       	1	19990226	G	5620	51116052	WINDOW          			CESSNA	421   	421C        	2076016	CE  										CABIN	CRACKED         	B			UE3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	13	81RD	1260 				421C0291				DURING AIRFRAME REFURBISHMENT, EMERGENCY EXIT WINDOW WAS FOUND CRACKED AND BROKEN BETWEEN PERIPHERY OF WINDOW AND SCREW 	HOLES AT 6 CONSECUTIVE HOLE LOCATIONS.  RETAINER RING HAD BEEN PREVIOUSLY INSTALLED.  DAMAGE WAS NOT APPARENT UNTIL RING	 WAS REMOVED FOR WINDOW REMOVAL.  EXTREME CARE SHOULD BE EXERCISED IN INSTALLATION TO ASSURE HOLES ARE PROPERLY ALIGNED 	AND SIZED, AND SCREWS ARE TORQUED EVENLY AND SLOWLY IN SMALL INCREMENTS.			1	L	7	2 	3O				A7CE    					 
1999032600184	19990326	00184		1999	3	26	99ZZZX1050       	4	19990223	G	2211	KFC200	COMPUTER        	KING        	K5270A      	BEECH 	33    	F33A        	1151425	CE  										AUTOFLIGHT	MALFUNCTIONED   	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	27	8241K				25251	CE1616				UNIT WAS REPAIRED AND RETURNED TO SERVICE BY A REPAIR STATION WHICH DID NOT POSSESS REQUIRED KTS-151 TEST SET TO PERFORM	 REQUIRED INSPECTIONS PER MANUFACTURER'S MM INSTRUCTIONS.					1	L	7	1 	3O				3A15    					 
1999032600185	19990326	00185	SO  	1999	3	26	99ZZZX1051       	1	19990202	G	3700	J303	CONNECTOR       			PIPER 	PA44  	PA44180     	7104402	SO  										INSTRUMENT PANEL	MISINSTALLED    	B			OG5R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	21	856ND	5371 				4495001				AIRCRAFT BROUGHT IN FOR VACUUM PUMP FAILURE.  BEFORE REPLACEMENT OF PUMP DURING RUN-UP AND OPS CHECK, THE OIL AREA ANNUN	CIATOR WAS INDICATING THE VACUUM SYSTEM AND THE VACUUM ANNUNCIATOR WERE INDICATING THE OIL SYSTEM.  TROUBLESHOOTING DISC	OVERED THE WIRES IN CONNECTOR J303 OF THE ANNUNCIATOR HAD BEEN SWAPPED.  RESEARCH OF MAINTENANCE RECORDS REVEALED NO WOR	K EVEN DONE TO THIS CONNECTOR.			1	L	7	2 	3O				A19S0   					 
1999032600186	19990326	00186	EA  	1999	3	26	99ZZZX1052       	2	19990208	G	7414	1050746Y	GEAR            	BENDIX      		PIPER 	PA28  	PA28140     	7102802	SO  	LYC   	O320  	O320E2A     	41508	EA  					RT MAGNETO	FAILED          	D				O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			NE	05	8776N				7704	2825600	L2504827A			PILOT FOUND RT MAGNETO INOPERATIVE ON PRE-FLIGHT RUN-UP.  INVESTIGATION FOUND MANY TEETH MISSING FROM DISTRIBUTOR GEAR A	ND A BURNED SPOT ON THE DISTRIBUTOR BLOCK.  THE ENGINE HAS 750 HOURS SMOH, BUT NO RECORD OF THE MAGS OR OTHER ACCESSORIE	S BEING DONE.  THE MAG WAS ALSO QUITE OILY INSIDE FROM AN APPARENT LEAKING SEAL.  THE MAGS AND ACCESSORIES SHOULD HAVE B	EEN OVERHAULED ALONG WITH THE ENGINE.			1	L	7	1 	3O	3	O		2A13    	E274				 
1999032600191	19990326	00191	SO  	1999	3	26	99ZZZX1057       	1	19990211	G	5711	6207302	SPAR            		3864308     	PIPER 	PA28  	PA28181     	7102807	SO  										LT/RT WING	WORN            	B			AW4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	11	8496F	4040 				287790254				DURING ANNUAL INSPECTION, FOUND FRETTING AT LEFT AND RIGHT MAIN GEAR LEGS (PN 35644-04 AND PN 35644-05) TO WING LOWER SP	AR CAP ATTACH POINTS.  INSPECTION REVEALED THAT LOWER ATTACH BOLTS (AN4-11A) WERE LOW ON TORQUE AND ATTACH HOLES IN GEAR	 LEGS AND SPAR CAPS WERE ELONGATED ALLOWING RELATIVE MOTION BETWEEN GEAR LEGS AND SPAR CAPS.  CAUSE OF LOW TORQUE NOT DE	TERMINED.  SUBMITTER RECOMMENDED CHECKING TORQUE OF BOLTS ON EACH 100 HR/ANNUAL INSPECTION.			1	L	7	1 	3O				2A13    					 
1999032600192	19990326	00192	SO  	1999	3	26	99ZZZX1058       	1	19990211	G	5711	6207303	SPAR            		3864309     	PIPER 	PA28  	PA28181     	7102807	SO  										LT/RT WING	WORN            	B			AW4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	11	8496F	4040 				287790254				DURING ANNUAL INSPECTION, FOUND FRETTING AT LEFT AND RIGHT MAIN GEAR LEGS (PN 35644-04 AND PN 35644-05) TO WING LOWER SP	AR CAP ATTACH POINTS.  INSPECTION REVEALED THAT LOWER ATTACH BOLTS (AN4-11A) WERE LOW ON TORQUE AND ATTACH HOLES IN GEAR	 LEGS AND SPAR CAPS WERE ELONGATED ALLOWING RELATIVE MOTION BETWEEN GEAR LEGS AND SPAR CAPS.  CAUSE OF LOW TORQUE NOT DE	TERMINED.  SUBMITTER RECOMMENDED CHECKING TORQUE OF BOLTS ON EACH 100 HR/ANNUAL INSPECTION.			1	L	7	1 	3O				2A13    					 
1999032600194	19990326	00194	CE  	1999	3	26	99ZZZX1060       	1	19990217	G	2820	0500106326	LINE            			CESSNA	185   	A185F       	2072821	CE  										FUEL SYSTEM	CHAFED          	B			WWKR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	94237	2081 				18503294				FLAP CABLE CHAFING FUEL LINE 7 INCHES FROM UPPER END.  CABLE RUBBED THROUGH PLASTIC SHIELDING AND .020 INCH DEEP INTO FU	EL LINE.					1	H	7	1 	3O				3A24    					 
1999032600316	19990326	00316	NM  	1999	3	26	99ZZZX1063       	1	19990122	G	5102		FABRIC          			GALAXY	GX8   	GALAXY8     	3760525	NM  										ENVELOPE	WORN            	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	5351U				1068	GLX1068				GORE TAPE ABRADED FABRIC AT GORE TAPE EDGES AT NUMEROUS PANELS THROUGHOUT THE ENTIRE ENVELOPE.  FABRIC PANELS NO LONGER 	MEET MINIMUM STRENGTH REQUIREMENTS WHERE ABRADED.  GORE TAPE MATERIAL AT EDGE IS CAUSING PREMATURE FABRIC WEAR AND DEGRA	DATION.  GORE TAPE MATERIAL SHOULD BE SUCH AS TO NOT WEAR THROUGH ADJACENT FABRIC PANELS.  GORE TAPE:  3.50 INCHES.				1	B	0	0 	3O			RT	A10NM   					 
1999032600317	19990326	00317	CE  	1999	3	26	99ZZZX1064       	1	19990305	G	3097		WIRE            			CESSNA	303   	T303        	2073820	CE  										PROPELLER DEICE	CHAFED          	H		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	03										THE PROBLEM WAS FROM THE HARNESS COVER THAT WAS USED TO PROTECT THE WIRES IN THE SPINNER FROM THE BULKHEAD TO THE DE-ICE	 BOOTS.  THE HARNESS COVER WAS THAT SPLIT LOOM COVER.  WHEN THE PROPS WERE MOVED INTO HIGH PITCH, THE LOOM WOULD BE STRE	TCHED AND THE WIRE WOULD SLIDE OUT CHAFING THE COVERING OFF THE WIRE; AND WHEN THE PROPS WERE MOVED BACK, THE WIRE WOULD	 SLIDE BACK INTO THE LOOM COVERING THE WIRES.  ONCE THE WIRES WERE BARE, THE WIRING WOULD SHORT OUT ON THE INSIDE OF THE	 SPINNER CAUSING THE DE-ICE BREAKER TO TRIP.		1	L	7	2 	3O			 	A34CE   					 
1999032600318	19990326	00318	GL  	1999	3	26	99ZZZX1065       	3	19990125	G	6114	7871300	STOP            			PIPER 	PA44  	PA44180     	7104402	SO  						HARTZL	HCC2Y	HCC2YK1     	GL  	PROPELLER	BROKEN          	H			DF2S	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	9290P	482  				4496019				PLASTIC STOP PLATE ASSY BROKE AT BOTTOM OF PLATE ON EACH SIDE DIRECTLY UNDER LT AND RT PROP CONTROL LEVERS.  THE BROKEN 	PIECES WERE RETAINED BY THE SPRING WHICH IS PART OF THE ASSY.  THESE PIECES PIVOT UP AND OUT WHEN THE PROP LEVERS WERE M	OVED TO FEATHER.  THE PIECE ON THE LEFT WAS THEN DIRECTLY BELOW THE RT THROTTLE LEVER.  THIS MAY BIND THE THROTTLE CONTR	OL OR REDUCE ITS TRAVEL AFT.  POSSIBLE CAUSE OF BREAKAGE IS FATIGUE OF THE HARD PLASTIC PLATE.  THIS AIRCRAFT IS USED IN	-FLIGHT TRAINING AND CONTROLS ARE OFTEN PLACED IN FEATHER.  RECOMMENDATION TO PREVENT RECURRENCE - MANUFACTURE PLATE FRO	M MORE DURABLE MATERIAL OR INCORPORATE A HINGE OR PIVOT WHERE FATIGUE OCCURS.	1	L	7	2 	3O				A19S0   		5	C	P920	 
1999032600323	19990326	00323	SO  	1999	3	26	99ZZZX1070       	2	19990201	G	7414	ES10357174	BREAKER ASSY    	BENDIX      	SGRN25      	BEECH 	35    	K35         	1151524	CE  	CONT  	O470  	IO470C      	17026	SO  					LT ENGINE	DEFECTIVE       	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	05	5340E	330  			1020424	D5842	715379C			DURING PERFORMANCE OF 100-HOUR INSPECTION, LT POSITION MAGNETO, BENDIX (TCM) PN 10-79020-10, RE-MANUFACTURED BY AIRBORNE	 ELECTROSYSTEMS, INC., AND INSTALLED AT ENGINE OVERHAUL BY CRS 764-88 IN MARCH 1984.  TT 1,228.8 BREAKER ASSY PN ES10-35	7174 CHANGED WHEN SUBJECT MAGNETO WOULD NOT HOLD CONSTANT E-GAP, TT OF BREAKER ASSY 330.2 HOURS.  INSPECTION OF ES10-257	174 BREAK DISCLOSED THE CAM FOLLOWER WAS LOOSE ON THE TWO RIVETS ATTACHING IT TO THE SPRING.			1	L	7	1 	3O	3	O		3A15    	E273				 
1999032600324	19990326	00324	CE  	1999	3	26	99ZZZX1071       	1	19990226	G	2434		WIRE            			CESSNA	172   	172R        	2072401	CE  										ALTERNATOR	SEPARATED       	B	P		N3XR	O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			SO	15	403ER	1315 				17280245				LOW VOLTAGE LIGHT CAME ON SEVERAL TIMES DURING FLIGHT.  PERFORMED ENGINE RUN-UP FOR OPERATIONAL CHECK OF ALTERNATOR.  AL	TERNATOR CHECKS OUT GOOD.  UPON FURTHER INSPECTION, THE 'GROUND' ALTERNATOR TERMINALS WERE FOUND BROKEN.  THESE WIRE TER	MINALS APPEAR TO BE TOO THIN AND ARE BREAKING JUST IN FRONT OF THE CRIMP.  THEY DO NOT SEEM TO BE AS HEAVY AS THE EARLIE	R 172 MODELS.  REPLACED WIRE TERMINALS TO ALTERNATOR AND OPERATION CHECK WAS GOOD.			1	H	7	1 	3O			NT	3A12    					 
1999032600325	19990326	00325	EA  	1999	3	26	99ZZZX1072       	2	19990222	G	8530		EXHAUST VALVE   			PIPER 	PA28  	PA28181     	7102807	SO  	LYC   	O360  	O360A4M     	41514	EA  					NR 2 CYLINDER	FAILED          	D				O				OTHER                   				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			EA	25	6124J	3375 	1376 			287690346	L2246736A			ENGINE RAN ROUGH IN-FLIGHT.  CHECKED ENGINE CYLINDER COMPRESSION, FOUND NR 2 CYLINDER HAS NO COMPRESSION.  REMOVED CYLIN	DER AND FOUND BAD EXHAUST VALVE.  INSTALLED AND OVERHAULED CYLINDER.  ENGINE RUN-UP GOOD.					1	L	7	1 	3O	3	O		2A13    	E286				 
1999032600328	19990326	00328	CE  	1999	3	26	99ZZZX1075       	1	19990218	G	3230	MS166241262	RETAINER        			CESSNA	172   	172R        	2072401	CE  										LT MLG	MISSING         	B			HG6S	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	11	722HG	196  				17280402				RETAINER MISSING ON OUTBOARD SIDE OF BUSHING PN 0541202-4 ON LEFT MAIN LANDING GEAR.						1	H	7	1 	3O			NT	3A12    					 
1999032600329	19990326	00329	SO  	1999	3	26	99ZZZX1076       	1	19990305	G	8120	STCSA4731NM	BYPASS PIPE     			PIPER 	PA28  	PA28R201T   	7102813	SO  	CONT  	O360  	TSIO360F    	17025	SO  					TURBOCHARGER	NOT INSTALLED   	G				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	03	6140H	4442 			STCSE4731NM	28R7803089				A TURBO HEAT BLANKET WAS INSTALLED ON 1-28-99.  SUBMITTER STATED DURING THE INSTALLATION OF THE TURBO HEAT BLANKET, THE 	MECHANIC FAILED TO REINSTALL THE EXHAUST BYPASS VALVE PIPE (STC SA4731 NM/STC 4731 NM) THAT DIRECTED EXHAUST GAS OUTBOAR	D OF THE ENGINE.  THE MISSING PIPE ALLOWED EXHAUST GASSES TO BLOW DIRECTLY ONTO THE ELECTRICAL WIRE BUNDLE FOR THE LANDI	NG GEAR SWITCHES.  THE EXTREME HEAT MELTED THE WIRE BUNDLE'S INSTALLATION AND SPARKED A FIRE SENDING SMOKE AND FUMES INT	O THE COCKPIT COMPARTMENT CUTTING ALL ELECTRICAL POWER TO THE LANDING GEAR.		1	L	7	1 	3O	3	O		2A13    	E9CE				 
1999032600331	19990326	00331	CE  	1999	3	26	99ZZZX1078       	1	19990201	G	5311	12116043	FRAME           			CESSNA	206   	U206G       	2073356	CE  										FUSELAGE	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	22306					020606570				RIGHT DOOR POST JAMB HAD A CRACK IN OUTBOARD EDGE OF JAMB THROUGH A SCREW HOLE AND EXTENDING 1 INCH FROM EDGE.						1	H	7	1 	3O				A4CE    					 
1999032600332	19990326	00332	GL  	1999	3	26	99ZZZX1079       	3	19990225	G	6111	90DHB16E	BLADE           			MOONEY	M20   	M20J        	5870219	SW  						MCAULY	2D34C	B2D34C214   	GL  	PROPELLER	SEPARATED       	G				B	A			EMER. DESCENT           	UNSCHED LANDING         			D			INFLIGHT SEPARATION       			NR	NOT REPORTED   	1			SO	15	4671H									PROPELLER BLADE SEPARATED AT APPROXIMATELY 2 INCHES FROM BUTT.  AIRPLANE DAMAGE WAS SUBSTANTIAL.  PILOT MADE A SUCCESSFU	L OFF-AIRPORT LANDING.  NTSB INVESTIGATION UNDERWAY.					1	L	7	1 	3O				2A3     		5	C	P7EA	 
1999032600333	19990326	00333	CE  	1999	3	26	99ZZZX1080       	1	19990226	G	6120	C290D3CT22	PROP GOVERNOR   		A20084      	CESSNA	182   	182R        	2072731	CE  										ENGINE	FAILED          	B			P25R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	05					772070					GOVERNOR WAS REMOVED DUE TO FAILURE TO CONTROL THE PROPELLER.  WHEN IT WAS RECEIVED FOR OVERHAUL, DISASSEMBLED FOR INSPE	CTION, AND FOUND THE FLYWEIGHT ASSY COMPLETELY DESTROYED DUE TO CATASTROPHIC FAILURE.  THERE WERE SHAVINGS OF METAL IN T	HE PUMP BODY.  OWNER WAS CONTACTED.  MCCAULEY SB 214 HAD NOT BEEN C/W.  SUBMITTER STRONGLY RECOMMENDED THAT COMPLIANCE B	E COMPLETED AS SOON AS POSSIBLE.			1	L	7	1 	3O			NT	3A13    					 
1999032600334	19990326	00334	CE  	1999	3	26	99ZZZX1081       	1	19990225	G	3230	AN5158R8	SCREW           		35815155610 	BEECH 	33    	G33         	1151435	CE  										MLG	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	166B	4240 				CD1293				DURING ANNUAL INSPECTION, FOUND 2 OF 4 MAIN GEAR RETRACT BRACE, PIVOT PIN, RETAINER SCREWS, WERE ABLE TO ROTATE.  REMOVE	D AND FOUND THE THREADS WORN FROM THE SHEAR ACTION OF THE PIN.  CORRECTED PROBLEM BY INSTALLING NEW A/N525R-832R8 SCREWS	 WHICH HAVE A SHOULDER PROVIDING HIGHER STRENGTH.				1	L	7	1 	3O				3A15    					 
1999032600335	19990326	00335	CE  	1999	3	26	99ZZZX1082       	1	19990201	G	3260	MS25125E3	SWITCH          			BEECH 	55    	95C55       	1152708	CE  										COCKPIT	MALFUNCTIONED   	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	11	225V					TE123				LANDING GEAR FAILED TO EXTEND.  DURING TROUBLESHOOTING, FOUND SELECTOR SWITCH FAILED.  CLEANED SWITCH AND GEAR OPERATED 	NORMALLY.  INSTALLED NEW SWITCH AND PERFORMED OPERATIONAL CHECK OF LANDING GEAR WITH SATISFACTORY RESULTS.					1	L	7	2 	3O				3A16    					 
1999032600336	19990326	00336	NE  	1999	3	26	99ZZZX1083       	1	19990315	G	3233	180029005	ROD             			CONAER	LA4   	LA4250      	5110320	NE  										MLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	8548U					105				INSPECTED NOSE GEAR ACTUATOR ROD FOR CRACKS AT THE THREADED END.  CRACK DISCOVERED IN THE BOTTOM OF THE THREAD GROOVE BE	LOW THE JAMB NUT SECURING FITTING, PN 2-4420-001.  SEVERAL PREVIOUS ACTUATORS ON OTHER AIRCRAFT REPLACED DUE TO CRACKING	 AND/OR SEPARATION OF THE ACTUATOR AT THIS POINT.				1	H	7	1 	3O				1A13    					 
1999032600337	19990326	00337		1999	3	26	99ZZZX1084       	3	19990301	G	6111	D495	FORK            																	PITCH CHANGE	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					3228NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH D-495 	PITCH CHANGE FORK, SN 3228NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600338	19990326	00338		1999	3	26	99ZZZX1085       	3	19990301	G	6111	D495	FORK            																	PITCH CHANGE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					3468NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 3468NR. THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600339	19990326	00339		1999	3	26	99ZZZX1086       	3	19990301	G	6111	D495	FORK            																	PITCH CHANGE	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					2840NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 2840NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600340	19990326	00340		1999	3	26	99ZZZX1087       	3	19990301	G	6111	D495	FORK            																	PITCH CHANGE	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					2357NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 3230NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600341	19990326	00341		1999	3	26	99ZZZX1088       	3	19990301	G	6111	D495	FORK            																	PITCH CHANGE	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					3069NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 3069NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600342	19990326	00342		1999	3	26	99ZZZX1089       	3	19990301	G	6111	D495	FORK            																	PITCH CHANGE	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					2357NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 2357NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600343	19990326	00343		1999	3	26	99ZZZX1090       	3	19990301	G	6111	D495	FORK            																	PROPELLER	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					1657NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 1657NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING.																		 
1999032600344	19990326	00344		1999	3	26	99ZZZX1091       	3	19990301	G	6111	D495	FORK            																	PROPELLER	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					2139NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 2139NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600345	19990326	00345		1999	3	26	99ZZZX1092       	3	19990301	G	6111	D495	FORK            																	PROPELLER	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					3399NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 3399NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600346	19990326	00346		1999	3	26	99ZZZX1093       	3	19990301	G	6111	D495	FORK            																	PROPELLER	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					3365NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 3365NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600347	19990326	00347		1999	3	26	99ZZZX1094       	3	19990301	G	6111	D495	FORK            																	PROPELLER	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					1104NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 1104NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600348	19990326	00348		1999	3	26	99ZZZX1095       	3	19990301	G	6111	D495	FORK            																	PROPELLER	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					2178NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 2178NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600349	19990326	00349		1999	3	26	99ZZZX1096       	3	19990301	G	6111	D495	FORK            																	PROPELLER	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					2198NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 2198NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600350	19990326	00350		1999	3	26	99ZZZX1097       	3	19990301	G	6111	D495	FORK            																	PROPELLER	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					2359NR					DURING THE OVERHAUL PROCESS, MAGNETIC PARTICLE INSPECTION REVEALED A CRACK IN THE FORK CHANNEL RADIUS OF ONE EACH, D-495	 PITCH CHANGE FORK, SN 2359NR.  THE FORK WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION.																		 
1999032600351	19990326	00351	NE  	1999	3	26	99ZZZX1098       	3	19990225	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			2743 					HJ568		NR 1 AND NR 4 BLADE EROSION SHIELDS DEBONDED.  REPAIRED NR 1 BLADE EROSION SHIELD.  SENT NR 4 BLADE TO HARTZELL FOR REPA	IR.															5	C	P10NE	 
1999032600352	19990326	00352	NE  	1999	3	26	99ZZZX1099       	3	19990225	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			2846 					HJ163A		NR 1 BLADE EROSION SHIELD DEBONDED.  OVERHAULED BLADE NR 1, REPLACED EROSION SHIELD, RE-ASSEMBLED PROPELLER, SET BLADE A	NGLES, STATIC BALANCED, AND LUBRICATED IAW MFG CMM.															5	C	P10NE	 
1999032600353	19990326	00353	NE  	1999	3	26	99ZZZX1100       	3	19990225	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			2088 					HJ437		NR 3 BLADE EROSION SHIELD DEBONDED UNDER DE-ICE BOOT.  DEBOND FOUND WITHIN LIMITS.  REPAIRED DEBOND IAW MFG COMM.																5	C	P10NE	 
1999032600354	19990326	00354	NE  	1999	3	26	99ZZZX1101       	3	19990225	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			2865 					HJ894		BLADES NR 1, NR 2, AND NR 3 EROSION SHIELDS 100 PERCENT DEBONDED UNDER DE-ICE BOOT.  DIS-ASSEMBLED PROPELLER AND CLEANED	.  INSTALLED NEW EROSION SHIELDS AND OVERHAULED BLADES SN'S 3005J, 3007J, AND 3012J IAW MFG CMM.  RE-ASSEMBLED PROPELLER	 AND SET BLADE ANGLES, STATIC BALANCED, AND LUBRICATED.														5	C	P10NE	 
1999032600355	19990326	00355	NE  	1999	3	26	99ZZZX1102       	3	19990225	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			1427 					HJ630		NR 4 BLADE EROSION SHIELD DEBONDED.  DEBONDED FROM BLADE BUTT END TO 4 INCHES OUTBOARD.  REPAIRED AND INSTALLED NEW DE-I	CE BOOT IAW MFG CMM.															5	C	P10NE	 
1999032600356	19990326	00356	NE  	1999	3	26	99ZZZX1103       	3	19990225	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			1139 					HJ275		NR 2 BLADE EROSION SHIELD DEBONDED.  DEBOND IS 1.50 INCHES OUTSIDE OF BOOT ABOUT .50 INCH SQUARE.  REPAIRED IAW MFG CMM.	  NR 3 BLADE EROSION SHIELD DEBONDED.  DEBOND IS IN DE-ICE BOOT AREA FROM BLADE BUTT END TO ABOUT 4 INCHES OUTBOARD.  RE	PAIRED AND INSTALLED NEW DE-ICE BOOT IAW MFG CMM.														5	C	P10NE	 
1999032600357	19990326	00357	NE  	1999	3	26	99ZZZX1104       	3	19990225	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			90   					HJ722		NR 1 BLADE EROSION SHIELD DEBONDED.  DEBOND IS ON CHAMBER SIDE, STARTING AT BLADE BUTT TO OUTBOARD 7 INCHES.  REPAIRED A	ND INSTALLED NEW BOOT IAW MFG CMM.															5	C	P10NE	 
1999032600358	19990326	00358	NE  	1999	3	26	99ZZZX1105       	3	19990225	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			1268 					HJ275		EROSION SHIELD DEBONDED ON BLADE NR 3.  REPAIRED DEBOND.  INSTALLED NEW DE-ICE BOOT IAW MFG COMM.  REPAIRED EROSION SHIE	LD ON NR 2 BLADE OUTSIDE DE-ICE BOOT IAW MFG CMM.															5	C	P10NE	 
1999032600359	19990326	00359	NE  	1999	3	26	99ZZZX1106       	3	19990215	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			1329 					HJ871		EROSION SHIELD DEBONDED ON FACE OF NR 4 BLADE.  REPAIRED EROSION SHIELD DEBOND AT 32 INCH STATION OF FACE OF NR 4 BLADE.	  SET PRELOADS AND ASSEMBLED PROPELLER.  SET BLADE ANGLES IAW MFG CMM.															5	C	P10NE	 
1999032600360	19990326	00360	NE  	1999	3	26	99ZZZX1107       	3	19990225	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			1362 					HJ621		EROSION SHIELD DEBONDED ON BLADE NR 1.  REPAIRED EROSION SHIELD.  REPLACED BOOT IAW MFG CMM.																5	C	P10NE	 
1999032600361	19990326	00361	NE  	1999	3	26	99ZZZX1108       	3	19990225	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			3661 					HJ229		EROSION SHIELD DEBONDED UNDER DE-ICE BOOT ON NR 3 BLADE.  DEBONDED AREA, FOUND WITHIN LIMITS.  REPAIRED EROSION SHIELD A	ND INSTALLED NEW DE-ICE BOOTS IAW MFG CMM.															5	C	P10NE	 
1999032600362	19990326	00362	EA  	1999	3	26	99ZZZX1109       	2	19990212	G	8520		BEARING         			PIPER 	PA28  	PA28180     	7102808	SO  	LYC   	O360  	O360A3A     	41514	EA  					CRANKSHAFT	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	7399W	3450 	1924 			281287	L598236			AIRCRAFT ENGINE LOST OIL PRESSURE. DURING ENGINE INSPECTION, TEAR-DOWN, DETERMINED THAT NR 4 ROD BEARING TURNED (SPUN) I	N THE ROD JOURNEL CREATING EXCESSIVE HEAT.  THE ROD CAME THROUGH THE SIDE OF THE CASE.					1	L	7	1 	3O	3	O		2A13    	E286				 
1999032600363	19990326	00363	EA  	1999	3	26	99ZZZX1110       	2	19990304	G	8520	31M22045	SUPPORT         			CESSNA	172   	172S        	2072439	CE  	LYC   	IO360 	IO360L2A    		EA  					CRANKSHAFT	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP	50   			V68671198	172S8035	L2790951A			NEW CESSNA WITH 50.0 HOURS UNDERGOING FIRST PHASE INSPECTION.  FOUND ENGINE STARTER RING GEAR SUPPORT ASSY, PN 31M22045,	 HAD VISIBLE CRACK ON FRONT FACE.  WHEN REMOVED, AFT SIDE ADJACENT TO CRACK HAD CASTING FLAW.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999032600364	19990326	00364	CE  	1999	3	26	99ZZZX1111       	1	19990304	G	8011	PM2401	STARTER         			CESSNA	172   	172S        	2072439	CE  										ENGINE	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP				80098132	172S8035				NEW CESSNA WITH 54.7 HOURS, STARTER FAILED.  REMOVED LAMAR STARTER, PN PM2401, SN 80098132, THE END CAP WAS REMOVED REVE	ALING TWO MELTED BRUSH TERMINAL LEADS WHERE THEY ATTACH TO THE BRUSHES.  TT ON STARTER 54.7 HOURS.					1	H	7	1 	3O			NT	3A12    					 
1999032600365	19990326	00365	CE  	1999	3	26	99ZZZX1112       	1	19990303	G	3246	C301721	WHEEL           			CESSNA	172   	172M        	2072418	CE  										MLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	6956H				750041	17265661				WHILE REPLACING TIRE, INSPECTED OUTER WHEEL FLANGE FOR CRACKS AND FOUND FLANGE CRACKED AT HUB CAP ATTACH POINTS.  REPLAC	ED OUTER WHEEL FLANGE.					1	H	7	1 	3O			NT	3A12    					 
1999032600367	19990326	00367	CE  	1999	3	26	99ZZZX1114       	1	19990219	G	2820	070014794	LINE            			CESSNA	185   	A185F       	2072821	CE  										COCKPIT	CHAFED          	B			ILIR	K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			WP	07	7239E	2800 				18502642				DURING AN ANNUAL INSPECTION, FUEL FUMES WERE DETECTED UNDER THE INSTRUMENT PANEL, NEAR THE COPILOT RUDDER PEDALS FUEL ST	AINS WERE FOUND ON THE CABIN FLOOR MAT.  INVESTIGATION REVEALED THE FUEL LINE HAD BEEN CHAFED THROUGH BY THE CABIN AIR C	ONTROL CABLE.  SUBMITTER SUGGESTED CLOSE INSPECTION IN THESE HARD TO REACH AND NEGLECTED PLACES.				1	H	7	1 	3O				3A24    					 
1999032600368	19990326	00368	CE  	1999	3	26	99ZZZX1115       	1	19990101	G	2750	C3010020104	MOTOR           			CESSNA	150   	152         	2071835	CE  										TE FLAPS	FAILED          	B			WIWR	O				OTHER                   				F			FLT CONT AFFECTED         			AP	APPROACH       	1			WP	07	69186	10991				15282536				WHILE A STUDENT PILOT WAS PRACTICING TOUCH AND GOES, THE FLAPS FAILED TO GO BEYOND 20 DEGREES.  THE STUDENT CYCLED THE F	LAP LEVER SEVERAL TIMES AND THE FLAPS STAYED AT 20 DEGREES.  THE STUDENT HIT THE RUNWAY NOSE FIRST AFTER FAILING TO FLAR	E THE AIRCRAFT OVER THE RUNWAY AND THEN DEPARTED THE RUNWAY.  MAINTENANCE LATER FOUND THE FLAP MOTOR HAD FAILED.  SUBMIT	TER STATED THE MOTOR GAVE NO INDICATIONS AT ALL OF IMPENDING FAILURE.			1	H	7	1 	3O			NT	3A19    					 
1999032600370	19990326	00370	SO  	1999	3	26	99ZZZX1117       	1	19990130	G	3297		WIRE            			PIPER 	PA28  	PA28R201T   	7102813	SO  										ENGINE BAY	DAMAGED         	G				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			GL	03	6140H	4442 				28R7803089				A FIRE STARTED ON THE RIGHT HAND SIDE OF THE ENGINE COMPARTMENT.  APPROXIMATELY ONE INCH BELOW, A SMALL BUNDLE OF WIRES 	FOR THE NOSE GEAR SWITCHES.  THE INSTALLATION COVERING EACH WIRE WAS EXTREMELY BRITTLE AND CRACKING EXPOSING THE BARE WI	RES.  IT APPEARS A WIRE TOUCHED ANOTHER WIRE IN THE BUNDLE SPARKING A FIRE, BELLOWING SMOKE INTO THE COCKPIT AREA AND CU	TTING THE ELECTRICAL POWER TO THE GEAR DOWN SWITCH.  12-GAUGE WIRE.			1	L	7	1 	3O			 	2A13    					 
1999032600373	19990326	00373	CE  	1999	3	26	99ZZZX1120       	1	19990115	G	2810	C1560010106	FUEL CAP        	WISCOPROD   		CESSNA	210   	T210F       	2073422	CE  										RT/LT FUEL CELLS	LOOSE           	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	01	6726R	5078 				T2100126				PILOT BELIEVED FUEL WAS LOST DUE TO SIPHONING FROM FUEL CAPS.  OBSERVED LIGHT FUEL STAIN BEHIND BOTH CAPS.  O-RINGS APPE	AR TO BE OKAY AND CAPS FEEL TIGHT.  CLEANED STAINS FROM LEFT WING, FLEW AIRCRAFT, OBSERVED NO NEW STAINS.  CAPS BEING RE	PLACED WITH MONARCH CAPS.				1	H	7	1 	3O				3A21    					 
1999032600374	19990326	00374	CE  	1999	3	26	99ZZZX1121       	1	19990216	G	3233	12810013	ACTUATOR        			CESSNA	172   	172RG       	2072438	CE  										RT MLG	LOOSE           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	13	9374B	5245 				172RG0807				WHILE DOING A ROUTINE GEAR RETRACTION, FOUND THE RIGHT MAIN GEAR ACTUATOR LEAKING.  UPON REMOVAL OF THE ACTUATOR, FOUND 	THE THREE ATTACHING BOLTS WERE LOOSE IN THE HOLES.  THE HOLE WEAR VARIED FROM .002 INCH TO .004 INCH BIGGER THAN THE NEW	 BOLTS.				1	H	7	1 	3O				3A17    					 
1999032600670	19990326	00670	EA  	1999	3	26	99ZZZX1123       	1	19990215	G	3246	50105711	WHEEL           			CNDAIR	CL600 	CL6002B19   		EA  										MLG	CRACKED         	B	P		CK4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					0987					DURING LIQUID PENETRANT INSPECTION IAW AIRCRAFT BRAKING SYTEMS NON-DESTRUCTIVE TESTING MANUAL, AP-736, CHAPTER 32-42-07,	 A 3 INCH CRACK WAS FOUND RUNNING PERPENDICULAR TO THE WHEEL SPOKE.  DEPTH OF CRACK IS UNKNOWN, BUT VISUAL INSPECTION WI	LL REVEAL CRACK WITHOUT ANY USE OF MAGNIFICATION DEVICES OR PENETRANT DYE.  CAUSE IS UNKNOWN AND UNIT HAS BEEN RETURNED 	TO CUSTOMER FOR FURTHER EVALUATION.			2	L	7	2 	4F			RT	A21EA   					 
1999032600671	19990326	00671	NE  	1999	3	26	99ZZZX1124       	2	19990211	G	7210	758300	GEARBOX         								PWA   	JT8   	JT8D217A    	52053	NE  					ENGINE	FAILED          	B			RA1R	E				ENGINE SHUTDOWN         				O			OTHER                     			NR	NOT REPORTED   	1			SW	05			9586 		RP9175		P709778			ENGINE WAS REMOVED FOR IN-FLIGHT SHUT DOWN DUE TO OIL LOSS AND GEARBOX FAILURE.  GEARBOX TOWERSHAFT BEARINGS HAD FAILED 	AND BEVEL GEAR MATERIAL LIBERATED THROUGH FRONT LOWER HOUSING.  FAILURE INVESTIGATION IS IN PROGRESS AT GEES DALLAS AND 	GE ARTEX.									4	F			E9NE				 
1999032600672	19990326	00672	NE  	1999	3	26	99ZZZX1125       	2	19990302	G	7313	775723	SEAL            		809892      						PWA   	JT8   	JT8*        	52044	NE  					FUEL NOZZLE	FAILED          	B			TU5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03					US1557					THE SUBJECT ASSY WAS OBSERVED TO HAVE BURN-THROUGH OF THE NOZZLE NUT DURING ENGINE BORESCOPE INSPECTIONS BY THE OWNER/OP	ERATOR, ALOHA AIRLINES.  THE ASSY WAS REMOVED FROM THE ENGINE AND RETURNED TO WOOD GROUP FUEL SYSTEMS, INC., FOR INVESTI	GATION OF THE REPORTED CONDITION.  UPON RECEIPT, THE ASSY WAS PRESSURE TESTED IAW THE P & W CMM AND OBSERVED TO HAVE EXT	ERNAL LEAKAGE.  TEAR-DOWN INSPECTIONS AND METALLURGICAL EVALUATION REVEALED CRACKS IN THE SEAL.  ALL FUEL NOZZLE AND SUP	PORT ASSY HARDWARE HAS BEEN FORWARDED TO P & W FOR CONTINUED EVALUATION.							4	F			E2EA				 
1999032600673	19990326	00673	SW  	1999	3	26	99ZZZX1126       	1	19990210	G	2730	443373	HORN            			GULSTM	112   	112A        	7630302	SW  										ELEVATOR	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	1420J					420				DURING ANNUAL INSPECTION, FOUND LT AND RT ELEVATOR TRIM TAB TO HORN FAYING SURFACE/CORRODED.  HORN PN 44337-3 FAYING SUR	FACES EXHIBIT LEVEL 1 CORROSION (RUST).  DUE TO SURFACE CONDITION, UNABLE TO ESTABLISH IF FAYING SURFACES TREATED/PRIMED	/COATED PRIOR TO INSTALLATION.  TRIM TAB PN 44020-9 AND DASH 10 FAYING SURFACES EXHIBIT LEVEL 2 CORROSION.  ESTABLISHED 	FROM SMALL UNCORRODED AREA, NO SURFACE PREPARATION WAS CARRIED OUT PRIOR TO ASSY.  UNCOATED DISSIMILAR METALS AND MODULE	 INGRESS IS FACTOR.  CONSIDERING FLEET AGE (20 PLUS YEARS), SUBMITTER SUGGESTED ONE-TIME INSPECTION FOR PROPER SURFACE P	REPARATION AND POTENTIAL CORROSION CLEAN-UP.	1	L	7	1 	3O				A12SO   					 
1999032600674	19990326	00674		1999	3	26	99ZZZX1127       	4	19990125	G	2370	9806005055	CVR             			DHAV  	DHC7  	DHC7102     	2802708	EA  										COCKPIT	FAILED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	177RA	7200 	20   		7259	85				CVR WAS SENT OUT FOR A READ-OUT AND RE-CERTIFICATION.  ALLIED SIGNAL INFORMED THAT THE TAPE DID NOT RECORD, THEY SAID TH	AT THIS PART NUMBERED CVR IS KNOWN TO FAIL.					2	H	7	4 	4T				A20EA   					 
1999032600675	19990326	00675	WP  	1999	3	26	99ZZZX1128       	2	19990302	G	7200		ENGINE          			SWRNGN	SA227 	SA227TT     		SW  	GARRTT	TPE331	TPE33110    	01514	WP  					RIGHT	SEIZED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	17	227TT					TT444	P35175C			A FUNCTIONAL CHECK FLIGHT WAS CONDUCTED WHICH CONSISTED OF 0.5 HOURS AND 1 CYCLE.  THE NORMAL COOL DOWN PERIOD WAS ACCOM	PLISHED, AFTER AN UNEVENTFUL FLIGHT AND SHUT DOWN WERE COMPLETED.  THE NEXT MORNING, A PRE-FLIGHT WAS CONDUCTED AND FOUN	D THE RT PROPELLER WOULD NOT TURN AND DETERMINED THE ENGINE HAD SEIZED.  THIS ENGINE HAS 594.2 HOURS SINCE OVERHAUL BY T	HE TURBINE GROUP IN FLORIDA.  THE ENGINE WAS REMOVED AND IS AT THE TURBINE GROUP FOR REPAIRS.  THE OPERATOR HAS CONTRACT	ED A THIRD PARTY AS AN OBSERVER FOR DISASSEMBLY AND REPAIRS.  TEAR DOWN INFORMATION WILL BE PROVIDED AFTER REPAIRS COMPL	ETED.	2	L	7	2 	4T	4	T	RT	A5SW    	E4WE				 
1999032600676	19990326	00676	CE  	1999	3	26	99ZZZX1129       	1	19990209	G	2750	2307024392	TUBE            			LEAR  	60    	60LEAR      	5170707	CE  										LT WING	CHAFED          	B			TJ4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	11	230FX	239  				138				LOST HYDRAULIC PRESSURE IN-FLIGHT.  NOTED LEFT FLAP ACTUATOR HYDRAULIC RETRACT TUBE ASSY WAS CHAFED THROUGH TO A PIN HOL	E AT THE FLAP ACTUATOR BELLCRANK.   CAUSED BY THE ACTUATOR PISTON ROD ATTACH BOLT WASHER CONTACTING THE TUBE WHEN THE FL	APS WERE CYCLED UP AND DOWN.				2	L	7	2 	4F			RT	A10CE   					 
1999032600677	19990326	00677	GL  	1999	3	26	99ZZZX1130       	3	19990303	G	6111		BOLTS           			BEECH 	200   	200BEECH    	1152920	CE  						HARTZL	HCB3T	HCB3TN3     	GL  	COUNTERWEIGHT	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	11	24SX		342  			BB455		BU11312		FOUND DURING PHASE INSPECTION.  COUNTERWEIGHT BOLTS FAILING DUE TO CORROSION.  PROPELLER HAS 324 HOURS TSOH.						1	L	7	2 	4T				A24CE   		6	C	P15EA	 
1999032600678	19990326	00678		1999	3	26	99ZZZX1131       	4	19990211	G	2350	9901081004	AUDIO PANEL     			ISRAEL	1125  	ASTRASPX    	4500205	EU  										COCKPIT	INOPERATIVE     	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	273RA	230  			9801001	097				SPEAKER BUTTON WOULD NOT ENGAGE.  REPLACED ENTIRE AUDIO PANEL.						2	L	7	2 	4F			RT	A16NM   					 
1999032600679	19990326	00679	EU  	1999	3	26	99ZZZX1132       	1	19990211	G	7732	10615N01K01	INDICATOR       			ISRAEL	1125  	ASTRASPX    	4500205	EU  										COCKPIT	STICKS          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	273RA		69   		B119	097				NEEDLES STICK/HANG-UP DURING TEST (LEFT AND RIGHT).  REPLACED GAUGE.						2	L	7	2 	4F			RT	A16NM   					 
1999032600682	19990326	00682	CE  	1999	3	26	99ZZZX1135       	1	19990224	G	2130	99120789	VALVE           			CESSNA	500   	550         	2076604	CE  										ACM	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	26496					550607				NEW FLAPPER TYPE CHECK VALVE WAS INSTALLED AND AIRCRAFT WAS PRESSURIZED WITH TEST UNIT.  EXCESSIVE CABIN LEAK RATE WAS T	RACED TO FAILED CHECK VALVE.  THE RUBBER LINER STARTED COMING LOOSE FROM THE FLAPPER PART OF THE VALVE AND FOLDED PREVEN	TING IT FROM CLOSING OFF PROPERLY.  IT APPEARS THE ADHESIVE IS BREAKING DOWN EVEN THOUGH THE VALVE IS ONLY ABOUT ONE MON	TH OLD.  SUBMITTER STATED THIS IS THE SECOND VALVE TO HAVE THIS PROBLEM AT THIS LOCATION.  THE OTHER VALVE WAS NOT NEW.			1	L	7	2 	4F				A22CE   					 
1999032600685	19990326	00685	CE  	1999	3	26	99ZZZX1138       	1	19990128	G	3710	442CW	PUMP            	AIRBORNE    		BEECH 	60    	B60         	1153605	CE  										LT ENGINE	MALFUNCTIONED   	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	03	30MM	403  			8AE861	D507				LEFT ENGINE VACUUM PUMP EXHIBITED LOW PRESSURE INDICATION.  REMOVED PUMP.  FOUND SHAFT HARD TO ROTATE.  IT DID NOT SHEAR	 AS EXPECTED.  REPLACED PUMP.					1	L	7	2 	3O				A12CE   					 
1999032600686	19990326	00686	CE  	1999	3	26	99ZZZX1139       	1	19990226	G	5610	10138402517	WINDSHIELD      			BEECH 	300   	300BEECH    	1152930	CE  										COCKPIT	CRACKED         	G				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	09	300TJ	564  			95219H2944	FA13				PILOT'S WINDSHIELD INNER PANE SUSTAINED SEVERE CRACKING AT FL 330.  PILOT REPORTED CABIN DIFFERENCE OF 6.5 PSI AND OAT O	F MINUS 41 DEGREES CELSIUS AT THE TIME OF THE WINDSHIELD FAILURE.  PILOT STATED WINDSHIELD HEAT HAD BEEN ON FOR APPROXIM	ATELY 1.5 HOURS.  PILOT ALSO REPORTED PARTICLES OF THE WINDSHIELD HAD BEGUN DROPPING ONTO THE GLARE SHIELD PRIOR TO LAND	ING.  POSSIBLE CAUSE UNKNOWN.  RECOMMENDATION:  NONE AT THIS TIME.  WINDSHIELD INSTALLED:  MAY 1996.			2	L	7	2 	4T				A24CE   					 
1999032600687	19990326	00687	NE  	1999	3	26	99ZZZX1140       	2	19990212	G	7314	5009986	FUEL PUMP       			DORNER	DO32  	DO328100    	2996000	NM  	PWA   	119   	PW119C      		NE  					LT ENGINE	FAILED          	B			VH2R	O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			AP	APPROACH       	1			SW	17	337PH				2597	3020	116029			PILOT REPORTED ON 10 MILE FINAL AT 3,000 FEET MSL, THE LEFT ENGINE ROLLED BACK WITH THE POWER LEVER PULLED BACK TO FLIGH	T IDLE.  REPLACED LT HMU AND FUEL PUMP WITH SERVICABLE, CONTINUED TIME HMU AND FUEL PUMP.  ENGINE TSN:  8,473.6 HOURS, C	SN:  9,993.				2	H	7	2 	4T	4	T	RT	A45NM   	E20NE				 
1999032600688	19990326	00688	NE  	1999	3	26	99ZZZX1141       	2	19990212	G	7320	8110993	HMU             			DORNER	DO32  	DO328100    	2996000	NM  	PWA   	119   	PW119C      		NE  					LT ENGINE	FAILED          	B			VH2R	O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			AP	APPROACH       	1			SW	17	337PH				F22409	3020	116029			PILOT REPORTED ON 10 MILE FINAL AT 3,000 FEET MSL, THE LEFT ENGINE ROLLED BACK WITH THE POWER LEVER PULLED BACK TO FLIGH	T IDLE.  REPLACED LT HMU AND FUEL PUMP WITH SERVICABLE, CONTINUED TIME HMU AND FUEL PUMP.  ENGINE TSN:  8,473.6 HOURS, C	SN:  9,993.				2	H	7	2 	4T	4	T	RT	A45NM   	E20NE				 
1999032600689	19990326	00689	WP  	1999	3	26	99ZZZX1142       	2	19990305	G	7261	30752071	OIL TANK        			BRAERO	DH125 	BAE125800A  	1500285	EU  	GARRTT	TFE731	TFE7315R    	01518	WP  					LT ENGINE	DAMAGED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	317CC					258093	P91294			AIRCRAFT TT:  4,375 HOURS.  LANDINGS:  3,197.  NORMAL PROCEDURES FOR REMOVING THE ALTERNATOR DID NOT WORK AS THE 0IL TAN	K HAD A BOW AT THE BOTTOM.  THE TOP PART OF THE TANK HAD NORMAL CLEARANCES.  AT THE TOP, THE NORMAL CLEARANCE IS THREE-F	OURTHS OF AN INCH.  THIS CLEARANCE IS NORMAL BY THE ALTERNATOR MOUNT TO ALLOW THE CLAMP WHICH HAS A MEASUREMENT OF .3125	 INCH TO BE EASILY REMOVED FOR REMOVAL AND INSTALLATION OF THE ALTERNATOR.			2	L	7	2 	4F	4	F	RT	A3EU    	E6WE				 
1999032600695	19990326	00695	NE  	1999	3	26	99ZZZX1148       	3	19990308	G	6114	A4959	BUSHING         			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	HUB	LOOSE           	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		1883 						HL271		PROPELLER S/N HL271 WAS RETURNED FOR VIBRATION AND COMPLIANCE OF SB'S HD-SB-61-005, 014 AND 020.  AFTER DISASSEMBLY, INS	PECTION REVEALED THE A-4959 VESPEL BUSHING HAD COME LOOSE FROM THE PITCH CHANGE ROD BORE SEAT IN THE ENGINE SIDE HALF OF	 THE HUB.  THE BUSHING WAS NOT DAMAGED, BUT WAS REMOVED WITH THE HYDRAULIC UNIT.				2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999032600696	19990326	00696	NE  	1999	3	26	99ZZZX1149       	3	19990308	G	6111	B60772	CAM FOLLOWER    			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05								HL271		PROPELLER S/N HL271 RETURNED FOR VIBRATION AND COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020.  INITIAL INSPECTION REVEAL	ED BLADE S/N 984C TO BE OUT OF ANGLE TOLERANCE.  AFTER DISASSEMBLY, INSPECTION REVEALED WEAR ON THE B-6077-2 CAM FOLLOWE	R INSIDE DIAMETER, AS INSTALLED ON BLADE S/N 984C, TO BE BEYOND ALLOWABLE TOLERANCE.  THE CAM FOLLOWER WAS RETIRED FROM 	SERVICE AND SENT TO HARTZELL ENGINEERING FOR EVALUATION.			2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999032600697	19990326	00697	NE  	1999	3	26	99ZZZX1150       	3	19990308	G	6111	D62772	BRACKET         			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		7239 	1384 		S164			HL112		PROPELLER S/N HL112 WAS RETURNED FOR COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020.  AFTER DISASSEMBLY, INSPECTION REVEA	LED PITCH CHANGE BRACKET S/N S164 TO BE WORN AT THE CAM FOLLOWER SUPPORT AREA BEYOND ALLOWABLE LIMITS.  THE BRACKET WAS 	RETURNED TO HARTZELL ENGINEERING FOR EVALUATION.				2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999032600698	19990326	00698	NE  	1999	3	26	99ZZZX1151       	3	19990308	G	6111	A6404	SPRING          			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05								HL140		AFTER DISASSEMBLY, INSPECTION REVEALED THE A-6404 SPRING BROKEN INTO 2 PIECES.  THE SPRING WAS RETIRED FROM SERVICE.						2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999032600699	19990326	00699	NE  	1999	3	26	99ZZZX1152       	3	19990308	G	6111	B60772	CAM FOLLOWER    			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05								HL268		DURING THE OVERHAUL PROCESS OF 6 EACH B-6077-2 CAM FOLLOWERS, INSPECTION REVEALED THE INSIDE DIAMETER TO BE WORN BEYOND 	ALLOWABLE LIMITS.  THE CAM FOLLOWERS WERE RETIRED FROM SERVICE.					2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999032600700	19990326	00700	NE  	1999	3	26	99ZZZX1153       	3	19990308	G	6111	D51105	FORK            			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		6880 	1384 		S9			HL112		PROPELLER S/N HL112 WAS RETURNED FOR COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020. AFTER DISASSEMBLY, INSPECTION REVEAL	ED PITCH CHANGE FORK S/N S9 WAS WORN, AT THE CAM FOLLOWER FORK SLOTS, BEYOND ALLOWABLE LIMITS.  THE FORK WAS RETURNED TO	 HARTZELL ENGINEERING FOR EVALUATION.				2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999032600701	19990326	00701	NE  	1999	3	26	99ZZZX1154       	3	19990308	G	6111	B60771	CAM FOLLOWER    			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05								HL112		PRPELLER S/N HL112 WAS RETURNED FOR COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020.  AFTER DISASSEMBLY, INSPECTION REVEAL	ED ONE EACH B-6077-1 CAM FOLLOWER INSIDE DIAMETER TO BE WORN BEYOND ALLOWABLE LIMITS.  THE CAM FOLLOWER WAS RETURNED TO 	HARTZELL ENGINEERING FOR EVALUATION.				2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999032600702	19990326	00702	NE  	1999	3	26	99ZZZX1155       	3	19990308	G	6111	D51105	FORK            			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		5810 			S140			HL268		DURING THE OVERHAUL PROCESS OF THE D-5110-5 FORK S/N S140, INSPECTION REVEALED THE CAM FOLLOWER FORK SLOTS WORN BEYOND A	LLOWABLE LIMITS.  THE FORK WAS RETIRED FROM SERVICE.					2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999032600703	19990326	00703	NE  	1999	3	26	99ZZZX1156       	3	19990308	G	6111	D51105	FORK            			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		4391 	1989 		S78			HL140		INSPECTION REVEALED 4 PITCH CHANGE FORK SLOTS WORN BEYOND ALLOWABLE LIMITS.  THE FORK WAS RETIRED FROM SERVICE.						2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999032600704	19990326	00704	NE  	1999	3	26	99ZZZX1157       	3	19990308	G	6111	D51105	FORK            			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	DAMAGED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					S223			HL271		PROPELLER S/N HL271 WAS RETURNED FOR COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020.  AFTER DISASSEMBLY, INSPECTION REVEA	LED SCORING LINES THROUGH THE CHROME PLATING OF THE D-5630 PITCH CHANGE ROD AS INSTALLED IN THE D-5990-1 HYDRAULIC UNIT 	S/N S223.  THE HYDRAULIC UNIT WAS RETURNED TO HARTZELL PROPELLER FOR REPAIR.				2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999032600705	19990326	00705	NE  	1999	3	26	99ZZZX1158       	3	19990308	G	6111	D62772	BRACKET         			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		1883 			S34			HL271		PROPELLER S/N HL271 WAS RETURNED FOR VIBRATION AND COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020.  INITIAL INSPECTION RE	VEALED BLADE S/N 984C TO BE OUT OF ANGLE TOLERANCE.  AFTER DISASSEMBLY, INSPECTION REVEALED WEAR ON THE CAM FOLLOWER SUP	PORT AREA OF THE D-6277-(2) PITCH CHANGE BRACKET, S/N S34, AS INSTALLED ON BLADE S/N 984C, TO BE BEYOND ALLOWABLE LIMITS	.  THE PITCH CHANGE BRACKET WAS RETIRED FROM SERVICE AND SENT TO HARTZELL ENGINEERING FOR EVALUATION.			2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999032600706	19990326	00706	NE  	1999	3	26	99ZZZX1159       	3	19990308	G	6111	D51105	FORK            			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		1883 			S335			HL271		PROPELLER S/N HL271 WAS RETURNED FOR VIBRATION AND COMPLIANCE OF SB'S HD-SB-61-005, 014, AND 020.  INITIAL INSPECTION RE	VEALED BLADE S/N 984C TO BE OUT OF ANGLE TOLERANCE.  AFTER DISASSEMBLY, INSPECTION REVEALED THE CAM FOLLOWER FORK SLOT O	F THE D-5110-5 FORK, S/N S335 AS INSTALLED ON BLADE S/N 984C TO BE WORN BEYOND ALLOWABLE LIMITS.  THE FORK WAS RETIRED F	ROM SERVICE AND RETURNED TO HARTZELL ENGINEERING FOR EVALUATION.			2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999032600707	19990326	00707	SO  	1999	3	26	99ZZZX1160       	1	19990118	G	5513	635672	BALANCE WEIGHT  			PIPER 	PA28  	PA28160     	7102806	SO  										STABILATOR	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	5487W	3328 				28571				DURING INSPECTION OF BALANCE WEIGHT TUBE PER AD NR 70-26-04, TUBE MOUNT ON STABILATOR FOUND CRACKED AT BOLT HOLES.  FUSE	LAGE DOES NOT HAVE ACCESS PANEL FORWARD OF STABILATOR INSTALLED.  PULLING BALANCE WEIGHT TUBE MUST BE DONE THROUGH TAILC	ONE REMOVING TUBE STRESSED MOUNTS POSSIBLY CAUSING CRACKS.  TUBE LUBRICATED BEFORE RE-ASSEMBLY FOR EASIER REMOVAL AT NEX	T INSPECTION.  TUBE MOUNT REPLACED WITH NEW.			1	L	7	1 	3O				2A13    					 
1999032600708	19990326	00708	SO  	1999	3	26	99ZZZX1161       	1	19990103	G	3260		SWITCH          			GULSTM	G1159 	G1159       	3953505	SO  										NLG	MALFUNCTIONED   	E				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			GL	03	555RS					3				NOSE GEAR DOWN AND LOCKED INDICATION WAS INOPERATIVE.  EMERGENCY DECLARED AND DIVERTED TO ORD.  LANDING GEAR WAS BACKED 	UP WITH NITROGEN AND AIRCRAFT LANDING WITHOUT INCIDENT.  INDICATION LIGHT CAME ON DURING TAXI.  POSSIBLE FROZEN DOWNLOCK	 SWITCH.				2	L	7	2 	4F			RT	A12EA   					 
1999040200047	19990402	00047	NE  	1999	4	2	99ZZZX1163       	2	19990117	G	7230		BEARING         			BOEING	747   	747283B     	1384867	NM  	PWA   	JT9   	JT9D7Q      	52054	NE  					NR 3	FAILED          	B	P		WA2D	E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			M	J		OVER TEMP                 	WARNING INDICATION        		NR	NOT REPORTED   	1			NE	03	622FF					22496	P702391			ENGINE IN-FLIGHT SHUTDOWN AND REMOVAL 1-17-99 DUE VIBRATION/FIRE WARNING.  DISASSEMBLY INSPECTION DISCLOSED EXTENSIVE FI	RE DAMAGE SEEMING TO ORIGINATE IN THE NR 3 BEARING AREA WITH EXTENSIVE SECONDARY DAMAGE. FAILED MATERIAL WILL BE FORWARD	ED TO PRATT & WHITNEY FOR ANALYSIS. ENGINE TT:  42,303:27 HOURS.  TC:  8,690.				2	L	7	4 	4F	4	F		A20WE   	E3NE				 
1999040200048	19990402	00048	CE  	1999	4	2	99ZZZX1164       	1	19990224	G	2435	23085004	GENERATOR       			CESSNA	500   	560CESSNA   	2076750	CE  										START/GENERATOR	FAILED          	G	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	25	7FE					5600063				FAN END BEARING IN THE NR 1 ENGINE STARTER/GENERATOR FAILED CAUSING THE FAN TO MAKE CONTACT WITH END HOUSING WHICH CAUSE	D A SUBSEQUENT VIBRATION IN THE NR 1 ENGINE.  THE GENERATOR CONTINUED TO SUPPLY POWER.  THE COMPONENT WAS REPLACED.					2	L	7	2 	4F			RT	A22CE   					 
1999040200052	19990402	00052	WP  	1999	4	2	99ZZZX1168       	2	19990121	G	7260	30721192	VALVE           			LEAR  	35    	35A         	5170602	CE  	GARRTT	TFE731	TFE7312     	01518	WP  					GEARBOX	INOPERATIVE     	G				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			GL	03	802JW					453	P89242			PILOT REPORTED SMOKE IN CABIN.  AIRCRAFT RETURNED TO ITS STARTING POINT (ORF).  PROBLEM ISOLATED TO GEARBOX BREATHER VAL	VE STUCK CLOSED.  UNIT REPLACED AND OPERATIONAL CHECK GOOD.					2	L	7	2 	4F	4	F		A10CE   	E6WE				 
1999040200053	19990402	00053	CE  	1999	4	2	99ZZZX1169       	1	19990204	G	2731	NAS312160283	CONTROL CABLE   	COLLINS     		BEECH 	B300  	B300        	1159232	CE  										ELEVATOR TRIM	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03	898MC	91   			9102	FL216				ELEVATOR TRIM SERVO CABLE BROKE IN-FLIGHT AT 6,000 FEET ALTITUDE.  POSSIBLY CABLE OR DRUM HAD FLAW OR WAS DAMAGED AT INS	TALLATION.  COMPONENT P/N 5MT65622-5735-002.					2	L	7	2 	4T			RT	A24CE   					 
1999040200054	19990402	00054	WP  	1999	4	2	99ZZZX1170       	2	19990215	G	7230	30733941	IMPELLER        		723010      	LEAR  	35    	35A         	5170602	CE  	GARRTT	TFE731	TFE73122B   	01518	WP  					COMPRESSOR	CRACKED         	B			IY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	97AN	4056 			9233651799	373	P74960			DURING ROUTINE CZI (COMPRESSOR ZONE INSPECTION), HIGH PRESSURE COMPRESSOR IMPELLER WAS SENT TO ALLIED SIGNAL FOR EDDY CU	RRENT INSPECTION OF SEAL RELIEF/BORE AREA PER ALERT SB A72-3641.  SUBSURFACE DISCONTINUITY WAS REVEALED BY THE INSPECTIO	N.  PART IS SCRAP.  SERVICE LIFE OF THIS PART IS 10,000 CYCLES.  AT THE TIME OF INSPECTION, 3,133 CYCLES HAD ACCRUED.  R	E:  WO NR GR2327.			2	L	7	2 	4F	4	F		A10CE   	E6WE				 
1999040200055	19990402	00055	CE  	1999	4	2	99ZZZX1171       	1	19990201	G	5620		WINDOW          			BEECH 	90    	C90         	1152913	CE  										CABIN	BROKEN          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	11	99CD					LJ601				NR 1 LEFT PASSENGER WINDOW BROKE AND BLEW OUT.  POLORIZER STAYED IN PLACE.						1	L	7	2 	3T				3A20    					 
1999040200057	19990402	00057	SO  	1999	4	2	99ZZZX1173       	2	19990226	G	7414	56RN1225	MAGNETO         			BEECH 	36    	A36         	1151604	CE  	CONT  	O520  	IO520B      	17032	SO  					ENGINE	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	10	1810L	816  				E834				WATER INTRUSION INTO MAGNETO CAUSING COMPLETE FAILURE; THIRD SIMILAR OCCURRENCE ON THE 1,200 SERIES MAG IN 20 MONTHS.  A	LL HAVE BEEN ON CONT IO520 ENGINES FRONT MOUNTED MAGS.  RECOMMEND DISCONTINUE USE OF THIS MAG ON LARGE CONT ENGINES I.E.	, 470, 520, 550 AIRCRAFT WITH SIMILAR FAILURES C-207A, C414A.				1	L	7	1 	3O	3	O		3A15    	E5CE				 
1999040200059	19990402	00059	NE  	1999	4	2	99ZZZX1175       	3	19990304	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01								HJ211		EROSION SHIELD ON BLADE NR 1 DEBONDED.  DISASSEMBLED AND CLEANED PROPELLER, INSTALLED NEW EROSION SHIELD, AND OVERHAULED	 BLADE NR 1.															5	C	P10NE	 
1999040200060	19990402	00060	NE  	1999	4	2	99ZZZX1176       	3	19990304	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			1399 					HJ621		EROSION SHIELD DEBONDED ON BLADE NR 3.  REPAIRED DEBOND, .50 INCH BY 3 INCHES, AT BASE OF EROSION SHIELD.  REPAIRED IAW 	MFG CMM.															5	C	P10NE	 
1999040200061	19990402	00061	NE  	1999	4	2	99ZZZX1177       	3	19990304	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			1771 					HJ183A		EROSION SHIELD ON NR 4 BLADE DEBONDED.  REPAIRED EROSION SHIELD DEBOND IN BOOT AREA.  REPLACED DE-ICE BOOT IAW MFG CMM.																5	C	P10NE	 
1999040200062	19990402	00062	NE  	1999	4	2	99ZZZX1178       	3	19990304	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			2005 					HJ941		EROSION SHIELD DEBONDED UNDER DE-ICE BOOT ON BLADE NR 4.  REPAIRED DEBOND AND INSTALLED NEW DE-ICE BOOT IAW MFG CMM.																5	C	P10NE	 
1999040200063	19990402	00063	NE  	1999	4	2	99ZZZX1179       	3	19990304	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			2312 					HJ536		EROSION SHIELD DEBONDED UNDER DE-ICE BOOT ON BLADE NR 1.  REPAIRED DEBOND, .50 INCH BY 2 INCHES AND .50 INCH BY 1 INCH, 	AT BASE OF EROSION SHIELD.  REPAIRED IAW MFG CMM.															5	C	P10NE	 
1999040200064	19990402	00064		1999	4	2	99ZZZX1180       	2	19990216	G	7314	5006050	COUPLING        																	FUEL PUMP	CRACKED         	B	P		XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01										REJECTED BY MAGNETIC PARTICLE INSPECTION ON P. O. FROM ONTIC ENG & MFG, INC. NR 121780.  FATIGUE CRACK.																			 
1999040200065	19990402	00065		1999	4	2	99ZZZX1181       	2	19990222	G	8520	59284	CRANKSHAFT      																	ENGINE	CRACKED         	B	P		XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01					PT59282					DETECTED FATIGUE CRACKS IN MAGNETIC PARTICLE INSPECTION.  INSPECTED ON R & B AIRCRAFT SUPPLY CO, P.O. NR 1276.																			 
1999040200066	19990402	00066		1999	4	2	99ZZZX1182       	1	19990218	G	3222	800905109	STRUT           																	NLT	CRACKED         	B	P		XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01										NOSE LANDING GEAR STRUT CRACKED.  FATIGUE CRACK.  DETECTED BY PENETRANT INSPECTION ON P.O. NR 25952 FROM PACIFIC SKY SUP	PLY, INC.																		 
1999040200067	19990402	00067		1999	4	2	99ZZZX1183       	1	19990216	G	7920	021578101	COVER           																	FILTER	CRACKED         	B	P		XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01										DETECTED IN MAGNETIC PARTICLE ON P.O NR 121780 FROM ONTIC ENG & MFG, INC.  COVER CRACKED ON OIL FILTER.																			 
1999040200068	19990402	00068	GL  	1999	4	2	99ZZZX1184       	3	19990308	G	6114	840139	HUB             													HARTZL	HCB4M	HCB4M       	GL  	PROPELLER ASSY	SCRAP           	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		2601 						EAA1130		HUB S/N'S EAA1130 AND EAA1149 WERE RETURNED FOR OVERHAUL.  AFTER REMOVAL OF THE HUB PILOT TUBES, INSPECTION REVEALED UNR	EPAIRABLE CORROSION ON THE INSIDE DIAMETER OF THE PILOT TUBE BORES.  THE HUBS WERE RETIRED FROM SERVICE AND SENT TO HART	ZELL ENGINEERING FOR EVALUATION.														6	C	P56GL	 
1999040200069	19990402	00069	GL  	1999	4	2	99ZZZX1185       	3	19990308	G	6114	840139	HUB             													HARTZL	HCB4M	HCB4M       	GL  	PROPELLER ASSY	SCRAP           	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		2601 						EAA1149		HUB S/N'S EAA1130 AND EAA1149 WERE RETURNED FOR OVERHAUL.  AFTER REMOVAL OF THE HUB PILOT TUBES, INSPECTION REVEALED UNR	EPAIRABLE CORROSION ON THE INSIDE DIAMETER OF THE PILOT TUBE BORES.  THE HUBS WERE RETIRED FROM SERVICE AND SENT TO HART	ZELL ENGINEERING FOR EVALUATION.														6	C	P56GL	 
1999040200070	19990402	00070	CE  	1999	4	2	99ZZZX1186       	1	19990227	G	3233	12805149	ACTUATOR        			CESSNA	182   	R182        	2072734	CE  										NLG	FRACTURED       	G	S	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	7301W	2573 			159	R18200051				DURING AN INCIDENT INVESTIGATION TO DETERMINE THE CAUSE OF A NOSE GEAR COLLAPSE, IT WAS DETERMINED THE CESSNA NOSE GEAR 	ACTUATOR LEFT SIDE DOWNLOCK PIN WAS FRACTURED AT THE ROLL PIN SECURING POINT OF THE ACTUATOR.  THIS HALF OF THE LOCK PIN	 WORKED ITS WAY OUT OF THE ATTACHMENT BOSS AND JAMMED THE ACTUATOR EXTEND/RETRACT PISTON.				1	H	7	1 	3O			RT	3A13    					 
1999040200071	19990402	00071	SO  	1999	4	2	99ZZZX1187       	1	19990206	G	3213	1318900	AXLE            			PIPER 	PA22  	PA22160     	7102214	SO  										LT MLG	BROKE           	G				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	05	8729D					225910				LEFT LANDING GEAR BROKE AT AXLE.  AIRCRAFT ON SKIS, LAKE DRIFTED.  TEMPERATURE MINUS 35 DEGREES FAHRENHEIT.						1	H	7	1 	3O				1A6     					 
1999040200072	19990402	00072	CE  	1999	4	2	99ZZZX1188       	1	19990215	G	3233	98820152	ACTUATOR        			CESSNA	172   	172RG       	2072438	CE  										RT MLG	FAILED          	B			NM2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	19	9506D	7024 				172RG1191				THE RIGHT HAND LANDING GEAR ACTUATOR FAILED DURING FLIGHT AND THE AIRCRAFT LANDED WITH ONLY THE LEFT AND NOSE GEAR EXTEN	DED.  THE ACTUATOR HOUSING WAS CRACKED AND BROKEN IN THREE PLACES TO CAUSE A TOTAL FAILURE OF THE ACTUATOR.  THE GEAR TE	ETH OF THE ACTUATOR AND THE LANDING GEAR STRUT SEPARATED.  THE LANDING GEAR OF THIS AIRCRAFT HAS 7,024 HOURS TOTAL TIME 	IN SERVICE AND APPROXIMATELY 20,000 TO 21,000 CYCLES.			1	H	7	1 	3O				3A17    					 
1999040200073	19990402	00073	SO  	1999	4	2	99ZZZX1189       	1	19990224	G	2434	6519900	BRACKET         			PIPER 	PA28  	PA28180     	7102808	SO  										ALTERNATOR	FAILED          	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	23	6395J					284810				ALTERNATOR SUPPORT BRACKET IS MADE WITH INSUFFICIENT WELD AT JOINTS.  (NO PENETRATION).  BRACKETS CRACK AT WELD JOINT.						1	L	7	1 	3O				2A13    					 
1999040200074	19990402	00074	CE  	1999	4	2	99ZZZX1190       	1	19990308	G	3230		SWITCH          			CESSNA	414   	414         	2075908	CE  										LT MLG	OUT OF ADJUST   	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	19	515FV					4140410				PILOT HAD NOT LEFT GEAR DOWN AND LOCKED LIGHT, TRIED TO REPLACE THE BULB.  WHEN TRYING TO REPLACE THE BULB, THE CIRCUIT 	BREAKER TRIPPED.  THE PILOT CYCLED GEAR TO THE UP POSITION ELECTRICALLY, THEN PULLED THE GEAR MOTOR CIRCUIT BREAKER AND 	PUT THE GEAR DOWN WITH THE HAND CRANK.  THE AIRCRAFT LANDED WITH NO PROBLEMS.  REPLACED TWO BURNT LIGHT BULBS.  ADJUSTED	 THE LEFT MAIN GEAR DOWN AND LOCK MICROSWITCH AND PERFORMED GEAR RETRACTION CHECK OK.			1	L	7	2 	3O			RT	A7CE    					 
1999040200075	19990402	00075	CE  	1999	4	2	99ZZZX1191       	1	19990301	G	2720		CONTROL CABLE   			CESSNA	150   	152         	2071835	CE  										RUDDER	FRAYED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	5111H	5043 				15284062				REMOVED RUDDER CABLES FOR LENGTH VARIFICATION.  FOUND BROKEN STRANDS AT AFT PULLEY POSITION.						1	H	7	1 	3O			NT	3A19    					 
1999040200076	19990402	00076	SO  	1999	4	2	99ZZZX1192       	2	19990103	G	8550	20195707	SEPARATOR FILTER			CESSNA	414   	414A        	2075907	CE  	CONT  	O520  	TSIO520NB   	17040	SO  					ENGINE OIL	MISMANUFACURED  	B		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	19	414RM					414A0306	290987R			FOUND 3 OUT OF 4 NEW FILTERS SENT FROM CESSNA (NEW FILTERS) WITH AT LEAST ONE LOOSE RIVET.  RIVETS FOUND BAD ARE NOT INS	TALLED PROPERLY AND COULD POSSIBLY ENTER ENGINE AND CAUSE MAJOR DAMAGE, BETTER QUALITY CONTROL COULD REMEDY THIS PROBLEM	 WHICH IS QUITE SERIOUS.				1	L	7	2 	3O	3	O		A7CE    	E8CE				 
1999040200077	19990402	00077	CE  	1999	4	2	99ZZZX1193       	1	19990308	G	2750	98600581	CONTROL CABLE   			CESSNA	210   	T210L       	2073449	CE  										TE FLAP	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	10419					T21061484				WHEN FLAP FOLLOW-UP CABLE IS INSTALLED IN AIRCRAFT, IT HAS AN INTERNAL BIND WHICH CAUSES THE BELLCRANK IN THE LEFT WING 	TO 'JERK' AS THE MOTION OF THE BELLCRANK OVERCOMES THE BINDING OF THE CABLE.  THIS 'JERKING' CAUSES THE RIB TO WHICH THE	 BELLCRANK IS ATTACHED TO 'OIL CAN' A CONSIDERABLE AMOUNT.  THE FLAP INDICATOR ALSO 'JERKS' AND CAUSES AN AUDIBLE POPPIN	G SOUND.  THE CABLE WORKS SMOOTH ON THE BENCH.  IF A 90 DEGREE BEND IS PUT ON THE CABLE (LESS THAN WHAT IT WOULD BE INST	ALLED) THE CABLE BINDS.  A CESSNA TECH REP DID NOT HAVE A SOLUTION OTHER THAN TO 'TRY A DIFFERENT CABLE'.  THREE ADDITIO	NAL NEW CABLES WERE TRIED WITH THE SAME RESULTS.	1	H	7	1 	3O			 	3A21    					 
1999040200078	19990402	00078	SO  	1999	4	2	99ZZZX1194       	1	19990305	G	3230	9572402	MOUNT           			PIPER 	PA34  	PA34200T    	7103406	SO  										NLG ACTUATOR	FAILED          	D		A		O				OTHER                   				O			OTHER                     			TO	TAKEOFF        	1			SW	17	XBKEQ					347350190				MOUNT ASSEMBLY - HYDRAULIC JACK NOSE GEAR, P/N 95724-2.  PART FAILED DURING TAKEOFF.  PRELIMINARY INSPECTION FOUND MOUNT	 ASSEMBLY TORN WHERE HYDRAULIC ACTUATOR BOLTS TO MOUNT.  THE RESULTING DAMAGE CAUSED THE DOWNLOCK TO SHIFT AND RELEASE T	ENSION ON THE LINK ASSEMBLY CAUSING THE NOSE GEAR TO COLLAPSE.  POSSIBLE CAUSE, PREVIOUS HARD LANDINGS.				1	L	7	2 	3O				A7SO    					 
1999040200079	19990402	00079	CE  	1999	4	2	99ZZZX1195       	1	19990118	G	5510	12326242	REINFORCEMENT   			CESSNA	210   	T210L       	2073449	CE  										HORIZ STABILIZER	CRACKED         	B		A	DPOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	93155	4088 				21060283				WHEN A 1 INCH LONG CRACK WAS NOTED ON ANOTHER T210 HORIZONTAL STABILIZER AFT SPAR, THIS AIRCRAFT WAS INSPECTED AND A CRA	CK WAS NOTED ON THE AFT SPAR REINFORCEMENT.  WHEN THE STABILIZER WAS REMOVED, THE LEFT FORWARD FITTING (PN 0732601-5) WA	S NOTED TO HAVE 4 OF 5 RIVETS SHEARED AND THE RIGHT FORWARD FITTING WAS NOTED TO HAVE 2 OT 5 RIVETS SHEARED.  THIS AIRCR	AFT DID NOT HAVE SIL 84-17 OR SB 88-3 (SK 210-125 AND 126) COMPLIED.  AIRCRAFT WAS OPERATED NORMALLY, SO CAUSE IS UNKNOW	N.  THERE IS NO WAY TO DETECT IF THE FORWARD FITTINGS, RIVETS HAVE SHEARED WITHOUT REMOVING STABILIZER.  RECOMMEND C/W S	B 88-3.	1	H	7	1 	3O				3A21    					 
1999040200080	19990402	00080	SO  	1999	4	2	99ZZZX1196       	2	19990301	G	8520		PISTON PIN      			LUSCOM	8     	8A          	8190104	SO  	CONT  	A65   	A658        	17003	SO  					ENGINE	MISMANUFACTURED 	H				A				UNSCHED LANDING         				W			INADEQUATE Q C            			NR	NOT REPORTED   	1			SO	11										A65-8 ENGINE INSTALLED IN A LUSCOMBE MODEL 8A.  WHILE IN-FLIGHT, THE ENGINE BEGAN TO MISFIRE AND RUN ROUGH.  THE PILOT W	AS ABLE TO MAKE A FORCED LANDING WITH ONLY MINOR INJURIES TO HIMSELF AND PASSENGER.  POST-ACCIDENT EXAMINATION OF THE EN	GINE REVEALED THE NR 4 PISTON PIN HAD FAILED.  FURTHER EXAMINATION OF THE PISTON PIN REVEALED IT HAD BEEN MANUFACTURED I	MPROPERLY.  THE OTHER THREE PISTON PINS WERE OF SIMILAR MANUFACTURE.  THIS ENGINE WAS EXPORTED TO GREAT BRITAIN IN OCTOB	ER 1990 WITH 201 HRS TIME-IN-SERVICE SINCE OVERHAUL.  THE ENGINE HAD SUBSEQUENTLY ACCUMULATED 900 ADDITIONAL HRS WHILE O	PERATING IN GREAT BRITAIN.  ALL REQUIRED INSPECTIONS HAD BEEN CONDUCTED DURING THE LIFE OF THE ENGINE.	1	H	7	1 	3O	3	O		A694    	E205				 
1999040200081	19990402	00081	CE  	1999	4	2	99ZZZX1197       	1	19990129	G	5521	043200121	SPAR            		043200152   	CESSNA	150   	152         	2071835	CE  										ELEVATOR	CRACKED         	B	P	A	SL5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	94784	6645 				15285786				DURING ANNUAL INSPECTION, FOUND RT ELEVATOR OUTBOARD HINGE P/N 043200171 BOLT HOLE ELONGATED.  AFTER REMOVING THREE FOR 	REPLACEMENT, FOUND ELEVATOR SPAR, PN 0432001-21 CRACKED AT HOME ATTACHMENT RIVET HOLES.  THERE IS NO WAY TO INSPECT THE 	SPAR WITHOUT DE-RIVETING COMPONENTS.  INSTALLED NEW SPAR ASSY (HINGE HAS ADDITIONAL RIVET FLANGES ON  MAIN SPAR).  LEFT 	ELEVATOR OUTBOARD HINGE WAS REMOVED ALSO FOR REPLACEMENT.  LEFT ELEVATOR SPAR WAS NOT CRACKED.			1	H	7	1 	3O			NT	3A19    					 
1999040200083	19990402	00083	CE  	1999	4	2	99ZZZX1199       	1	19990127	G	3411	S11391	CONNECTOR       			CESSNA	172   	172R        	2072401	CE  										AIRSPEED IND	LOOSE           	B	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	255HP	410  				17280308				WHILE REPLACING SUPPORT GUIDE FOR CONTROL YOKE ON LEFT SIDE, REMOVED INSTRUMENT PANEL, FOUND FITTING FINGER TIGHT ITEM 2	9 AND ITEM 22 ON AIRSPEED INDICATOR (IPC 34-11-00-01) TIGHTENED CONNECTORS.  LEAK CHECKED NORMAL.  RECOMMENDATION:  TIGH	TEN CONNECTORS AT ASSY.				1	H	7	1 	3O			NT	3A12    					 
1999040200084	19990402	00084	SO  	1999	4	2	99ZZZX1200       	2	19990301	G	8520	6419311075	BOLT            			CESSNA	421   	421C        	2076016	CE  	CONT  	O520  	GTSIO520N   	17032	SO  					NR 5 CYLINDER	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	215MP		371  			421C1231	608468			WHILE TROUBLESHOOTING AN OIL LEAK, THE LOWER THRU-BOLT BETWEEN THE NR 4 AND NR 5 CYLINDER WAS FOUND BROKEN APPROXIMATELY	 .50 INCH FROM THE END.  AFTER CYLINDER REMOVAL AND COMPLETE CRANKCASE AND TORQUE INSPECTION, NO OTHER DEFECTS WERE FOUN	D.				1	L	7	2 	3O	3	O		A7CE    	E7CE				 
1999040200085	19990402	00085	CE  	1999	4	2	99ZZZX1201       	1	19990222	G	3230	SM50D7	RELAY           	EATON       		BEECH 	36    	A36         	1151604	CE  										MLG	MALFUNCTIONED   	H				A				UNSCHED LANDING         				O			OTHER                     			CL	CLIMB          	1			WP	17	801NH	3131 				E2692				LANDING GEAR RETRACT MOTOR C/B TRIPPED AFTER TAKEOFF.  LANDING GEAR MANUALLY EXTENDED TO DOWN AND LOCKED POSITION.  INVE	STIGATION SHOWED THAT LANDING GEAR DYNAMIC BRAKE RELAY HAD CONTACT POINTS FUSED TOGETHER TO ALLOW POWER TO BE APPLIED TO	 MOTOR CONSTANTLY.  THIS CONDITION IS BELIEVED TO BYPASS ANY SAFETY SWITCH INSTALLED TO PREVENT RETRACTION OF THE LANDIN	G GEAR ON THE GROUND IF C/B WAS RESET.  RELAY HAD APPROX 3,131 HRS TIS AND 15,000 LANDING GEAR CYCLES.  ACFT IS USED IN 	AN AIRLINE TRAINING OPER WITH HIGH CYCLE COUNTS.  OTHER RELAYS IN THE FLEET HAVE ALSO EXPERIENCED RELAY MALFUNCTIONS, BU	T NEVER HAD CONTACT POINTS FUSED TOGETHER.  RECOMMEND THIS ITEM BE FUNCTIONALLY TESTED OR REPLACED AT A 2,000 HR INTERVA	1	L	7	1 	3O				3A15    					 
1999040200087	19990402	00087	SO  	1999	4	2	99ZZZX1203       	1	19990201	G	5540	6345100	SUPPORT         			PIPER 	PA28  	PA28180     	7102808	SO  										RUDDER	CRACKED         	D	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	55803	3497 				287305475				DURING AN ANNUAL INSPECTION, EXCESSIVE PLAY WAS FOUND IN THE RUDDER CROSS BAR.  THE PLAY WAS DUE TO THE MOVEMENT IN THE 	CENTER SUPPORT.  CRACKS WERE FOUND IN THE SUPPORT.					1	L	7	1 	3O				2A13    					 
1999040200088	19990402	00088	SO  	1999	4	2	99ZZZX1204       	1	19990308	G	3213	653194	CYLINDER        			PIPER 	PA28  	PA28140     	7102802	SO  										LT MLG	CRACKED         	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	33595	7354 			V655	287525211				LEFT MAIN GEAR CYLINDER, PN 65319-4, ATTACHMENT EARS FOR UPPER TORQUE LINK (PN 78033-00) BROKE OFF DURING LANDING OF STU	DENT PILOT.  POSSIBLE CAUSE WAS MANY SIDE LOADS IMPOSED BY STUDENTS DURING LANDINGS.  NO RECOMMENDATION TO PREVENT RECUR	RENCE OTHER THAN NORMAL INSPECTION OF LANDING GEAR.  PIPER SL 760 PERTAINS TO THIS SUBJECT.  POSSIBILITY THAT AN AD SHOU	LD BE GENERATED.			1	L	7	1 	3O				2A13    					 
1999040200091	19990402	00091		1999	4	2	99ZZZX1207       	1	19990204	G	7120	2050601051	MOUNT           																	ENGINE BAY	CRACKED         	B			XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01										MOUNTS MAGNETIC AND PARTICLE INSPECTED ON P.O. NR 3670 FROM SKY CONTROL INC.  TWO OF 10 PARTS CRACKED IN WELDS.																			 
1999040200092	19990402	00092		1999	4	2	99ZZZX1208       	1	19990204	G	7120	2050601061	MOUNT           																	ENGINE BAY	CRACKED         	B			XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01										MOUNTS MAGNETIC AND PARTICLE INSPECTED ON P.O. NR 3670 FROM SKY CONTROL INC.  TWO OF 10 PARTS CRACKED IN WELDS.																			 
1999040200096	19990402	00096	CE  	1999	4	2	99ZZZX1212       	1	19990310	G	2434	ALX9424	ALTERNATOR      	ELECTROSYS  		BEECH 	35    	V35A        	1151544	CE  	CONT  	O520  	IO520B      	17032	SO  					ALTERNATOR	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	21	2722A				8112157	D9050	1226028			INSTALLED ALTERNATOR AND UNIT FAILED TO OPERATE.  AFTER INSPECTION, CAUSE OF FAILURE WAS THE BRUSHES.  DURING ASSEMBLY, 	SOMEONE HAD PUT SOME TYPE OF EPOXY ON BRUSHES TO HOLD THEM IN THE BRUSH HOLDER.  THIS, IN EFFECT, KEPT THE BRUSHES FROM 	MAKING CONTACT.				1	L	7	1 	3O	3	O		3A15    	E5CE				 
1999040200097	19990402	00097	CE  	1999	4	2	99ZZZX1213       	1	19990311	G	2820	0500106326	LINE            			CESSNA	185   	A185F       	2072821	CE  										FUEL SYSTEM	CHAFED          	B		A	WWKR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	94237	2081 				18503294				AILERON CABLE CHAFED FUEL LINE.  RUBBED THROUGH PLASTIC PROTECTOR AND INTO ALUMINUM LINE.  CAUSED BY MISALIGNED FUEL LIN	E.					1	H	7	1 	3O				3A24    					 
1999040200098	19990402	00098	CE  	1999	4	2	99ZZZX1214       	1	19990311	G	2820	0500106325	LINE            			CESSNA	185   	A185F       	2072821	CE  										FUEL SYSTEM	CHAFED          	B			WWKR	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			AL	03	94237	2081 				18503294				FUEL LINE DAMAGED DURING PRIOR REPAIR, NOT LEAKING, BUT NICKED BY DRILLING AND INSTALLATION ALIGNMENT CAUSING CHAFING.						1	H	7	1 	3O				3A24    					 
1999040200101	19990402	00101	EA  	1999	4	2	99ZZZX1217       	2	19990227	G	8530	41A21926	LINE            			PIPER 	PA32  	PA32R301T   	7103220	SO  	LYC   	O540  	TIO540A1A   	41532	EA  					AIR INLET	CRACKED         	B			SO5R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	03	481CA	19   				3257081	L1013761A			CRACKED/BROKEN ELBOW ADAPTER WELD.  AREA AROUND WELD WAS CRACKED CAUSING ADAPTER TO BREAK OFF WITH MINIMAL FORCE.  WHEN 	ADAPTER BREAKS OFF, A 1 INCH HOLE IS LEFT IN AIR INLET PIPE CAUSING A DROP IN M.A.P.					1	L	7	1 	3O	3	O		A3SO    	E14EA				 
1999040200102	19990402	00102	CE  	1999	4	2	99ZZZX1218       	1	19990222	G	5540	57310261	BRACKET         			CESSNA	421   	421C        	2076016	CE  										RUDDER	MISINSTALLED    	B			R2JR	O				OTHER                   				W			INADEQUATE Q C            			NR	NOT REPORTED   	1			EA	21	5534G					421C0247				CREW REPORTED RUDDER CATCHING ON TAILCONE COVER SCREWS.  MAINTENANCE CREW FOUND RUDDER HAD SLIPPED DOWN FROM ITS NORMAL 	POSITION BECAUSE THE BEARING IN THE LOWER ATTACH HINGE HAD FALLEN OUT OF BRACKET.  THE BEARING FELL OUT DUE TO THE WEIGH	T OF THE RUDDER.  BRACKET INSTALLED UPSIDE DOWN WHEN AIRCRAFT WAS MADE.  THERE IS A LIP ON THE BRACKET FOR THE BEARING T	O SET IN, BUT WITH THE BRACKET IN 180 DEGREE OUT, THE BRACKET FAILED TO HOLD BEARING UP.  NEW BRACKET NEEDS TO BE INSTAL	LED PROPERLY.  THIS SHOP HAS SEEN THIS PROBLEM ON 2 OTHER ACFT.  ACFT FERRIED BY OWNER.  CESSNA KNOWS OF PROBLEM.		1	L	7	2 	3O				A7CE    					 
1999040200103	19990402	00103	CE  	1999	4	2	99ZZZX1219       	1	19990127	G	3411	S11331	CONNECTOR       			CESSNA	172   	172R        	2072401	CE  										AIRSPEED IND	LOOSE           	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	255HP	410  				17280308				WHILE REPLACING SUPPORT GUIDE FOR CONTROL YOKE ON LEFT SIDE, REMOVED INSTRUMENT PANEL, FOUND FITTING FINGER TIGHT ITEM 2	9 AND ITEM 22 ON AIRSPEED INDICATOR (IPC 34-11-00-01) TIGHTENED CONNECTORS.  LEAK CHECKED NORMAL.  RECOMMENDATION:  TIGH	TEN CONNECTORS AT ASSY.				1	H	7	1 	3O			NT	3A12    					 
1999040200235	19990402	00235	SW  	1999	4	2	99ZZZX1222       	1	19990308	G	7120	206064103101	BEARING         		206064107101	BELL  	206   	206L1       	1182107	SW  										LEG ASSY	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1084Y					45433				DURING INSPECTION FOUND WORN BEARING						1	G	7	1 	3U				H2SW    					 
1999040200237	19990402	00237	SW  	1999	4	2	99ZZZX1224       	1	19990209	G	6210	206015001107	BLADE           			BELL  	206   	206L4       	1182110	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	174AL	3412 			A2107	52067				DISCOVERED DURING DAILY INSPECTION, CORROSION AND SEPARATION AT TIP.						1	G	7	1 	3U			NC	H2SW    					 
1999040200240	19990402	00240	SW  	1999	4	2	99ZZZX1227       	1	19990308	G	7120	206064103001	BEARING         		206064107101	BELL  	206   	206L1       	1182107	SW  										LEG ASSY	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3179V					45782				DURING INSPECTION, FOUND BEARING WORN.						1	G	7	1 	3U				H2SW    					 
1999040200241	19990402	00241	SW  	1999	4	2	99ZZZX1228       	1	19990308	G	7120	206064103001	BEARING         		206064107103	BELL  	206   	206L1       	1182107	SW  										LEG ASSY	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3192P					45780				DURING INSPECTION, BEARING LOOSE AND WORN IN RACE.						1	G	7	1 	3U				H2SW    					 
1999040200243	19990402	00243	SW  	1999	4	2	99ZZZX1230       	1	19990308	G	7120	206064103001	BEARING         		206064107103	BELL  	206   	206L3       	1182108	SW  										LEG ASSY	LOOSE           	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	343AL					51372				DURING INSPECTION, FOUND BEARING WITH EXCESSIVE PLAY.						1	G	7	1 	3U				H2SW    					 
1999040200244	19990402	00244	SW  	1999	4	2	99ZZZX1231       	1	19990308	G	7120	206064103101	BEARING         		206064107101	BELL  	206   	206L3       	1182108	SW  										LEG ASSY	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350AL					51429				DURING INSPECTION, FOUND LOOSE/WORN BEARING.						1	G	7	1 	3U				H2SW    					 
1999040200245	19990402	00245	SW  	1999	4	2	99ZZZX1232       	1	19990308	G	7120	206064103001	BEARING         		206064107103	BELL  	206   	206L3       	1182108	SW  										LEG ASSY	LOOSE           	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350AL					51429				DURING INSPECTION, FOUND BEARING WORN AND LOOSE IN RACE.						1	G	7	1 	3U				H2SW    					 
1999040200246	19990402	00246	SW  	1999	4	2	99ZZZX1233       	1	19990308	G	7120	206064103001	BEARING         		206064107101	BELL  	206   	206L3       	1182108	SW  										LEG ASSY	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	364AL					51434				DURING INSPECTION, FOUND LOOSE/WORN BEARING.						1	G	7	1 	3U				H2SW    					 
1999040200249	19990402	00249	SW  	1999	4	2	99ZZZX1236       	1	19990217	G	6520		BALANCE WHEEL   		206040402003	BELL  	206   	206L3       	1182108	SW  										T/R GEARBOX	DAMAGED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	367AL		3395 		AFS2724	51443				TEAR-DOWN TO PERFORM REPAIR.  BALANCE WHEEL PN 206-011-716-001 NOT TORQUED ON SHAFT, CAUSED WHEEL AND SHAFT TO BE DAMAGE	D BEYOND LIMITS.					1	G	7	1 	3U				H2SW    					 
1999040200250	19990402	00250	SW  	1999	4	2	99ZZZX1237       	1	19990308	G	7120	206064103001	BEARING         		206064107101	BELL  	206   	206L1       	1182107	SW  										LEG ASSY	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3890B					45480				DURING INSPECTION, FOUND WORN BEARING.						1	G	7	1 	3U				H2SW    					 
1999040200252	19990402	00252	SW  	1999	4	2	99ZZZX1239       	1	19990309	G	7120	206064103001	BEARING         		407060111101	BELL  	407   	407         		SW  										LEG ASSY	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427AL	330  				53107				DURING INSPECTION, FOUND WORN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999040200253	19990402	00253	SW  	1999	4	2	99ZZZX1240       	1	19990217	G	6310	406040516101	INPUT SHAFT     		406040500123	BELL  	407   	407         		SW  										TRANSMISSION	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427AL	2487 			AFS1124	53107				F/W/U REMOVED FOR 2,500-HOUR OVERHAUL.  FOUND AT TEAR-DOWN INSPECTION.  INPUT SPLINES WORN BEYOND LIMITS.  SHAFT SCRAPPE	D.					1	G	7	1 	3U			O	H2SW    					 
1999040200254	19990402	00254	SW  	1999	4	2	99ZZZX1241       	1	19990301	G	6310	406040516101	INPUT SHAFT     		406040500123	BELL  	407   	407         		SW  										TRANSMISSION	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	477AL	2484 			AFS1212	53203				FREE WHEELING UNIT REMOVED FOR 2,500-HOUR OVERHAUL.  FOUND AT TEAR-DOWN INSPECTION.  INPUT SPLINES WORN BEYOND LIMITS. S	HAFT SCRAPPED.					1	G	7	1 	3U			O	H2SW    					 
1999040200256	19990402	00256	SW  	1999	4	2	99ZZZX1243       	1	19990305	G	5302		SKIN            		407030801101	BELL  	407   	407         		SW  										TAILBOOM	CRACKED         	B	P		ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	547AL				53239	53240				DURING A POST-FLIGHT INSPECTION, FOUND CRACK IN TAILBOOM SKIN AT FORWARD EDGE OF HORIZONTAL STABILIZER MOUNT AREA ON LEF	T HAND SIDE.					1	G	7	1 	3U			O	H2SW    					 
1999040200257	19990402	00257	SW  	1999	4	2	99ZZZX1244       	1	19990214	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	547AL					53240				DISCOVERED DURING 25-HOUR AD 97-24-17, PARAGRAPHS A, B, AND E.  FOUND NR 7 DISC PACK CRACKED.  NR 1 DISC CRACKED FORWARD	 DISC OF NR 7 DISC PACK.					1	G	7	1 	3U			O	H2SW    					 
1999040200258	19990402	00258	SW  	1999	4	2	99ZZZX1245       	1	19990308	G	7120	206064103001	BEARING         		206064107103	BELL  	206   	206L1       	1182107	SW  										LEG ASSY	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5751Q					45524				DURING INSPECTION, FOUND BEARING WORN.						1	G	7	1 	3U				H2SW    					 
1999040200261	19990402	00261		1999	4	2	99ZZZX1248       	4	19990219	G	3457	00110005400	GPS             			HUGHES	369   	369D        	4470706	WP  										COCKPIT	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	369AW		140  		81506744	470117D				GPS WILL NOT COME UP.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999040200262	19990402	00262	WP  	1999	4	2	99ZZZX1249       	1	19990215	G	7712	369145267	GAUGE           			HUGHES	369   	369D        	4470706	WP  										TORQUE	READS HIGH      	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	5070J				857	121096D				TORQUE GAUGE READING 6 PSI HIGH.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999040200263	19990402	00263	SW  	1999	4	2	99ZZZX1250       	1	19990225	G	6320	204040129001	RETAINER        		206040004111	BELL  	206   	206L1       	1182107	SW  										M/R GEARBOX	BROKEN          	B			ZV1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	577E	13067	1587 		BMC45241	45577				UPON DISASSEMBLYING TRANSMISSION FOR INSPECTION REMOVING SCREEN ASSY FOR CHIPS OF RETAINER ASSY IN SCREEN, LOOKED OVER P	LANETARY, FOUND 1 EACH GEAR ASSY RETAINER MISSING PIECES.  UPGRADE USING NEW HOUSING ASSY, P/N 214-040-515-001.					1	G	7	1 	3U				H2SW    					 
1999040200264	19990402	00264	SW  	1999	4	2	99ZZZX1251       	1	19990218	G	6220	212011102105	YOKE            			BELL  	212   	212         	1181420	SW  										MAIN ROTOR	WORN            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530B	1637 			A545M	30702				BEARING JOURNALS WORN.  FOUND AT 1,600 HOUR INSPECTION.  REPLACED.						1	G	7	1 	4U				H4SW    					 
1999040200265	19990402	00265		1999	4	2	99ZZZX1252       	4	19990127	G	3453	06601148111	LORAN           		KLN89       	BOLKMS	117   	BK117A3     	5626015	EU  										COCKPIT	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	1140H				100956	7078				DISPLAY ON LORAN FAILING.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999040200281	19990402	00281	EU  	1999	4	2	99ZZZX1268       	1	19990129	G	6410	10531791	BLADE           			BOLKMS	105   	BO105LSA3   	5626020	EU  										TAIL ROTOR	PEELING         	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	8118Y	1092 			185	2017				PAINT PEELING ON BLADE AFTER ONLY 420.7 HOURS SINCE REPAIR.  REMOVED AND REPLACED.						1	G	7	2 	3U				H3AU    					 
1999040200282	19990402	00282	EU  	1999	4	2	99ZZZX1269       	1	19990129	G	6410	10531791	BLADE           			BOLKMS	105   	BO105LSA3   	5626020	EU  										TAIL ROTOR	PEELING         	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	8118Y	1092 			258	2017				PAINT ON BLADE PEELING AFTER ONLY 420.7 HOURS SINCE REPAIR.  REMOVED AND REPLACED.						1	G	7	2 	3U				H3AU    					 
1999040200302	19990402	00302		1999	4	2	99ZZZX1282       	4	19990309	G	2312	KY196	TRANSCEIVER     			HUGHES	369   	369D        	4470706	WP  										COCKPIT	MALFUNCTIONED   	B			EOOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	5074R					1151D				UPON TRANSMIT (INTERMITTENTLY), THE EPO SYSTEM WOULD BE ENERGIZED AS WELL AS THE FREQUENCY DISPLAY WOULD BLINK OUT.  REM	OVED AND REPLACED RADIO AND ALL WAS CURED.					1	G	7	1 	3U				H3WE    					 
1999040200303	19990402	00303	SW  	1999	4	2	99ZZZX1283       	1	19990205	G	6210	206015001107	BLADE           			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2758L	2388 			A2085	45266				DISCOVERED DURING DAILY INSPECTION, TRAILING EDGE EXTRUSION CORRODED.						1	G	7	1 	3U				H2SW    					 
1999040200491	19990402	00491	NM  	1999	4	2	99ZZZX1286       	1	19990212	G	7120	R1842353C	BOLT            			BOEING	727   	727227      	1384078	NM  										FORWARD CONE	MISDRILLED      	B			KT3R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	07	79754					21363				CONE BOLT THROUGH-BOLT HOLE IS NOT CONCENTRIC AND HAS AN .010 INCH DEVIATION BETWEEN LEFT AND RIGHT SIDES, E.G., HOLE IS	 NOT STRAIGHT WHICH CONTRIBUTED TO THE THROUGH-BOLT BEING FOUND CRACKED UPON INSPECTION AFTER ENGINE REMOVAL FOR MAINTEN	ANCE C-CHECK.				2	L	7	3 	4F				A3WE    					 
1999040200492	19990402	00492	NM  	1999	4	2	99ZZZX1287       	1	19990211	G	5315		FLOORBEAM       			BOEING	727   	727227      	1384078	NM  										E/E BAY	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON FLOOR BEAM STA 380, E/E BAY.						2	L	7	3 	4F				A3WE    					 
1999040200493	19990402	00493	NM  	1999	4	2	99ZZZX1288       	1	19990211	G	5347		SEAT TRACK      			BOEING	727   	727227      	1384078	NM  										BS 950	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 950A - STA 950B, LBL 45.5.						2	L	7	3 	4F				A3WE    					 
1999040200494	19990402	00494	NM  	1999	4	2	99ZZZX1289       	1	19990211	G	5347		SEAT TRACK      			BOEING	727   	727227      	1384078	NM  										BS 848	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION NOTED ON STA 848 - STA 740, LBL 45.5.						2	L	7	3 	4F				A3WE    					 
1999040200495	19990402	00495	NM  	1999	4	2	99ZZZX1290       	1	19990211	G	5330		SKIN            			BOEING	727   	727227      	1384078	NM  										BS 277	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION NOTED ON SKIN FS 277 AT STR 18R.						2	L	7	3 	4F				A3WE    					 
1999040200496	19990402	00496	NM  	1999	4	2	99ZZZX1291       	1	19990211	G	5320		WEB             			BOEING	727   	727227      	1384078	NM  										BS 1166	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON CENTER OF FLOOR WEB STA 1166, BL ZERO.						2	L	7	3 	4F				A3WE    					 
1999040200497	19990402	00497	NM  	1999	4	2	99ZZZX1292       	1	19990211	G	5320		SHEAR TIE       			BOEING	727   	727227      	1384078	NM  										BS 540	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION NOTED AT STA 540 BETWEEN STA 28L AND STA 28R.						2	L	7	3 	4F				A3WE    					 
1999040200498	19990402	00498	NM  	1999	4	2	99ZZZX1293       	1	19990211	G	5320		SUPPORT         			BOEING	727   	727227      	1384078	NM  										BS 1130-1148	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION NOTED ON FLOOR SUPPORT RIGHT BETWEEN STA 1130 AND STA 1148.						2	L	7	3 	4F				A3WE    					 
1999040200499	19990402	00499	NM  	1999	4	2	99ZZZX1294       	1	19990211	G	5311	6516338202	FRAME           			BOEING	727   	727227      	1384078	NM  										BS 950	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION NOTED ON KEEL BEAM CHORD STA 950R.						2	L	7	3 	4F				A3WE    					 
1999040200500	19990402	00500	NM  	1999	4	2	99ZZZX1295       	1	19990211	G	5313		STRINGER        			BOEING	727   	727227      	1384078	NM  										BS 950	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION NOTED ON STR 29R AT STA 950.						2	L	7	3 	4F				A3WE    					 
1999040200501	19990402	00501	NM  	1999	4	2	99ZZZX1296       	1	19990212	G	5320	69133833	FITTING         			BOEING	727   	727281      	138408N	NM  										BS 1183	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED AT BL ZERO, STA 1183, JACK PAD FITTING.						2	L	7	3 	4F				A3WE    					 
1999040200502	19990402	00502	NM  	1999	4	2	99ZZZX1297       	1	19990212	G	5313		STRINGER        			BOEING	727   	727281      	138408N	NM  										BS 440	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON STR 24R STA 440.						2	L	7	3 	4F				A3WE    					 
1999040200503	19990402	00503	NM  	1999	4	2	99ZZZX1298       	1	19990212	G	5313		STRINGER        			BOEING	727   	727281      	138408N	NM  										BS 440	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON STR 25L STA 440.						2	L	7	3 	4F				A3WE    					 
1999040200504	19990402	00504	NM  	1999	4	2	99ZZZX1299       	1	19990212	G	5320		INTERCOSTAL     			BOEING	727   	727281      	138408N	NM  										BS 1110-1130	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON INTERCOSTAL AT STA 1110 - STA 1130 CENTER LINE.						2	L	7	3 	4F				A3WE    					 
1999040200505	19990402	00505	NM  	1999	4	2	99ZZZX1300       	1	19990212	G	5210		WEB             			BOEING	727   	727281      	138408N	NM  										PASSENGER DOOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON WEB FORWARD OF VENT DOOR IN C2 DOOR.						2	L	7	3 	4F				A3WE    					 
1999040200506	19990402	00506	NM  	1999	4	2	99ZZZX1301       	1	19990212	G	5315		FLOORBEAM       			BOEING	727   	727281      	138408N	NM  										BS 312	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED AT STA 312 LBL 24 ON FLOORBEAM (AFT OF COCKPIT DOOR).						2	L	7	3 	4F				A3WE    					 
1999040200507	19990402	00507	NM  	1999	4	2	99ZZZX1302       	1	19990212	G	5347		SEAT TRACK      			BOEING	727   	727281      	138408N	NM  										BS 997	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON SEAT TRACK AT STA 997, APPROXIMATELY 44.5 LBL.						2	L	7	3 	4F				A3WE    					 
1999040200508	19990402	00508	NM  	1999	4	2	99ZZZX1303       	1	19990212	G	5754		PANEL           			BOEING	727   	727281      	138408N	NM  										SLAT	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON LT SLAT PANEL NR 6205.						2	L	7	3 	4F				A3WE    					 
1999040200509	19990402	00509	NM  	1999	4	2	99ZZZX1304       	1	19990212	G	5541		SKIN            			BOEING	727   	727281      	138408N	NM  										RUDDER	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DUIRNG A C-CHECK, CORROSION NOTED ON LOWER RUDDER LEFT SURFACE.						2	L	7	3 	4F				A3WE    					 
1999040200510	19990402	00510	NM  	1999	4	2	99ZZZX1305       	1	19990212	G	5347		SEAT TRACK      			BOEING	727   	727281      	138408N	NM  										BS 1050-1070	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON SEAT TRACK STA 1050 - STA 1070, LBL 45.5.						2	L	7	3 	4F				A3WE    					 
1999040200511	19990402	00511	NM  	1999	4	2	99ZZZX1306       	1	19990212	G	5321		FLOOR PANEL     			BOEING	727   	727281      	138408N	NM  										CABIN	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED IN FORWARD LAVATORY FLOOR PANEL FROM BULKHEAD TO STA 312.						2	L	7	3 	4F				A3WE    					 
1999040200512	19990402	00512	NM  	1999	4	2	99ZZZX1307       	1	19990212	G	5347		SEAT TRACK      			BOEING	727   	727281      	138408N	NM  										BS 1170-1110	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON SEAT TRACK STA 1070 - STA 1110, LBL 45.5						2	L	7	3 	4F				A3WE    					 
1999040200513	19990402	00513	NM  	1999	4	2	99ZZZX1308       	1	19990212	G	5347		SEAT TRACK      			BOEING	727   	727281      	138408N	NM  										BS 1130	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON SEAT TRACK STA 1130 LBL 24.75.						2	L	7	3 	4F				A3WE    					 
1999040200514	19990402	00514	NM  	1999	4	2	99ZZZX1309       	1	19990212	G	5320		SUPPORT         			BOEING	727   	727281      	138408N	NM  										CABIN	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED AT FORWARD LAVATORY FLOOR SUPPORT STA 312.						2	L	7	3 	4F				A3WE    					 
1999040200516	19990402	00516	NM  	1999	4	2	99ZZZX1311       	1	19990211	G	5510	65245712	BEAM            			BOEING	727   	727281      	138408N	NM  										HORIZONTAL STAB	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON RIGHT HORIZONTAL STABILIZER TRAILING EDGE UPPER BEAM.						2	L	7	3 	4F				A3WE    					 
1999040200517	19990402	00517	NM  	1999	4	2	99ZZZX1312       	1	19990212	G	5320	69459431	HINGE           			BOEING	727   	727281      	138408N	NM  										EMERGENCY EXIT	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON RT AFT EMERGENCY EXIT STEP HINGE.						2	L	7	3 	4F				A3WE    					 
1999040200518	19990402	00518	NM  	1999	4	2	99ZZZX1313       	1	19990212	G	5313		STRINGER        			BOEING	727   	727281      	138408N	NM  										BS 440	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED AT STA 440 ON STR 23R.						2	L	7	3 	4F				A3WE    					 
1999040200519	19990402	00519	NM  	1999	4	2	99ZZZX1314       	1	19990212	G	5320		SHEAR TIES      			BOEING	727   	727281      	138408N	NM  										BS 1130	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON NUMEROUS SHEAR TIES STA 1130 STR 28L - STR 28R.						2	L	7	3 	4F				A3WE    					 
1999040200520	19990402	00520	NM  	1999	4	2	99ZZZX1315       	1	19990211	G	5320		INTERCOSTAL     			BOEING	727   	727281      	138408N	NM  										BS 1070-1090	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON INTERCOSTAL STR 29R - STA 1070 - STA 1090.						2	L	7	3 	4F				A3WE    					 
1999040200521	19990402	00521	NM  	1999	4	2	99ZZZX1316       	1	19990212	G	5320		SHEAR TIES      			BOEING	727   	727281      	138408N	NM  										BS 1148	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON NUMEROUS SHEAR TIES AT STA 1148, STR 28L - STR 28R.						2	L	7	3 	4F				A3WE    					 
1999040200522	19990402	00522	NM  	1999	4	2	99ZZZX1317       	1	19990211	G	5320		SHEAR TIES      			BOEING	727   	727281      	138408N	NM  										BS 1166	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON NUMEROUS SHEAR TIES, STA 1166 STR 28L - STR 28R.						2	L	7	3 	4F				A3WE    					 
1999040200523	19990402	00523	NM  	1999	4	2	99ZZZX1318       	1	19990212	G	5313		STRINGER        			BOEING	727   	727281      	138408N	NM  										BS 1070-1130	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON STR 28L AT STA 1070 - STA 1130.						2	L	7	3 	4F				A3WE    					 
1999040200524	19990402	00524	NM  	1999	4	2	99ZZZX1319       	1	19990212	G	5522	65266613	PANEL           			BOEING	727   	727281      	138408N	NM  										LT ELEVATOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON LEFT ELEVATOR SKIN PANEL FORWARD OUTBOARD AREA.						2	L	7	3 	4F				A3WE    					 
1999040200525	19990402	00525	NM  	1999	4	2	99ZZZX1320       	1	19990212	G	5313		STRINGER        			BOEING	727   	727281      	138408N	NM  										BS 720	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON STR 27R, STA 720E - STA 720F.						2	L	7	3 	4F				A3WE    					 
1999040200526	19990402	00526	NM  	1999	4	2	99ZZZX1321       	1	19990211	G	5522	652564054	PANEL           			BOEING	727   	727281      	138408N	NM  										RT ELEVATOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON UPPER/LOWER SKIN PANEL, RT ELEVATOR STA 209 TO OUTBOARD TIP AND SKIN SEPARATING.						2	L	7	3 	4F				A3WE    					 
1999040200527	19990402	00527	NM  	1999	4	2	99ZZZX1322       	1	19990211	G	5522	652564056	PANEL           			BOEING	727   	727281      	138408N	NM  										RT ELEVATOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON UPPER/LOWER SKIN PANEL, RT ELEVATOR STA 209 TO OUTBOARD TIP AND SKIN SEPARATING.						2	L	7	3 	4F				A3WE    					 
1999040200528	19990402	00528	NM  	1999	4	2	99ZZZX1323       	1	19990211	G	5313		STRINGER        			BOEING	727   	727281      	138408N	NM  										BS 740	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON STR 27L AT STA 740.						2	L	7	3 	4F				A3WE    					 
1999040200529	19990402	00529	NM  	1999	4	2	99ZZZX1324       	1	19990211	G	5532		PANEL           			BOEING	727   	727281      	138408N	NM  										VERTICAL STAB	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON PANEL NR 9501, VERTICAL STABILIZER.						2	L	7	3 	4F				A3WE    					 
1999040200530	19990402	00530	NM  	1999	4	2	99ZZZX1325       	1	19990211	G	5330		SKIN            			BOEING	727   	727281      	138408N	NM  										BS 1166 - 1183	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED AT STA 1166 - STA 1183, RT BL ZERO ON SKIN.						2	L	7	3 	4F				A3WE    					 
1999040200531	19990402	00531	NM  	1999	4	2	99ZZZX1326       	1	19990210	G	5320		SHEAR TIE       			BOEING	727   	727281      	138408N	NM  										BS 480	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED AT STA 480, STR 22R ON SHEAR TIE TO FRAME.						2	L	7	3 	4F				A3WE    					 
1999040200532	19990402	00532	NM  	1999	4	2	99ZZZX1327       	1	19990210	G	5330		SKIN            			BOEING	727   	727281      	138408N	NM  										BS 440	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON SKIN AT STA 440, STR 20R (AROUND OXYGEN BLOW-OUT DISC AREA).						2	L	7	3 	4F				A3WE    					 
1999040200533	19990402	00533	NM  	1999	4	2	99ZZZX1328       	1	19990210	G	5330		SKIN            			BOEING	727   	727281      	138408N	NM  										BS 440	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON SKIN STA 440 AT STR 25R.						2	L	7	3 	4F				A3WE    					 
1999040200534	19990402	00534	NM  	1999	4	2	99ZZZX1329       	1	19990210	G	5730		SKIN            			BOEING	727   	727281      	138408N	NM  										LT WING	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED IN NUMEROUS AREAS OF UPPER SURFACE OF SKIN LT WING SPAR FORWARD OF NR 5 AND NR 6 SPOIL	ERS.					2	L	7	3 	4F				A3WE    					 
1999040200535	19990402	00535	NM  	1999	4	2	99ZZZX1330       	1	19990211	G	5522		SKIN            			BOEING	727   	727281      	138408N	NM  										LT ELEVATOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON SKIN PANEL LT ELEVATOR LOWER SURFACE (STA 17.2 - STA 53.5 APPROXIMATELY).						2	L	7	3 	4F				A3WE    					 
1999040200546	19990402	00546	WP  	1999	4	2	99ZZZX1340       	1	19990311	G	2910	34000831001559	LINE            			CVAC  	640   	640340D     	2422814	WP  										HYDRAULIC SYS	BROKEN          	C			WPAB	O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		AP	APPROACH       	1			SW	01	3410					27				ON APPROACH, HYDRAULIC SELECTOR WAS PUT TO DOWN POSITION, A THUD WAS HEARD FOLLOWED BY LOSS OF HYDRAULIC FLUID.  LANDING	 GEAR WAS EXTENDED BY FREE-FALL PROCEDURE.  LANDING WAS MADE WITHOUT A PROBLEM.					2	L	7	2 	4T			RT	A793    					 
1999040200547	19990402	00547	NM  	1999	4	2	99ZZZX1341       	1	19990211	G	5522		SKIN            			BOEING	727   	727281      	138408N	NM  										LT ELEVATOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION NOTED ON SKIN PANEL, LEFT ELEVATOR OUTBOARD MOST CORNER LOWER SURFACE TRAILING EDGE.						2	L	7	3 	4F				A3WE    					 
1999040200789	19990402	00789	NM  	1999	4	2	99ZZZX1342       	1	19990202	G	2810	4015779101	FUEL TANK       			BOEING	757   	7572J4      	1384966	NM  										FUSELAGE	RUPTURED        	B				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	770BB	1578 			8509238	25220				THE FORWARD AND AFT AUXILIARY FUEL TANKS WERE REMOVED AND RE-INSTALLED FOR FUSELAGE LOWER LOBE INSPECTION AND FUEL TANK 	INSPECTION.  AFTER RE-INSTALLATION, THE AUXILIARY TANKS WERE BEING FUELED FOR OPS AND LEAK CHECK.  DURING FUELING, THE F	ORWARD NR 4 AUXILIARY FUEL TANK RUPTURED.  THE CAUSE IS STILL BEING INVESTIGATED BY THE REPAIR STATION AND THE AUXILIARY	 FUEL TANK MANUFACTURER.			2	L	7	2 	4F			RT	A2NM    					 
1999040200790	19990402	00790	CE  	1999	4	2	99ZZZX1343       	2	19990308	G	8550		DIP STICK TUBE  			PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					ENGINE OIL	SEPARATED       	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	25	497MA					3449011	321353			ON BOTH ENGINES, THE DIP STICK TUBE HAS PULLED OUT OF THE ENGINE BLOCK.  THE TUBE IS HELD BY A RUBBER TUBE AND CLAMPS. T	T:  460.					1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999040200791	19990402	00791	SW  	1999	4	2	99ZZZX1344       	1	19990302	G	2841	407375006101	INDICATOR       			BELL  	407   	407         		SW  										COCKPIT	MALFUNCTIONED   	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	407WH	291  			0036	53027				H.A.S. REPLACED WITH NEW FUEL QUANTITY INDICATOR FROM BELL HELICOPTER.						1	G	7	1 	3U			O	H2SW    					 
1999040200792	19990402	00792		1999	4	2	99ZZZX1345       	4	19990215	G	2310	CI177	ANTENNA         			HUGHES	369   	369D        	4470706	WP  										FUSELAGE	BROKEN          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	1097J		977  		9725	900801D				TIP MISSING BAD RECEPTION.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999040200793	19990402	00793		1999	4	2	99ZZZX1346       	4	19990215	G	2312	KY296	TRANSCEIVER     			BELL  	206   	206B3       	1181506	SW  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY		1    		20678	2871				RADIO WILL NOT TRANSMIT AND WAS VERY WARM UPON REMOVAL.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999040200794	19990402	00794	SW  	1999	4	2	99ZZZX1347       	1	19990215	G	6730	206076031023	SERVO           			BELL  	206   	206B3       	1181506	SW  										FLT CONTROL	LEAKING         	B			LS1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13	206BY		3011 		RH1787	2871				LEAKS AT PILOT VALVE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999040200795	19990402	00795		1999	4	2	99ZZZX1348       	4	19990215	G	2312	KY196	TRANSCEIVER     			BELL  	206   	206B3       	1181506	SW  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY		743  		2512	2871				WILL NOT HOLD STATION AND SHUTS OFF INTERMITTENTLY.  SENT FOR REPAIR.						1	G	7	1 	3U				H2SW    					 
1999040200796	19990402	00796	SW  	1999	4	2	99ZZZX1349       	1	19990203	G	6720	206301052103	ACTUATOR        			BELL  	206   	206L4       	1182110	SW  										TAIL ROTOR	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	3310	245  			0061	52094				LINEAR ACTUATOR FAILED AT FULL STROKE WITH HIGH ALTITUDE.  TAIL ROTOR PITCH FIXED AT 100 PERCENT.  ACTT:  1,228.2 HOURS.						1	G	7	1 	3U			NC	H2SW    					 
1999040200797	19990402	00797	WP  	1999	4	2	99ZZZX1350       	1	19990215	G	6410	369D2161361	BLADE           			HUGHES	369   	369D        	4470706	WP  										TAIL ROTOR	DAMAGED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	500DC	4761 			6017	290456D				BLADE HAS VOID AND LIFTED ABRASION STRIP.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999040200798	19990402	00798	WP  	1999	4	2	99ZZZX1351       	1	19990215	G	7722	369A4521	INDICATOR       			HUGHES	369   	369D        	4470706	WP  										COCKPIT	STICKS          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	500DC		2854 		414	290456D				HANGS UP AT 250 DEGREES CELSIUS DURING START-UP.  BEFORE, 14 PERCENT N1 ON SECOND START OF DAY ENGINE LIGHT OFF.  REMOVE	D AND REPLACED.					1	G	7	1 	3U				H3WE    					 
1999040200799	19990402	00799	WP  	1999	4	2	99ZZZX1352       	1	19990215	G	6310	369A5350605	CLUTCH          			HUGHES	369   	369D        	4470706	WP  										ENGINE	MAKING METAL    	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	500DC		944  		7510	290456D				LOW OIL, BELOW MINIMUM.  METAL IN OIL AND DISCOLORED.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999040200800	19990402	00800	GL  	1999	4	2	99ZZZX1353       	2	19990219	G	7323	252476913	GOVERNOR        			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	5027P		1497 		26217	611002D				SURGING.  REMOVED AND REPLACED.  SENT FOR EVALUATION/REPAIR.						1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999040200801	19990402	00801		1999	4	2	99ZZZX1354       	4	19990215	G	3420	5050010902	GYRO            			BELL  	206   	206B        	1181511	SW  										COCKPIT	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	90322		555  		20168	1736				WILL NOT HOLD HEADING.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999040200802	19990402	00802	NE  	1999	4	2	99ZZZX1355       	2	19990211	G	7250	411105064	ROTOR ASSY      								LYC   	LTS101	LTS101650B1 	41560	NE  					GAS PRODUCER	ERODED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05		2383 			4407		LE45223			BLADES ERODED FORM CARBON BALL EROSION.  REMOVED AND REPLACED.											3	U			E5NE				 
1999040200805	19990402	00805	CE  	1999	4	2	99ZZZX1358       	1	19990302	G	2820	3011861	LINE            			CESSNA	421   	421C        	2076016	CE  										FUEL PRESSURE	CHAFED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	02	81RD	2383 				421C0291				THIS AIRCRAFT INCORPORATES PRATT & WHITNEY PT6-135A ENGINES INSTALLED IAW STC SA136150. INSPECTION REVEALED SEVERE CHAFI	NG OF THE SECONDARY FUEL PRESSURE TUBE ASSEMBLIES OF BOTH ENGINES APPROXIMATEY 2.50 INCHES AFT OF THE TUBE FORWARD ENDS 	DUE TO CONTACT WITH THE ALTERNATE AIR ACTUATOR BELLCRANK FULCRUM SHAFTS WHICH ARE MOUNTED ON THE LOWER COWLING HALVES.				1	L	7	2 	3O				A7CE    					 
1999040200806	19990402	00806	CE  	1999	4	2	99ZZZX1359       	1	19990310	G	2910	2607003368	LINE            			LEAR  	35    	35A         	5170602	CE  										HYDRAULIC SYSTEM	LEAKING         	B			DINR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	258G	4731 				443				DURING OPERATIONAL CHECKS OF HYDRAULIC SYSTEM (AFTER REPLACEMENT OF FLAP CONTROL VALVE), NOTED A HYDRAULIC LEAK OUT OF A	N ALUMINUM HYDRAULIC LINE, PN 260-7003-368, FOR THE FLAP EXTEND SYSTEM.  THE LEAK WAS FROM A CORROSION PIN HOLE ABOAUT 1	.50 INCHES FROM END OF LINE AND IN A 90 DEGREE BEND.  THE LINE IS PAINTED WITH ZINC CHROMATE INCLUDING THE AREA WITH THE	 PIN HOLE.  THE LINE APPEARS TO BE ORIGINAL.  THIS LINE IS LOCATED ABOVE THE WING, AFT OF THE LEFT MAIN WHEELWELL.			2	L	7	2 	4F				A10CE   					 
1999040200808	19990402	00808	EA  	1999	4	2	99ZZZX1361       	1	19990310	G	2434	ZCDB9A023	RELAY           			CNDAIR	CL600 	CL6002B16   	1900305	EA  										NR 1 GENERATOR	BROKEN          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	76CS	2653 				5103				NR 1 GENERATOR WOULD FALL OFF-LINE WHEN A BUS LOAD WAS APPLIED.  THE PROBLEM WAS ISOLATED TO THE NR 1 GENERATOR LINE CON	TACTOR.  WHEN REMOVED, TWO OF THE CONNECTING STUDS WERE BROKEN.  THIS IS THE SECOND RELAY, SAME PART NUMBER, REMOVED FRO	M THIS AIRCRAFT THAT HAS BROKEN STUDS.				2	L	7	2 	4F			RT	A21EA   					 
1999040200809	19990402	00809	EU  	1999	4	2	99ZZZX1362       	1	19990227	G	3000	1818001A	ANTI ICE VALVE  	DUKES       		AMD   	FALCON	FALCON20    	2730103	EU  										LT ENGINE	INOPERATIVE     	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	620A	1107 			0231	412				CREW SQUAWKED THE LEFT ENGINE ANTI-ICE VALVE AS INOPERATIONAL.  MAINTENANCE DEPT VERIFIED THE VALVE WAS CLOSED, AND POWE	R TO THE VALVE WAS NORMAL.  REPLACED VALVE AND OPS CHECK NORMAL.					2	L	7	2 	4F			RT	A7EU    					 
1999040200810	19990402	00810	GL  	1999	4	2	99ZZZX1363       	3	19990308	G	6114	C840139	HUB             			MTSBSI	MU2   	MU2*        		SW  						HARTZL	HCB4T	HCB4TN5     	GL  	PROPELLER	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05					CDA3086			CDA3086		HUB S/N CDA3086 WAS RETURNED FOR COMPLIANCE OF AD-95-01-02 AND SB'S A182A AND A183A.  AFTER REMOVAL OF THE PILOT TUBE FR	OM BLADE ARM NR 3, CORROSION WAS DISCOVERED AT THE BOTTOM OF THE BORE COVERING APPROXIMATELY 25 PERCENT OF THE SURFACE A	REA.  THE CORROSION WAS REPAIRED AND THE HUB RETURNED TO SERVICE.				1	H	7	2 	3T				A2PC    		6	C	P40EA	 
1999040200811	19990402	00811	CE  	1999	4	2	99ZZZX1364       	1	19990201	G	5350	504100529	SKIN            			BEECH 	100   	B100        	1152919	CE  										TAILCONE	CRACKED         	B	P		ERYR	O				OTHER                   				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			SO	11	CGTCL					BE130				PILOT REPORTED FLUTTER/VIBRATION IN-FLIGHT.  UPON INVESTIGATION, DISCOVERED TAILCONE CRACKED CIRCUMFERENTIALLY APPROXIMA	TELY 60 PERCENT, ABOUT 18 INCHES IN FROM TIP OF TAIL CONE.  FURTHER INVESTIGATION REVEALED SEVERAL SMALLER CRACKS BEGINN	ING AT STIFFENER FASTENER HOLES IN SEVERAL LOCATIONS.  STIFFENER COMPLETELY BROKEN IN TWO AT POINT WHERE SKIN CRACK INTE	RSECTS WITH EVIDENCE OF CHAFING WEAR ON BROKEN ENDS.  THIS APPEARS TO BE INITIAL CRACK PROPAGATION POINT AS THERE IS SOO	TING/DIRT IN EDGE OF CRACK FOR SEVERAL INCHES ON EITHER SIDE.		1	L	7	2 	4T				A14CE   					 
1999040200812	19990402	00812	CE  	1999	4	2	99ZZZX1365       	1	19990308	G	5210		FRAME           			BEECH 	300   	B300C       		CE  										PASSENGER DOOR	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	55947					FM3				UPON REMOVAL OF THE CABIN DOOR SEAL, FOUND SEVERE CORROSION AND A 9 INCH CRACK IN THE DOOR STEEL STRUCTURE JUST BELOW TH	E SEAL RETAINER NEAR THE AFT SIDE OF THE HINGE AREA.  AIRCRAFT TT:  2,441.4 HOURS.					2	L	7	2 	4T			RT	A24CE   					 
1999040200813	19990402	00813	SO  	1999	4	2	99ZZZX1366       	1	19990212	G	2400	29233002	RESISTOR        			PIPER 	PA31T 	PA31T2      	7103127	SO  										COCKPIT	FAILED          	B	L		GW1R	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			EA	03	58PL	2354 				31T8166024				PILOT REPORTED SMOKE IN COCKPIT AND STRONG BURNING ODOR.  INVESTIGATION REVEALED THE CIGAR LIGHTER RESISTOR BOARD, PN 29	233-002, OVERHEATED AND BURNED.  ALL THREE CIGAR LIGHTERS WERE CHECKED FOR SHORTS, NONE FOUND.  FUSE WAS FOUND TO BE OPE	RATIVE AND CORRECT AMPERAGE RATING -- SYSTEM WAS DEACTIVATED BY REMOVING FUSE, RESISTOR BOARD, AND CAPPED SYSTEM WIRING.				1	L	7	2 	3T			RT	A8EA    					 
1999040200814	19990402	00814		1999	4	2	99ZZZX1367       	4	19990320	G	2563	5415185	DRAG CHUTE      			LEAR  	55    	55LEAR      	5170702	CE  										TAIL	MISSING         	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	09	520SC					087				PILOT NOTICED DRAG CHUTE LID SEEMED LOOSE DURING PRE-FLIGHT INSPECTION.  PILOT (IA RATED) RE-SECURED LID AFTER CONSULTIN	G WITH MAINTENANCE.  AFTER MAKING NEXT SCHEDULED FLIGHT, PILOT NOTED DRAG CHUTE MISSING FROM AIRCRAFT.  PILOT NOTED NO A	BNORMALITIES DURING PREVIOUS FLIGHT. UNKNOWN WHEN DRAG CHUTE DEPARTED ACFT.  LEAR TECH REP INVESTIGATED AND FOUND DISCRE	PANCY WITH DRAG CHUTE LOCK RING AND DEPLOY MECHANISM.  IT APPEARS LOCK RING HAD INTERFERENCE WITH ROUND HEAD RIVETS WHER	E FLUSH HEAD RIVETS SHOULD HAVE BEEN INSTALLED.  MAINT IS FOLLOWING UP ON CORRECTIVE ACTION TO LOCK RING AND DEPLOY MECH	ANISM.  DRAG CHUTE ASSY IS NOTED IN ACFT RECORDS AS HAVING BEEN INSTALLED BY LEARJET 11 YEARS PRIOR TO THIS INCIDENT.	2	L	7	2 	4F				A10CE   					 
1999040200815	19990402	00815	SO  	1999	4	2	99ZZZX1368       	1	19990308	G	3230	4081011	PIN             			GULSTM	G1159 	G1159       	3953505	SO  										MLG	MISMANUFACTURED 	B	P		RO3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03	623MW					94				WHILE ACCOMPLISHING LT MAIN GEAR SIDE BRACE FITTING PIN INSPECTION, INSP REQUIRED THE SIDE BRACE ACTUATOR BE REMOVED TO 	INSPECT THE UPPER SIDE BRACE PIN.  INSP REQUIRED TO CHECK AND INSPECT PIN, BUSHING, AND ATTACHING HARDWARE FOR CORROSION	, GALLING AND FRETTING.  REPLACED COMPONENTS AS REQUIRED.  NOTED SIDE BRACE PIN INSIDE DIAMETER WHERE TIE ROD PASSES THR	OUGH WAS SCARRED AND HEAVY MACHINE MARKS EVIDENT.  PIN WAS REJECTED AND REMOVED.  A NEW PIN WAS ORDERED AND RECEIVED IN 	THE SAME CONDITION (HEAVY MACHINE MARKING).  THE NEW PIN WAS REJECTED AND A SECOND PIN RECEIVED AND INSTALLED.  RECOMMEN	D ALL SIDE BRACE PINS BE CHECKED FOR DAMAGE AND HEAVY MACHINE MARKINGS.  MFG INDICATED THIS WAS ACCEPTABLE.	2	L	7	2 	4F			RT	A12EA   					 
1999040200817	19990402	00817		1999	4	2	99ZZZX1370       	4	19990306	G	3417	8220842142	COMPUTER        	COLLINS     		CNDAIR	CL600 	CL6002B16   	1900305	EA  										COCKPIT	FAILED          	B			SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	555WD	282  			3271	5355				DURING TOLERANCE CHECK OF THE R.V.S.M. REQUIREMENTS OF T.L.M.C. OF 604 MM, IT WAS NOTED THE A.D.C. DID NOT MEET THE TOLE	RANCES CALLED OUT.  THE FAILED UNIT WAS REMOVED AND SENT BACK TO THE MFG FOR REPAIR.  REPLACMENT (REPAIRED) UNIT WAS INS	TALLED IN ITS PLACE.				2	L	7	2 	4F			RT	A21EA   					 
1999040200818	19990402	00818		1999	4	2	99ZZZX1371       	4	19990306	G	3417	8220842142	COMPUTER        	COLLINS     		CNDAIR	CL600 	CL6002B16   	1900305	EA  										COCKPIT	FAILED          	B			SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	555WD	282  			3360	5355				DURING THE TOLERANCE CHECK OF THE R.V.S.M. REQUIREMENTS OF T.L.M.C. OF 604 MM, IT WAS NOTED THAT THE A.D.C. DID NOT MEET	 THE TOLERANCES CALLED OUT.  THE FAILED UNIT WAS REMOVED AND SENT BACK TO THE MFG FOR REPAIR.  REPLACEMENT (REPAIRED UNI	T WAS INSTALLED IN ITS PLACE.				2	L	7	2 	4F			RT	A21EA   					 
1999040200819	19990402	00819	CE  	1999	4	2	99ZZZX1372       	1	19990322	G	3320	PWFLC28	POWER SUPPLY    	PRECISION   		BEECH 	200   	200BEECH    	1152920	CE  										BS 198	FAILED          	D		A		K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			SO	07	4430V	482  				BB323				THIS AIRCAFT WAS IN THE SHOP FOR AN INSPECTION.  THREE TO FOUR MINUTES AFTER TURNING ON ELEC POWER, SMOKE WAS SEEN COMIN	G FROM AROUND THE THIRD CABIN WINDOW, FROM AFT, ON THE LT SIDE OF THE ACFT.  REMOVED WINDOW TRIM TO EXPOSE FLUORESCENT L	IGHT AND POWER SUPPLY.  POWER SUPPLY HAD BEEN VERY HOT AND WAS THE SOURCE OF SMOKE.  THE INTERIOR LIGHT SWITCH HAD BEEN 	LEFT IN THE DIM POSITION.  REPLACED THE POWER SUPPLY AND NO OTHER PROBLEMS NOTED.			1	L	7	2 	4T				A24CE   					 
1999040200820	19990402	00820	NM  	1999	4	2	99ZZZX1373       	1	19990312	G	7830		T/R UNIT        			DOUG  	MD11  	MD11        	3023602	NM  										RT ENGINE	BROKEN          	H				C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			WP	03	105ZV				D1292	48544				PILOT ABORTED TAKEOFF DUE TO HEARING THE WARNING AND 'STABILIZER' MESSAGE APPEARED DURING TAKEOFF IN ANC.  CAUSED THE RT	 T/R COWLING TO BREAK.  ZVA SENT ONE SERVICEABLE RT T/R COWLING TO ANC FOR REPLACING ON 3-12-99.					2	L	7	3 	4F			RT	A22WE   					 
1999040200821	19990402	00821	CE  	1999	4	2	99ZZZX1374       	1	19990309	G	5297		WIRE            			LEAR  	35    	35A         	5170602	CE  										LATCH PIN SWITCH	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	111KK	7338 				425				WHILE C/W LEARJET SB 35/36-52-10 (UPPER CABIN DOOR TORSION BAR ARM ASSEMBLIES); IT WAS FOUND THAT THE SHEATHING AND ALL 	THE WIRES INSIDE IT WERE BROKEN.  THESE WIRES ARE FOR THE UPPER DOOR LATCH PIN SWITCHES.  ACCORDING TO CHAPTER 52-10-10,	 PAGE 3 OF THE LEARJET 35 WIRING MANUAL, THESE SWITCHES GIVE A GROUND TO THE DOOR UNSAFE LIGHT.  WITH THESE WIRES BROKEN	, THERE WOULD BE NO LIGHT EVEN WITH THE 2 CENTER LATCH PINS NOT LATCHED.  THIS FAILURE WAS CAUSED BY REPETITIVE CABIN DO	OR OPENING AND CLOSING.		2	L	7	2 	4F			 	A10CE   					 
1999040200822	19990402	00822	NE  	1999	4	2	99ZZZX1375       	2	19990310	G	7320		CDP LINE        			DOUG  	DC10  	DC1030F     	3023504	WP  	GE    	CF6   	CF650C2     	30018	NE  					NR 3 ENGINE	CONTAMINATED    	H			M8BR	A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CL	CLIMB          	1			WP	33	10MB					47907	455137			TEN MINUTES AFTER T/O OUT OF NARITA ON CLIMBING TO 10,000 FEET, CREWS NOTICED NR 3 ENGINE POWER LAGGING BEHIND COMPARED 	WITH ENG 1 AND ENG 2.  ATTEMPTS TO RESTORE NORMAL POWER TO THAT ENGINE FAILED AND ACFT MADE AN ATB.  DURING T/S, CHECKED	 MAIN FUEL FILTER AND LEAK CHECK CIT SENSOR OKAY.  REMOVED CDP LINE, CLEANED AND BLEW OUT LINE WITH SHOP AIR TO DISLODGE	 ANY FOREIGN MATERIALS.  RE-INSTALLED LINE, ACFT TOWED FOR POWER ASSURANCE RUN.  FOUND SATISFACTORY.  POSSIBLE CAUSE COU	LD BE DUE TO PLUGGING OF AN ORIFICE IN THE CDP TUBE WHICH RESTRICTS AIR FLOW TO THE MEC.  GE RECOMMENDED CDP LINE BE REM	OVED FROM ENG ONLY DURING SHOP VISIT AND CLEANED, SUBMITTER WILL DISLODGE ANY FOREIGN MAT'L COLLECTED AS RECOMMENDED BY	2	L	7	3 	4F	4	F	RT	A22WE   	E23EA				 
1999040200823	19990402	00823	CE  	1999	4	2	99ZZZX1376       	1	19990311	G	2710	MS276454	BEARING         			LEAR  	35    	35A         	5170602	CE  										LT WING	ROUGH           	B	P	A	TJ4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	11	593LR					593				AILERONS FELT A LITTLE STIFF IN FLIGHT.  CHECKED FOR FREEDOM OF MOVEMENT AND GROUND BY MOVING AILERONS UP AND DOWN BY HA	ND.  NO ABNORMALITIES NOTED.  WHILE RESTRICTING AILERON MOVEMENT BY HOLDING PRESSURE ON THE AILERON SURFACE, ROUGH BEARI	NGS WERE NOTED.  ALL THREE BEARINGS IN BOTH DRIVE YOKES WERE REPLACED.  FLIGHT CHECK GOOD.  ACFT TT:  5,912.0 HOURS.				2	L	7	2 	4F				A10CE   					 
1999040200824	19990402	00824	CE  	1999	4	2	99ZZZX1377       	1	19990311	G	2710	MS276454	BEARING         			LEAR  	35    	35A         	5170602	CE  										RT WING	ROUGH           	B		A	TJ4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	11	593LR					593				AILERONS FELT A LITTLE STIFF IN FLIGHT.  CHECKED FOR FREEDOM OF MOVEMENT AND GROUND BY MOVING AILERONS UP AND DOWN BY HA	ND.  NO ABNORMALITIES NOTED.  WHILE RESTRICTING AILERON MOVEMENT BY HOLDING PRESSURE ON THE AILERON SURFACE, ROUGH BEARI	NGS WERE NOTED.  ALL THREE BEARINGS IN BOTH DRIVE YOKES WERE REPLACED.  FLIGHT CHECK GOOD.  ACFT TT:  5,912.0 HOURS				2	L	7	2 	4F				A10CE   					 
1999040200826	19990402	00826	EU  	1999	4	2	99ZZZX1379       	1	19990310	G	3510	25SF16379	LINE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										COCKPIT	CORRODED        	D	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	290EC	4610 				NA0444				WHILE PERFORMING RAYTHEON SB 35-3034 REPLACEMENT OF OXYGEN FITTINGS, FOUND OXYGEN LINE, PN 25SF1637-9, LOCATED AT FRAME 	7 CORRODED ABOVE SLEEVE AT T-FITTING END.  CAUSE OF CORROSION BELIEVED TO BE INSULATING BLANKET MADE FROM ULTRASUEDE LYI	NG AGAINST THE LINE ON THE UNPAINTED PORTION OF SAID LINE.  WHEN OXYGEN PRESSURE WAS RE-APPLIED TO SYSTEM, A SEVERE LEAK	 PRESENTED ITSELF AT THIS POINT.  ACFT LANDINGS:  3,670.			2	L	7	2 	4F			RT	A3EU    					 
1999040200827	19990402	00827	CE  	1999	4	2	99ZZZX1380       	1	19990316	G	3233	2341123023	PILLER ASSY     			LEAR  	60    	60LEAR      	5170707	CE  										RT MLG ACTUATOR	CRACKED         	B			KW3R	A				UNSCHED LANDING         				J			WARNING INDICATION        			NR	NOT REPORTED   	1			WP	07	50776					146				AIRCRAFT ABORTED FLIGHT DUE TO RT MAIN GEAR UNSAFE LIGHT ILLUMINATED.  INSPECTED LANDING GEAR AND FOUND THE RT MAIN GEAR	 ACTUATOR PILLER ASSY WAS CRACKED AT WELDED JOINT.   INSPECTED AREA AROUND PILLER ASSY AND FOUND NO OTHER DAMAGE.  INSTA	LLED NEW PILLER ASSY.				2	L	7	2 	4F			RT	A10CE   					 
1999040200828	19990402	00828	EA  	1999	4	2	99ZZZX1381       	1	19990304	G	2913	6310806	PUMP            			CNDAIR	CL600 	CL6002B16   	1900305	EA  										HYDRAULIC SYSTEM	FAILED          	B			G1FR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	13	1622	602  			255785	5077				DURING FLIGHT, CREW NOTICED A COMPLETE LOSS OF PRESSURE ON THE NR 3 HYDRAULIC SYSTEM, SUBSEQUENTLY, MAKING A PRECAUTIONA	RY UNSCHEDULED LANDING WITHOUT INCIDENT.  AS HALF OF THE MAIN WHEEL BRAKES OPERATE FROM THE NR 3 HYDRAULIC SYSTEM AND TH	E OTHER HALF OPERATE FROM THE NR 2 SYSTEM, THIS LEFT ONLY HALF OF BRAKING SYSTEM TO STOP ACFT.  INSP AND T/S REVEALED A 	SHAFT SEAL ON THE NR 3 HYDRAULIC MECHANICAL PUMP AND MOTOR ASSY WAS LEAKING DUE TO FAILING AND LOOSE MOTOR BEARING.  REM	OVED AND REPLACED NR 3 HYDRAULIC PUMP, PN 63108-06 AND MOTOR ASSY, PN 9008015-2; INSTALLING REPAIRED AND OVERHAULED UNIT	S.	2	L	7	2 	4F			RT	A21EA   					 
1999040200829	19990402	00829		1999	4	2	99ZZZX1382       	1	19990308	G	5242	1052659	HOUSING         																	E/E BAY DOOR	CRACKED         	B	P		R1XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	09										PART IS FROM B747 ELECTRONIC ACCESS DOOR (PRESSURIZED).  FOUND CRACKED (AS REMOVED) IN TWO COMPONENTS.  TIME ON PART UNK	NOWN.  SUGGEST MORE FREQUENT INSPECTION OF THIS ASSEMBLY.																		 
1999040200830	19990402	00830	EA  	1999	4	2	99ZZZX1383       	3	19990222	G	6111		BOLT            			DIAMON	DA20  	DA20C1      	2990001	GL  						SNSNCH	W69EK	W69EK63     	EA  	PROPELLER	SHEARED         	B		A	OG5R	O				OTHER                   				E			VIBRATION/BUFFET          			CL	CLIMB          	1			GL	21	233ND	40   				C0033		78389		PILOT REPORTED SEVERE VIBRATION ON CLIMB-OUT.  UPON INITIAL INSPECTION, FOUND SPINNER CRACKED.  UPON REMOVAL OF SPINNER,	 FOUND 5 OUT OF THE 6 PROP BOLTS SHEARED.  AIRCRAFT MANUFACTURER NOTIFIED.					1	L	7	1 	3O			NT	TA4CH   		5	N	TA4CH	 
1999040200831	19990402	00831	EA  	1999	4	2	99ZZZX1384       	3	19990222	G	6114		HUB             			DIAMON	DA20  	DA20C1      	2990001	GL  						SNSNCH	W69EK	W69EK63     	EA  	PROPELLER	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	206ND					C0020		78389		ON 100-HOUR INSPECTION, CHECKED PROPELLER BOLT TORQUE.  NOTED WERE NOT TO SPECS.  RE-TORQUED AND RE-SAFETIED.  RE-CHECKE	D TORQUE AFTER 10 HOURS OF TACH TIME.  FOUND NOT TO SPECS.  REMOVED PROPELLER TO INSPECT PROP HUB, MOUNT HOLES, ETC.  FO	UND A CRACK EXTENDING .50 INCH FROM ONE BOLT HOLE TO A DEPTH OF .0625 INCH.  CONTACTED FACTORY, REMOVED PROPELLER FROM S	ERVICE AND SENT TO FACTORY FOR INSPECTION OR REPAIR.			1	L	7	1 	3O			NT	TA4CH   		5	N	TA4CH	 
1999040900073	19990409	00073	SO  	1999	4	9	99ZZZX1387       	2	19990122	G	8530		CYLINDERS       			CESSNA	210   	210L        	2073448	CE  	CONT  	O520  	IO520L      	17032	SO  					ENGINE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	27JR		1354 			21059706	270093R			CYLINDERS WERE FOUND CRACKED DURING COMPRESSION CHECKS. THE ONLY WAY THE CRACKS WERE FOUND WAS BY USING LEAK CHECK FLUID	 AS THE COMPRESSION CHECKS WERE GOOD. NR 6 CYLINDER WAS REPLACED AT 50.0 HOURS PRIOR TO THIS BECAUSE OF A CRACK.  THE CR	ACKS ARE ALL EMANATING FROM THE UPPER SPARK PLUG HOLES OVER AND PAST THE INJECTOR HOLES.  THIS ENGINE WAS OVERHAULED BY 	T.W. SMITH ENGINE CO. IN CINCINNATI, OHIO.			1	H	7	1 	3O	3	O		3A21    	E5CE				 
1999040900074	19990409	00074	CE  	1999	4	9	99ZZZX1388       	1	19990222	G	7810	642067	EXHAUST STACK   			BEECH 	58    	58TC        	1152746	CE  										ENGINE	MISOVERHAULED   	B			R2JR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	21	23712					TK67				DURING ANNUAL INSPECTION, INSPECTORS FOUND ENGINE MOUNT PN 102-91002B-131 PARTIALLY GROUND AWAY. CHARGER ILLEGALLY REPAI	RED AND WOULD NOT FIT PROPERLY. PARTIES UNKNOWN GROUND AWAY MAJOR ENGINE TRUSS TO ALLOW INSTALLATION OF AN IMPROPER PART	.  PER RAYTHEON, TRUSS REQUIRED MAJOR REPAIR.  NEW FACTORY EXHAUST STACK INSTALLED.  TRUSS REQUIRED REMOVAL AND WAS SENT	 OUT TO APPROVED CRS FOR REPAIR.  VERY EXPENSIVE REPAIR FOR ACFT OWNER.  THIS AIRCRAF'TS RECORDS SHOWED ACFT NOT MAINTAI	NED AT AN FAA APPROVED CRS.		1	L	7	2 	3O				A23CE   					 
1999040900075	19990409	00075	EA  	1999	4	9	99ZZZX1389       	2	19990307	G	8530		PUSH ROD        			MOONEY	M20   	M20J        	5870219	SW  	LYC   	O360  	IO360A1B6   	41514	EA  					ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	1083L					243398				TWO SEPARATE ENGINE FAILURES BEFORE CYLINDER REPLACED UNDER WARRANTY BY LYCOMING. SIGNIFICANT ALUMINUM FILINGS IN OIL SI	NCE REPLACEMENT.					1	L	7	1 	3O	3	O		2A3     	1E10				 
1999040900076	19990409	00076	CE  	1999	4	9	99ZZZX1390       	1	19990127	G	2710	05600156	YOKE ASSY       			CESSNA	172   	172R        	2072401	CE  										COCKPIT	MALFUNCTIONED   	B	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	4HP	461  				17280302				LEFT UPPER SIDE OF CONTROL YOKE ROLLER IS DISENGAGING FROM SUPPORT GUIDE WHEN SIDE PRESSURE IS APPLIED TO YOKE. CESSNA H	AS FOUND THAT THE CONTROL YOKES IN ARE NOT WELDED CORRECTLY. REPLACED YOKE AND LEFT GUIDE SUPPORT, OPS CHECKS NORMAL.					1	H	7	1 	3O			NT	3A12    					 
1999040900077	19990409	00077	CE  	1999	4	9	99ZZZX1391       	1	19990127	G	2710	05130893	GUIDE ASSY      			CESSNA	172   	172R        	2072401	CE  										FUSELAGE	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	4HP	461  				17280302				LEFT UPPER SIDE OF CONTROL YOKE ROLLER IS DISENGAGING FROM SUPPORT GUIDE WHEN SIDE PRESSURE IS APPLIED TO YOKE. CESSNA H	AS FOUND THAT THE CONTROL YOKES IN ARE NOT WELDED CORRECTLY. REPLACED YOKE AND LEFT GUIDE SUPPORT, OPS CHECKS NORMAL.					1	H	7	1 	3O			NT	3A12    					 
1999040900078	19990409	00078	CE  	1999	4	9	99ZZZX1392       	1	19990127	G	2710	05600156	YOKE ASSY       			CESSNA	172   	172R        	2072401	CE  										COCKPIT	MALFUNCTIONED   	B	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	25	858CP	20   				17280539				DURING INSPECTION FOUND LEFT UPPER YOKE ROLLER DISENGAGING FROM SUPPORT GUIDE. REPLACED YOKE ASSY AND LEFT GUIDE SUPPORT	. OPS CHECKS NORMAL.					1	H	7	1 	3O			NT	3A12    					 
1999040900079	19990409	00079	CE  	1999	4	9	99ZZZX1393       	1	19990127	G	2710	05130893	GUIDE           			CESSNA	172   	172R        	2072401	CE  										FUSELAGE	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	25	858CP	20   				17280539				DURING INSPECTION FOUND LEFT UPPER YOKE ROLLER DISENGAGING FROM SUPPORT GUIDE. REPLACED YOKE ASSY AND LEFT GUIDE SUPPORT	. OPS CHECKS NORMAL.					1	H	7	1 	3O			NT	3A12    					 
1999040900081	19990409	00081	GL  	1999	4	9	99ZZZX1395       	3	19990315	G	6114		PROPELLER       			CESSNA	172   	172P        	2072436	CE  						MCAULY	1C160	1C160DTM    	GL  	HUB	CRACKED         	H			CE8S	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	5302K	2911 				17274054		735877		PROPELLER REMOVED FOR OVERHAUL. FOUND TO BE CRACKED.						1	H	7	1 	3O			NT	3A12    		5	N	P910	 
1999040900082	19990409	00082	SO  	1999	4	9	99ZZZX1396       	1	19990303	G	2434	ALV95102L	ALTERNATOR      	PRESTOLITE  		PIPER 	PA31  	PA31P       	7103120	SO  										ENGINE	FAILED          	B			EKIR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	252MA		46   		8031639	31P33				ALTERNATOR OVERHAULED 5-21-98. INSTALLED 1-11-99. ONLY HAD 46.3 HOURS PRIOR TO FAILURE.						1	L	7	2 	3O				A8EA    					 
1999040900083	19990409	00083	SO  	1999	4	9	99ZZZX1397       	1	19990303	G	8011	LW18506	SUPPORT         			PIPER 	PA44  	PA44180     	7104402	SO  										STARTER	MISMANUFACTURED 	B			NX42	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	15	921ER	1804 				4496008				REAR V-BELT GROOVE CASTING MATERIAL THICKNESS OF APPROXIMATELY .024 INCH IS CONSIDERED INSUFFICIENT AND RESULTS IN THE R	EAR V-BELT GROOVE BEING HIGHLY PRONE TO BREAKAGE. THIS IS ONE OF THREE SEPARATE OCCURRENCES OF REAR V-BELT GROOVE BREAKA	GE NOTED THAT SEEM ISOLATED TO PN LW-18506 STARTER RING GEAR SUPPORT ASSEMBLIES. ONE STARTER RING GEAR SUPPORT WAS FOUND	 BROKEN WHEN RECEIVED FROM THE MANUFACTURER.			1	L	7	2 	3O				A19S0   					 
1999040900085	19990409	00085	CE  	1999	4	9	99ZZZX1399       	1	19990224	G	2510	10253004019	ESCUTCHEON      			BEECH 	36    	A36         	1151604	CE  										BREAKER PANEL	DAMAGED         	B			PAIR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	363MB	151  				E3143				THE SPECIFIC PART LISTED IS THE FRAME WORK WHICH HOLDS THE SIDEWALL CIRCUIT BREAKER PANEL SECURED. THIS FRAME WORK IS MA	DE OF PLASTIC. SUBMITTER STATED IT BREAKS VERY EASILY AND COULD CAUSE ELECTRICAL FAILURE.					1	L	7	1 	3O				3A15    					 
1999040900086	19990409	00086	CE  	1999	4	9	99ZZZX1400       	1	19990107	G	2500	161102101	LOCK            			CESSNA	182   	182S        	2072701	CE  										SEAT	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	07	820HP	518  				18280115				PILOT AND COPILOT CONTROL ASSEMBLY SEAT LOCKS PN 1611021-01 ARE MOUNTED WITH 2 SCREWS. THESE 2 SCREWS VIBRATING LOOSE. C	ONTROL COULD FALL OFF CAUSING PILOT OR COPILOT NOT TO  BE ABLE TO MOVE SEAT.  SCREWS HAVE NO LOCKING DEVICE.  PILOT AND 	COPILOT SEAT, PN 0514212-3 AND -4.				1	H	7	1 	3O			NT	3A13    					 
1999040900087	19990409	00087	EA  	1999	4	9	99ZZZX1401       	2	19990303	G	7414	4371	MAGNETO         	SLICK       		PIPER 	PA28  	PA28161     	7102803	SO  	LYC   	O320  	O320D3G     	41508	EA  					ENGINE	FAILED          	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	153ER	757  			97050745	2841178				WHEN THE MAGNETO WAS DISASSEMBLED, NOTED THE BEARING CAP ASSEMBLY HAD WORN ENOUGH TO BECOME A LOOSE FIT IN THE MAGNETO H	OUSING RESULTING IN CONTACT BETWEEN THE ROTOR AND POLE SHOES DURING OPERATION. THE BEARING CAP ASSEMBLY RETAINING HARDWA	RE WAS STILL IN A TORQUED CONDITION.				1	L	7	1 	3O	3	O		2A13    	E274				 
1999040900088	19990409	00088	CE  	1999	4	9	99ZZZX1402       	1	19990201	G	2820		LINE            			CESSNA	500   	560CESSNA   	2076750	CE  										FUEL SYSTEM	LOOSE           	B			JGVR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CE	09										LOW FUEL PRESSURE LIGHT COMES ON INTERMITTENTLY. AFTER 3 AIRCRAFT HAD TROUBLE, DISCOVERED FUEL LINES WERE LEFT LOOSE AT 	FACTORY INSIDE FUEL CELL.					2	L	7	2 	4F			RT	A22CE   					 
1999040900089	19990409	00089	CE  	1999	4	9	99ZZZX1403       	1	19990201	G	3340		LENS            			CESSNA	500   	560CESSNA   	2076750	CE  										TAIL	BROKEN          	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09										AIRCRAFT EQUIPPED WITH TALL FLOOD LIGHTS, LENS HAVE A 80 PERCENT FAILURE RATE, OFTEN PARTS OF LENS ARE MISSING ALLOWING 	WATER TO ENTER HORIZONTAL STABILIZER.					2	L	7	2 	4F			RT	A22CE   					 
1999040900090	19990409	00090	GL  	1999	4	9	99ZZZX1404       	1	19990202	G	3230		MOTOR           			CULVER	TD2C1 	TD2C1       	8730420	GL  										MLG	FAILED          	G	P			O				OTHER                   				O			OTHER                     			LD	LANDING        	1			WP	23	2775	334  				4559043				AIRCRAFT WAS ON APPROACH FOR LANDING. THE CONTROL TOWER REPORTED SEEING THREE LANDING GEAR IN THE DOWN POSITION. UPON TO	UCHDOWN, THE LANDING GEAR COLLAPSED.  THE LINK/RETRACTING MOTOR WHICH IS A 12 INCH ROD ATTACHING THE GEAR MOTOR TO THE G	EAR TRAIN, FAILED UNDER COMPRESSION FORCES AND ULTIMATELY BROKE IN TWO RESULTING IN THE GEAR COLLAPSING.				1	L	7	1 	3O			RT	CAR9    					 
1999040900091	19990409	00091		1999	4	9	99ZZZX1405       	2	19990211	G	8530		PISTON          			AMTR  		SEAWIND3000 			LYC   		IO540*      							NR 2 CYLINDER	FAILED          	G				B	A			EMER. DESCENT           	UNSCHED LANDING         			R			PARTIAL RPM/PWR LOSS      			CL	CLIMB          	1			SO	14	76SW	331  				008	L853148			DURING CLIMB, ENGINE LOST POWER. AIRCRAFT MADE EMERGENCY LANDING. NR 2 PISTON HAD HOLE THROUGH SIDE IN RING LAND AREA. N	OSE SEAL DISLODGED, ALL OIL LOST OVERBOARD.  CRANKSHAFT BEARINGS OVERHEATED.  BAD MAG DROP REPAIRED BY CLEANING PLUGS PR	IOR TO FLIGHT.							0 										 
1999040900092	19990409	00092	CE  	1999	4	9	99ZZZX1406       	1	19990301	G	2701	051178216	CONTROL YOKE    			CESSNA	172   	172G        	2072420	CE  										COCKPIT	CRACKED         	D	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	10	6070R	3030 				17253739				WHILE TIED DOWN, AIRCRAFT SUBJECTED TO TAILWINDS REPORTEDLY AS HIGH AS 77 KNOTS. CONTROL LOCK IN PLACE, NO SURFACE CONTR	OL GUST LOCKS INSTALLED. AIRCRAFT OWNERS FIRST NOTED SLIGHT ELEVATOR DROOP FROM NORMAL 'LOCKED' POSITION, ATTRIBUTED TO 	STRETCHED CABLES. NEXT DAY, ELEVATOR IN FULL DOWN POSITION.  INVESTIGATION REVEALED FAILURE OF CONTROL YOKE CENTER COLUM	N BETWEEN PIVOT BOLT AND ELEVATOR BELLCRANK.  TUBE BEARING AT BOTTOM.  EXAMINATION OF COLUMN INTERIOR REVEALED HEAVY COR	ROSION IN AREA OF BREAK.		1	H	7	1 	3O			NT	3A12    					 
1999040900093	19990409	00093	CE  	1999	4	9	99ZZZX1407       	1	19990125	G	3210	071349561	BRACKET         			CESSNA	185   	A185F       	2072821	CE  	CONT  	O520  	IO520D      	17032	SO  					MLG	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	05	78RD					18503676				BRACKET HAD INTERGRANULAR CORROSION ON THE BOTTOM OF THE MAIN LANDING GEAR CUT.						1	H	7	1 	3O	3	O		3A24    	E5CE				 
1999040900095	19990409	00095	CE  	1999	4	9	99ZZZX1409       	1	19990301	G	2750		TORQUE TUBE     			CESSNA	340   	340CESSNA   	2076404	CE  										TE FLAP	DAMAGED         	B			PG2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	11	387MC	4000 				3400509				WHILE MOVING THE FLAP MOTOR AND GEARBOX ASSY PER STC SA474NW, DISCOVERED DAMAGE TO THE FLAP DRIVE TORQUE TUBES, PN 31B16	4-3. UPON REMOVAL OF THE TORQUE TUBES, DISCOVERED WEAR ON THE TUBES WHERE THEY PASS THROUGH THE FUSELAGE. THE SEAL ASSY 	(PN 21158-0013, RETAINER ASSY, PN 34172-11) FOR THE LT TORQUE TUBE HAD FAILED CAUSING THE TORQUE TUBE TO RUB AGAINST THE	 RETAINER HOUSING OF THE SEAL.  THIS CAUSED A GROOVE TO FORM INTO THE TORQUE TUBE. THIS GROOVE WAS APPROX  HALF THE WALL	 THICKNESS OF THE TUBE.  THE RT TORQUE TUBE SEAL WAS FOUND INTACT; THE TUBE WAS STARTING TO FORM A GROOVE AT THE SEAL CO	NTACT AREA.  THE TUBE SHOWED SIGNS OF WEAR CAUSED BY MOVEMENT OTBD AND INBD BETWEEN FLAP JACK SCREW AND FLAP GEARBOX.	1	L	7	2 	3O				3A25    					 
1999040900096	19990409	00096	CE  	1999	4	9	99ZZZX1410       	1	19990305	G	3230	504501033	TORQUE TUBE     			CESSNA	310   	310Q        	2074242	CE  										LT MLG	CRACKED         	B			AHTR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	11	69836					310Q1009				RT AND LT MLG TORQUE TUBES WERE REMOVED DURING INSTALLATION OF SK414-8E. BOTH WERE FOUND CRACKED AT THE WELD AREA FOR TH	E FORK BOLT BOSS.					1	L	7	2 	3O				3A10    					 
1999040900097	19990409	00097	CE  	1999	4	9	99ZZZX1411       	1	19990305	G	3230	504501032	TORQUE TUBE     			CESSNA	310   	310Q        	2074242	CE  										RT MLG	CRACKED         	B			AHTR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	11	69836					310Q1009				RT AND LT MLG TORQUE TUBES WERE REMOVED DURING INSTALLATION OF SK414-8E. BOTH WERE FOUND CRACKED AT THE WELD AREA FOR TH	E FORK BOLT BOSS.					1	L	7	2 	3O				3A10    					 
1999040900098	19990409	00098	CE  	1999	4	9	99ZZZX1412       	1	19990313	G	7603		THROTTLE CONTROL			CESSNA	150   	152         	2071835	CE  										LEVER	SEPARATED       	H				O				OTHER                   				F			FLT CONT AFFECTED         			AP	APPROACH       	1			NM	03	89732					15282846				WHILE LANDING AT INDEPENDENCE, MO, PULLED BACK ON THE THROTTLE AND THE THROTTLE KNOBS AND SHAFT DISCONNECTED AT THE CABL	E AND CAME OUT OF THE INSTRUMENT PANEL. ENGINE RPM WAS LOCKED AT 1,000 RPM. NOTIFIED THE TOWER OF THE PROBLEM AND LANDED	 WITHOUT INCIDENT.				1	H	7	1 	3O			NT	3A19    					 
1999040900099	19990409	00099	CE  	1999	4	9	99ZZZX1413       	1	19990222	G	2720		CABLES          			BEECH 	58    	58TC        	1152746	CE  										RUDDER	MISINSTALLED    	B	P		R2JR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	21	23712	3122 				TK67				WHEN C/W ANNUAL INSPECTION, FOUND CABLE FOR RUDDER ROUTED ACROSS FS 271.92 BULKHEAD INSTEAD OF THROUGH IT. THIS CAUSED A	 CHAFING NOISE. CABLE TENSION WAS WAY OUT OF LIMITS ON THE LOW SIDE, SO NO 'SAWING' DAMAGE WAS NOTICED.  COMPONENTS INSP	ECTED AND RESTORED TO PROPER SPECIFICATIONS.				1	L	7	2 	3O				A23CE   					 
1999040900100	19990409	00100	GL  	1999	4	9	99ZZZX1414       	3	19990225	G	6114		HUB             			PIPER 	PA32  	PA32RT300T  	7103216	SO  						HARTZL	HCE2Y	HCE2YR1BF   	GL  	PROPELLER	DAMAGED         	B			J3PR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	17	21469		435  			32R7887214		DK1789A		EXCESSIVE AMOUNT OF MARKINGS PROTRUDING FROM THE INTERIOR AND EXTERIOR SURFACES OF THE HUB.						1	L	7	1 	3O				A3SO    		5	C	P9EA	 
1999040900101	19990409	00101	NM  	1999	4	9	99ZZZX1415       	1	19990301	G	2497		WIRE            			UNIVAR	415   	415C        	0420302	NM  										FUSELAGE	SHORTED         	G		A		O				OTHER                   				A			FLAME/FIRE                			NR	NOT REPORTED   	1			GL	21	99349					1972				AFTER PRELIMINARY INVESTIGATION OF THE INCIDENT, IT WAS DETERMINED THAT FAILURE OF AN ELECTRICAL WIRE CAUSED A FIRE TO D	EVELOP.					1	L	7	1 	3O			 	A718    					 
1999040900102	19990409	00102		1999	4	9	99ZZZX1416       	1	19990305	G	2560	C19347114	LINK            	AIRCRUISERS 																SLIDE	MISMANUFACTURED 	B	P			K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	09					0720					EVACUATION SLIDE RECEIVED IN PACKED CONDITION WITH INCORRECT FRANGIBLE LINK, PN C19347-114, ATTACHED TO HALF-TIES. THE F	RANGIBLE LINK WAS BROKEN AND RE-ATTACHED (BOTH HALVES) WITH RED SAFETY TIE THREAD.																		 
1999040900103	19990409	00103	WP  	1999	4	9	99ZZZX1417       	2	19990301	G	7260	8968553	HOUSING         			MTSBSI	MU2   	MU2B36      	5780412	CE  	GARRTT	TPE331	TPE3316251M 	01514	WP  					ACCY GEARBOX	DAMAGED         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	99	687HB	4882 	2073 			687	P20264			THREADS FOR FITTING OF AFT OIL SCAVENGE PUMP LINE, IN ACCESSORY/GEAR HOUSING, STRIP OUT CAUSING OIL LEAK.						1	H	7	2 	3T	4	T	RT	A10SW   	E2WE				 
1999040900104	19990409	00104	CE  	1999	4	9	99ZZZX1418       	1	19990105	G	2460		HARNESS         			BEECH 	90    	C90A        	1152911	CE  										COCKPIT	CHAFED          	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	3138B	33   				LJ1538				DURING AN AVIONICS INSTALLATION AND ASSOCIATED WIRING, FOUND MAIN WIRE BUNDLE GOING TO COPILOT'S CIRCUIT BREAKER PANEL W	AS CHAFING ON THE LOWER FORWARD CIRCUIT BREAKER PANEL MOUNT.					1	L	7	2 	3T			RT	3A20    					 
1999040900105	19990409	00105	CE  	1999	4	9	99ZZZX1419       	1	19990107	G	2497		WIRE            			BEECH 	90    	C90A        	1152911	CE  										COCKPIT	CHAFED          	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	88XJ	150  				LJ1525				DURING AN AVIONICS INSTALLATION AND ASSOCIATED WIRING, FOUND A WIRE BUNDLE WHICH RUNS TO THE COPILOT'S CIRCUIT BREAKER P	ANEL CHAFING ON PANEL LOWER MOUNT WITH ONLY 150 HOURS TT. ONE OF THE MAIN POWER WIRES HAD CHAFED THROUGH TO BARE METAL A	ND HAD BEEN ARCING ON THE MOUNT. REPAIRED WIRE AND REPOSITIONED WIRE BUNDLE TO CLEAR THE MOUNT.				1	L	7	2 	3T			RT	3A20    					 
1999040900106	19990409	00106	NE  	1999	4	9	99ZZZX1420       	2	19990323	G	7261	L792M3004235	SHAFT           		L792M3004103	UROCOP	EC135 	EC135P1     	8680990	EU  	PWA   	PW206 	PW206B      	0	NE  					OIL COOLER	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	914ET	712  				0018				DRIVE SPLINES WERE DOWN AND WOULD NOT TURN BLOWER.						1	G	7	2 	3U	3	U	O	H88EU   	E42NE				 
1999040900107	19990409	00107	EU  	1999	4	9	99ZZZX1421       	1	19990323	G	6320	L630M1001052	TRANSMISSION    			UROCOP	EC135 	EC135P1     	8680990	EU  										MAIN ROTOR	MAKING METAL    	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	914ET	419  			208	0018				METAL CONTAMINATION OF OIL SYSTEM.						1	G	7	2 	3U			O	H88EU   					 
1999040900108	19990409	00108	EU  	1999	4	9	99ZZZX1422       	1	19990323	G	6330	L633M2001105	MOUNT           			UROCOP	EC135 	EC135P1     	8680990	EU  										TRANSMISSION	LEAKING         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	914ET	19   			BOA973920	0018				FLUID LEAKED OUT-PIN RETRACTED.						1	G	7	2 	3U			O	H88EU   					 
1999040900109	19990409	00109	SO  	1999	4	9	99ZZZX1423       	1	19990317	G	3230	JL18891	UPLOCK          			LKHEED	1329  	132925      	5263125	SO  										NLG	CRACKED         	B			FGQR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	701JH	7703 				5230				DURING REPLACEMENT OF THE NOSE GEAR ACTUATOR, THE PIN RETAINER FOR THE ACTUATOR/UPLOCK WAS FOUND CRACKED UNDER THE HEAD 	OF THE RETAINING BOLT. SUBMITTER STATED IF FAILURE HAD OCCURRED, IT MAY HAVE GONE UNDETECTED FOR SOME TIME DUE TO THE LO	CATION. MALFUNCTION OF NG RETRACTION WOULD HAVE RESULTED.				2	L	7	4 	4F				2A1SO   					 
1999040900110	19990409	00110	CE  	1999	4	9	99ZZZX1424       	1	19990201	G	2810		LABELS          			CESSNA	650   	650         	2076802	CE  										FUEL CELL	LOOSE           	B		A	JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09										LINE LABELS IN FUEL CELLS COMING LOOSE. LABEL MIGRATED TO SUMP AREAS FOULING SCREENS, FLAPPER VALVES, AND JET PUMPS. TWO	 SEPARATE AIRCRAFT HAD FUEL PRESSURE PROBLEM RELATED TO THIS PROBLEM.  LOOSE LABELS SHOULD BE REMOVED AT PHASE 5 INSPECT	ION.				2	L	7	2 	4F				A9NM    					 
1999040900111	19990409	00111	EA  	1999	4	9	99ZZZX1425       	1	19990316	G	2823	AV16B20823	VALVE           	ITT         		CNDAIR	CL600 	CL6002B16   	1900305	EA  										AUX FUEL CELL	FAILED          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	07	881TW	480  			P80163	5348				RIGHT AUXILIARY FUEL SHUT-OFF VALVE FAILED IN OPEN POSITION CAUSING FUEL IMBALANCE.						2	L	7	2 	4F			RT	A21EA   					 
1999040900164	19990409	00164	SO  	1999	4	9	99ZZZX1429       	2	19990211	G	8530	654651A2	VALVE           			CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  					ENGINE	WORN            	B			NZBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	4689U		381  			U20605058	810103R			AT ENGINE TT 378.8 HOURS, REMOVED ALL CYLINDERS AND HONED DUE TO 'GLAZING'. AT ENGINE TT 380.0 HRS, PILOT REPORTED ENGIN	E RUNNING ROUGH. REPLACED NR 6 CYLINDER ASSY DUE TO 'LOW' COMPRESSION 20/80 PSI.  FURTHER INSPECTION OF CYLINDER REVEALE	D EXCESSIVELY WORN INTAKE VALVE AND SEAT.  CSB9811B C/W AND SUBMITTED 8-7-98 AT ENGINE TT 285.6 HRS.				1	H	7	1 	3O	3	O		A4CE    	E5CE				 
1999040900165	19990409	00165		1999	4	9	99ZZZX1430       	1	19990210	G	7920	LW16974	BAFFLE          																	OIL SYSTEM	CRACKED         	B	P		NJ1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	23										CRACKS IN BOLT HOLES MOUNTING FLANGE AND INNER SCREEN IN 90 DEGREE BENDS.																			 
1999040900166	19990409	00166	CE  	1999	4	9	99ZZZX1431       	1	19990201	G	5330		PANEL           			CESSNA	500   	560CESSNA   	2076750	CE  										NLG WW	CRACKED         	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09										WHEELWELL CLOSE-OUT PANEL CRACKING. REPLACED AT LEAST 25 IN 9 MONTH PERIOD.						2	L	7	2 	4F			RT	A22CE   					 
1999040900167	19990409	00167	SO  	1999	4	9	99ZZZX1432       	1	19990220	G	2720	63451000	SUPPORT         			PIPER 	PA28  	PA28235     	7102810	SO  										RUDDER PEDAL	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	09	845BY	2268 				287510043				CRACKS IN BOTH LOWER FRONT CORNERS OF RUDDER PEDAL SUPPORT. FOUND ON ANNUAL INSPECTION.						1	L	7	1 	3O				2A13    					 
1999040900168	19990409	00168	CE  	1999	4	9	99ZZZX1433       	1	19990217	G	7160	63966013	BOOT            			BEECH 	58    	58P         	1152744	CE  										INDUCTION SYSTEM	LOOSE           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	05	112Z					TJ371				THE INDUCTION BOOT SLIPPED OFF THE INDUCTION TUBE AT THE INNER COOLER OUTLET CONNECTION. THE WORM CLAMP SECURING THE BOO	T WAS APPARENTLY NOT FULLY OVER THE RIDGE ON THE INDUCTION TUBE CAUSING THE BOOT TO EVENTUALLY SLIP OFF THE TUBE AT HIGH	 MANIFOLD PRESSURE.				1	L	7	2 	3O				A23CE   					 
1999040900170	19990409	00170	WP  	1999	4	9	99ZZZX1435       	1	19990315	G	3246	9543536	WHEEL           		AUG74585    	DOUG  	DC8   	DC8F61      	3021954	WP  										NLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					9550328					NDT SPECIF MIL-I 6870 DETECTED CRACK IN TUBE WALL. NO CRACKS PERMITTED IN THIS AREA. ABS OHM 32-40-01 REV 2 DATE SEPT 15	, 1989.  CHECK SECTION PARA 3A.					2	L	7	4 	4J			RT	4A25    					 
1999040900171	19990409	00171	SO  	1999	4	9	99ZZZX1436       	2	19990317	G	8530	652541	NUT             								CONT  	O470  	IO470J      	17026	SO  					NR 2 CYLINDER	CRACKED         	B				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	99										FAILURE OCCURRED AT THE THINNEST PART OF THE NUT. THE NUT WAS FOUND WHILE TROUBLESHOOTING AN OIL LEAK AT THE CYLINDER BA	SE FLANGE AT OPPOSING CYLINDER NR 3. THE NUT WAS ON THE STUD BACKED OFF 4 TURNS.										3	O			3E1				 
1999040900173	19990409	00173	CE  	1999	4	9	99ZZZX1438       	1	19990324	G	5510	21131332	DOUBLER         			CESSNA	210   	T210R       	2073459	CE  										HORIZ STABILIZER	CRACKED         	B			CGFR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03	7687U	3177 				T21064977				THIS PART WAS ADDED TO STABILIZER ATTACHMENT SYSTEM BY SB SEB 87-2. SUBMITTER STATED STABILIZER ATTACH BULKHEAD WAS ALSO	 NOTED TO BE CRACKED IN AN AREA THAT THIS SB WAS SUPPOSED TO ADDRESS.					1	H	7	1 	3O			RT	3A21    					 
1999040900174	19990409	00174		1999	4	9	99ZZZX1439       	4	19990317	G	2562	7A1140	ELT             	LEIGH       																CABIN	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	03					19206					DURING ROUTINE INSPECTION AND PERFORMANCE TEST OF ELT, THE UNIT COULD NOT BE ACTIVATED BY MEANS OF THE G-SHOCK SWITCH US	ING REASONABLE FORCES. A FINAL EXTREME FORCE WAS APPLIED BREAKING THE CASE, HOWEVER, THE UNIT STILL FAILED TO ACTIVATE.																		 
1999040900175	19990409	00175		1999	4	9	99ZZZX1440       	4	19990317	G	2562	754189	ELT             	LEIGH       																CABIN	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	03					159125					DURING ROUTINE INSPECTION AND PERFORMANCE TEST OF THE ELT, THE UNIT COULD NOT BE ACTIVATED BY MEANS OF THE G-SHOCK SWITC	H USING REASONABLE FORCES.																		 
1999040900176	19990409	00176		1999	4	9	99ZZZX1441       	4	19990317	G	2562	7A1201	ELT             	LEIGH       																CABIN	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	03					137864					DURING ROUTINE INSPECTION AND PERFORMANCE TEST OF ELT, THE UNIT COULD NOT BE ACTIVATED BY MEANS OF THE G-SHOCK SWITCH US	ING REASONABLE FORCES. THE UNIT WAS FINALLY ACTIVATED BY A SHOCK FORCE, HOWEVER, THE REQUIRED FORCE ALSO DESTROYED THE C	ASE OF THE UNIT. ESTIMATED IMPACT 25 PLUS G'S.																	 
1999040900177	19990409	00177	CE  	1999	4	9	99ZZZX1442       	1	19990219	G	3397		WIRE            			CESSNA	172   	172N        	2072434	CE  										CABIN	SHORTED         	G				B	A			EMER. DESCENT           	UNSCHED LANDING         			A			FLAME/FIRE                			NR	NOT REPORTED   	1			WP	23	5174D					17272439				ON 2-19-99, THE ACCIDENT-AIRCRAFT WAS CONDUCTING 'TRAFFIC WATCH' OPERATIONS UNDER FAR PART 91. WHILE IN VICINITY OF THE 	ELMONTE AIRPORT AT APPROX 16:52 LOCAL, THE TRAFFIC REPORTER/PASSENGER SEATED IN THE LT FWD (PILOT) SEAT, SWITCHED ON PIL	OT MAP LIGHT LOCATED ON LT FWD DOOR POST IN ORDER TO READ A ROAD MAP. WHEN SWITCH ACTIVATED, A LOUD 'POP' WAS HEARD, SIM	ULTANEOUSLY, FLAMES PROJECTED BOTH FORE AND AFT OF MAP LIGHT.  FIRE WAS NOT CONTROLLABLE AND PILOT MADE EMERGENCY LANDIN	G.  UPON LANDING, PILOT AND PASSENGER EVACUATED ACFT ON THE RUNWAY.  ACFT WAS SUBSTANIALLY DAMAGED BY ENSUING FIRE.  DUE	 TO FIRE DAMAGE, IT COULD NOT BE DETERMINED IF COVER (INSULATOR), CESSNA PN 0511080-1 WAS IN PLACE.	1	H	7	1 	3O			NT	3A12    					 
1999040900178	19990409	00178	CE  	1999	4	9	99ZZZX1443       	1	19990312	G	3230	12416185	SUPPORT         			CESSNA	210   	T210M       	2073451	CE  										RT MLG	LOOSE           	B		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	761KC	3284 				21062308				DURING ANNUAL INSPECTION, ALL 4 NAS565-33 BOLTS LT AND RT SIDE WERE FOUND LOOSE ALLOWING THE MLR SADDLE AND SHIMS TO MOV	E.					1	H	7	1 	3O				3A21    					 
1999040900179	19990409	00179	CE  	1999	4	9	99ZZZX1444       	1	19990311	G	7810	70121	MUFFLER         			BEECH 	36    	A36         	1151604	CE  										ENGINE	DAMAGED         	B			AKGR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	05	85EC					E2278				PILOT REPORTED DURING FLIGHT, HE COULD SMELL EXHAUST AND ENGINE NOISE WITH CABIN HEAT ON. HE ALSO FELT BAD AFTER THE FLI	GHT FROM ST. LOUIS TO KANSAS CITY. THE HEAT MUFFLER WAS FOUND TO HAVE A ONE INCH HOLE IN IT AND SIGNS OF EXTREME DETERIO	RATION.				1	L	7	1 	3O				3A15    					 
1999040900180	19990409	00180	CE  	1999	4	9	99ZZZX1445       	1	19990210	G	2560	CIR112	ELT             			BEECH 	P35   	P35         	1151530	CE  										CABIN	SHORTED         	B			VT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	09	6525C				20335	D6871				DURING ELT BATTERY REPLACEMENT, NOTED ELT WAS INOPERATIVE WHEN BATTERY COVER WAS INSTALLED. UNIT CHECKED OK WITH COVER R	EMOVED.  FOUND METAL COVER SEPARATING BATTERY FROM ELT.  ELECTRONICS WAS GETTING DISPLACED BY BATTERY CAUSING THE ELT TO	 BE INOPERATIVE.  REMOVED COVER, APPLIED POLYURETHANE TAPE ON INSIDE OF COVER, AND RE-INSTALLED.  FUNCTION CHECK OK.				1	L	7	1 	3O			RT	3A15    					 
1999040900182	19990409	00182	SO  	1999	4	9	99ZZZX1447       	1	19990301	G	3246	16106900	WHEEL           	CLEVELAND   	40116       	PIPER 	PA23  	PA23250     	7102308	SO  										MLG	CRACKED         	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	54195	6500 				277405472				DURING TIRE CHANGE, FOUND WHEEL CRACKED.						1	L	7	2 	3O				1A10    					 
1999040900183	19990409	00183	SW  	1999	4	9	99ZZZX1448       	1	19990315	G	7120		MOUNT           			MOONEY	M20   	M20K        	5870220	SW  										ENGINE	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	1149H	2222 				250607				LEFT FRONT ENGINE MOUNT - LORD MOUNT SEVERELY CORRODED DUE EXHAUST GAS LEAKING ON IT AT THE SLIP JOINT IN EXHAUST PIPE S	YSTEM.					1	L	7	1 	3O				2A3     					 
1999040900184	19990409	00184	SO  	1999	4	9	99ZZZX1449       	2	19990316	G	8510	632612	GEARS           		646220A41   						CONT  	O360  	TSIO360LB   	17025	SO  					STARTER	WORN            	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	15		66   								MENTIONED GEARS HAD ALL TEETH WORN OFF. THIS ALLOWED METAL FITTINGS TO CONTAMINATE ENGINE NECESSATATING ENGINE REMOVAL. 	CAUSE UNKNOWN.  8130-3 FORM INFO FROM TCM W.O. DS10-28913.										3	O			E9CE				 
1999040900185	19990409	00185	SO  	1999	4	9	99ZZZX1450       	2	19990316	G	8510	632617	GEARS           		646220A41   						CONT  	O360  	TSIO360LB   	17025	SO  					STARTER	WORN            	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	15		66   								MENTIONED GEARS HAD ALL TEETH WORN OFF. THIS ALLOWED METAL FITTINGS TO CONTAMINATE ENGINE NECESSATATING ENGINE REMOVAL. 	CAUSE UNKNOWN.  8130-3 FORM INFO FROM TCM WO.O DS10-28913.										3	O			E9CE				 
1999040900186	19990409	00186		1999	4	9	99ZZZX1451       	1	19990312	G	3244	600X6	TIRE            																	MLG	MISMANUFACTURED 	H				O				OTHER                   				W			INADEQUATE Q C            			NR	NOT REPORTED   	1			EA	03					AIE4018					INSTALLED 2 NEW TIRES ON RETRACTABLE A/C 600X6-6 PLY TIRES AND TUBES. CHECKED FOR PROPER CLEARANCE ON RETRACT TEST. FIRS	T FLIGHT ON TAXI, RT MAIN INDICATED UNUSUAL THUMPING WHICH VIBRATED THROUGH ACFT.  REMOVED TIRE AND VISUAL INSPECTION SH	OWED PECULIAR (UNUSUAL) TEXTURE LINES IN RUBBER.  TIRE COMPANY REPLACED TIRE (SAID THIS WAS NOT FIRST OCCURRENCE).  PROB	LEM WAS RESOLVED WITH THE REPLACEMENT TIRE OF SAME MAKE AND SIZE.																 
1999040900187	19990409	00187	EA  	1999	4	9	99ZZZX1452       	2	19990322	G	8530	05K21123	CYLINDER        								LYC   	O235  	O235N2C     	41505	EA  					ENGINE	MISMANUFACTURED 	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	13										VISUAL INSPECTION OF FACTORY NEW CYLINDER KIT P/N 05K21123 PRIOR TO INSTALLATION, REVEALED THE WRONG PART NUMBER OUTER E	XHAUST VALVE SPRING SEAT WAS INSTALLED. THE PROPER PART NUMBER FOR THIS PART IS LW-10077. THE NEW CYLINDER WAS RECEIVED 	FROM A FACTORY DISTRIBUTOR WITH A P/N LW-16475 SEAT INSTALLED.  THE LW-16475 SEAT DID NOT ALLOW THE VALVE KEGS (OR KEEPE	RS) TO PROPERLY SEAT ON THE VALVE STEM.  IF INSTALLED, THE KEEPERS WOULD LIKELY FAIL AND ALLOW THE EXHAUST VALVE TO ENTE	R THE CYLINDER WHICH COULD LEAD TO ENGINE FAILURE.							3	O			E223				 
1999040900188	19990409	00188	SO  	1999	4	9	99ZZZX1453       	1	19990326	G	3260	487862	SWITCH          			PIPER 	PA31  	PA31325     	7103105	SO  										LT MLG	CONTAMINATED    	D				O				OTHER                   				O			OTHER                     			AP	APPROACH       	1			WP	17	27975	6539 				317912047				PILOT LOWERED LANDING GEAR. LEFT MLG DOWN INDICATOR LIGHT (GREEN) FAILED TO ILLUMINATE AND LANDING GEAR WARNING HORN ALE	RTED PILOT OF POSSIBLE UNSAFE LEFT MLG CONDITION. PILOT RE-CYCLED LANDING GEAR INCIDENT.  FURTHER INVESTIGATION INDICATE	D LEFT MLG MICROSWITCH, SPRING-LOADED PLUNGER STUCK BEFORE REACHING ITS FULLY EXTENDED POSITION.  REMEDY, CLEAN AND LUBE	 SPRING-LOADED PLUNGER.			1	L	7	2 	3O				A20SO   					 
1999040900189	19990409	00189	CE  	1999	4	9	99ZZZX1454       	1	19990311	G	3411		PITOT SYSTEM    			CESSNA	421   	421C        	2076016	CE  										FWD FUSELAGE	CONTAMINATED    	H				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			WP	03	321FL					421C0207				DURING CRUISE FLIGHT AFTER BEING ON THE GROUND IN A RAINSTORM, THE PILOT'S INSTRUMENTS BEGAN ACTING ERRATICALLY.  THE PI	LOT'S AIRSPEED WENT TO ZERO THEN 240 KNOTS. COPILOT'S INSTRUMENTS READ APPROPRIATELY. CLEARING THE ENTIRE SYSTEM OF MOIS	TURE, THEN PERFORMING A COMPLETE PITOT/STATIC TEST AND REPLACING BOTH THE USI, ALTIMETER AND AIRSPEED.  THE AIRCRAFT RET	URNED TO SERVICE.  SUBMITTER STATED MOISTENING CAN BE DIFFICULT TO REMOVE WITH ONLY THE DRAINS PROVIDED.  PURGED WITH DR	Y NITROGEN.		1	L	7	2 	3O				A7CE    					 
1999040900190	19990409	00190	CE  	1999	4	9	99ZZZX1455       	1	19990225	G	3230	AN5158R8	SCREW           		35815155610 	BEECH 	33    	G33         	1151435	CE  										MLG	WORN            	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	166B	4240 				CD1293				DURING AN ANNUAL INSPECTION, NOTED 2 OF 4 MAIN GEAR RETRACT BRACE, PIVOT PIN, RETAINER SCREWS WERE ABLE TO ROTATE. REMOV	ED AND FOUND THE THREADS WORN FROM THE SHEAR ACTION OF THE PIN. CORRECTED PROBLEM BY INSTALLING NEW ANS525R-832R8 SCREWS	 WHICH HAVE A SHOULDER PROVIDING HIGHER SHEAR STRENGTH.				1	L	7	1 	3O				3A15    					 
1999040900191	19990409	00191	EA  	1999	4	9	99ZZZX1456       	2	19990303	G	8530	73806TT	PUSHROD         			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  					ENGINE	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	25	67975		1469 			15282122	L14797615			UPON 100-HOUR INSPECTION TO DETERMINE APPLICABILITY TO AD 80-25-02 R2, NOTED THAT NR 4 CYLINDER INTAKE PUSH ROD P/N 7380	6T-T WHICH DOES NOT APPLY TO AD, WAS FOUND CRACKED AT END OF ALUMINUM TUBE THAT SWAGES ONTO BALL END OF PUSH ROD, TWO CR	ACKS WERE OBVIOUS VISUALLY. A FURTHER INSPECTION OF ALL OTHER CYLINDER PUSH RODS REVEALED THE SAME DEFECT ON ONE OR MORE	 OF THE PUSH RODS. THESE PUSH RODS ARE EXEMPT FROM THIS AD.			1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999040900192	19990409	00192	SO  	1999	4	9	99ZZZX1457       	2	19990224	G	8540	643259A28	ADAPTER         		EQ664WR     	CESSNA	421   	421C        	2076016	CE  	CONT  	O520  	GTSIO520N   	17032	SO  					STARTER	SPALLED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	09	745CA	700  				421C1043	277042R			AIRCRAFT IN FOR ROUTINE (SCHEDULED) 100 HOUR INSPECTION. STARTER ADAPTERS WERE REMOVED FROM BOTH ENGINES, AND INSPECTED 	IAW TCM SB NR CS894-4A. THE ADAPTER ASSY AND CRANKSHAFT GEAR ON THE NR 2 ENGINE (ITEM 3) DID NOT PASS INSPECTION CRITERI	A OUTLINED, (DEEP SPALLING ON VARIOUS TEETH). UNIT WAS REPLACED WITH SERVICEABLE UNIT.  BOTH ADAPTER ASSY'S ARE CURRENT 	DESIGN UNITS AND PER SB'S, NO FURTHER INSPECTIONS ARE REQUIRED UPON INSTALLATION UNTIL TBO, (OVERHAUL).			1	L	7	2 	3O	3	O		A7CE    	E7CE				 
1999040900193	19990409	00193	SO  	1999	4	9	99ZZZX1458       	2	19990224	G	8520	653580	GEAR            		EQ664WR     	CESSNA	421   	421C        	2076016	CE  	CONT  	O520  	GTSIO520N   	17032	SO  					CRANKSHAFT	SPALLED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	09	745CA	700  				421C1043	277042R			AIRCRAFT IN FOR ROUTINE (SCHEDULED) 100 HOUR INSPECTION. STARTER ADAPTERS WERE REMOVED FROM BOTH ENGINES, AND INSPECTED 	IAW TCM SB NR CS894-4A. THE ADAPTER ASSY AND CRANKSHAFT GEAR ON THE NR 2 ENGINE (ITEM 3) DID NOT PASS INSPECTION CRITERI	A OUTLINED, (DEEP SPALLING ON VARIOUS TEETH). UNIT WAS REPLACED WITH SERVICEABLE UNIT.  BOTH ADAPTER ASSY'S ARE CURRENT 	DESIGN UNITS AND PER SB'S, NO FURTHER INSPECTIONS ARE REQUIRED UPON INSTALLATION UNTIL TBO, (OVERHAUL).			1	L	7	2 	3O	3	O		A7CE    	E7CE				 
1999040900195	19990409	00195	CE  	1999	4	9	99ZZZX1460       	1	19990324	G	3340	CM358910	SWITCH          			CESSNA	172   	172R        	2072401	CE  										COCKPIT	OVERHEATED      	D				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			CL	CLIMB          	1			SW	99	431ER	1127 				17280301				PILOT TOOK OFF AND NOTICED A BURNING SMELL. THEY IMMEIDATELY LANDED AFTERWARDS. THE PILOT NOTICED THE LANDING LIGHT SWIT	CH WAS EXTREMELY HOT TO THE TOUCH.  REPLACEMENT OF THE SWITCH/BREAKER SOLVED THE PROBLEM.					1	H	7	1 	3O			NT	3A12    					 
1999040900196	19990409	00196	CE  	1999	4	9	99ZZZX1461       	1	19990323	G	3411	S10711	LINE            			CESSNA	172   	172R        	2072401	CE  										PITOT SYSTEM	DAMAGED         	B			N3XR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	15	410ER	1380 				17280257				THE AIRSPEED INDICATOR REPORTEDLY WAS INCREASING WITH ALTITUDE. THE PITOT WAS FOUND BURNED THROUGH BY PITOT HEAT WIRING.	 REPOSITIONED WIRING AND REPLACED PITOT LINE.					1	H	7	1 	3O			NT	3A12    					 
1999040900197	19990409	00197	EA  	1999	4	9	99ZZZX1462       	2	19990312	G	7414	M3007	IMPULSE COUPLING	SLICK       		PIPER 	PA28  	PA28151     	7102805	SO  	LYC   	O320  	O320E3D     	41508	EA  					MAGNETO	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	01	33319	54   				287515328				CUSTOMER COMPLAINED OF HARD STARTING. REMOVED LEFT MAGNETO AND FOUND IMPULSE FLYWEIGHTS (PAWLS) NOT ENGAGING THE STOP PI	NS WHEN ROTATED AT STARTING SPEED DUE TO SEVERE WEAR OF THE PAWL OR PIVOT PINS. IMPULSE COUPLING HAD BEEN INSTALLED 54 H	OURS AGO.				1	L	7	1 	3O	3	O		2A13    	E274				 
1999040900320	19990409	00320	CE  	1999	4	9	99ZZZX1463       	1	19990207	G	3213	508100324	KNEE            			BEECH 	90    	C90         	1152913	CE  										RT MLG	FAILED          	B	P		EHHR	O				OTHER                   				O			OTHER                     			LD	LANDING        	1			EA	17	74CC		170  			LJ620				AIRCRAFT LANDED AT TTN. ON TOUCH-DOWN, AIRCRAFT PULLED TO RIGHT AND TRAVELED OFF RUNWAY WITHOUT FURTHER INCIDENT. ON INV	ESTIGATION, FOUND RIGHT LANDING GEAR UPPER TORQUE KNEE FAILED WHICH ALLOWED LOWER LANDING GEAR (PISTON ASSY) TO TURN SID	EWAYS.				1	L	7	2 	3T				3A20    					 
1999040900321	19990409	00321	NM  	1999	4	9	99ZZZX1464       	1	19990319	G	3250	22490110000	BRACKET         			ISRAEL	1125  	1125        		NM  										NLG STEERING	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	500AJ	1995 			IL074	074				DURING SCHEDULED INSPECTION, FOUND UPPER NOSE STEERING ACTUATORS SUPPORT BRACKET BROKEN AT UPPER OUTBOARD MOUNT BOLT TO 	FORWARD BULKHEAD ATTACH. DISASSEMBLED/REMOVED STEERING ACTUATOR/YOKE ASSY. DURING DISASSEMBLY, NOTED CENTERING SPRING HO	USING MOUNT SHAFT SEIZED INSIDE BUSHING ON UPPER BRACKET.  REPLACED BROKEN BRACKET AND THOROUGHLY CLEANED AND LUBED CENT	ERING SPRING SHAFT.  INSTALLED ACTUATOR/YOKE ASSY AND OPS CHECKED GOOD.  SUSPECT SEIZED CENTERING SPRING HOUSING SHAFT C	AUSED UNDUE STRESS TO UPPER BRACKET CAUSING BREAK.		2	L	7	2 	4F			RT	A16NM   					 
1999040900322	19990409	00322	NM  	1999	4	9	99ZZZX1465       	1	19990319	G	2781	834403	SENSOR          			BOEING	767   	7673T7      	1385201	NM  										SLATS	FAILED          	H				A				UNSCHED LANDING         				N			FALSE WARNING             			CL	CLIMB          	1			WP	03	602EV					25117				AFTER TAKEOFF, 'LE SLAT ASYM' MESSAGE SHOWN ON EICAS CAUSED AIR RETURN. MAINTENANCE BITE PSEU, FOUND L/E SLAT S282 (NR 1	) AND S302 (NR 10) 2 SENSORS FAILURE. REPLACED TWO EACH SENSORS, PN 834403 AND OPERATIONAL CHECK, CONDITION IS NORMAL.					2	L	7	2 	4F			RT	A1NM    					 
1999040900323	19990409	00323	EU  	1999	4	9	99ZZZX1466       	2	19990308	G	7260	EU10297	NUT             			GULSTM	G1159 	GIV         	3980115	SO  	RROYCE	TAY   	TAY6118     		EU  					GEARBOX	LOOSE           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	500E	3237 				1072	16254			DURING STRIP OF THIS SUB-ASSEMBLY, NOTED THERE WAS LITTLE OR NO TORQUE ON THE RETAINING NUT, ALLOWING SHAFT TO SPIN IN R	ELATION TO THE THRUST BEARING.					2	L	7	2 	4F	4	F	RT	A12EA   	E25NE				 
1999040900324	19990409	00324	EU  	1999	4	9	99ZZZX1467       	1	19990322	G	5413	06650001804	INDICATOR       			AMD   	FALC50	FALCON50MYST	2730106	EU  										COCKPIT	MALFUNCTIONED   	B			EYKR	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			SO	17	76FD	116  			8288	041				TCAS/VSI INDICATOR SHORTED INTERNALLY CAUSING SMOKE IN THE COCKPIT WHILE AIRCRAFT WAS REPOSITIONING FROM JET AVIATION TO	 SIGNATURE FLIGHT SERVICES FOR NEXT DAY DEPARTURE.					2	L	7	3 	4F				A46EU   					 
1999040900325	19990409	00325		1999	4	9	99ZZZX1468       	1	19990318	G	7120	IK83060	BUSHING         																	ENGINE MOUNT	CRACKED         	B			XE5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	21			24953							BUSHING IS PART OF THE FORWARD ENGINE MOUNT ASSEMBLY. BUSHING HAD ONE VISIBLE CRACK PROPAGATING AXIALLY FROM THE EDGE OF	 THE BUSHING APPROXIMATELY TO THE CENTER (WIDTH OF BUSHING), THEN CHANGING DIRECTION TO CIRCUMFERENTIAL DIRECTION. THE C	RACK MEASURED APPROXIMATELY 1.422 INCHES FROM THE ORIGIN TO THE VISIBLE CRACK TERMINATION.  THERE WAS VISIBLE CORROSION 	ON THE EXPOSED PORTION OF THE BUSHING AND AT THE CRACK ORIGIN.																 
1999040900326	19990409	00326	WP  	1999	4	9	99ZZZX1469       	2	19990210	G	7322	30743202	METERING VALVE  		3070880011  	RKWELL	NA265 	NA26565     	7630107	CE  	GARRTT	TFE731	TFE7313R1D  	01518	WP  					NR 1 ENGINE	WORN            	B			IY2R	B	A			EMER. DESCENT           	UNSCHED LANDING         			X			ENGINE FLAMEOUT           			AP	APPROACH       	1			SW	15	91BZ				A6162T	465019	P83142			MINUTES PRIOR TO MALFUNCTION, NR 2 ENGINE, SN P83141, FAILED. THIS FAILURE REPORTED 1-26-99. DURING SINGLE ENG DESCENT T	HROUGH 13,000 FEET, CREW RETARDED POWER LEVER OF NR 1 ENG TO FLIGHT IDLE TO INCREASE DESCENT RATE.  MOMENTS LATER, NR 1 	GENERATOR FAIL LIGHT ILLUMINATED.  NR 1 ENG FLAMED OUT.  CREW RELIT ENG AND LANDED AT LIT WITHOUT INCIDENT.  FUEL CONTRO	L REMOVED FOR TESTING.  TEST REVEALED EXCESSIVE FUEL DROOP CAUSED BY WORN METERING VALVE ASSY.  THE DROOP IN FUEL FLOW R	EDUCED FLOW BELOW MINIMUM AMOUNT OF FUEL REQUIRED TO MAINTAIN ENG OPERATION.  METERING VALVE ASSY, PN 3074320-2 REPLACED	.	2	L	7	2 	4J	4	F		A2WE    	E6WE				 
1999040900327	19990409	00327	EU  	1999	4	9	99ZZZX1470       	1	19990309	G	5610	343017183	WINDOW          			ISRAEL	1124  	1124A       	4500103	EU  										COCKPIT	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	494BP	1220 				307				IAW IAI MM CHAP 5-20-02 PG 202 PARA D(4), THIS COCKPIT SIDE WINDOW IS NO LONGER INSPECTED AT THE 800-HOUR INTERNAL. THIS	 NEW STYLE WINDOW, PN 343017-183, CRACKED AT A MOUNT BOLT HOLE ALONG THE UPPER EDGE OF THE D.V. WINDOW. THIS CRACK WAS D	ETECTED WITH THE USE OF A PRISM DURING A PRE-PURCHASE EVALUATION.				2	M	7	2 	4F				A2SW    					 
1999040900328	19990409	00328	SO  	1999	4	9	99ZZZX1471       	1	19990308	G	3810	115677114	DRAIN MAST      			GULSTM	G1159 	GIV         	3980115	SO  										FUSELAGE	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	25	475QS					1275				PILOT REPORTED AFT SINKS (GALLEY AND LAV) WOULD NOT DRAIN. T/S SYSTEM, FOUND DRAIN MAST NOT HEATING UP. REMOVED MAST AND	 INSTALLED NEW MAST OF SAME P/N, S/N 396.  PERFORMED OPERATIONAL CHECK OF DRAIN MAST HEATING ELEMENT, NO DEFECTS NOTED. 	 SINKS WERE NOT DRAINING DUE TO MAST FREEZING UP AT ALTITUDE, SINKS NOW DRAIN PROPERLY IN-FLIGHT.  ALL WORK PERFORMED IA	W GIV MM.  ACFT TT:  3,388.2 HOURS.			2	L	7	2 	4F			RT	A12EA   					 
1999040900329	19990409	00329	EU  	1999	4	9	99ZZZX1472       	1	19990212	G	2910	199900G530CD	LINE            			AGUSTA	A109  	A109A2      	0260120	EU  										HYDRAULIC SYSTEM	RUPTURED        	D				A				UNSCHED LANDING         				K	J		FLUID LOSS                	WARNING INDICATION        		NR	NOT REPORTED   	1			NM	01	55NW	4799 				7267				DURING FLIGHT, PILOT EXPERIENCED LOSS OF NR 2 HYDRAULIC PRESSURE, NR 2 HYDRAULIC SERVO CAUTION LIGHT, THEN LOSS OF PRESS	URE TO THE UTILITY HYDRAULIC SYSTEM. AIRCRAFT WAS LANDED AT BOEING FIELD WITHOUT INCIDENT AT 23:15 HOURS. CAUSE OF FAILU	RE WAS DETERMINED TO BE A RUPTURED HOSE ASSEMBLY SUPPLYING PRESSURE TO THE NR 2 FLIGHT CONTROL SYSTEM.  HOSE WAS REPLACE	D WITH A SERVICEABLE PART.			1	G	7	2 	3U				H7EU    					 
1999040900330	19990409	00330	WP  	1999	4	9	99ZZZX1473       	1	19990319	G	7921	369A8326	VALVE           			HUGHES	369   	369HS       	4470728	WP  										ENGINE BAY	BROKEN          	D				R	A			AUTOROTATION            	UNSCHED LANDING         			J			WARNING INDICATION        			TO	TAKEOFF        	1			NM	08	9486F	8000 				5406035				DURING TAKEOFF, ENGINE OIL PRESSURE DROPPED BELOW MINIMUMS. THROTTLE WAS CLOSED AND AIRCRAFT WAS AUTOROTATED. CHECK VALV	E NIPPLE HAD SEVERED AT OIL COOLER INLET.					1	G	7	1 	3U				H3WE    					 
1999040900331	19990409	00331		1999	4	9	99ZZZX1474       	1	19990304	G	6310	3130S6010004	ROLLER          																	FREEWHEEL UNIT	CORRODED        	B			FF6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11										ROLLERS HAVE CORROSION AND MICROPITTING. REF: R.O. 18896.																			 
1999040900332	19990409	00332	SO  	1999	4	9	99ZZZX1475       	1	19990312	G	3221	9572305	TRUNNION        			PIPER 	PA34  	PA34200     	7103405	SO  										NLG	CRACKED         	G				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	09	15202	6230 				347350034				THE SIDE BRACE WELD ON THE NOSE GEAR TRUNNION FAILED AT THE PIVOT POINT DUE TO EXCESSIVE SIDE LOADS AND HARD LANDINGS.						1	L	7	2 	3O				A7SO    					 
1999040900387	19990409	00387	SW  	1999	4	9	99ZZZX1479       	1	19990217	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	627AL	109  			RNFS7716	53284				DURING COMPLIANCE OF AD 97-24-17, FOUND DISC PACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999040900388	19990409	00388	WP  	1999	4	9	99ZZZX1480       	1	19990216	G	6210	369D21100517	BLADE           			HUGHES	369   	369D        	4470706	WP  										MAIN ROTOR	DELAMINATED     	B			NZBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	513SB	847  			J383	1120D				MAIN ROTOR BLADE DELAMINATED AT LEADING EDGE ABRASION STRIP BOND. DELAMINATION WAS FOUND BEYOND LIMITS. TSN:  846.9. THI	S MAIN ROTOR BLADE WAS REPAIRED AT TSN:  664.1 FOR SAME DISCREPANCY AS NOTED 6-23-98.					1	G	7	1 	3U				H3WE    					 
1999041700265	19990417	00265	EA  	1999	4	17	99ZZZX1523       	2	19990301	G	7313		INJECTOR        			PIPER 	PA32  	PA32300     	7103212	SO  	LYC   	O540  	IO540K1A5   	41532	EA  					FUEL SYSTEM	CRACKED         	I				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	1132Q		148  			327740046				NOTED FUEL STAINS ON NR 3 FUEL INJECTOR AND SUPPLY TUBE.  UPON REMOVAL OF INJECTOR, FOUND 2 SMALL CRACKS IN THE TOP LIP 	AREA WHERE THE BALL END OF THE INJECTOR LINE SEATS.					1	L	7	1 	3O	3	O		A3SO    	1E4				 
1999041700267	19990417	00267	NM  	1999	4	17	99ZZZX1525       	1	19990108	G	5313	655624539	STRINGER        			BOEING	727   	7272B7      	138407L	NM  										BS 950-990	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION NOTED ON STR 27L STA 950 - STA 990.						2	L	7	3 	4F				A3WE    					 
1999041700268	19990417	00268	NM  	1999	4	17	99ZZZX1526       	1	19990108	G	5313	655624540	STRINGER        			BOEING	727   	7272B7      	138407L	NM  										BS 950-990	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION NOTED ON STR 28L, STA 950C - STA 990.						2	L	7	3 	4F				A3WE    					 
1999041700269	19990417	00269	NM  	1999	4	17	99ZZZX1527       	1	19990108	G	5311		FRAME           			BOEING	727   	7272B7      	138407L	NM  										BS 990	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION NOTED ON FAIL SAFE FRAME AND SPLICE STA 990 AFT SIDE ABOVE STR 28L.						2	L	7	3 	4F				A3WE    					 
1999041700274	19990417	00274	NE  	1999	4	17	99ZZZX1532       	3	19990329	G	6111	57C0792	BEARING         			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	BLADE	CRACKED         	B			EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03		7276 	2747 					HJ454		INNER BEARING RACE CRACKED ONE-HALF WAY AROUND ON PROPELLER BLADE.						2	L	7	2 	4T			RT	A24CE   		5	C	P10N	 
1999041700275	19990417	00275	NE  	1999	4	17	99ZZZX1533       	3	19990329	G	6111	57C0792	BEARING         			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	BLADE	CRACKED         	B			EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03		7825 	4283 					HJ368		INNER BEARING BRACE CRACKED THREE-FOURTHS WAY AROUND ON PROPELLER BLADE.						2	L	7	2 	4T			RT	A24CE   		5	C	P10N	 
1999041700276	19990417	00276		1999	4	17	99ZZZX1534       	4	19990318	G	2300	030236816	CONNECTOR       	BENDIX      	KFS598      	BELL  	206   	206L3       	1182108	SW  										COMM SYSTEM	FAILED          	H				K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			AL	05	17238				3816	51492				PART HAS SHOWN HISTORY OF ARCING BETWEEN PINS 15 AND 14.  THIS IS A HIGH VOLTAGE PROBLEM AND HAS BEEN SEEN IN NUMEROUS U	NITS.  IT CAUSES THE CIRCUIT BOARD TO BURN AND CAUSES A SHORT ON TEH 180V LINE, SOMETIMES DAMAGING THE POWER SUPPLY IN T	HE RADIO.				1	G	7	1 	3U				H2SW    					 
1999041700277	19990417	00277	SW  	1999	4	17	99ZZZX1535       	1	19990322	G	2432	RG380E40	BATTERY         			BELL  	212   	212         	1181420	SW  										DC SYSTEM	DISCHARGED      	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530B				CBC296242	30702				BATTERY WEAK.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999041700278	19990417	00278	WP  	1999	4	17	99ZZZX1536       	1	19990322	G	6220	369D21200503	HUB             			HUGHES	369   	369E        	4470707	WP  										MAIN ROTOR	CRACKED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8330P	2615 	455  		1114	0330E				MAIN ROTOR HUB STRAP CRACKED IN LEAD LAG AREA. REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999041700279	19990417	00279	GL  	1999	4	17	99ZZZX1537       	2	19990322	G	7230	23007879	BLEED VALVE     			HUGHES	369   	369E        	4470707	WP  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	CORRODED        	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8330P		1155 		FF46186	0330E	CAE83626E			BLEED VALVE CORRODED AND SHAFT BUSHING WORN.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999041700280	19990417	00280	GL  	1999	4	17	99ZZZX1538       	2	19990322	G	7230	23057142	CASE HALVES     			HUGHES	369   	369E        	4470707	WP  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	CRACKED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8330P	1155 				0330E	CAE83626E			CASE LINING CRACKED AND CORRODED UNDER LINING.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999041700281	19990417	00281	SW  	1999	4	17	99ZZZX1539       	1	19990315	G	7722	212075562003	INDICATOR       			BELL  	212   	212         	1181420	SW  										COCKPIT	INCORRECT       	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530F		1354 		06302M	30920				INDICATOR READING INCORRECT DURING BARFIELD TEST.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999041700282	19990417	00282		1999	4	17	99ZZZX1540       	4	19990322	G	2312	9210121	TRANSCEIVER     			BELL  	206   	206B3       	1181506	SW  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY				F0542	2871				TRANSCEIVER SQUELCH SENSING NEEDS ADJUSTING (SET TOO LOW).  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999041700283	19990417	00283	SW  	1999	4	17	99ZZZX1541       	1	19990322	G	7712	206075185001	GAUGE           			BELL  	206   	206B3       	1181506	SW  										COCKPIT	LOOSE           	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY				3276	2871				GAUGE FACE SEPARATED FROM MOUNTING BASE AND GLASS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999041700284	19990417	00284	EU  	1999	4	17	99ZZZX1542       	1	19990318	G	5302	1053025151001	FRAME           		11730055    	BOLKMS	117   	BK117B1     	5626012	EU  	LYC   	LTS101	LTS101750B1 	41560	NE  					TAIL BOOM	CRACKED         	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03	211SL	8345 				7201	145666			DURING ROUTINE TAIL BOOM INSPECTION, FOUND FRAME 10L CRACKED ALL THE WAY THROUGH.  REPORTED DISCREPANCY TO AMERICAN EURO	COPTER.  AMERICAN EUROCOPTER SENT TECH REP TO REMOVE FRAME 10L AND INSTALL NEW FRAME.					1	G	7	2 	3U	3	U		H13EU   	E5NE10				 
1999041700285	19990417	00285	WP  	1999	4	17	99ZZZX1543       	1	19990322	G	2432	G641E	BATTERY         		G01742075   	HUGHES	369   	369D        	4470706	WP  										E/E BAY	DISCHARGED      	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	500DC	1425 				290456D				BATTERY DOES NOT PRODUCE ENOUGH POWER FOR COLD MORNING STARTS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999041700286	19990417	00286	WP  	1999	4	17	99ZZZX1544       	1	19990315	G	7810	369A8230504	EXHAUST STACK   			HUGHES	369   	369D        	4470706	WP  										ENGINE	CRACKED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	369AW	529  				470117D				EXHAUST STACK CRACKED AT END.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999041700287	19990417	00287	WP  	1999	4	17	99ZZZX1545       	1	19990322	G	2435	2303222	START/GENERATOR 			HUGHES	369   	369D        	4470706	WP  										ENGINE	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	5027P		769  		17702	611002D				STARTER/GENERATOR FAILED INTERNALLY.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999041700288	19990417	00288		1999	4	17	99ZZZX1546       	4	19990322	G	2312	064101900	TRANSCEIVER     			BELL  	206   	OH58A       	1181579	SW  										COCKPIT	INTERMITTENT    	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	54AG				6348	7120721				LOUD SAFE TONE, CANNOT TELL IF TRANSMITTING.  RADIO INTERMITTENT, INOPERATIVE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999041700290	19990417	00290		1999	4	17	99ZZZX1548       	4	19990322	G	3421	5040017901	INDICATOR       			HUGHES	369   	369D        	4470706	WP  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	1097J				1209	900801D				INDICATOR WILL NOT CAGE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999041700291	19990417	00291	GL  	1999	4	17	99ZZZX1549       	2	19990322	G	7323	252466714	GOVERNOR        			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	1097J		1076 		21535	900801D				GOVERNOR SURGES ABOVE 70 PSI TORQUE.  ERRATIC BEEP RANGE.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999041700292	19990417	00292		1999	4	17	99ZZZX1550       	4	19990322	G	3422	RCA15BK1	GYRO            			HUGHES	369   	369D        	4470706	WP  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	1097J				11571	900801D				GYRO DOES NOT FLAG.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999041700293	19990417	00293	GL  	1999	4	17	99ZZZX1551       	1	19990405	G	5310		TUBE            			HOWARD	DGA15 	DGA15P      	4690506	GL  										FUSELAGE	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	1010					1010				DURING RESTORATION, THE FUSELAGE WAS STRIPPED OF ALL SYSTEMS AND COMPONENTS.  THERE IS A FELT ANTI-CHAFE MATERIAL ON BOT	TOM OF FUSELAGE TUBING WHERE THE FUEL TANKS ARE ATTACHED.  UPON REMOVING THE FELT STRIPS, FOUND THE MATING SURFACE OF SO	ME OF THE TUBING WAS CORRODED INCLUDING SOME FAIRLY SEVERE PITTING.				1	H	7	1 	3R				A717    					 
1999041700294	19990417	00294	GL  	1999	4	17	99ZZZX1552       	1	19990405	G	5320		ADHESIVE        			HOWARD	DGA15 	DGA15P      	4690506	GL  										FUSELAGE	FAILED          	B		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	1010					1010				THIS AIRCRAFT WAS MANUFACTURED IN 1944 WITH CASEIN GLUE USED FOR BONDING ALL WOOD STRUCTURE INCLUDING WINGS, FLAPS, AILE	RONS, AND CABIN ROOF.  INSPECTION DURING RESTORATION FOUND MANY GLUED JOINTS DISBONDED WITH ONLY THE NAILS AND FABRIC CO	VERING HOLDING THE JOINTS TOGETHER.  ALL REPAIRS MADE USING RESORCINOL GLUE AS CASEIN GLUE IS NO LONGER RECOMMENDED IN A	C43.13-1.			1	H	7	1 	3R				A717    					 
1999041700295	19990417	00295	GL  	1999	4	17	99ZZZX1553       	3	19990320	G	6114		HUB             													MCAULY	2D36C	2D36C14     	GL  	PROPELLER ASSY	CRACKED         	B			NWOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05								59259		HUB IS CRACKED IN THREAD AREA.  REF:  W.O.  5337.																5	C	P901	 
1999041700296	19990417	00296	EA  	1999	4	17	99ZZZX1554       	2	19990309	G	8530		VALVE           			PIPER 	PA28  	PA28161     	7102803	SO  	LYC   	O320  	O320D3G     	41508	EA  					NR 1 CYLINDER	DAMAGED         	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	15	94PF	1157 				288516042	L915739A			EXHAUST VALVE STUCK CAUSING ZERO COMPRESSION AND BENT PUSH ROD.  OVERHAUL SHOP REPORTED GALLING OF VALVE STEM AND GUIDE.	  NO INDICATION AS TO CAUSE.					1	L	7	1 	3O	3	O		2A13    	E274				 
1999041700300	19990417	00300	CE  	1999	4	17	99ZZZX1558       	1	19990203	G	3411	CM29446600	HOSE            			CESSNA	500   	560CESSNA   	2076750	CE  										RT STATIC SYSTEM	LEAKING         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03	19PV	1010 				5600416				DURING RECERTIFICATION OF THE COPILOT'S STATIC SYSTEM (FAR 91.411), A 1350 FPM LEAK WAS NOTED AT 25,000 FEET.  TROUBLESH	OOTING REVEALED THAT ALL FOUR FLEXIBLE STATIC LINES WERE LEAKING.  THE HOSES CURE DATE IS 2Q95.  THE HOSES WERE STIFF AN	D BRITTLE.  REPLACEMENT HOSES FROM CESSNA HAVE A 4Q96 CURE DATE AND ARE SOFT AND PLIABLE.  NO LEAKS WERE NOTED AFTER REP	LACEMENT OF HOSES.			2	L	7	2 	4F			RT	A22CE   					 
1999041700301	19990417	00301	SO  	1999	4	17	99ZZZX1559       	1	19990330	G	3245	6303P0041A	TIRE            			PIPER 	PA42  	PA42        	7104202	SO  										MLG	MISMANUFACTURED 	B			TIMR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	07	175AA					428001017				TIRE WAS RE-CAPPED BY HAWKINS AIRCRAFT TIRE CO.  TIRE WOULD NOT ALLOW GEAR DOOR TO FULLY CLOSE.						1	L	7	2 	4T				A23SO   					 
1999041700302	19990417	00302	EA  	1999	4	17	99ZZZX1560       	2	19990315	G	7414		GASKET          	BENDIX      	D2000       	CESSNA	177   	177RG       	2073709	CE  	LYC   	O360  	IO360A1B    	41514	EA  					MAGNETO	WRONG PART      	B			CB5Y	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	35	45277					177RG1100	L1649451A			DURING 100-HOUR ANNUAL INSPECTION, MAGNETO TYPE BENDIX D2000 SERIES REMOVED FOR CONTACT BREAKER REPLACEMENT AND INTERNAL	 TIMING CHECK.  MAGNETO REFITTING WITH LYCOMING GASKET P/N 62224 INSTEAD OF LW-12681.  THE MAGNETO BECAME LOOSE AND BACK	ED OFF FROM THE ENGINE DRIVE.  THE ENGINE STOPPED IN-FLIGHT AND THE AIRCRAFT WAS FORCED TO LAND ON A NEARBY AIRFIELD.  T	HERE WAS NO DAMAGE OR INJURY SUSTAINED TO AIRCRAFT OR PERSONNEL.			1	H	7	1 	3O	3	O		A20CE   	1E10				 
1999041700304	19990417	00304	CE  	1999	4	17	99ZZZX1562       	1	19990323	G	7810	NH10089710	COUPLING        			CESSNA	340   	340A        	2076405	CE  										LT ENGINE	CRACKED         	B			DPOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	200CC	316  				340A0674				DURING A PHASE INSPECTION WHILE C/W AD 75-23-08R5 EXHAUST INSPECTION ON LEFT ENGINE, DISCOVERED WYE FOR WASTEGATE ELBOW 	V-CLAMP (ONE-PIECE COUPLING) CRACKED 3 INCHES AROUND CIRCUMFERENCE.  THIS PART WAS CHANGED DURING A RAM CONVERSION 12-97	.  DURING THE PRESSURE CHECK OF THE EXHAUST SYSTEM, THE COUPLING DID NOT LEAK.  THE RIGHT ENGINE COUPLING WAS REPLACED F	OR THE SAME REASON ON THE LAST PHASE (8010-4 SUBMITTED 12-22-98).			1	L	7	2 	3O				3A25    					 
1999041700305	19990417	00305	NE  	1999	4	17	99ZZZX1563       	2	19990329	G	7250	6002T57P01	BLUCKET         		6028T47601  						GE    	CF700 	CF7002D2    	30010	NE  					FAN	FAILED          	B			IY2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	15		8408 	3288 		779CF		299G008			RECEIVED SLIP IN ENGINE WITH FOD IN THE FAN AND COMPRESSOR SECTION.  THE FOD APPEARS TO BE CAUSED BY SEPARATION OF FAN B	LADE (S/N 779CE) IN THE HOT SECTION PART OF THE BLADE.  THE FAN BLADES ARE EDDY CURRENT INSPECTED AT EACH HOT SECTION (1	,000 HOURS).  THE LAST HOT SECTION WAS ACCOMPLISHED 350 HOURS PRIOR TO SEPARATION.									4	F			E7EA				 
1999042300347	19990423	00347	EA  	1999	4	23	99ZZZX1564       	2	19990225	G	7414		SCREW           	SLICK       	4330        	PIPER 	PA44  	PA44180     	7104402	SO  	LYC   	O360  	O360E1A6    	41514	EA  					MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	926ER	482  			98032406	4496016				BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	L	7	2 	3O	3	O		A19S0   	E286				 
1999042300348	19990423	00348	EA  	1999	4	23	99ZZZX1565       	2	19990226	G	7414		SCREW           	SLICK       	4371        	PIPER 	PA44  	PA44180     	7104402	SO  	LYC   	O360  	O360E1A6    	41514	EA  					MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	923ER	450  			97030200	4496010				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	L	7	2 	3O	3	O		A19S0   	E286				 
1999042300349	19990423	00349	CE  	1999	4	23	99ZZZX1566       	1	19990325	G	5542	169640000603	RUDDER ASSY     			BEECH 	23    	23          	1151202	CE  										TAIL	OUT OF ADJUST   	C				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	8761M	2680 				M549				RUDDER SKIN BINDING AGAINST VERTICAL STABILIZER SKIN DURING FULL DEFLECTION.						1	L	7	1 	3O				A1CE    					 
1999042300350	19990423	00350	CE  	1999	4	23	99ZZZX1567       	1	19990326	G	8011	EBB124A	DRIVE           	PRESTOLITE  	MHJ4004     	BEECH 	65    	65          	1152802	CE  										STARTER	LOOSE           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	5078G	24   				LF8				DRIVE TEETH CAME LOOSE ON STARTER.						1	L	7	2 	3O				3A20    					 
1999042300351	19990423	00351	CE  	1999	4	23	99ZZZX1568       	1	19990326	G	2810		VENT            		23306L      	CESSNA	310   	310N        	2074234	CE  										LT WING	LEAK            	G		A		O				OTHER                   				K	A		FLUID LOSS                	FLAME/FIRE                		LD	LANDING        	1			SO	35	5080Q				2156	310N0180				AFTER LANDING, LEFT WING EXPLODED.  IGNITION SOURCE POSSIBLY AUXILIARY FUEL PUMP RELAY OR RELATED WIRING.  FUEL LEAK AT 	LEFT AUXILIARY TANK VENT OUTLET NIPPLE DUE TO LOOSE FIT BETWEEN VENT TUBE AND RUBBER NIPPLE.  VENT LINE INSTALLATION NEE	DS MODIFICATION TO ALLOW NIPPLE TO BE CLAMPED ONTO METAL TUBE RATHER THAN ON RUBBER HOSE SLIPPED OVER METAL TUBE.  SUBMI	TTER RECOMMENDED PERIODIC PRESSURE TEST OF CELL INSTALLATION AND ADDITIONAL WING STRUCTURE VENTILATION (SECOND OCCURRENC	E ON THIS MODEL ACFT IN THE LAST YEAR).		1	L	7	2 	3O				3A10    					 
1999042300352	19990423	00352	SO  	1999	4	23	99ZZZX1569       	1	19990318	G	3211	40616001	BRACKET         			PIPER 	PA31T 	PA31T       	7103124	SO  										RT MLG	CRACKED         	D				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			WP	11	155CA	7917 				31T7820024				GEAR UNSAFE LIGHT STAYED ON AFTER GEAR RETRACTION.  FOUND FORWARD SUPPORT BRACKET FOR RT MLG UPLOCK FRACTURED AND UPLOCK	 ASSY BENT.  BOLT HOLE ACROSS FRACTURE SHOWS EVIDENCE OF PRE-EXISTING CRACK.  NOT VISIBLE WITHOUT REMOVAL OF UPLOCK ASSY	.				1	L	7	2 	3T				A8EA    					 
1999042300353	19990423	00353	EU  	1999	4	23	99ZZZX1570       	1	19990322	G	5313		STRINGER        			BRAERO	DH125 	HS125700A   	4230170	EU  										BS 8	CORRODED        	B			VJ1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	415RD					257094				CORROSION WAS NOTED ON THE LOWER FUSELAGE SKIN STRINGER 19, FRAME 8.  AIRCRAFT TT: 6,772.6 HOURS.  LANDINGS:  5,517.						2	L	7	2 	4F				A3EU    					 
1999042300354	19990423	00354	SW  	1999	4	23	99ZZZX1571       	1	19990405	G	2720	5000401	CONTROL CABLE   			GULSTM	690TP 	695A        	7630519	SW  										RUDDER CONTROL	FRAYED          	B			VR1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	7031J	1900 				96006				DURING INSPECTION, FOUND RIGHT RUDDER BALANCE CABLE FRAYED AT LOWER PULLEY.  TT:  APPROX 1,900 HOURS.  INSTALLED NEW CAB	LE ASSY, RIGHT.					1	H	7	2 	4T			 	2A4     					 
1999042300356	19990423	00356	SO  	1999	4	23	99ZZZX1573       	1	19990326	G	5230	594094	WASHER          			PIPER 	PA42  	PA42        	7104202	SO  										CARGO DOOR	MISSING         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	23	29TF					425501003				CABIN COULD NOT PRESSURIZE ABOVE 2.5 PSI.  FOUND CARGO DOOR SEAL, SEALING WASHER MISSING.  INSTALLED NEW SEALING WASHER.						1	L	7	2 	4T				A23SO   					 
1999042300357	19990423	00357	EU  	1999	4	23	99ZZZX1574       	1	19990401	G	3710	723017139	LINE            			ISRAEL	1124  	1124        	4500102	EU  										BS 246	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	148H	8000 				206				CABIN PRESSURIZATION VACUUM SUPPLY TUBE ASSY CHAFED AND CORRODED THROUGH UNDER CABIN FLOOR AT STA 246.  TUBE WAS CHAFED 	BY CONDITIONED AIR DUCT.					2	M	7	2 	4F				A2SW    					 
1999042300358	19990423	00358	EU  	1999	4	23	99ZZZX1575       	1	19990401	G	3242	C201811007	BRAKE ASSY      			AMD   	FALC50	FALCON900   	2700160	EU  										MLG	MISOVERHAULED   	B			JZBR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	25	1868M	807  			V411	157				PART RECEIVED AS REPAIRED.  FOUND MOUNTING FLANGE TO HAVE SIX HOLES INSTEAD OF 5 HOLES.  ON TALKING TO MFG, FOUND THAT F	LANGE TO BE FOR A FALCON 2000.  THE PART NUMBER ON BRAKE WAS FOR A FALCON900.					2	L	7	3 	4F			RT	A46EU   					 
1999042300359	19990423	00359	NE  	1999	4	23	99ZZZX1576       	3	19990407	G	6111	57D0495	FORK            			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	PROPELLER	CRACKED         	B			EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03			4479 		2212NR			HJ278		FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS.  4 CRACKS.						2	L	7	2 	4T			RT	A24CE   		5	C	P10N	 
1999042300360	19990423	00360	NE  	1999	4	23	99ZZZX1577       	3	19990407	G	6111	RFC11M1R6A	BLADE           			EMB   	120   	EMB120      	3260201	SO  						HAMSTD	14RF	14RF9       	NE  	PROPELLER	CRACKED         	B			EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03			5693 		869421					CRACK IN ZONE 2B OUTER EDGE OF FILLET RADIUS ON PROPELLER.						2	L	7	2 	4T			RT	A31SO   		6	C	P11N	 
1999042300361	19990423	00361	NM  	1999	4	23	99ZZZX1578       	1	19990108	G	5311		FRAME           			BOEING	727   	727259      	138408J	NM  										BS 970	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON FRAME, SHEAR TIE, AND SPLICE ANGLE STA 970, STR 28L - STR 28R.						2	L	7	3 	4F				A3WE    					 
1999042300362	19990423	00362	NM  	1999	4	23	99ZZZX1579       	1	19990108	G	5313	65564417	STRINGER        			BOEING	727   	727259      	138408J	NM  										BS 950 - 1009	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON STR 29L, STA 950 - STA 1009.						2	L	7	3 	4F				A3WE    					 
1999042300363	19990423	00363	NM  	1999	4	23	99ZZZX1580       	1	19990108	G	5313	655835872	STRINGER        			BOEING	727   	727259      	138408J	NM  										BS 950 - 1009	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON STR 28R, STA 950 - STA 1009.						2	L	7	3 	4F				A3WE    					 
1999042300365	19990423	00365	EU  	1999	4	23	99ZZZX1582       	1	19990330	G	3231	AIR400390	SEAL            			SAAB  	SF340 	340B        	7860101	EU  										NLG	LEAKING         	B			FW1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NE	03					CK9700894					PREMATURE DETERIORATION OF GLAND SEAL FOR RAMROD LEADING TO LEAKAGE OF HYDRAULIC FLUID.  3,234 CYCLES AT 24,000-CYCLE OV	ERHAUL.  PART TC:  29,896.  REF:  P.O. RO-00149272.					2	L	7	2 	4T			RT	A52EU   					 
1999042300366	19990423	00366	EU  	1999	4	23	99ZZZX1583       	1	19990330	G	3231	AIR400390	SEAL            		AIR864141   	SAAB  	SF340 	340B        	7860101	EU  										NLG	LEAKING         	B			FW1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NE	03		3369 			LK9701290					PREMATURE FAILURE OF GLAND SEAL FOR RAMROD LEADING TO LEAKAGE OF HYDRAULIC FLUID.  3,892 CYCLES AT 24,000-CYCLE OVERHAUL	 SCHEDULE.  SAAB P. O. NR X900964.					2	L	7	2 	4T			RT	A52EU   					 
1999042300367	19990423	00367	EU  	1999	4	23	99ZZZX1584       	1	19990329	G	3231	AIR40040L	SEAL            		AIR864101   	SAAB  	SF340 	340B        	7860101	EU  										MLG	LEAKING         	B			FW1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NE	03					CK9003919					PREMATAURE DETERIORATION OF SEAL FOR RAMROD LEADING TO LEAKAGE OF HYDRAULIC FLUID.  20 PERCENT OF OVERHAUL CYCLES.  REF:	  EXPRESS AIRLINES, P.O. RO-0287313M.					2	L	7	2 	4T			RT	A52EU   					 
1999042300368	19990423	00368	EU  	1999	4	23	99ZZZX1585       	1	19990330	G	7500	C46P181711	LINE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										RT ENGINE	CRACKED         	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			GL	13	317CC	4403 				258093				ENGINE HAD LOW POWER ON A FIVE-POINT RUN.  FOUND PIPE CRACKED.  JET-CARE ENGINE MONITORING DID NOT SHOW ANY ABNORMALITY.	  THIS PIPE IS FOR THE RUDDER BIAS SYSTEM.  THERE IS NO REPAIR FOR THIS PIPE, AND MUST BE REPLACED.					2	L	7	2 	4F			RT	A3EU    					 
1999042300371	19990423	00371	WP  	1999	4	23	99ZZZX1588       	2	19990312	G	7230	30756451	SEAL            		307172213   						GARRTT	TFE731	TFE73122B   	01518	WP  					COMPRESSOR	FAILED          	B	P		IY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15		571  			980515820033		P89122			571 HOURS FOLLOWING INSTALL OF NEW MAINLINE CARBON SEALS PER SB 731-72-3596, REV 5, ENGINE EXPERIENCED FLUCTUATING OIL P	RESSURE.  INSP OF ENG OIL FILTER SCREEN REVEALED A LARGE AMOUNT OF CARBON PARTICLES.  ENG REMOVED FOR INSPECTION.  CARBO	N AND METAL DEBRIS WAS FOUND IN HIGH PRESSURE (N2) COMPRESSOR IMPELLER AREA DURING BORESCOPE.  INTERMITTENT BINDING OF N	2 ROTATING GROUP FELT DURING ROTATION OF SPOOL AS ENG WAS BORESCOPED.  ENG DISASSEMBLED, FOUND CARBON MATERIAL ORIGINATE	D FROM FAILED NR 5 CARBON SEAL.  IN ADDITION, SEAL FAILURE CAUSED CERAMIC SEAL RUNNER TO FRACTURE.  THE 'BINDING' OF THE	 N2 SPOOL WAS THE RESULT OF A SMALL PIECE OF SEAL TENSION SPRING WEDGED BETWEEN ONE VANE OF THE HP IMPELLER AND SHROUD.						4	F			E6WE				 
1999042300373	19990423	00373	NE  	1999	4	23	99ZZZX1590       	2	19990304	G	7230	1B5129	BEARING         								PWA   	2037  	PW2037      		NE  					COMPRESSOR	FAILED          	B			WA2D	E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			J			WARNING INDICATION        			NR	NOT REPORTED   	1			NE	03					0441		P72743			ENGINE WAS IN-FLIGHT SHUTDOWN 3-4-99 DUE TO ZERO OIL PRESSURE AND OIL PRESSURE WARNING LIGHT.  ENGINE WINDMILLED OVER 2 	HOURS WITH ZERO OIL PRESSURE.  DISASSEMBLY INSPECTION REVEALED FAILED NR 1 MAIN BEARING.  BEARING CONDITION AS RECEIVED:	  OUTER RACE SPALLED OVER 90-DEGREE ARC.  CAGE BROKEN IN HALF.  BALL SPALLING.  BEARING IS NOT PART OF SUSPECT LOT.  BEA	RING TURNED OVER TO P & W ENGINEERING EAST HARTFORD, CT FOR INVESTIGATION.  ENG TT:  5,249 HRS.  TC:  1,784.								4	F			E17NE				 
1999042300376	19990423	00376	SO  	1999	4	23	99ZZZX1591       	1	19990329	G	5320	1159FH410393	IRU SHELF       			GULSTM	G1159 	GIV         	3980115	SO  										E/E BAY	DAMAGED         	B	P		RO3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03	428GA					1199				THE IRU RACK IS INSTALLED WITH 3 ADJUSTABLE SCREWS/BOLTS FOR ALIGNING THE RACK.  THERE ARE 2 OUTBOARD SCREWS AND ONLY 1 	INBOARD. THIS INBOARD FASTENER HAS BEEN OVER-STRESSED EITHER BY MAINTENANCE CREWS ADJUSTING (OVER-TIGHTENING THIS FASTEN	ER FOR ADJUSTMENTS), OR OVER-STRESSED BY FLIGHT LOADS.  IN EITHER CASE, THIS INSERT HAS ALMOST COMPLETELY PULLED THROUGH	 THE FLOOR PANEL ALLOWING THE IRU TO BE LOOSE ON THE SHELF WHICH COULD GIVE ERRATIC INPUTS TO THE NAV SYSTEM FROM THE IR	U WHICH COULD BECOME MORE SERIOUS IF THE IRU COMES COMPLETELY LOOSE FROM THE SHELF.		2	L	7	2 	4F			RT	A12EA   					 
1999042300377	19990423	00377	WP  	1999	4	23	99ZZZX1592       	1	19990329	G	6220	5143711	HUB             			HILLER	UH12  	UH12        	4360102	WP  										MAIN ROTOR	CRACKED         	B			CHIR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09					3136					DURING NDT INSPECTION, FOUND A CRACK IN THE HUB GOING DOWN 0.25 INCH FROM A STUD HOLE IN THE VERTIAL BORE.						1	G	7	1 	3O				6H1     					 
1999042300736	19990423	00736	EA  	1999	4	23	99ZZZX1593       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					LT MAGNETO	LOOSE           	B		A	NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	445ER	486  			95051478	17280662				BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300737	19990423	00737	EA  	1999	4	23	99ZZZX1594       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					RT MAGNETO	LOOSE           	B		A	NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	445ER	486  			98051570	17280662				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300739	19990423	00739	EA  	1999	4	23	99ZZZX1596       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					RT MAGNETO	LOOSE           	B		A	NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	474ER	484  			98031292	17280623				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300740	19990423	00740	EA  	1999	4	23	99ZZZX1597       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					MAGNETO	LOOSE           	B		A	NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	478ER	481  			98031400	17280623				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300741	19990423	00741	EA  	1999	4	23	99ZZZX1598       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					LT MAGNETO	LOOSE           	B		A	NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	458ER	485  			98031302	17280613				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300742	19990423	00742	EA  	1999	4	23	99ZZZX1599       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					RT MAGNETO	LOOSE           	B		A	NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	458ER	485  			98031303	17280613				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300743	19990423	00743	EA  	1999	4	23	99ZZZX1600       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					LT MAGNETO	LOOSE           	B		A	NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	490ER	482  			98031231	17280633				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300744	19990423	00744	EA  	1999	4	23	99ZZZX1601       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					RT MAGNETO	LOOSE           	B		A	NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	490ER	482  			98031238	17280633				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300745	19990423	00745		1999	4	23	99ZZZX1602       	4	19990414	G	6113	08550303	SUPPORT         			CESSNA	340   	340A        	2076405	CE  										PROPELLER	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	340ME	5    				340A0550				SPINNER SUPPORT CRACKED.						1	L	7	2 	3O				3A25    					 
1999042300746	19990423	00746	EA  	1999	4	23	99ZZZX1603       	2	19990226	G	7414		SCREW           	SLICK       	4371        	PIPER 	PA28  	PA28161     	7102803	SO  	LYC   	O360  	O360A4M     	41514	EA  					MAGNETO	LOOSE           	B		A	NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	147ER	472  			97021406	2841142				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	L	7	1 	3O	3	O		2A13    	E286				 
1999042300747	19990423	00747	CE  	1999	4	23	99ZZZX1604       	1	19990330	G	5312	07126167	BULKHEAD        			CESSNA	182   	182P        	2075816	CE  										FUSELAGE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	20884					18261285				THIS REPORT SUBMITTED IAW PARAGRAPH I OF AD 72-07-09.  REAR FUSELAGE BULKHEAD CRACKED AT TOP OF RIGHT RUDDER CABLE CUT-O	UT BY RUDDER STOP BOLT.					1	H	7	1 	3O			NT	TA13    					 
1999042300748	19990423	00748	SO  	1999	4	23	99ZZZX1605       	2	19990313	G	8530	SA21361	KEEPER          	SUPAIRPART  	CL61        	CESSNA	150   	150L        	2071826	CE  	CONT  	O200  	O200A       	17020	SO  					EXHAUST	WRONG PART      	D	L			O				OTHER                   				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		AP	APPROACH       	1			SO	06	16245	5    			6829120H	15073568	21448272A			WHILE INBOUND FOR LANDING, ENGINE BEGAN TO RUN ROUGH.  PILOT LANDED SAFELY.  MECHANIC REMOVED SPARK PLUGS.  FOUND NR 2 C	YLINDER PLUGS OILY.  REMOVED ROCKER COVER TO FIND INTAKE ROCKER BROKEN.  VALVE STEM REVEALED GALLING AND SHARP EDGES ON 	STEM.  INTAKE VALVE COVERS ON OTHER VALVES TO REVEAL THE SAME.  EXHAUST VALVES OK.  SUBMITTER STATED WRONG KEEPERS WERE 	USED.			1	H	7	1 	3O	3	O		3A19    	E252				 
1999042300749	19990423	00749	SO  	1999	4	23	99ZZZX1606       	2	19990313	G	8530	SA21361	KEEPER          	SUPAIRPART  	CL61        	CESSNA	150   	150L        	2071826	CE  	CONT  	O200  	O200A       	17020	SO  					EXHAUST	WRONG PART      	D				O				OTHER                   				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		AP	APPROACH       	1			SO	06	16245	5    			6829106H6	15073568	21448272A			WHILE INBOUND FOR LANDING, ENGINE BEGAN TO RUN ROUGH.  PILOT LANDED SAFELY.  MECHANIC REMOVED SPARK PLUGS.  FOUND NR 2 C	YLINDER PLUGS OILY.  REMOVED ROCKER COVER TO FIND INTAKE ROCKER BROKEN.  VALVE STEM REVEALED GALLING AND SHARP EDGES ON 	STEM.  INTAKE VALVE COVERS ON OTHER VALVES TO REVEAL THE SAME.  EXHAUST VALVES OK. SUBMITTER STATED WRONG KEEPERS WERE U	SED.			1	H	7	1 	3O	3	O		3A19    	E252				 
1999042300750	19990423	00750		1999	4	23	99ZZZX1607       	1	19990305	G	3242	9533131	SLEEVE          	GOODYEARAERO	9560685     															BRAKE	BROKEN          	B			LV52	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	11					AUG890051					BRAKE LEAKING.  DURING DISASSEMBLY, DISCOVERED ONE PISTON SLEEVE WAS BROKEN BETWEEN THE TOP OF THE SLEEVE AND WHERE THE 	THREADS END.  THE SLEEVE IS ITEM 33 OF CMM 32-40-01.																		 
1999042300751	19990423	00751	CE  	1999	4	23	99ZZZX1608       	1	19990326	G	2810	S14956	LINE            			CESSNA	172   	172M        	2072418	CE  										FUEL VENT	LEAKING         	D		A		A				UNSCHED LANDING         				B	O		SMOKE/FUMES/ODORS/SPARKS  	OTHER                     		NR	NOT REPORTED   	1			SO	03	80842	3150 				17266770				ODOR OF AVIATION FUEL (STRONG) IN CABIN.  AIRCRAFT RETURNED TO BASE.  MAINTENANCE INSPECTION DISCOVERED LEAKS AT TWO OF 	SIX HOSES.  SUBMITTER STATED ALL HOSES WERE NEAR TOTAL FAILURE.					1	H	7	1 	3O			NT	3A12    					 
1999042300752	19990423	00752	CE  	1999	4	23	99ZZZX1609       	1	19990325	G	5531	NAS22415	BOLT            			CESSNA	180   	180         	2072602	CE  										VERT STABILIZER	WRONG PART      	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	15	9240C					31347				DURING ANNUAL INSPECTION, FOUND INCORRECT HARDWARE INSTALLED ON AFT VERTICAL FIN SPAR ATTACH.  BOLTS INSTALLED WERE STAN	DARD AN HARDWARE.  BOLT SHOULD HAVE BEEN A NAS224-15.  CONTACTED CESSNA PARTS DEPT AND FOUND THE PART NUMBER HAD BEEN SU	PERCEDED TO MS27039-6-15.  INCORRECT HARDWARE HAS BEEN FOUND ON 2 OTHER AIRCRAFT DURING INSPECTIONS.				1	H	7	1 	3O			NC	5A6     					 
1999042300753	19990423	00753	CE  	1999	4	23	99ZZZX1610       	1	19990401	G	5312	085112131	BULKHEAD        			CESSNA	340   	340A        	2076405	CE  										FUSELAGE	CORRODED        	D	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	06	340EZ	4090 				340A0118				DURING ANNUAL INSPECTION AND C/W AD 75-23-08R5 EXHAUST SYSTEM, IT WAS NOTED BEHIND LT ENGINE EXHAUST OUTLET TUBE A RAISE	D SPOT OF CORROSION ON OUTBOARD MOUNT BEAM.  TOUCHING WITH SCRIBE, HOLE PUNCHED THROUGH EASILY.  WITH OUTLET TUBE REMOVE	D, CORROSION WAS NOTED ON AFT CANTED BULKHEAD WEB, PN 08516 01-27 ALSO.  4,089.9 HOURS TOTAL TIME.  BOTH BEAM AND WEB WE	RE REPLACED.			1	L	7	2 	3O				3A25    					 
1999042300754	19990423	00754		1999	4	23	99ZZZX1611       	1	19990312	G	8011	646275	STARTER         	TELEDYNESYST																ENGINE	MISOVERHAULED   	B			R5ER	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	05					A11673					AT LAST OVERHAUL, INSULATION SLEEVES WERE INSTALLED AROUND THE 4 THROUGH-BOLTS WHICH HOLD THE UNIT TOGETHER.  THE INSULA	TION ON ONE OF THE BOLTS CAME IN CONTACT WITH THE ROTATING ARMATURE.  THREE-FOURTHS OF THE INSULATION WAS DESTROYED SEND	ING FIBERS THROUGHOUT THE STARTER.  FIBERS FOULED THE COMMUTATOR END OF THE ARMATURE CAUSING PREMATURE BEARING AND SHIM 	FAILURE.																 
1999042300755	19990423	00755	EA  	1999	4	23	99ZZZX1612       	3	19990311	G	6110		PROPELLER       			PIPER 	PA28  	PA28140     	7102802	SO  						SNSNCH	74DM	M74DM       	EA  	FORWARD	BENT            	B			W59R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07								K12939		PROPELLER SUBMITTED FOR 'POLISH AND CLEAN-UP'.  UPON FURTHER INSPECTION, THE PROPELLER WAS FOUND SEVERELY CORRODED, BENT	, AND UNDER LIMITS, .200 INCH AT THE 33.3 INCH STATIONS.  PROPELLER RETURNED TO CUSTOMER RED FLAGGED.					1	L	7	1 	3O				2A13    		5	N	P886	 
1999042300756	19990423	00756		1999	4	23	99ZZZX1613       	1	19990409	G	2701	2594034	YOKE ASSY       	HONEYWELL   	23929D444   															COCKPIT	MISREPAIRED     	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CE	07					79113506					THE MFG SETSCREW HAS BEEN REMOVED AND A HOLE HAS BEEN DRILLED IN YOKE AND LONGER SETSCREW HAS BEEN ADDED.  BY DOING THIS	, THE TORQUE RETAINING RING IS NOT ALLOWED TO SLIP IN THE EVENT THAT SOMETHING SHOULD BIND UP CAUSING DAMAGE TO THE YOKE	, GEARS, OR UNIT.  THIS ALSO RUINS THE INTEGRITY OF THE YOKE.  THERE IS NO HONEYWELL DOCUMENTATION STATING THAT THIS IS 	AN ACCEPTABLE FIX.  THIS CAN BE PREVENTED BY STOPPING THIS PROCEDURE.  SETSCREW ADDED BY DUNCAN AVIATION..																 
1999042300757	19990423	00757	GL  	1999	4	23	99ZZZX1614       	3	19990406	G	6114	675577	HUB             													MCAULY	2A36C	2A36C23     	GL  	PROPELLER	CRACKED         	B			ME4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19			643  					675577		PROPELLER RECEIVED FOR INSPECTION FOR RED DYE OIL LEAK (SMALL).  DISASSEMBLED PROPELLER, INSPECTED HUB WITH 10X POWER MI	CROSCOPE, FOUND CRACK IN NR 2 BLADE SOCKET, IN 2 O'CLOCK POSITION, 1.50 INCHES TO 2 INCHES LONG.  AD NOTE 89-26-08:  OIL	 FILLING THIS PROPELLER PREVENTED A CATASTROPHIC FAILURE.														5	C	P880	 
1999042300759	19990423	00759	EA  	1999	4	23	99ZZZX1616       	2	19990225	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					RT MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	426ER	484  			98031376	17280647				BREAKER POINT CONTACT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300760	19990423	00760	EA  	1999	4	23	99ZZZX1617       	2	19990225	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					LT MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	426ER	484  			98031350	17280647				DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300761	19990423	00761	EA  	1999	4	23	99ZZZX1618       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					RT MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	427ER	485  			98031408	17280606				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT ASSEMBLY SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300762	19990423	00762	EA  	1999	4	23	99ZZZX1619       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					LT MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	427ER	485  			98031405	17280606				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT ASSEMBLY SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300763	19990423	00763	EA  	1999	4	23	99ZZZX1620       	2	19990225	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	480ER	478  			98031254	17280624				BOTH DISTIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300764	19990423	00764	EA  	1999	4	23	99ZZZX1621       	2	19990225	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					RT MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	483ER	480  			98031325	17280608				BREAKER POINT PIVOT SCREW AND BOTH DISTRIBUTOR BLOCK SCREWS FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300765	19990423	00765	EA  	1999	4	23	99ZZZX1622       	2	19990225	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					LT MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	483ER	480  			98031332	17280608				BREAKER POINT PIVOT SCREW AND BOTH DISTRIBUTOR BLOCK SCREWS FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300766	19990423	00766	EA  	1999	4	23	99ZZZX1623       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					RT MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	429ER	479  			98031410	17280608				BOTH DISTRIBUTOR BLOCK SCREWS, BREAKER POINT PIVOT SCREW, AND COIL GROUND SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPEC	TION.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300767	19990423	00767	EA  	1999	4	23	99ZZZX1624       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					LT MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	429ER	479  			98031406	17280608				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT ASSEMBLY SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300768	19990423	00768	EA  	1999	4	23	99ZZZX1625       	2	19990225	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	446ER	464  			98031131	17280638				BOTH DISTRIBUTOR BLOCK SCREWS FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300769	19990423	00769	EA  	1999	4	23	99ZZZX1626       	2	19990225	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	476ER	485  			98031411	17280638				MAGNETO HOUSING SCREWS, BREAKER POINT CONTACT SCREW, AND BOTH DISTRIBUTOR BLOCK SCREWS FOUND LOOSE DURING FIRST 500-HOUR	 INSPECTION.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300770	19990423	00770	EA  	1999	4	23	99ZZZX1627       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	421ER	481  			98031151	17280638				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300771	19990423	00771	EA  	1999	4	23	99ZZZX1628       	2	19990225	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	421ER	481  			98031358	17280638				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300772	19990423	00772	EA  	1999	4	23	99ZZZX1629       	2	19990225	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	424ER	483  			98031369	17280640				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300773	19990423	00773	EA  	1999	4	23	99ZZZX1630       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	478ER	481  			98031383	17280623				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300774	19990423	00774	EA  	1999	4	23	99ZZZX1631       	2	19990225	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	448ER	482  			98021708	17280610				BOTH DISTRIBUTOR BLOCK SCREWS, BREAKER POINT PIVOT SCREW, AND COIL GROUND SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPEC	TION.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300775	19990423	00775	EA  	1999	4	23	99ZZZX1632       	2	19990226	G	7414		SCREW           	SLICK       	4371        	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					MAGNETO	LOOSE           	B			NX42	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	474ER	484  			98031381	17280616				BOTH DISTRIBUTOR BLOCK SCREWS AND BREAKER POINT PIVOT SCREW FOUND LOOSE DURING FIRST 500-HOUR INSPECTION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999042300776	19990423	00776	CE  	1999	4	23	99ZZZX1633       	1	19990314	G	2810	07260015	TANK            			CESSNA	180   	180G        	2072616	CE  										LT WING	CONTAMINATED    	H				A				UNSCHED LANDING         				Y	J		ENGINE STOPPAGE           	WARNING INDICATION        		CR	CRUISE         	1			AL	05	4721U	800  				18051421				AIRCRAFT LOST POWER AFTER TAKEOFF IN CRUISE FLIGHT.  THE PILOT WAS IN LOCAL AIRPORT AREA AND GOING TO MAKE 3 TOUCH AND G	O'S, AFTER POWER LOST, PILOT LANDED 150 FEET SHORT OF RUNWAY AND NOSED-OVER.  INVESTIGATION REVEALED SOME WATER IN GASCO	LATOR.  THE LT FUEL TANK HAD MANY WRINKLES IN THE DRAIN AREA FOR SUMPING TANK.  BOTH TANKS REPLACED 1985 AND FUEL DRAINS	 INSTALLED PER 84-10-01 R1 AND FUEL TANK CAPS HAD O-RING REPLACED PARA 3 (IV) WAS CHECKED AND STATED IN LOG THAT THERE W	AS LESS THAN 3 OUNCES OF FLUID IN CHECK OF THANKS, NO FURTHER ACTION.		1	H	7	1 	3O				5A6     					 
1999042300777	19990423	00777	SO  	1999	4	23	99ZZZX1634       	1	19990326	G	3213	AN522	BOLT            			PIPER 	PA28  	PA28140     	7102802	SO  										LT MLG	FAILED          	D				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			EA	11	1499H					287725146				DURING ROUTINE SOFT FIELD LANDING AT HOME AIRPORT, LT MLG STUB AXLE AND OLEO PISTON ASSY (PN 78738-002) DEPARTED MATING 	CYLINDER ASSY (PN 65319-004) AND CAUSED AIRCRAFT TO SWERVE OFF RUNWAY AND COME TO REST IN GRASS AREA ALONGSIDE RUNWAY. A	IRCRAFT SUSTAINED DAMAGE TO LT FLAP, STUB AXLE AND TORQUE LINKS.  EXTREME OUTBOARD LEADING EDGE OF WING WAS DAMAGED AFTE	R COLLIDING WITH RUNWAY LIGHT FIXTURE.  NO INJURIES TO CFI AND STUDENT.  POSSIBLE CAUSE, FAILURE OF MOUNT BOLT (AN5-22) 	SECURING LOWER TORQUE LINK (PN 78033-000) TO STUB AXLE.		1	L	7	1 	3O				2A13    					 
1999042300779	19990423	00779	CE  	1999	4	23	99ZZZX1636       	1	19990329	G	3510		LINE            			CESSNA	414   	414A        	2075907	CE  										NOSE BAY	CHAFED          	B		A	FEHR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	13	37448					414A0843				OXYGEN AND CAPILLARY LINE CHAFE ON RAM AIR DUCT.  THIS MAY NOT BE FOUND UNTIL OXYGEN SYSTEM IS TURNED ON.  THIS CHAFING 	OCCURS JUST FORWARD OF THE AVIONICS BULKHEAD COMPARTMENT.					1	L	7	2 	3O				A7CE    					 
1999042300780	19990423	00780		1999	4	23	99ZZZX1637       	4	19990301	G	3416		CONNECTOR       	NARCO       		PIPER 	PA30  	PA30        	7103002	SO  										E/E BAY	MISINSTALLED    	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	7206Y					30232				CONNECTOR TO ENCODER WAS SECURED ON ONE SIDE ONLY ALLOWING SOME OF CONTACTS TO BE OPEN UNDER CERTAIN CONDITIONS.  SUBMIT	TER SUGGESTED POSSIBLE CAUSE, CONNECTOR WAS NOT FULLY ENGAGED WHEN LOCK WAS MOVED TO LOCKED POSITION.					1	L	7	2 	3O				A1EA    					 
1999042300781	19990423	00781	SO  	1999	4	23	99ZZZX1638       	2	19990401	G	8530	649358	HEAD            			CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  					ENGINE	CRACKED         	B			J2SR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	05	6400X		1072 			U20605865	570995			HEAD CRACKED, STARTING FROM THE EXHAUST VALVE SEAT AND TRAVELING UP ABOVE THE SPARK PLUG BOSS AND BACK DOWN APPROXIMATEL	Y ONE INCH FROM THE INTAKE VALVE SEAT.  THE ENTIRE LENGTH OF THE CRACK WAS APPROXIMATELY FOUR INCHES.  A .1250 INCH BY O	NE INCH HOLE HAD OPENED UP NEAR THE EXHAUST SEAT AND SEVERAL FINS HAD PIECES MISSING.				1	H	7	1 	3O	3	O		A4CE    	E5CE				 
1999042300782	19990423	00782	SO  	1999	4	23	99ZZZX1639       	2	19990329	G	8530	654649A3BP	VALVE GUIDE     			CESSNA	182   	182M        	2072728	CE  	CONT  	O470  	O470R       	17026	SO  					CYLINDER	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	91767	210  				18259899				EXHAUST VALVE GUIDES WORN OUT SEVERELY ON ALL 6 CYLINDERS.  210.3 HOURS SINCE NEW.						1	H	7	1 	3O	3	O	NT	3A13    	E273				 
1999042300783	19990423	00783	SO  	1999	4	23	99ZZZX1640       	2	19990329	G	8530	65464943BP	VALVE GUIDE     			CESSNA	182   	182M        	2072728	CE  	CONT  	O470  	O470R       	17026	SO  					CYLINDER	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	91767	133  				18259899				EXHAUST VALVE GUIDES WORN OUT SEVERELY ON ALL 6 CYLINDERS.  133.0 HOURS SINCE NEW.						1	H	7	1 	3O	3	O	NT	3A13    	E273				 
1999042300784	19990423	00784	SW  	1999	4	23	99ZZZX1641       	1	19990329	G	2730		NUT             			BBAVIA	7     	7ECA        	21101NN	SW  										ELEVATOR	MISSING         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	9510S					7ECA275				DURING ANNUAL INSPECTION, COTTER PIN AND NUT WERE FOUND MISSING FROM UP ELEVATOR CABLE ATTACH AT REAR CONTROL STICK.  EL	EVATOR CABLE PULLEYS UNDER AND AFT OF BAGGAGE AREAS WERE FOUND VERY DRY.  CABLES WERE FRAYED AT PULLEY LOCATIONS.  THESE	 AREAS ARE NOT EASILY ACCESSIBLE FOR INSPECTION.				1	H	7	1 	3O				A759    					 
1999042300785	19990423	00785	SW  	1999	4	23	99ZZZX1642       	1	19990216	G	2820	2540537	REGULATOR       	BENDIX      	2524054     	MOONEY	M20   	M20F        	5870214	SW  										FUEL SYSTEM	CONTAMINATED    	G				O				OTHER                   				Y	W		ENGINE STOPPAGE           	INADEQUATE Q C            		NR	NOT REPORTED   	1			GL	15	21NA	2072 	1174 		54863	680203				ENGINE QUIT WHILE AIRCRAFT WAS FLYING.						1	L	7	1 	3O				2A3     					 
1999042300786	19990423	00786		1999	4	23	99ZZZX1643       	4	19990331	G	3457		RECEIVER        		M3          	PIPER 	PA32  	PA32300     	7103212	SO  										GPS	FAILED          	H				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			CE	01	3504Q				AL13203	327740064				THE NORTHSTAR M3 GPS RECEIVER, SN AL13203, RECENTLY INSTALLED IN PIPER CHEROKEE 6, PA-32-300, N3504Q, SN 32-7740064, WIL	L NOT PROPERLY ILLUMINATE APR, MSG, WPT, OR PTK ANNUNCIATORS IN SEPARATE MSI AVIONICS MODEL INSSDU-IV NAV-1/GPS NAVIGATI	ON SELECTOR/ANNUNCIATOR ASSEMBLY, PN 97-10354AR-14.  THE NORTHSTAR M3 UNIT IN THIS AIRCRAFT WILL NOT ILLUMINATE ANY OF T	HE FOUR ANNUNCIATORS IN THE INSSDU-IV UNIT BECAUSE THE M3'S ANNUNCIATOR DRIVERS CANNOT HANDLE THE 0.120 AMP INCANDESCENT	 CURRENT LOAD.		1	L	7	1 	3O				A3SO    					 
1999042300789	19990423	00789	EU  	1999	4	23	99ZZZX1644       	3	19990412	G	6110	2202	BEARING         													CNPSL	AW2	AW2*        	EU  	PROPELLER ASSY	CRACKED         	B	S		NWOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05								W342035		BEARING SLEEVE SHATTERED AROUND FIRST AND SECOND OUTSIDE THREADS.																6	C	P9EU	 
1999042300790	19990423	00790	EA  	1999	4	23	99ZZZX1645       	2	19990301	G	8520		PISTON PIN      			PIPER 	PA46  	PA46350P    		SO  	LYC   	O540  	TIO540AE2A  	41532	EA  					ENGINE	PEELED          	B			BJ3R	O				OTHER                   				Y			ENGINE STOPPAGE           			NR	NOT REPORTED   	1			WP	15	9167R	250  				4622032	L898561A			ENGINE FAILURE.  HIGH AMOUNTS OF FERROUS AND NON-FERROUS METALS FOUND IN OIL FILTER.  FOUND THAT UP TO .1250 INCH OF MET	AL PEELED FROM NR 1, NR 2, AND NR 6 PISTON RING PLUGS.  ALL 6 ROD BEARINGS SEVERELY SCORED FROM FOREIGN METAL.  FRONT MA	IN BEARING ALSO SEVERELY SCORED.  ONLY 250 HOURS SMOH.				1	L	7	1 	3O	3	O	RT	A25SO   	E14EA				 
1999042300791	19990423	00791	EA  	1999	4	23	99ZZZX1646       	2	19990419	G	7414	10349276	CAPACITOR       		S6LN1200    	PIPER 	PA32  	PA32300     	7103212	SO  	LYC   	O540  	IO540K1A5   	41532	EA  					LT MAGNETO	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	07	55209	250  				327340105	L1054548			DURING GROUND RUN, NOTED THE LEFT MAG HAD NO RPM DROP DURING A MAG CHECK.  SWITCHED THE LEFT MAG OFF AND THE ENGINE STAY	ED RUNNING.  CHECKED THE IGNITION SWITCH SYSTEM AND DETERMINED IT TO BE CONNECTED AND OPERATING PROPERLY.  REPLACED THE 	CAPACITOR AND THE SYSTEM OPERATIONAL CHECKED OK.				1	L	7	1 	3O	3	O		A3SO    	1E4				 
1999042300792	19990423	00792	CE  	1999	4	23	99ZZZX1647       	1	19990419	G	3221	12434025	TRUNNION        			CESSNA	210   	210N        	2073453	CE  										NLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	25	5197C					21063714				DURING INSPECTION OF NOSE GEAR LOWER TRUNNION FOR C/W CESSNA SEB 94-19, NO CRACKS WERE NOTED.  EIGHTY HOURS LATER DURING	 REPLACEMENT OF LOWER TRUNNION FOR FINAL C/W SEB 94-19, CRACKS WERE NOTED ON BOTH SIDES OF TRUNNION AS DESCRIBED IN SEB 	94-19.  FAILURE OF THIS PART WOULD BE VERY COSTLY AND POSSIBLY DANGEROUS.				1	H	7	1 	3O				3A21    					 
1999042300793	19990423	00793	SO  	1999	4	23	99ZZZX1648       	1	19990118	G	3211	67054003	TRUNNION        			PIPER 	PA32  	PA32RT300   	7103215	SO  										MLG	FAILED          	D	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	39540				13940	32R7885229				TRUNNION FOUND DAMAGED ON PRE-FLIGHT INSPECTION.						1	L	7	1 	3O				A3SO    					 
1999042300794	19990423	00794	SO  	1999	4	23	99ZZZX1649       	1	19990331	G	5711	6207007	SPAR            		6660105     	PIPER 	PA28  	PA28180     	7102808	SO  										RT WING	CORRODED        	B			AW4R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	11	9738J	3710 				283932				DURING ANNUAL INSPECTION, BOTH LEFT AND RIGHT FUEL TANK VENTS WERE FOUND INSTALLED BACKWARDS.  UPON REMOVAL OF TANKS TO 	REPOSITION VENTS, LARGE AMOUNTS OF CORROSION WERE FOUND ON BOTH LEFT AND RIGHT INBOARD SPAR CAPS.  ON RIGHT SPAR (PN 620	70-07), THE SPAR CAP AT THE OUTBOARD END OF THE RIGHT FUEL TANK (AT RIB, PN 66601-05), THE CAP SHOWS EVIDENCE OF INTERGR	ANULAR/EXFOLIATION CORROSION.  TOTAL EXTENT OF CORROSION HAS NOT BEEN DETERMINED AT THIS DATE.  RECORDS REVIEW SHOWS THA	T PIPER MANDATORY SB 1006 (WHICH ADDRESSES THIS SUBJECT) HAD NOT BEEN ACCOMPLISHED.		1	L	7	1 	3O				2A13    					 
1999042300795	19990423	00795	CE  	1999	4	23	99ZZZX1650       	1	19990322	G	7920	035A862129	LINE            			MTSBSI	MU2   	MU2B26      	5780408	CE  										COCKPIT	CRACKED         	H		A		O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			GL	15	688RA					688				FLIGHT CREW NOTICED LOW OIL PRESSURE.  UPON INVESTIGATION, FOUND CRACKED FLARE ON OIL PRESSURE GAUGE PORT LINE.  REPLACE	MENT LINE WAS INSTALLED BY AIRCRAFT OPERATOR PERSONNEL.					1	H	7	2 	3T			RT	A10SW   					 
1999042300796	19990423	00796		1999	4	23	99ZZZX1651       	4	19990309	G	3417	HG180U323	ADC             			BOEING	737   	737*        		NM  										E/E BAY	DAMAGED         	B	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15					X145699					THIS AIR DATA COMPUTER IS USED ON A BOEING 737.  EXCESSIVE LOAD ON J3 PINS CAUSED CONNECTOR J3 TO MELT AROUND THESE PINS	.  ADAPTER DG120 WAS NOT INCLUDED WITH AIR DATA COMPUTER.  SUSPECT WATER DAMAGE TO DG120, WHICH CAUSED SHORTS AND OVERLO	ADS.  IN THIS CONDITION EVEN IF HG180U POWER IS TURNED OFF, OUTPUT SIGNALS WILL BE POSSIBLE ON THESE FUNCTIONS.				2	L	7	2 	4F			RT	A16WE   					 
1999042300797	19990423	00797	CE  	1999	4	23	99ZZZX1652       	1	19990409	G	2730	5052416110R	ACTUATOR        			BEECH 	90    	E90         	1152914	CE  										RT ELEVATOR	MISOVERHAULED   	B			EBVD	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	09	274KA					LW274				DURING PHASE INSPECTIONS, BOTH LT AND RT ELEVATOR TRIM ACTUATORS WERE FOUND OUT OF FREE-PLAY LIMITS PER BEECH E90 MM.  A	CQUIRED 2 NEW ACTUATORS.  BOTH INSTALLED WITH ALL NEW BUSHINGS AND BOLTS IN SYSTEM.  AFTER FINAL RIGGING, ANOTHER FREE-P	LAY CHECK WAS MADE.  THE RT ACTUATOR WAS IN LIMITS BY .001 INCH, LT OUT OF LIMITS BY .009 INCH.  ANOTHER OVERHAULED LT A	CTUATOR WAS ACQUIRED AND INSTALLED.  FINAL FREE-PLAY CHECK SHOWED IT TOO WAS OUT OF LIMITS.  ALL 3 ACTUATORS OVERHAULED 	BY SAME FACILITY.  ANOTHER SET OF LT AND RT ACTUATORS WERE FOUND, BUT SENT BACK TO O/H FACILITY TO BE RE-CHECKED FOR PRO	PER O/H LIMITS.  SUBMITTER RECOMMENDED ALL BEECH E90 ELEVATOR TRIM ACTUATOR CHANGES HAVE A FINAL FREE-PLAY CHECK MADE.	1	L	7	2 	3T				3A20    					 
1999042300798	19990423	00798	CE  	1999	4	23	99ZZZX1653       	1	19990409	G	2730	5052416111R	ACTUATOR        			BEECH 	90    	E90         	1152914	CE  										LT ELEVATOR	MISOVERHAULED   	B			EBVD	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	09	274KA					LW274				DURING PHASE INSPECTIONS, BOTH LT AND RT ELEVATOR TRIM ACTUATORS WERE FOUND OUT OF FREE-PLAY LIMITS PER BEECH E90 MM.  A	CQUIRED 2 NEW ACTUATORS.  BOTH INSTALLED WITH ALL NEW BUSHINGS AND BOLTS IN SYSTEM.  AFTER FINAL RIGGING, ANOTHER FREE-P	LAY CHECK WAS MADE.  THE RT ACTUATOR WAS IN LIMITS BY .001 INCH, LT OUT OF LIMITS BY .009 INCH.  ANOTHER OVERHAULED LT A	CTUATOR WAS ACQUIRED AND INSTALLED.  FINAL FREE-PLAY CHECK SHOWED IT TOO WAS OUT OF LIMITS.  ALL 3 ACTUATORS OVERHAULED 	BY SAME FACILITY.  ANOTHER SET OF LT AND RT ACTUATORS WERE FOUND, BUT SENT BACK TO O/H FACILITY TO BE RE-CHECKED FOR PRO	PER O/H LIMITS.  SUBMITTER RECOMMENDED ALL BEECH E90 ELEVATOR TRIM ACTUATOR CHANGES HAVE A FINAL FREE-PLAY CHECK MADE.	1	L	7	2 	3T				3A20    					 
1999043000010	19990430	00010	NE  	1999	4	30	99ZZZX1657       	1	19990324	G	6210	64M57685936	BLADE           			SKRSKY	S64   	S64E        	8142604	NE  										MAIN ROTOR	CRACKED         	B	S		JYDR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	194AC	6249 			641520201048	64017				BLADE REMOVED FROM AIRCRAFT DUE TO BIM INDICATION.  ALL CRACKS WERE LOCATED ON BOTTOM SIDE OF THE BLADE.  SB-64E-62-10-0	1, WHICH ULTRASONICALLY INSPECTS THE TWO MOST OUTBOARD BOLT HOLES ON THE TOP AND BOTTOM SIDE, WAS C/W 39.8 HOURS PRIOR T	O REMOVAL OF THE BLADE FOR BIM INDICATION.  NO DEFECTS WERE NOTED.				2	G	7	2 	4U				H4EA    					 
1999043000024	19990430	00024	WP  	1999	4	30	99ZZZX1662       	1	19990223	G	5320		STIFFENER       			DOUG  	DC10  	DC1030      	3023501	WP  										BS 555-595	CRACKED         	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				STIFFENER FROM STA 555 TO STA 595 JUST OUTBOARD OF EXHAUST DOOR IS CRACKED AT NR 1 AIRCRAFT BAY.						2	L	7	3 	4F				A22WE   					 
1999043000025	19990430	00025	WP  	1999	4	30	99ZZZX1663       	1	19990223	G	5320		TRUNNION        			DOUG  	DC10  	DC1030      	3023501	WP  										NLG	CORRODED        	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				NOSE LANDING GEAR TRUNNION, LEFT SIDE LOWER SURFACE HAS CORROSION AROUND FASTENERS.						2	L	7	3 	4F				A22WE   					 
1999043000026	19990430	00026	WP  	1999	4	30	99ZZZX1664       	1	19990223	G	5320		FITTING         			DOUG  	DC10  	DC1030      	3023501	WP  										RT NLG	CORRODED        	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				RIGHT NOSE GEAR TRUNNION FITTING LOWER SURFACE HAS CORROSION ON INBOARD LOWER FLANGE.						2	L	7	3 	4F				A22WE   					 
1999043000027	19990430	00027	WP  	1999	4	30	99ZZZX1665       	1	19990223	G	5313		STRINGER        			DOUG  	DC10  	DC1030      	3023501	WP  										RT MLG WW	CRACKED         	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				RIGHT MLG WHEELWELL AFT OUTBOARD LOWER BULKHEAD STRINGER CRACKED IN 2 PLACES.						2	L	7	3 	4F				A22WE   					 
1999043000028	19990430	00028	WP  	1999	4	30	99ZZZX1666       	1	19990223	G	5311		FRAME           			DOUG  	DC10  	DC1030      	3023501	WP  										BS 590	CORRODED        	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				NR 1 AIRCRAFT BAY AT APPROXIMATELY STA 590, HAS CORROSION ON FORWARD SIDE OF FRAME 5 INCHES BELOW OPENING.						2	L	7	3 	4F				A22WE   					 
1999043000029	19990430	00029	WP  	1999	4	30	99ZZZX1667       	1	19990223	G	5400		FAIRING         			DOUG  	DC10  	DC1030      	3023501	WP  										NR 2 ENGINE	CHAFED          	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				NR 2 ENGINE AFT PYLON LOWER FAIRING MATING SURFACE TO EXHAUST NOZZLE IS CHAFED 100 PERCENT MATERIAL LOSS.						2	L	7	3 	4F				A22WE   					 
1999043000030	19990430	00030	WP  	1999	4	30	99ZZZX1668       	1	19990223	G	7810		NOZZLE          			DOUG  	DC10  	DC1030      	3023501	WP  										NR 2 ENGINE	CHAFED          	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				NR 2 ENGINE EXHAUST NOZZLE IS HEAVILY CHAFED FROM AFT PYLON LOWER FAIRING AT TAIL END POSITION OF NOZZLE.						2	L	7	3 	4F				A22WE   					 
1999043000031	19990430	00031	WP  	1999	4	30	99ZZZX1669       	1	19990223	G	5400	C22177763	FAIRING         			DOUG  	DC10  	DC1030      	3023501	WP  										NR 3 PYLON	CHAFED          	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				NR 3 PYLON EXHAUST FAIRING, PN C221776-3, HAS FIVE AREAS CHAFING ON LOWER SURFACE, WORST AREA IS 1.6 INCHES BY 1 INCH BY	 .023 INCH DEEP.					2	L	7	3 	4F				A22WE   					 
1999043000032	19990430	00032	WP  	1999	4	30	99ZZZX1670       	1	19990223	G	5400		WEB             			DOUG  	DC10  	DC1030      	3023501	WP  										NR 1 PYLON	CRACKED         	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				LOWER BOTTOM WEB ON NR 1 PYLON, FORWARD END, IS CRACKED IN SEVERAL PLACES IN FIRST SECTION.						2	L	7	3 	4F				A22WE   					 
1999043000033	19990430	00033	WP  	1999	4	30	99ZZZX1671       	1	19990223	G	5400		WEB             			DOUG  	DC10  	DC1030      	3023501	WP  										NR 1 PYLON	CRACKED         	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				LOWER BOTTOM WEB ON FORWARD END OF NR 1 PYLON IS CRACKED AT TWO RIVETS, IN SECOND SECTION.						2	L	7	3 	4F				A22WE   					 
1999043000034	19990430	00034	WP  	1999	4	30	99ZZZX1672       	1	19990223	G	5320		STANCHION       			DOUG  	DC10  	DC1030      	3023501	WP  										BS 1970	CORRODED        	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				AFT BAGGAGE PIT STANCHION STA 1970 CORRODED 10 PERCENT, 100 PERCENT MATERIAL LOSS.						2	L	7	3 	4F				A22WE   					 
1999043000035	19990430	00035	WP  	1999	4	30	99ZZZX1673       	1	19990223	G	5330		SKIN            			DOUG  	DC10  	DC1030      	3023501	WP  										BS 1967-1987	CORRODED        	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				INNER SKIN FROM STA 1967 TO STA 1987 FROM LONGERON 48L TO  LONGERON 48R HAS CORROSION.						2	L	7	3 	4F				A22WE   					 
1999043000036	19990430	00036	WP  	1999	4	30	99ZZZX1674       	1	19990223	G	7110		COWL            			DOUG  	DC10  	DC1030      	3023501	WP  										NR 1 ENGINE	CRACKED         	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				NR 1 ENGINE BOTTOM AFT CORNER OF FAN COWL CRACK IN FAIRING.						2	L	7	3 	4F				A22WE   					 
1999061000011	19990610	00011	WP  	1999	6	10	99ZZZX1675       	1	19990203	G	5320		SUPPORT         			DOUG  	DC10  	DC1030      	3023501	WP  										BS 1521	CRACKED         	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				AT STA 1521 BETWEEN NR 2 AND NR 3 SEAT TRACKS, FLOOR BOARD SUPPORT IS CRACKED, LEFT SIDE.						2	L	7	3 	4F				A22WE   					 
1999043000037	19990430	00037	WP  	1999	4	30	99ZZZX1676       	1	19990223	G	5712		RIB             			DOUG  	DC10  	DC1030      	3023501	WP  										WS 314.6 & 325.1	CRACKED         	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				RIGHT WING DROOPED LEADING EDGE HAS 2 EACH RIBS CRACKED AT AFT END STA XDRE 314.677 AND XDRE 325.114.						2	L	7	3 	4F				A22WE   					 
1999043000038	19990430	00038	WP  	1999	4	30	99ZZZX1677       	1	19990223	G	5730		SKIN            			DOUG  	DC10  	DC1030      	3023501	WP  										RT WING	CRACKED         	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				RIGHT WING DROOPED LEADING EDGE HAS A 4 INCH CRACK ON RT TIP TRAILING EDGE CORNER.						2	L	7	3 	4F				A22WE   					 
1999043000039	19990430	00039	WP  	1999	4	30	99ZZZX1678       	1	19990223	G	3610		DUCT            			DOUG  	DC10  	DC1030      	3023501	WP  										NR 3 ENGINE	CRACKED         	B			D7XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	141AA					46713				NR 3 ENGINE PRE-COOLER DUCT HAS A CRACKED WELD AT 2 INCH DUCT SUPPORT BOSS.						2	L	7	3 	4F				A22WE   					 
1999043000043	19990430	00043	SW  	1999	4	30	99ZZZX1682       	1	19990317	G	6210	206015001107	BLADE           			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1068S	3474 			A2178	45436				GRIP FINGER DOUBLER CORRODED AND DEBONDED BEYOND LIMITS.						1	G	7	1 	3U				H2SW    					 
1999043000044	19990430	00044	SW  	1999	4	30	99ZZZX1683       	1	19990209	G	6220	206011120103	TRUNNION        		206011100159	BELL  	206   	206L4       	1182110	SW  										M/R HUB	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	174AL				A2533	52067				SPLINES BADLY CORRODED.  TRUNNION SCRAPPED AT 1/2 LIFE.						1	G	7	1 	3U			NC	H2SW    					 
1999043000045	19990430	00045	SW  	1999	4	30	99ZZZX1684       	1	19990302	G	6220	206011120103	TRUNNION        		206011100159	BELL  	206   	206L4       	1182110	SW  										M/R HUB	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	173AL	1167 			A3322	52066				MAIN ROTOR HUB REMOVED FOR 1,200-HOUR INSPECTION.  SPLINES BADLY CORRODED.  TRUNNION SCRAPPED AT 1/2 LIFE.						1	G	7	1 	3U			NC	H2SW    					 
1999043000049	19990430	00049	SW  	1999	4	30	99ZZZX1688       	1	19990218	G	6230	206040535105	MAST            		206040014103	BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	351AL	1483 			N2588	51431				MAST WAS SCRAPPED DUE TO EXCESSIVE CORROSION PITTING ON UPPER SPLINES.  THIRTY PERCENT OF RETIREMENT LIFE.						1	G	7	1 	3U				H2SW    					 
1999043000052	19990430	00052	SW  	1999	4	30	99ZZZX1691       	1	19990325	G	7120	2060641031	BEARING         		407060111101	BELL  	407   	407         		SW  										ENGINE MOUNT	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467AL	2471 				53190				ENGINE MOUNT BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999043000053	19990430	00053	SW  	1999	4	30	99ZZZX1692       	1	19990314	G	6220	407310102101	BEARING         		407010100111	BELL  	407   	407         		SW  										M/R HUB	DEBONDED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457AL	1992 			LK3592	53151				MAIN ROTOR HUB REMOVED FOR BEARING SEPARATION.  BEARING COMPLETELY DEBONDED AT 9TH CONE FROM FLANGE.						1	G	7	1 	3U			O	H2SW    					 
1999043000054	19990430	00054	SW  	1999	4	30	99ZZZX1693       	1	19990306	G	6220	407310102101	BEARING         		407010100111	BELL  	407   	407         		SW  										M/R HUB	DEBONDED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	487AL	774  			LK3515	53204				MAIN ROTOR HUB REMOVED FOR BEARING EXTRUDING.  BEARING COMPLETELY DEBONDED AT 2ND CONE FROM FLANGE.						1	G	7	1 	3U			O	H2SW    					 
1999043000105	19990430	00105	SW  	1999	4	30	99ZZZX1700       	1	19990405	G	7720	2060751901	INDICATOR       			BELL  	206   	206B        	1181511	SW  										COCKPIT TOT	MALFUCNTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	9907K				874	2040				GAUGE 20 DEGREES OFF OF CALIBRATION.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999043000106	19990430	00106		1999	4	30	99ZZZX1701       	4	19990330	G	2312	KX165	TRANSCEIVER     			HUGHES	369   	369E        	4470707	WP  										COCKPIT	MALFUNCTIONED   	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	8330P				45749	0330E				VHF RADIO INOPERATIVE.  FADES OUT DURING FLIGHT.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999043000107	19990430	00107	WP  	1999	4	30	99ZZZX1702       	1	19990405	G	6420	369A21712313	PITCH           			HUGHES	369   	369D        	4470706	WP  										TAIL ROTOR	WORN            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	5027P					611002D				ROD END BEARING WORN.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999043000108	19990430	00108	SW  	1999	4	30	99ZZZX1703       	1	19990405	G	7500	3032247	AIR FILTER      			BELL  	212   	212         	1181420	SW  										ENGINE	CLOGGED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530B	758  				30702				AIR FILTER CLOGGED.  LOW AIR FLOW.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999043000109	19990430	00109	SW  	1999	4	30	99ZZZX1704       	1	19990405	G	7722	3030083	COMPENSATOR     			BELL  	212   	212         	1181420	SW  										ENGINE	INOPERATIVE     	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530F				9B252	30920				COMPENSATOR INOPERATIVE.  WILL NOT ADJUST ITT TRIM.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999043000110	19990430	00110	WP  	1999	4	30	99ZZZX1705       	1	19990405	G	7330	369H81443	BYPASS SWITCH   			HUGHES	369   	369D        	4470706	WP  										FUEL PUMP	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	1097J					900801D				BYPASS SWITCH HAS A BROKEN WIRE - SWITCH HOUSING.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999043000111	19990430	00111		1999	4	30	99ZZZX1706       	4	19990405	G	3421	5040017908	GYRO            			HUGHES	369   	369D        	4470706	WP  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	500DC				9627B	290456D				GYRO WILL NOT CAGE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999043000112	19990430	00112	WP  	1999	4	30	99ZZZX1707       	1	19990405	G	6420	369D2172313	PITCH LINK      			HUGHES	369   	369D        	4470706	WP  										TAIL ROTOR	WORN            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	500DC					290456D				PITCH LINK BEARING WORN.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999043000113	19990430	00113		1999	4	30	99ZZZX1708       	4	19990331	G	3422	5050031903	DIRECTIONAL GYRO			HUGHES	369   	369D        	4470706	WP  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	500DC				915	290456D				DIRECTIONAL GYRO PRESETS 10 DEGREES OFF OF MAG COMPASS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999043000114	19990430	00114	WP  	1999	4	30	99ZZZX1709       	1	19990405	G	6420	369D2172313	PITCH LINK      			HUGHES	369   	369D        	4470706	WP  										TAIL ROTOR	WORN            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	369AW					470117D				PITCH LINK BEARING WORN.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999043000115	19990430	00115	WP  	1999	4	30	99ZZZX1710       	1	19990322	G	2810	369A8119	VENT            			HUGHES	369   	369D        	4470706	WP  										FUEL TANK	MISINSTALLED    	H				K				NONE                    				K	W		FLUID LOSS                	INADEQUATE Q C            		IN	INSP/MAINT     	1			AL	03	5074R					1151D				THE AIRCRAFT HAD FUEL DRIPPING FROM THE BELLY.  FOUND FORWARD FUEL VENT WAS MIS-SHIMMED AT INSTALLATION.  RE-SHIMMED AND	 REPLACED SEALS.					1	G	7	1 	3U				H3WE    					 
1999043000116	19990430	00116		1999	4	30	99ZZZX1711       	4	19990301	G	3416	A30	ENCODER         	ACK         		HUGHES	269   	269C1       	8059504	SW  										COCKPIT	MALFUNCTIONED   	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	61482				57046	0081				THE ENCODER WAS GIVING A FALSE ALTITUDE INDICATION.  UNIT WAS STILL UNDER WARRANTY SO UNIT WAS REMOVED AND SENT TO SCHWE	IZER HELICOPTER FOR NEW REPLACEMENT ENCODER.  NEW UNIT WAS INSTALLED AND OPERATIONALLY CHECKED OK.					1	G	7	1 	3O			O	4H12    					 
1999043000118	19990430	00118	SW  	1999	4	30	99ZZZX1713       	1	19990323	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	DAMAGED         	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	98VG	256  				53171				TAIL ROTOR DISC PACK SPREAD BEYOND LIMITS.  REPLACED WITH NEW DISC PACK FROM BELL HELICOPTER.						1	G	7	1 	3U			O	H2SW    					 
1999043000119	19990430	00119	SW  	1999	4	30	99ZZZX1714       	1	19990323	G	6322	406040320101	SHAFT           			BELL  	407   	407         		SW  										COOLER BLOWER	DAMAGED         	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	98VG	256  				53171				COOLER BLOWER SHAFT DAMAGED.  REPLACED WITH NEW SHAFT FROM BELL HELICOPTER.						1	G	7	1 	3U			O	H2SW    					 
1999043000120	19990430	00120	SW  	1999	4	30	99ZZZX1715       	1	19990406	G	6510	40604034010	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	FAILED          	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	97SP	28   			8198	53297				DISC PACK FAILED.  REPLACED WITH NEW DISC PACKS FROM BELL HELICOPTER.  C/W AD 97-24-17.						1	G	7	1 	3U			O	H2SW    					 
1999043000121	19990430	00121	SW  	1999	4	30	99ZZZX1716       	1	19990406	G	6510	40604034010	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	FAILED          	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	97SP	28   			8221	53297				DISC PACK FAILED.  REPLACED WITH NEW DISC PACKS FROM BELL HELICOPTER.  C/W AD 97-24-17.						1	G	7	1 	3U			O	H2SW    					 
1999043000122	19990430	00122	SW  	1999	4	30	99ZZZX1717       	1	19990406	G	6510	40604034010	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	FAILED          	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	97SP	28   			8217	53297				DISC PACK FAILED.  REPLACED WITH NEW DISC PACKS FROM BELL HELICOPTER.  C/W AD 97-24-17.						1	G	7	1 	3U			O	H2SW    					 
1999043000123	19990430	00123	SW  	1999	4	30	99ZZZX1718       	1	19990406	G	6520	406040453101	SEAL            			BELL  	407   	407         		SW  										T/R GEARBOX	LEAKING         	B			GS1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	03	97SP	28   				53297				INPUT SEAL LEAKING.  REPLACED WITH NEW SEALS FROM BELL HELICOPTER.						1	G	7	1 	3U			O	H2SW    					 
1999043000124	19990430	00124	EA  	1999	4	30	99ZZZX1719       	2	19990324	G	7414	10382807	CAPACITOR       			ENSTRM	F28   	F28F        	3300412	GL  	LYC   	O360  	HIO360F1AD  	41514	EA  					MAGNETO	FAILED          	D		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	756H	31   				756	L2143351A			POINTS CLOSED AND MAGNETO QUIT DUE TO MELTED CAM FOLLOWER.  LYCOMING FACTORY OVERHAULED ENGINE, TELEDYNE CONT FACTORY OV	ERHAULED MAG, AND SLICK OVERHAULED HARNESS.					1	G	7	1 	3O	3	O		H1CE    	1E10				 
1999043000125	19990430	00125	EA  	1999	4	30	99ZZZX1720       	2	19990324	G	7414	10400184	POINTS          			ENSTRM	F28   	F28F        	3300412	GL  	LYC   	O360  	HIO360F1AD  	41514	EA  					MAGNETO	FAILED          	D		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	756H	31   				756	L2143351A			POINTS CLOSED AND MAGNETO QUIT DUE TO MELTED CAM FOLLOWER.  LYCOMING FACTORY OVERHAULED ENGINE, TELEDYNE CONT FACTORY OV	ERHAULED MAG, AND SLICK OVERHAULED HARNESS.					1	G	7	1 	3O	3	O		H1CE    	1E10				 
1999043000126	19990430	00126	SW  	1999	4	30	99ZZZX1721       	1	19990405	G	6310	70010G000X116	LINE            			BELL  	206   	206B        	1181511	SW  										TRANSMISSION	LEAKING         	B			LS1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13	90322					1736				OIL SEEPING, NEEDS PRESSURE TEST.  REPLACED.						1	G	7	1 	3U				H2SW    					 
1999043000127	19990430	00127	SW  	1999	4	30	99ZZZX1722       	1	19990331	G	5520	205001914103	HORN ASSY       			BELL  	212   	212         	1181420	SW  										TAIL BOOM	MISMANUFACTURED 	B			LS1R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	13	8530F				A1003	30920				RECEIVED FROM BELL HELICOPTER NEW.  THICKNESS OF LUG WAS NOT MACHINED PROPERLY PROHIBITING CORRECT SHIMMING.  REPLACEMEN	T PART OBTAINED AND INSTALLED.  MALFUNCTION REPORT FORWARDED TO BELL.					1	G	7	1 	4U				H4SW    					 
1999043000128	19990430	00128	NE  	1999	4	30	99ZZZX1723       	1	19990401	G	3240	50075551	BRAKE ASSY      			SKRSKY	S76   	S76C        	8143008	NE  										LT MLG	DAMAGED         	B		A	JZBR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	25	165ML	250  			NOV970765	760471				RIVETS SHEARED OFF ON THE 6 O'CLOCK POSITION (6 EACH), AND DAMAGED THE WHEEL ASSY ON THE INNER SIDE.  THIS IS THE SECOND	 TIME THAT THIS PROBLEM OCCURRED IN THE SAME SIDE, LT MAIN WHEEL.					1	G	7	2 	3U			NC	H1NE    					 
1999043000129	19990430	00129	SW  	1999	4	30	99ZZZX1724       	1	19990322	G	2432	RG206	BATTERY         			BELL  	206   	206B3       	1181506	SW  										DC SYSTEM	DISCHARGED      	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY	1084 			R32678	2871				BATTERY DEAD.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999043000130	19990430	00130	EU  	1999	4	30	99ZZZX1725       	1	19990415	G	3340	4580	BULB            	GE          		SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	INOPERATIVE     	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	16	4059W	1    				2933				THE LANDING LIGHT BULBS ARE CONTINUALLY REQUIRING CHANGING.  THIS BULB ONLY LASTED FOR 1.1 FLIGHT HOURS WITH 10 NIGHT LA	NDINGS.   THE PREVIOUS BULB LASTED FOR 19 FLIGHT HOURS.  OPERATING 3 EACH AS350B HELICOPERS, APPEAR TO BE AVERAGING BETW	EEN 20 AND 30 FLIGHT HOURS PER BULB.  SUBMITTER STATED THE CONFINED AREA OF THIS INSTALLATION DOESN'T APPEAR TO HAVE ENO	UGH COOLING AIR FLOW.			1	G	7	1 	3U				H9EU    					 
1999043000131	19990430	00131	NE  	1999	4	30	99ZZZX1726       	1	19990415	G	3240	50075551	BRAKE ASSY      		AUG81819    	SKRSKY	S76   	S76C        	8143008	NE  										MLG	LEAKING         	B			J2BR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			GL	15	1875P					760488				BRAKE ASSY WAS LEAKING AT THE 6 O'CLOCK AND 4 O'CLOCK POSITIONS FROM THE BRAKE PADS.  NOTE:  LEAKING AT INSTALLATION FRO	M INVENTORY.					1	G	7	2 	3U			NC	H1NE    					 
1999043000132	19990430	00132	CE  	1999	4	30	99ZZZX1727       	1	19990409	G	2752	232507913	BRACKET         			LEAR  	35    	35A         	5170602	CE  										FLAP ACTUATOR	CRACKED         	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	11	10AH					657				BRACKET CRACKED AT OPPOSITE END OF WHERE ACTUATOR MOUNTS.  LEFT FLAP ACTUATOR BRACKET FOUND CRACKED AT INSPECTION.  THE 	ENTIRE BRACKET IS COMPOSED OF 5 PIECES.  THE TOP BRACKET IS CRACKED.					2	L	7	2 	4F				A10CE   					 
1999043000133	19990430	00133	CE  	1999	4	30	99ZZZX1728       	1	19990331	G	7931	1013890235	TRANSDUCER      			BEECH 	200   	B200        	1152922	CE  										NR 1 ENGINE	FAILED          	B			DBCR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	13	670DF	188  			6013642	BB1631				NR 1 ENGINE OIL PRESSURE FLUCTUATES HIGH.  TROUBLESHOT TO OIL PRESSURE TRANSMITTER.  REPLACED TRANSMITTER, PN 101-389023	-5, SN 6013-6-42 OFF, SN 5624-5-29 ON.  OPERATIONS CHECKED OK.					1	L	7	2 	4T				A24CE   					 
1999043000138	19990430	00138	EA  	1999	4	30	99ZZZX1731       	2	19990331	G	7250	3032651	STATOR          								PWA   	PT6   	PT6A27      	52043	EA  					COMPRESSOR	CRACKED         	B	P		W5RR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	19		4921 	111  		3042046					THE PART HAD BEEN SENT IN FOR AN OVERHAUL EVALUATION, BUT VISUAL INSPECTION OF THE TRAILING EDGES SHOWED SEVERE BOWING. 	 THE TRAILING EDGE THICKNESSES WERE VERY GOOD SO THAT MATERIAL THICKNESS WAS NOT THE CAUSE.  THE OPERATOR REPORTED 111.1	 HOURS SINCE OVERHAUL.  VISUAL INSPECTION OF THE PART SHOWED A COLORATION INDICATIVE OF SOME TYPE OF PENNY INSERT APPROX	IMATELY .5 INCH DEEP FROM THE TRAILING EDGE.  GIVEN THE THICKNESS OF THE VANES AND THE LOW TIME SINCE OVERHAUL, THE EXTE	NT OF DISTORTION AND CREEP WOULD STRONGLY SUGGEST INSUFFICIENT STRENGTH IN THE INSERT MATERIAL ITSELF.							4	T			E4EA				 
1999043000139	19990430	00139	CE  	1999	4	30	99ZZZX1732       	1	19990330	G	2510	05142158	FITTING         		051421223   	CESSNA	172   	172S        	2072439	CE  										COCKPIT SEAT	BENT            	A		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	494SP	26   				172S8035				NEW CESSNA, PILOT'S SEAT BACK IN FULL UPRIGHT POSITION WAS RECLINED APPROXIMATELY 4 INCHES.  FOUND L-SEATBACK ATTACH FIT	TING P/N 0514215-8 WAS BENT ONE INCH AFT.  SUBMITTER STATED THIS PART WAS REPLACED FOR THE SAME PROBLEM 25.7 HOURS AGO.					1	H	7	1 	3O			NT	3A12    					 
1999043000140	19990430	00140	CE  	1999	4	30	99ZZZX1733       	1	19990412	G	2820	641481	FUEL LINE       		643723A7    	CESSNA	421   	421C        	2076016	CE  	CONT  	O520  	GTSIO520N   	17032	SO  					LT ENGINE	BROKEN          	D				E				ENGINE SHUTDOWN         				E	K	J	VIBRATION/BUFFET          	FLUID LOSS                	WARNING INDICATION        	NR	NOT REPORTED   	1			GL	17	264DC		1309 			421C1248	610455			PILOT LANDED AND STATED THAT DURING FLIGHT, THE LEFT ENGINE STARTED TO VIBRATE AND EGT INDICATION ON NR 4 CYLINDER WENT 	TO ZERO.  PILOT ELECTED TO SHUT DOWN THE LEFT ENGINE, FEATHER THE PROPELLER AND CONTINUE ON TO HOME BASE.  INSPECTION OF	 THE LT ENGINE NR 4 CYLINDER FOUND THE FUEL LINE TO THE NR 4 INJECTOR HAD BROKEN AT THE BALL END OF THE SPECIAL SILVER S	OLDERED FLARE FITTING.  TOTAL TIME ON THE FUEL LINE IS UNKNOWN AND THE ENGINE TSO IS 1,309.4 HOURS.  VISUAL INSPECTION O	F BOTH ENDS OF THE REMAINING FUEL TUBES WITH 10X MAGNIFICATION DETECTED NO ADDITIONAL DEFECTS.		1	L	7	2 	3O	3	O		A7CE    	E7CE				 
1999043000141	19990430	00141		1999	4	30	99ZZZX1734       	4	19990323	G	3416		ENCODER         	MORROW      	4282003     	PIPER 	PA28  	PA28R200    	7102811	SO  										COCKPIT	INACCURATE      	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	09	2876R	1000 			M553	28R35316				ENCODER REPORTED INVALID ATTITUDE BY ATCT SEVERAL TIMES.  REPLACED ENCODER.						1	L	7	1 	3O				2A13    					 
1999043000146	19990430	00146	SO  	1999	4	30	99ZZZX1739       	1	19990329	G	7820	9948200	MUFFLER         			PIPER 	PA28  	PA28140     	7102802	SO  										EXHAUST	DAMAGED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	28	5589F	2800 				2824922				DURING ANNUAL INSPECTION, MUFFLER REMOVED TO CHECK FOR MUFFLER-TO-HEATER SHROUD INTEGRITY.  NUMEROUS HOLES IN OUTER SKIN	 NOTED.  REPLACED PIPER MUFFLER WITH KNISLEY MUFFLER, K99482-00.					1	L	7	1 	3O				2A13    					 
1999043000147	19990430	00147	NE  	1999	4	30	99ZZZX1740       	3	19990408	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			3505 					HJ847		EROSION SHIELD DEBOND.  DEBOND ON BLADE NR 2 UNDER DEICE BOOT.  REPAIRED AND INSTALLED NEW DEICE BOOT IAW MFG CMM.																5	C	P10N	 
1999043000148	19990430	00148	NE  	1999	4	30	99ZZZX1741       	3	19990408	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			3745 					HJ834		NR 1 BLADE EROSION SHIELD DEBONDED UNDER BOOT BLADE.  PRELOADS AND LOOSE.  DISASSEMBLED AND CLEANED PROPELLER, REQUIRED 	DEBONDED EROSION SHIELD ON NR 1 BLADE AND INSTALLED NEW DEICE BOOT.  SET PRELOADS ON ALL BLADES, RE-ASSEMBLED PROP, SET 	BLADE ANGLES AT 42 INCH RADIUS RA 14.5, LP 18.5, FA 79, STATIC BALANCED AND LUBRICATED WITH AEROSHELL NR 6 IAW HARTZELL 	CMM.													5	C	P10N	 
1999043000149	19990430	00149		1999	4	30	99ZZZX1742       	2	19990401	G	7414		WASHER          																	MAGNETO	MISSING         	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15										POINTS, PN ES10-382585, WILL NOT MAKE OR BREAK CONTACT DUE TO MISSING INSULATING WASHER ON MAIN MOUNTING SCREW.																			 
1999043000150	19990430	00150	NE  	1999	4	30	99ZZZX1743       	3	19990408	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			3376 					HJ450		DE-ICE BOOT LIFTING, EROSION SHIELD DEBOND UNDER BOOT, NR 1 BLADE.  REPAIRED EROSION SHIELD DEBOND AND INSTALLED DEICE B	OOT ON NR 1 BLADE IAW HARTZELL CMM.															5	C	P10N	 
1999043000151	19990430	00151	EA  	1999	4	30	99ZZZX1744       	2	19990302	G	7414	M3635	INPULSE COUPLING	SLICK       	6355        	PIPER 	PA32  	PA32260     	7103206	SO  	LYC   	O540  	O540E4B5    	41532	EA  					MAGNETO	MISMANUFACTURED 	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NE	01	4830S	1500 				321261				PER AD 99-4-4, FOUND THE IMPULSE COUPLING TO BE MISSING ONE OF THE FLY-WEIGHT SPRINGS AND EXCESSIVE PLAY AT THE RIVETS.						1	L	7	1 	3O	3	O		A3SO    	E295				 
1999043000152	19990430	00152	CE  	1999	4	30	99ZZZX1745       	1	19990331	G	3340	CM35895	CIRCUIT BREAKER 			CESSNA	402   	402C        	207590R	CE  										COCKPIT	FAILED          	D				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			TX	TAXI/GRND HDL  	1			NE	01	1376G					402C0271				AFTER LANDING IN ACK, CREW SHUT OFF ALL EXTERNAL LIGHTS EXCEPT BELLY STROBE AND NAV LIGHTS.  NOTICED SMOKE COMING FROM N	AV LIGHT SWITCH/BREAKER.  SHUT OFF SWITCH, TAXIED TO GATE, AND NOTIFIED MAINTENANCE.  FOUND RT WING NAV LIGHT POWER WIRE	 SHORTED TO GROUND, CIRCUIT BREAKER SWITCH INOPERATIVE, DID NOT TRIP.  REMOVED AND REPLACED CIRCUIT BREAKER SWITCH.  CHE	CKED OK AFTER REPAIRING WIRING.			1	L	7	2 	3O				A7CE    					 
1999043000153	19990430	00153	NM  	1999	4	30	99ZZZX1746       	1	19990412	G	5320	66157751	HINGE           			BOEING	727   	727251      	138408H	NM  										LAVATORY	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON UPPER/LOWER HINGES ON AFT LAVATORY SERVICE DOOR.						2	L	7	3 	4F				A3WE    					 
1999043000154	19990430	00154	NM  	1999	4	30	99ZZZX1747       	1	19990412	G	5320	66157752	HINGE           			BOEING	727   	727251      	138408H	NM  										LAVATORY	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON UPPER/LOWER HINGES ON AFT LAVATORY SERVICE DOOR.						2	L	7	3 	4F				A3WE    					 
1999043000155	19990430	00155	NM  	1999	4	30	99ZZZX1748       	1	19990412	G	5320	66157753	HINGE           			BOEING	727   	727251      	138408H	NM  										LAVATORY	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON UPPER/LOWER HINGES ON AFT LAVATORY SERVICE DOOR.						2	L	7	3 	4F				A3WE    					 
1999043000156	19990430	00156	NM  	1999	4	30	99ZZZX1749       	1	19990412	G	5320	66157754	HINGE           			BOEING	727   	727251      	138408H	NM  										LAVATORY	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON UPPER/LOWER HINGES ON AFT LAVATORY SERVICE DOOR.						2	L	7	3 	4F				A3WE    					 
1999043000157	19990430	00157	NM  	1999	4	30	99ZZZX1750       	1	19990412	G	4910		ANGLE           			BOEING	727   	727251      	138408H	NM  										APU	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON APU AIR INLET SCREEN MOUNT FLANGE (ANGLES).						2	L	7	3 	4F				A3WE    					 
1999043000158	19990430	00158	NM  	1999	4	30	99ZZZX1751       	1	19990323	G	5315		FLOORBEAM       			BOEING	727   	727224      	1384076	NM  										BS 720	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79750					22452				DURING A C-CHECK, CORROSION WAS NOTED AT STA 720L, STR 27.						2	L	7	3 	4F				A3WE    					 
1999043000159	19990430	00159	NM  	1999	4	30	99ZZZX1752       	1	19990323	G	5320		STRAP           			BOEING	727   	727224      	1384076	NM  										BS 540	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79750					22452				DURING A C-CHECK, CORROSION WAS NOTED ON STRAP IN C-1 PIT FLOOR AREA JUST FORWARD OF STA 540 THAT CROSSES FLOORBEAM.						2	L	7	3 	4F				A3WE    					 
1999043000160	19990430	00160	NM  	1999	4	30	99ZZZX1753       	1	19990323	G	5510		BEAM            			BOEING	727   	727224      	1384076	NM  										HORIZ STABILIZER	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79750					22452				DURING A C-CHECK, CORROSION WAS NOTED ON RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM.						2	L	7	3 	4F				A3WE    					 
1999043000161	19990430	00161	NM  	1999	4	30	99ZZZX1754       	1	19990323	G	5754	6521749SA	SKIN            			BOEING	727   	727224      	1384076	NM  										LE FLAP	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79750				734323A	22452				DURING A C-CHECK, CORROSION WAS NOTED ON NR 1 NOSE FLAP OF NR 1 KREUGER FLAP AT BUSHING FLANGE ATTACH POINT.						2	L	7	3 	4F				A3WE    					 
1999043000162	19990430	00162	NM  	1999	4	30	99ZZZX1755       	1	19990323	G	5210	655615033	HINGE           			BOEING	727   	727224      	1384076	NM  										PASSENGER DOOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79750					22452				DURING A C-CHECK, CORROSION WAS NOTED ON R-1 DOOR'S LOWER HINGE.						2	L	7	3 	4F				A3WE    					 
1999043000163	19990430	00163	NM  	1999	4	30	99ZZZX1756       	1	19990323	G	5320	6519606198	CHANNEL         			BOEING	727   	727224      	1384076	NM  										BS 1137-1176	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79750					22452				DURING A C-CHECK, CORROSION WAS NOTED ON A SECTION OF HAT CHANNEL LEFT AFT LAVATORY STA 1137 - STA 1176.						2	L	7	3 	4F				A3WE    					 
1999043000164	19990430	00164	NM  	1999	4	30	99ZZZX1757       	1	19990323	G	5313	65583872	STRINGER        			BOEING	727   	727224      	1384076	NM  										BS 950-990	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79750					22452				DURING A C-CHECK, CORROSION WAS NOTED ON STR 28R, STA 950F - STA 990.						2	L	7	3 	4F				A3WE    					 
1999043000165	19990430	00165	NM  	1999	4	30	99ZZZX1758       	1	19990323	G	5347		SEAT TRACK      			BOEING	727   	727224      	1384076	NM  										BS 1060-1110	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79750					22452				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 1060 - STA 1110, LBL 45.						2	L	7	3 	4F				A3WE    					 
1999043000166	19990430	00166	NM  	1999	4	30	99ZZZX1759       	1	19990310	G	5730	6516216227	SKIN            			BOEING	727   	727281      	138408N	NM  										LT WING	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON UPPER SURFACE LT WING (ABOVE NR 7 SPOILER ACTUATOR).						2	L	7	3 	4F				A3WE    					 
1999043000167	19990430	00167	NM  	1999	4	30	99ZZZX1760       	1	19990310	G	5313		STRINGER        			BOEING	727   	727281      	138408N	NM  										BS 1070-1130	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON STR 27L BETWEEN STA 1070 - STA 1130.						2	L	7	3 	4F				A3WE    					 
1999043000168	19990430	00168	NM  	1999	4	30	99ZZZX1761       	1	19990310	G	3010	BAC1522126	DEICER          			BOEING	727   	727281      	138408N	NM  										HORIZ STABILIZER	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON LT HORIZONTAL STABILIZER UPPER AFT TRAILING EDGE BEAM AREA BETWEEN NR 4 AND NR 	5 HINGE ON ICE BREAKER.					2	L	7	3 	4F				A3WE    					 
1999043000169	19990430	00169	NM  	1999	4	30	99ZZZX1762       	1	19990310	G	5730		SKIN            			BOEING	727   	727281      	138408N	NM  										LT WING	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON LEFT WING UPPER SURFACE (FORWARD OF NR 7 SPOILER).						2	L	7	3 	4F				A3WE    					 
1999043000170	19990430	00170	NM  	1999	4	30	99ZZZX1763       	1	19990310	G	5522	65C8067872	SKIN            			BOEING	727   	727281      	138408N	NM  										ELEVATOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON RIGHT ELEVATOR PANEL LOWER SURFACE (INBOARD END STA 17.5 - STA 66).						2	L	7	3 	4F				A3WE    					 
1999043000171	19990430	00171	NM  	1999	4	30	99ZZZX1764       	1	19990310	G	5313		STRINGER        			BOEING	727   	727281      	138408N	NM  										BS 1070-1130	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED AT STA 1070 - STA 1130 AT STR 29L.  (BOTH STRINGER AND SPLICE WERE CORRODED).						2	L	7	3 	4F				A3WE    					 
1999043000172	19990430	00172	NM  	1999	4	30	99ZZZX1765       	1	19990310	G	5313		STRINGER        			BOEING	727   	727281      	138408N	NM  										BS 1090	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON STR 29R AT STA 1090.						2	L	7	3 	4F				A3WE    					 
1999043000173	19990430	00173	NM  	1999	4	30	99ZZZX1766       	1	19990310	G	5522	6525634100	SKIN            			BOEING	727   	727281      	138408N	NM  										ELEVATOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON RIGHT ELEVATOR SKIN SURFACE STA 17.2 - STA 118.						2	L	7	3 	4F				A3WE    					 
1999043000174	19990430	00174	NM  	1999	4	30	99ZZZX1767       	1	19990310	G	5730	6516216227	SKIN            			BOEING	727   	727281      	138408N	NM  										LT WING	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON LEFT WING SURFACE (FORWARD OF NR 6 SPOILER OF PANEL.						2	L	7	3 	4F				A3WE    					 
1999043000175	19990430	00175	NM  	1999	4	30	99ZZZX1768       	1	19990323	G	5754	65217506A	BULLNOSE        			BOEING	727   	727281      	138408N	NM  										LE FLAP	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON RIGHT NR 5 LEADING EDGE FLAP NOSE FAIRING AND OUTER DRIVE FITTING.						2	L	7	3 	4F				A3WE    					 
1999043000176	19990430	00176	NM  	1999	4	30	99ZZZX1769       	1	19990323	G	5754	69179232	FITTING         			BOEING	727   	727281      	138408N	NM  										LE FLAP	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON RIGHT NR 5 LEADING EDGE FLAP NOSE FAIRING AND OUTER DRIVE FITTING.						2	L	7	3 	4F				A3WE    					 
1999043000177	19990430	00177	NM  	1999	4	30	99ZZZX1770       	1	19990310	G	5230	65562348	SKIN            			BOEING	727   	727281      	138408N	NM  										CARGO	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON C-1 DOOR SKIN.						2	L	7	3 	4F				A3WE    					 
1999043000178	19990430	00178	NM  	1999	4	30	99ZZZX1771       	1	19990323	G	5330		SKIN            			BOEING	727   	727281      	138408N	NM  										BS 460	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON SKIN AT FS 460 AT STR 19R.						2	L	7	3 	4F				A3WE    					 
1999043000179	19990430	00179	NM  	1999	4	30	99ZZZX1772       	1	19990323	G	5510	65245711	BEAM            			BOEING	727   	727281      	138408N	NM  										HORIZ STABILIZER	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON LEFT HORIZONTAL STABLIZER UPPER TRAILING EDGE BEAM.						2	L	7	3 	4F				A3WE    					 
1999043000180	19990430	00180	NM  	1999	4	30	99ZZZX1773       	1	19990323	G	5230	65657491	VENT DOOR       			BOEING	727   	727281      	138408N	NM  										CARGO DOOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON FORWARD AND AFT VENT DOORS IN C-2 DOOR.						2	L	7	3 	4F				A3WE    					 
1999043000181	19990430	00181	NM  	1999	4	30	99ZZZX1774       	1	19990323	G	5522	65C8067873	SKIN            			BOEING	727   	727281      	138408N	NM  										ELEVATOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	906PG					20728				DURING A C-CHECK, CORROSION WAS NOTED ON TRAILING EDGE OF INBOARD LOWER SKIN LEFT ELEVATOR.						2	L	7	3 	4F				A3WE    					 
1999043000182	19990430	00182	NM  	1999	4	30	99ZZZX1775       	1	19990412	G	5347		SEAT TRACK      			BOEING	727   	727227      	1384078	NM  										BS 1030-1090	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK AT STA 1030 - STA 1090 (R-2 DOOR).						2	L	7	3 	4F				A3WE    					 
1999043000183	19990430	00183	NM  	1999	4	30	99ZZZX1776       	1	19990412	G	5347		SEAT TRACK      			BOEING	727   	727227      	1384078	NM  										BS 950-1010	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK AT STA 950 - STA 1010, RBL 45.5.						2	L	7	3 	4F				A3WE    					 
1999043000184	19990430	00184	NM  	1999	4	30	99ZZZX1777       	1	19990412	G	5347		SEAT TRACK      			BOEING	727   	727227      	1384078	NM  										BS 950-1010	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK AT STA 950 - STA 1010 AT RBL 45.5.						2	L	7	3 	4F				A3WE    					 
1999043000185	19990430	00185	NM  	1999	4	30	99ZZZX1778       	1	19990412	G	5347		SEAT TRACK      			BOEING	727   	727227      	1384078	NM  										BS 950-990	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK AT STA 950 - STA 990 RBL 24.75.						2	L	7	3 	4F				A3WE    					 
1999043000186	19990430	00186	NM  	1999	4	30	99ZZZX1779       	1	19990412	G	5313		STRINGER        			BOEING	727   	727227      	1384078	NM  										BS 480	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON STR 28R AT STA 480.						2	L	7	3 	4F				A3WE    					 
1999043000187	19990430	00187	NM  	1999	4	30	99ZZZX1780       	1	19990412	G	5330		SKIN            			BOEING	727   	727227      	1384078	NM  										BS 680	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON SKIN UNDER LEVELING COMPOUND AT STA 680 STR 27L.						2	L	7	3 	4F				A3WE    					 
1999043000188	19990430	00188	NM  	1999	4	30	99ZZZX1781       	1	19990412	G	5313		STRINGER        			BOEING	727   	727227      	1384078	NM  										BS 720	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED AT STA 720C, STR 28L - STR 28R.						2	L	7	3 	4F				A3WE    					 
1999043000189	19990430	00189	NM  	1999	4	30	99ZZZX1782       	1	19990412	G	5342		SEAT TRACK      			BOEING	727   	727227      	1384078	NM  										BS 1050-1070	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 1050 - STA 1070 BL 45.5 R.						2	L	7	3 	4F				A3WE    					 
1999043000190	19990430	00190	NM  	1999	4	30	99ZZZX1783       	1	19990412	G	5755		ANGLE           			BOEING	727   	727227      	1384078	NM  										SPOILER	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON AFT INBOARD ATTACH ANGLE JUST AFT OF NR 5 SPOILER FITTING.						2	L	7	3 	4F				A3WE    					 
1999043000191	19990430	00191	NM  	1999	4	30	99ZZZX1784       	1	19990412	G	5320		ANGLE           			BOEING	727   	727227      	1384078	NM  										AIRSTAIR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON SEVERAL SUPPORT ANGLE ON AFT AIRSTAIR STEPS.						2	L	7	3 	4F				A3WE    					 
1999043000192	19990430	00192	NM  	1999	4	30	99ZZZX1785       	1	19990412	G	5720	65C8067810	RETAINER        			BOEING	727   	727227      	1384078	NM  										RT WING	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON RIGHT WING TRAILING EDGE PANEL SEAL RETAINER (APPROXIMATELY WS 220).						2	L	7	3 	4F				A3WE    					 
1999043000193	19990430	00193	NM  	1999	4	30	99ZZZX1786       	1	19990412	G	5347		SEAT TRACK      			BOEING	727   	727227      	1384078	NM  										BS 848	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 848.95 - STA 870 LBL 24.75.						2	L	7	3 	4F				A3WE    					 
1999043000194	19990430	00194	NM  	1999	4	30	99ZZZX1787       	1	19990412	G	5347		SEAT TRACK      			BOEING	727   	727227      	1384078	NM  										BS 740-760	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK AT STA 740 - STA 760 LBL 45.5.						2	L	7	3 	4F				A3WE    					 
1999043000195	19990430	00195	NM  	1999	4	30	99ZZZX1788       	1	19990412	G	5315		FLOORBEAM       			BOEING	727   	727227      	1384078	NM  										BS 380	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM STA 380 AT R-1 DOOR.						2	L	7	3 	4F				A3WE    					 
1999043000196	19990430	00196	NM  	1999	4	30	99ZZZX1789       	1	19990412	G	5315		FLOORBEAM       			BOEING	727   	727227      	1384078	NM  										BS 400	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM STA 400.						2	L	7	3 	4F				A3WE    					 
1999043000197	19990430	00197	NM  	1999	4	30	99ZZZX1790       	1	19990412	G	5313		STRINGER        			BOEING	727   	727227      	1384078	NM  										BS 1060	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON STR 28R AT STA 1060.						2	L	7	3 	4F				A3WE    					 
1999043000198	19990430	00198	NM  	1999	4	30	99ZZZX1791       	1	19990412	G	5330		SKIN            			BOEING	727   	727227      	1384078	NM  										BS 950	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON BELLY SKIN STR 28R TO STA 950F.						2	L	7	3 	4F				A3WE    					 
1999043000199	19990430	00199	NM  	1999	4	30	99ZZZX1792       	1	19990412	G	5313		STRINGER        			BOEING	727   	727227      	1384078	NM  										BS 1130-1150	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON STR 28L BETWEEN STA 1130 - STA 1150.						2	L	7	3 	4F				A3WE    					 
1999043000200	19990430	00200	NM  	1999	4	30	99ZZZX1793       	1	19990412	G	5320		SHEAR TIE       			BOEING	727   	727227      	1384078	NM  										BS 1166	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON SHEAR TIE AT STA 1166 BETWEEN STR 27 - STR 29R.						2	L	7	3 	4F				A3WE    					 
1999043000201	19990430	00201	NM  	1999	4	30	99ZZZX1794       	1	19990412	G	5313		STRINGER        			BOEING	727   	727227      	1384078	NM  										BS 1166-1183	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON STR 29L BETWEEN STA 1166 - STA 1183.						2	L	7	3 	4F				A3WE    					 
1999043000202	19990430	00202	NM  	1999	4	30	99ZZZX1795       	1	19990412	G	5320	651759318	ANGLE           			BOEING	727   	727227      	1384078	NM  										BS 259	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED IN COCKPIT ON FLOORBEAM ATTACH ANGLE STA 259.5.						2	L	7	3 	4F				A3WE    					 
1999043000203	19990430	00203	NM  	1999	4	30	99ZZZX1796       	1	19990412	G	5313		STRINGER        			BOEING	727   	727227      	1384078	NM  										BS 620	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON STR 27R AT STA 620.						2	L	7	3 	4F				A3WE    					 
1999043000648	19990430	00648	EA  	1999	4	30	99ZZZX1811       	2	19990407	G	8530	LW11633	CYLINDER        			PIPER 	PA38  	PA38112     	7103812	SO  	LYC   	O235  	O235L2C     	41505	EA  					ENGINE	CRACKED         	D				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			CE	01	2426N		1434 			3879A0837				OIL LEAK AT NR 1 CYLINDER APPEARED TO BE COMING FROM PUSHROD TUBE SEALS.  FURTHER INVESTIGATION AND PRESSURE CHECK DISCL	OSED LEAK UNDER INTAKE PUSHROD AT HEAD/BARREL JOINT.  A 2 INCH CRACK, 1.50 INCHES DOWN FROM TOP OF CYLINDER WALL WAS VIS	IBLE INSIDE THE CYLINDER.  CYLINDER HAD BEEN CHROMED.  CYLINDER SHOP STATED THIS IS COMMON PROBLEM ON CHROME CYLINDERS.				1	L	7	1 	3O	3	O		A18SO   	E223				 
1999043000649	19990430	00649		1999	4	30	99ZZZX1812       	4	19990218	G	3416		TRANSPONDER     	NARCO       	AT50A       	CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					ENCODER	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	09	734ST				43513	17269083	RL1831239A			FOUND TRANSPONDER TRANSMITTING A CONSTANT A2 CODE IN MODE C.  REPLACED DEFECTIVE INTEGRATED CIRCUIT U106 (PN 740190001).	  NO RECOMMENDATIONS TO PREVENT RECURRENCE.					1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999043000650	19990430	00650	CE  	1999	4	30	99ZZZX1813       	1	19990301	G	2400	S327111	SWITCH          			CESSNA	172   	172R        	2072401	CE  										COCKPIT	MALFUNCTIONED   	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03	718EH					17280061				SWITCH IS A DOUBLE POLE, SINGLE THROW, ROCKER SWITCH.  WHEN SWITCH IS SELECTED TO 'OFF', SOME RADIOS MAY STAY ON, ONE-HA	LF OF SWITCH STAYS CLOSED.  THERE ARE 4 NR 10 GAUGE WIRES GOING TO SWITCH, THESE WIRES PUT TENSION ON SWITCH CONTACTS. W	HEN SWITCH IS REMOVED IT WILL TEST NORMAL.  NO 'DC' CURRENT RATINGS ARE MARKED ON SWITCH.  SWITCH IS LABELED MEXICO.  RE	COMMENDATIONS:  REPLACE WITH A 'UL', 'DC' RATED SWITCH OF HIGHER QUALITY.			1	H	7	1 	3O			NT	3A12    					 
1999043000651	19990430	00651	CE  	1999	4	30	99ZZZX1814       	1	19990317	G	2400	S327111	SWITCH          			CESSNA	172   	172R        	2072401	CE  										COCKPIT	FAILED          	B			PRIR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	03	718EH					17280061				THIS SWITCH NEW FROM CESSNA HAS ALMOST INSTANT FAIL RATE.  OVER 5 SWITCHES HAVE BEEN INSTALLED IN THIS S/N AIRCRAFT AND 	FAILED.  SUBMITTER STATED A NEW SWITCH NEEDS TO BE USED INSTEAD OF THIS ONE.  MANUFACTURER DOES NOT PROVIDE.					1	H	7	1 	3O			NT	3A12    					 
1999043000652	19990430	00652	CE  	1999	4	30	99ZZZX1815       	1	19990407	G	5720	58411401	BRACKET         			CESSNA	441   	441         	2076020	CE  										RT WING	CRACKED         	B			WTXR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	88834	5757 				4410269				DURING A PHASE INSPECTION, FOUND THAT THE RIGHT MAIN GEAR OUTBOARD UPLOCK HOOK STEEL BRACKET WAS UPWARD TO THE END OF BR	ACKET.  INSTALLED NEW BRACKET.					1	L	7	2 	3T			RT	A28CE   					 
1999043000653	19990430	00653	CE  	1999	4	30	99ZZZX1816       	1	19990301	G	8120	4664129003R	BLADE           			CESSNA	414   	414A        	2075907	CE  										TURBOCHARGER	DAMAGED         	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	09	414P					414A0507				RAM SERIES VII CONVERSION WITH LARGER TURBO.  STC SE09104SC.  AIR INTAKE AIR INDUCER INSTALLED BY RAM CAME LOOSE IN-FLIG	HT AND DAMAGED THE BLADES IN THE TURBO INLET IMPELLER.  439 HOURS ON TURBO.					1	L	7	2 	3O				A7CE    					 
1999043000654	19990430	00654	SO  	1999	4	30	99ZZZX1817       	1	19990301	G	5320		WEB             			PIPER 	PA28  	PA28180     	7102808	SO  										COPILOT	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	09	7389W					281274				PRIOR TO INSTALLING NEW CARPETS, REMOVED PIPER CARPET PADS UNDER PILOT'S SEATS.   FOUND CORROSION WHERE CARDBOARD PADS W	ERE INCOMPLETELY GLUED (ONLY IN NON-GLUE AREAS). PANEL BETWEEN SEAT RAILS CORRODED HALF WAY THROUGH IN SOME PLACES.					1	L	7	1 	3O				2A13    					 
1999043000655	19990430	00655	SO  	1999	4	30	99ZZZX1818       	1	19990330	G	8120	4078009003	TURBOCHARGER    	GARRTT      		PIPER 	PA31  	PA31P       	7103120	SO  										EXHAUST	LEAKING         	B			EKIR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	07	6805L		235  		2D01196	31P7				TURBO OVERHAULED BY GARRETT 2-11-98.  LEAKING OIL INTO COMPRESSOR SIDE OF UNIT.						1	L	7	2 	3O				A8EA    					 
1999043000657	19990430	00657	NM  	1999	4	30	99ZZZX1820       	1	19990125	G	2820	3360	ACTUATOR        	GENDESIGN   	40575       	BOEING	727   	72725       	1384006	NM  										FUEL SYSTEM	MISOVERHAULED   	B			HN6R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	01	508FE		2400 		5537	18279				THE GREASE APPLIED TO THE ACTUATOR IS NOT WHAT IS SPECIFIED IN THE MANUFACTURER'S OHM (GENERAL DESIGN, 28-20-03).  THE L	UBRICANT USED IN THIS UNIT'S GEAR TRAIN HAS EMULSIFIED AND MIGRATED INTO THE MOTOR ASSEMBLY.  THE MOTOR ASSEMBLY IS CONT	AMINATED WITH GREASE WHICH APPEARS TO CAUSE POOR CONDUCTIVITY BETWEEN BRUSHES AND MOTOR ARMATURE COMMUTATOR.  RECOMMEND:	  USE CORRECT GREASE IAW OHM INSTRUCTIONS.			2	L	7	3 	4F				A3WE    					 
1999043000659	19990430	00659	EA  	1999	4	30	99ZZZX1822       	1	19990415	G	3213	200811218	AXLE            	ROTOL       	6048500221  	CNDAIR	CL600 	CL6002B16   	1900305	EA  										NLG	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	05	43R	663  			DCL3396	5334				WHILE DOING DOWTY-MESSIER SB 20020-32-4, NLG AXLE WAS FOUND PITTED DUE TO CORROSION WHERE OLEO INSERTS INTO AXLE ASSY. L	OW TSN.  MESSIER DOWTY LANDING GEAR HAVE HAD EXTENSIVE CORROSION PROBLEMS ON 'ALL' CHALLENGERS 600, 601, AND 604'S.					2	L	7	2 	4F			RT	A21EA   					 
1999043000661	19990430	00661	SO  	1999	4	30	99ZZZX1824       	1	19990422	G	3222	45318	STRUT           			PIPER 	PA31T 	PA31T       	7103124	SO  										NLG	RUPTURED        	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	01	716WA					31T8020042				THE OLEO CYLINDER RUPTURED NEAR THE BOTTOM WHERE THE PISTON SEATS WITH THE GEAR FULLY EXTENDED.  IT APPEARS AS THOUGH TH	E PIN HOLDING THE PISTON ON THE GEAR STRUT WAS FORCED THROUGH THE CYLINDER WALL.  THE SUBMITTER DID NOT SPECIFY HOW THE 	DAMAGE WAS DISCOVERED, BUT DID INDICATE THE NOSE GEAR HAD BEEN STICKING PRIOR TO DISASSEMBLY.				1	L	7	2 	3T				A8EA    					 
1999043000662	19990430	00662		1999	4	30	99ZZZX1825       	4	19990224	G	3432	M390166209L	RELAY           			BEECH 	200   	B200        	1152922	CE  										E/E BAY	CONTAMINATED    	G				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	03	200QS	5576 				BB1130				COPILOT'S GLIDESLOPE REMAINS CENTERED AT ALL ITEMS ON ILS APPROACH.  NO FLAG ON HSI.  TROUBLESHOOTING REVEALED THAT PINS	 ON RELAY M39016/6-209L OR CONTACTS ON PRINTED CIRCUIT BOARD WERE DIRTY OR OXIDATED.  RELAY K1 IN RELAY BOX PL-A.  SAME 	RELAY FOR GLIDESLOPE UP/DOWN.  ALSO, PULLS FLAG.  SUBMITTER RECOMMENDED VISUAL INSPECTION OF PCB AND RELAYS ON ANNUAL BA	SIS.			1	L	7	2 	4T				A24CE   					 
1999043000663	19990430	00663	CE  	1999	4	30	99ZZZX1826       	1	19990301	G	5533		DELTA FIN       			LEAR  	35    	31A         	5170531	CE  										FUSELAGE	CRACKED         	B			TJ4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	11	119FX	1314 				136				TOP SKIN OF RIGHT DELTA FIN CRACKED UNDER THE OUTBOARD STATIC WICK.  CRACK EXTENDED ALONG SIDE OF STATIC WICK BASE.  WAS	 NOTICED BY BLACK STREAKING ALONG ONE SIDE.					2	L	7	2 	4F			RT	A10CE   					 
1999043000665	19990430	00665	CE  	1999	4	30	99ZZZX1828       	1	19990405	G	5610	99143806	WINDSHIELD      			CESSNA	650   	650         	2076802	CE  										COCKPIT	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	03	40N	2132 			93097H7532	6507031				RIGHT WINDSHIELD CRACKED AT FL 39,000 FEET.  PPG NOW HAS IMPROVED WINDSHIELD P/N 991438-10 WHICH WAS INSTALLED.						2	L	7	2 	4F				A9NM    					 
1999043000667	19990430	00667	SW  	1999	4	30	99ZZZX1830       	1	19990329	G	6320	212040365023	QUILL ASSY      		212040154001	BELL  	212   	212         	1181420	SW  										TAIL ROTOR	CONTAMINATED    	B		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	98W	1212 			AFS6656	35100				NOTED WHEN OVERHAULING TAIL ROTOR DRIVE QUILL, MANUFACTURING MACHINING FERROUS SHAVINGS EVIDENT IN THE SPACE OR GAP BETW	EEN WHERE THE BEARING LINER IS PRESSED INTO SLEEVE OF QUILL. TOOK RIGHT ANGLE SCRIBE TOOL AND REMOVED FERROUS SHAVINGS F	ROM THE GAP BETWEEN BEARING LINER AND QUILL ASSY.				1	G	7	1 	4U				H4SW    					 
1999050700001	19990507	00001		1999	5	7	99ZZZX1831       	1	19990112	G	5230	69472361	SPRING          	BOEING      	65599333    															COUNTERBALANCE	WEAK            	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01										SPRING FAILS COMPRESSION TEST AT 13.23 INCHES OF COMPRESSION.  LIMITS PER THE OHM ARE 102.7 TO 114.7 POUNDS, SPRING READ	S AT 97 POUNDS.																		 
1999050700006	19990507	00006		1999	5	7	99ZZZX1836       	1	19990125	G	3222	S6026	BODY            	SARGENT     	S60252      															STRUT	LEAKING         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					959					PIN HOLE LEAK IN HOUSING AT CYLINDER 1 PORT.  FATIGUE, OVERTIGHTENING OF FITTING OR IMPACT COULD HAVE CAUSED CRACK.  FIT	TING REMOVED FROM PORT SHOWS SIGNS OF A HARD IMPACT.																		 
1999050700007	19990507	00007		1999	5	7	99ZZZX1837       	1	19990106	G	2742	69778551	SPRING          	BOEING      	654997025   															HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		18398			KE01583					SPRINGS, P/N 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SP	RINGS.  SPRINGS, P/N 69-77855-1, SHOULD BE REPLACED WITH, P/N 69-77855-2, SPRINGS PER BOEING TELEX AEO-AUB-94-0195RR.																		 
1999050700008	19990507	00008		1999	5	7	99ZZZX1838       	1	19990106	G	2742	69778551	SPRING          	BOEING      	654997025   															HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		16001	18869		KE00782					SPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPRIN	GS.  SPRINGS PN 69-77855-1 SHOULD BE REPLACED WITH PN 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB-94-0195RR.																		 
1999050700009	19990507	00009		1999	5	7	99ZZZX1839       	1	19990108	G	2742	69778551	SPRING          	BOEING      	654997025   															HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		18470			KE01544					SPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPRIN	GS.  SPRINGS PN 69-77855-1 SHOULD BE REPLACED WITH PN 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB-94-0195RR.																		 
1999050700010	19990507	00010		1999	5	7	99ZZZX1840       	1	19990128	G	2720	69356081	CAM SEAT        	BOEING      	69356491    															RUDDER CONTROL	GOUGED          	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		12052								PART HAS GOUGES ON THE INTERFACE OF PIN, (8).																			 
1999050700012	19990507	00012		1999	5	7	99ZZZX1842       	1	19990317	G	2742	69778551	SPRING          	BOEING      	65C3475111  															HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		36924	10858		00459					SPRING PN 69-77855-1 IS BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPRING.	  SPRING PN 69-77855-1 SHOULD BE REPLACED WITH PN 69-77855-2 SPRING PER BOEING TELEC AEO-AUB-94-0195RR.																		 
1999050700013	19990507	00013		1999	5	7	99ZZZX1843       	1	19990204	G	2742	69778551	SPRING          	BOEING      	65C364863   															HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		55815	15394		00273					SPRING PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPRING	S.  SPRINGS PN 69-77855-1 SHOULD BE REPLACED WITH PN 69-77855-1 SHOULD BE REPLACED WITH PN 69-77855-2 SPRINGS PER BOEING	 TELEX AEO-AUB-94-0195RR.																	 
1999050700014	19990507	00014		1999	5	7	99ZZZX1844       	1	19990120	G	5754	65463077	SPAR            	BOEING      																LE FLAP	DAMAGED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					BN26					UPON REMOVAL OF AN UNSERVICEABLE LEADING EDGE SKIN REPAIR, DISCOVERED THE LOWER SPAR HAD BEEN SEVERELY DAMAGED BY IMPACT	.  THE SPAR HAD BEEN CUT IN SEVEN LOCATIONS IN AN ATTEMPT TO STRAIGHTEN THE SPAR, AND A DOUBLER WAS THEN INSTALLED.  THE	 DOUBLER DOES NOT COVER 100 PERCENT OF THE DAMAGE OF THE SPAR AND DOES NOT RESTORE STRUCTURAL STRENGTH TO THE SPAR.																	 
1999050700015	19990507	00015		1999	5	7	99ZZZX1845       	1	19990226	G	3240	511531	HOUSING         	PNEUDRAULICS	50601       															BRAKE SYSTEM	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					229					HOUSING IS CRACKED AT EDGE OF MOUNT BOLT HOLE.  CASTING FATIGUE OR OVERTORQUE OF BOLT.  SINGLE MOLD CASTING INSTEAD OF D	OUBLE MOLD CASTING.																		 
1999050700016	19990507	00016		1999	5	7	99ZZZX1846       	1	19990318	G	2750	1775E1	BODY            	SARGENT     	1775EA      															TE FLAP	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01			1814 		1524					BODY IS CRACKED IN PORT 5.  FATIGUE, IMPACT OR OVERTORQUING.  AVOID IMPACT AND OVERTORQUING OF BODY.																			 
1999050700017	19990507	00017		1999	5	7	99ZZZX1847       	1	19990318	G	2761	120611	PISTON          	BOEING      	65449617    															SPOILER ACTUATOR	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					125730					PISTON IS CRACKED IN CORNERS OF KEY SLOTS.  FATIGUE.																			 
1999050700018	19990507	00018		1999	5	7	99ZZZX1848       	1	19990318	G	2742	69778551	SPRING          	BOEING      	65C347517   															HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		18658	15293		KE00090					SPRING PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPRING	S.  SPRINGS PN 69-77855-1 SHOULD BE REPLACED WITH PN 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB-94-0195RR.																		 
1999050700019	19990507	00019		1999	5	7	99ZZZX1849       	1	19990318	G	2752	580867	SCREW           	SPERRYVICRS 																TE FLAP	LOOSE           	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01										SHAFT SEAL RETAINING SCREWS, 6 EACH, WERE SUSPECTED TO HAVE BACKED OUT OF THEIR RESPECTIVE SCREW HOLES IN THE BEARING SL	EEVE PN 79092 CAUSING LEAKAGE PAST THE SHAFT SEAL O-RING, PN 271202.  SCREWS NY-LOCK INSERT IS ONLY ENGAGING ONE THREAD 	DUE TO INSUFFICIENT NY-LOCK MATERIAL AND THE SHORT GRIP LENGTH OF THE SCREW.  INSTALL A SCREW OF THE SAME DESIGN WITH A 	LONGER GRIP LENGTH AND FULL NY-LOCK INSERT FOR BETTER THREAD ENGAGEMENT INTO THE SCREW HOLE.  STAKE THE SCREW ON INSTALL	ATION.  COMPONENT P/N MS9391130ZE4C.															 
1999050700020	19990507	00020		1999	5	7	99ZZZX1850       	1	19990210	G	2752	580867	SCREW           	SPERRYVICRS 																FLAP ACTUATOR	FAILED          	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					MX31178D					SHAFT SEAL RETAINING SCREWS, 6 EACH, WERE FOUND BACKED OUT OF THEIR RESPECTIVE SCREW HOLES IN BEARING SLEEVE PN 79092 CA	USING EXCESSIVE LEAKAGE PAST THE SHAFT SEAL O-RING PN 271202.  THIS HAS BEEN NOTED TO HAVE OCCURRED ON ANOTHER MOTOR ASS	Y.  STAKE SCREW UPON INSTALLATION OR USE OF LOCKTITE ON SCREW THREADS.  INSTALLING A LONGER SCREW FOR BETTER THREAD ENGA	GEMENT OR REPLACE THE SCREW WITH A DIFFERENT TYPE/DESIGN.  COMPONENT P/N MS9391130ZE4C.																 
1999050700021	19990507	00021		1999	5	7	99ZZZX1851       	1	19990315	G	2742	69778551	SPRINGS         	BOEING      	65C3475111  															HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		35590			KE00612					SPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPRIN	GS.  SPRINGS PN 69-77855-1 SHOULD BE REPLACED WITH PN 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB-94-0195RR.																		 
1999050700022	19990507	00022		1999	5	7	99ZZZX1852       	1	19990317	G	2742	69778551	SPRINGS         																	HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		35912	16245		KE00493					SPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPRIN	GS.  SPRINGS PN 69-77855-1 SHOULD BE REPLACED WITH PN 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB-94-0195RR.																		 
1999050700023	19990507	00023		1999	5	7	99ZZZX1853       	1	19990210	G	2731	69733611	SPRING          	BOEING      	65C2456512  															ELEVATOR	BROKEN          	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		9594 			343					FRACTURED SPRING.  BUSHING (475) WAS NOTED TO BE ROTATING FREELY ON PIN (460).																			 
1999050700024	19990507	00024		1999	5	7	99ZZZX1854       	1	19990205	G	2742	69778551	SPRINGS         	BOEING      	65C364866   															HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		37011	1161 		KE00328					SPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPRIN	GS.  SPRINGS PN 69-77855-1 SHOULD BE REPLACED WITH PN 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB-94-0195RR.																		 
1999050700025	19990507	00025		1999	5	7	99ZZZX1855       	1	19990208	G	3243	65445214	VALVE           	BOEING      																BRAKE	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					261G					BODY IS CRACKED AT PORT (5).  POSSIBLE OVERTIGHTENING OF FITTING OR IMPACT COULD HAVE CAUSED CRACK.  DEFECTIVE PLUG INST	ALLATION OR FATIGUE ALSO SUSPECT.  PROPER TORQUE OF THE FITTING AND/OR CORRECT PLUG INSTALLATION PREVENTING ANY IMPACT T	O AREA WOULD BE HELPFUL.																	 
1999050700026	19990507	00026		1999	5	7	99ZZZX1856       	1	19990125	G	2780	69358521	SLEEVE          	BOEING      	65447417    															LE FLAP	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					M05					SLEEVE IS CRACKED NEAR OIL PASSAGE CUT-OUT IN SLEEVE SEAT.  COULD HAVE HAPPENED DURING INSTALLATION OF SLEEVE INTO THE H	OUSING AT MANUFACTURE.																		 
1999050700027	19990507	00027		1999	5	7	99ZZZX1857       	1	19990125	G	3230	65446915	VALVE           	BOEING      																MLG	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		54350			1859					OUTER MOST FLUID HOLE OF THE DOWN PRIORITY VALVE PORT WAS FOUND CRACKED DURING NDI.																			 
1999050700028	19990507	00028		1999	5	7	99ZZZX1858       	1	19990217	G	3252	59561015501	VALVE           	DOUG        																SHIMMY DAMPENER	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01			3173 		SH13837BB					ON PRELIMINARY FUNCTIONAL TEST, THE BODY WAS NOTED TO HAVE A PIN HOLE CRACK WITH 3,000 PSI APPLIED TO THE P1 PORT.  THE 	CRACK IS ADJACENT TO THE C1 PORT.																		 
1999050700029	19990507	00029		1999	5	7	99ZZZX1859       	1	19990222	G	2742	69778551	SPRING          	BOEING      	65C3475111  															HORIZ STABILIZER	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		34657	15269		KE00481					SPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.																			 
1999050700030	19990507	00030		1999	5	7	99ZZZX1860       	1	19990224	G	2720	69356081	CAM SEAT        	BOEING      	69356491    															RUDDER	GOUGED          	B	P	A	IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01										SEVERE GOUGES ON INTERFACE OF PIN (8).																			 
1999050700031	19990507	00031		1999	5	7	99ZZZX1861       	1	19990224	G	2720	69356071	SEGMENT         	BOEING      	69356491    															RUDDER	WORN            	B	P	A	IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		9065 								EXCESSIVE WEAR ON BALL END.  FROM  RUBBING ON YAW DAMPER.																			 
1999050700032	19990507	00032		1999	5	7	99ZZZX1862       	1	19990224	G	3243	65445231	MASTER CYLINDER 	BOEING      	M25         															MLG	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01										BODY IS CRACKED AT PORT 5.  FATIGUE, OVERTORQUE OR IMPACT OF FITTING, OR DEFECT IN CASTING.  STRENGTHEN CASTING.																			 
1999050700033	19990507	00033		1999	5	7	99ZZZX1863       	1	19990222	G	2742	69778551	SPRING          	BOEING      	654997025   															HORIZ STABILIZER	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		18853			KE01571					SPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.																			 
1999050700034	19990507	00034		1999	5	7	99ZZZX1864       	1	19990112	G	5230	69472361	SPRING          	BOEING      	65599333    															CARGO DOOR	FAILED          	B			IU6R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			NM	01										SPRING FAILS COMPRESSION TEST OF 9.87 INCHES OF COMPRESSION.  LIMITS PER THE OHM ARE 160.4 TO 178.4 POUNDS, SPRING READS	 AT 148 POUNDS.																		 
1999050700038	19990507	00038	EU  	1999	5	7	99ZZZX1868       	1	19990310	G	2530	80037110V	COFFEE POT      			BRAERO	DH125 	BAE125800A  	1500285	EU  										GALLEY	OVERHEATED      	H		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	75CS	300  				1258066				PILOT COMPLAINED WHEN HE TRIED TO GET A CUP OF COFFEE, HE WAS NEARLY BURNED FROM COFFEE SPEWING UNDER STEAM PRESSURE.  U	NIT WAS OVERHEATING AND WAS REMOVED FROM AIRCRAFT.  AS THIS IS THE SECOND UNIT TO OVERHEAT, CONTACTED PRECISION PATTERN 	INC, WHO INFORMED THEY KNEW OF THE PROBLEM AND LATER UNITS INCORPORATED A FUSE.  THEY EXPRESSED NO DESIRE TO CORRECT THE	 SITUATION WITH THE OLDER UNITS.			2	L	7	2 	4F			RT	A3EU    					 
1999050700039	19990507	00039	EA  	1999	5	7	99ZZZX1869       	1	19990310	G	2530	80017110V	COFFEE POT      			CNDAIR	CL600 	CL6002B16   	1900305	EA  										GALLEY	OVERHEATED      	H				O				OTHER                   				M			OVER TEMP                 			NR	NOT REPORTED   	1			SW	99	76CS	500  				5103				PASSENGER COMPLAINED COFEE WAS TOO HOT.  CREW FOUND UNIT OVERHEATING.  THIS IS THE SECOND UNIT TO FAIL BY OVERHEATING. T	HE MANUFACTURER ACKNOWLEDGED THE PROBLEM, BUT WAS UNWILLING TO ADDRESS THE UNITS NOW IN AIRCRAFT.					2	L	7	2 	4F			RT	A21EA   					 
1999050700041	19990507	00041	SO  	1999	5	7	99ZZZX1871       	1	19990413	G	2432		STUD            	CHRYSLER    	3656024     	PIPER 	PA28  	PA28140     	7102802	SO  										BATTERY	BROKEN          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	19	1506H		58   		8071773	287725147				THIS ALTERNATOR WAS INSTALLED 3-6-99.  THIS UNIT QUIT CHARGING AFTER 58.12 HOURS TPOL.  INVESTIGATED PROBLEM, FOUND BATT	ERY STUD WAS BROKEN LOOSE FROM ITS ATTACH POINT INTERNALLY.  WHEN REMOVING BATTERY WIRE FROM STUD, IT DID NOT APPEAR TO 	BE OVERTORQUED.  SUBMITTER SUGGESTED THE DEFECT WAS NOT A RESULT OF OVERTORQUING OF THE BATTERY WIRE TO THE STUD.				1	L	7	1 	3O				2A13    					 
1999050700043	19990507	00043	CE  	1999	5	7	99ZZZX1873       	1	19990423	G	7800		EXHAUST         			CESSNA	182   	182S        	2072701	CE  										NR 1 CYLINDER	LOOSE           	B			MINR	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			NM	05	182EL					18280009				PILOT NOTICED EXHAUST FUMES IN CABIN.  INVESTIGATED AND FOUND NR 1 EXHAUST GASKET BLOWN OUT AND ATTACHING HARDWARE MISSI	NG.  NUTS WERE LATER LOCATED IN THE BOTTOM OF ENGINE COWLING.  RIGHT HEAT SHROUD HAD SLID DOWN EXHAUST MUFFLER WHICH ALL	OWED EXHAUST FUMES TO ENTER CABIN THROUGH THE HEATER SYSTEM.  RETENTION HARDWARE ON HEAT SHROUD WAS STILL TIGHT.  THIS A	IRCRAFT HAD SB 97-78-01 C/W AT 59.2 HOURS AND SB 98-78-03 C/W AT 131.3 HRS.  AIRCRAFT TT:  145.7 HOURS.			1	H	7	1 	3O			NT	3A13    					 
1999050700044	19990507	00044	SO  	1999	5	7	99ZZZX1874       	2	19990408	G	7414	10400309	IMPULSE COUPLING	BENDIX      	S6RM122J    	BEECH 	33    	F33A        	1151425	CE  	CONT  	O520  	IO520BB     	17032	SO  					LT MAGNETO	DAMAGED         	B			EB1R	A				UNSCHED LANDING         				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	37050					CE926	285928R			ON A ROUTINE FLIGHT, PILOT NOTICED A DIFFERENT SOUND TO ENGINE.  UPON LANDING, PERFORMED A MAGNETO CHECK AND WHEN SWITCH	ED TO LEFT MAGNETO, THE ENGINE STOPPED RUNNING.  INSPECTION REVEALED THE LEFT MAGNETO IMPULSE COUPLING SPRING HAD BROKEN	 ALLOWING MAGNETO TIMING TO SLIP 30 DEGREES TO 40 DEGREES.  THE IMPULSE COUPLING SPRING WAS REPLACED AND ENGINE RUN PERF	ORMED.  MAGNETO CHECKS WERE GOOD.			1	L	7	1 	3O	3	O		3A15    	E5CE				 
1999050700045	19990507	00045	CE  	1999	5	7	99ZZZX1875       	1	19990420	G	3411		WIRE            			CESSNA	182   	182S        	2072701	CE  										PITOT SYSTEM	MELTED          	B	P	A	DPOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	2352B	102  				18280416				DURING AN ANNUAL INSPECTION, PITOT HEAT WIRING WAS FOUND MELTED/CHAFED INTO PITOT TUBING APPROXIMATELY .0625 INCH.  THE 	PITOT HEAT WIRING HAS VERY LITTLE CLEARANCE FROM THE TUBING.  NEED TO ENSURE WIRING IS SECURED AWAY FROM TUBING.					1	H	7	1 	3O			NT	3A13    					 
1999050700046	19990507	00046	EA  	1999	5	7	99ZZZX1876       	2	19990419	G	7322	565548041	MIXTURE CONTROL 			CESSNA	172   	172S        	2072439	CE  	LYC   	IO360 	IO360L2A    		EA  					CARBURETOR	OUT OF ADJUST   	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	03	940SP	9    				172S8135				NEW CESSNA WITH 9.0 HOURS FOUND MIXTURE CONTROL WOULD NOT HIT FULL RICH STOP ON FUEL CONTROL AND CONTROL IN COCKPIT HAD 	NO CUSHION.  RE-ADJUSTED MIXTURE CONTROL, OPERATIONAL CHECK SATISFACTORY.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999050700047	19990507	00047	CE  	1999	5	7	99ZZZX1877       	1	19990419	G	2510	05142158	FITTING         			CESSNA	172   	172S        	2072439	CE  										SEAT	BENT            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	940SP	9    				172S8135				NEW CESSNA WITH 9.0 HOURS HAD COPILOT'S SEAT BACK RECLINED APPROXIMATELY 4 INCHES.  FOUND SEAT BACK SUPPORT FITTING BENT	.  REPLACED SUPPORT FITTING WITH CESSNA SUPPLIED PART.  THIS IS 3RD FAILURE OF SEAT BACK SUPPORT FITTING ON TWO NEW CESS	NA C-172S AIRCRAFT.				1	H	7	1 	3O			NT	3A12    					 
1999050700048	19990507	00048	CE  	1999	5	7	99ZZZX1878       	1	19990419	G	2730	05341221	BELLCRANK       			CESSNA	172   	172S        	2072439	CE  										ELEVATOR	OUT OF ADJUST   	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	940SP	9    				172S8135				FOUND NEW CESSNA AT FACTORY HAD ELEVATOR HALVES MISALIGNED BY .25 INCH.  WHEN STREAMLINED WITH LOWER HORIZONTAL STABILIZ	ER, ONE SIDE WAS .25 INCH OUT OF ALIGNMENT WITH OTHER SIDE.  AFTER FERRY FLIGHT TO HOME STATION, ELEVATOR BELLCRANK BOLT	S WERE LOOSENED, ELEVATOR HALVES ALIGNED, AND BOLTS RE-TORQUED.				1	H	7	1 	3O			NT	3A12    					 
1999050700049	19990507	00049	CE  	1999	5	7	99ZZZX1879       	1	19990419	G	2731	053200110	TRIM TAB        			CESSNA	172   	172S        	2072439	CE  										ELEVATOR	OUT OF ADJUST   	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	940SP	9    				172S8135				FOUND NEW CESSNA AT FACTORY HAD TRIM TAB INCORRECTLY ADJUSTED.  WHEN TRIM WHEEL IN COCKPIT ALIGNED TO TAKEOFF POSITION, 	TRIM TAB WAS DOWN .25 INCH INSTEAD OF STREAMLINED.  AFTER FERRY-FLIGHT TO HOME STATION, TAB WAS ADJUSTED TO NEUTRAL AND 	STOPS ADJUSTED FOR CORRECT TRAVEL.				1	H	7	1 	3O			NT	3A12    					 
1999050700050	19990507	00050	CE  	1999	5	7	99ZZZX1880       	1	19990419	G	3411	201314218	SELECTOR VALVE  			CESSNA	172   	172S        	2072439	CE  										PITOT SYSTEM	LEAKING         	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NM	03	940SP	9    				172S8135				NEW CESSNA C-172'S ON FERRY FLIGHT FROM FACTORY, ALTIMETER AND VERTICAL VELOCITY INDICATORS HAD EXCESSIVE FLUX.  FOUND S	TATIC LINE TO STATIC SELECTOR VALVE CROSS-THREADED AND LEAKING.  REPLACED LINE AND FITTING, AND ACCOMPLISHED STATIC CHEC	K SATISFACTORY WITH NO LEAKAGE.				1	H	7	1 	3O			NT	3A12    					 
1999050700051	19990507	00051	CE  	1999	5	7	99ZZZX1881       	1	19990419	G	7800	15550142	CLAMP           			CESSNA	172   	172S        	2072439	CE  										EXHAUST SYSTEM	LEAKING         	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NM	03	940SP	9    				172S8135				NEW CESSNA WITH 9.0 HOURS.  ON ACCEPTANCE INSPECTION, FOUND EXHAUST RISER CLAMPS NOT PROPERLY SEATED AND LEAKING EXHAUST	.  LOOSENED CLAMPS AND EXHAUST RISER FLANGES AT CYLINDER ENDS.  ALIGNED AND TIGHTENED CLAMPS, THEN TORQUED RISER FLANGES	.  EXHAUST CLAMPS SEATED PROPERLY.				1	H	7	1 	3O			NT	3A12    					 
1999050700052	19990507	00052	SO  	1999	5	7	99ZZZX1882       	1	19990408	G	3230	AN425	BOLT            			MAULE 	MX7   	MXT7180     	5470206	SO  										NLG STEERING	DAMAGED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	9221Y	1334 				14028C				DURING AN INVESTIGATION OF A NOSE WHEEL SHIMMY COMPLAINT, AN INSPECTION OF THE BOLT THAT GOES THROUGH THE NOSE GEAR AND 	THE STEERING CONTROL ARM WAS FOUND PARTIALLY SHEARED AT BOTH THE HEAD AND THREAD ENDS.  LOSS OF CONTROL COULD RESULT FRO	M A FULL SHEAR OF THIS BOLT.  SUBMITTER RECOMMENDED FREQUENT INSPECTION OF THIS BOLT AND REPLACEMENT AS REQUIRED OR INST	ALLATION OF A MORE SHEAR RESISTANT BOLT.  THIS IS THE SECOND TIME THIS HAS BEEN NOTED ON LIKE AIRCRAFT.  FIRST AIRCRAFT 	TT:  1,770 HOURS.		1	H	7	1 	3O			NC	3A23    					 
1999050700053	19990507	00053	SO  	1999	5	7	99ZZZX1883       	2	19990416	G	7320	632557	ROD END         		642283A2    	CESSNA	210   	P210R       	2073455	CE  	CONT  	O520  	TSIO520CE   	17040	SO  					PRESSURE CONTROL	WORN            	B			BJ3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	15	5194A	754  				P21000886	530162			DURING ANNUAL INSPECTION, PLAY WAS NOTED IN ROD ASSEMBLY LINKING VAPC WITH THE THROTTLE BODY.  UPON DISASSEMBLY OF LINK 	ROD UNIT, NOTED THE ROD END 63251 WAS WORN WHERE IT CONNECTED TO THE VAPC LINKAGE.  APPROXIMATELY 20 PERCENT REDUCTION I	N DIAMETER WAS NOTED.  INSTALLATION OF A NEW ROD END CURED PLAY.				1	H	7	1 	3O	3	O	RT	3A21    	E8CE				 
1999050700054	19990507	00054	SO  	1999	5	7	99ZZZX1884       	2	19990416	G	7320	632557	ROD END         		642283A2    	CESSNA	210   	P210R       	2073455	CE  	CONT  	O520  	TSIO520CE   	17040	SO  					PRESSURE CONTROL	WORN            	B			BJ3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	15	5545A	1104 				P21000864	530105			DURING AN ENGINE CHANGE, PLAY WAS NOTED IN ROD ASSEMBLY LINKING VAPC WITH THE THROTTLE BODY.  UPON DISASSEMBLY OF THE LI	NK ROD UNIT, NOTED THE ROD END 632557 WAS WORN WHERE IT CONNECTED TO THEVAPC  LINKAGE.  APPROXIMATELY 20 PERCENT REDUCTI	ON IN DIAMETER WAS NOTED.  INSTALLATION OF A NEW ROD END CURED PLAY.				1	H	7	1 	3O	3	O	RT	3A21    	E8CE				 
1999050700056	19990507	00056	CE  	1999	5	7	99ZZZX1886       	1	19990410	G	3233	35810117	SECTOR GEAR     			BEECH 	95    	95          	1153402	CE  										ACTUATOR	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	21JC	6700 				TD224				DURING ANNUAL INSPECTION GEAR OPERATION, ADJUSTED DOORS TO FIT TIGHTER, AND ACTUATOR SECTOR SHEARED TEETH.  ACCORDING TO	 BEECH SHOP MANUAL AND OWNER'S MANUAL, IF GEAR ACTUATOR MOTOR FAILS TO SHUT OFF AFTER GEAR UP OR DOWN POSITIONS, ADJUST 	OR REPLACE LIMIT SWITCHES.  BUT SHOULD STATE TO ALSO DYE PENETRATE INSPECT LANDING GEAR ACTUATOR SECTOR AND WORM GEARS F	OR CRACKS.  THIS IS THE WEAKEST LINK IN THE GEAR SYSTEM SINCE THERE ARE 14 SECTORS BACK ORDERED.			1	L	7	2 	3O				3A16    					 
1999050700057	19990507	00057	CE  	1999	5	7	99ZZZX1887       	1	19990414	G	2751	9511002245	FLAP TRACK      			BEECH 	58    	58          	1152740	CE  										WING	DAMAGED         	B			AKGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	05	38023	5205 				TH1209				MECHANIC FOUND DEFECT IN FLAP TRACK AT INBOARD END OF BOTH FLAPS.  DEFECT WAS CAUSED BY FLAP ROLLERS IN FULL UP POSITION	.  SUGGEST FLAP REMOVAL AT ANNUAL AND/OR 100-HOUR FOR PROPER INSPECTION.  ALSO, AN INBOARD FLAP BUMPER MAY BE NEEDED TO 	STOP VIBRATION AND SIDE LOAD.  NOTE:  SIMILAR DEFECT FOUND ON BEECH MODELS 33, 35, A36 AND 55.				1	L	7	2 	3O				3A16    					 
1999050700058	19990507	00058	NE  	1999	5	7	99ZZZX1888       	2	19990329	G	7314	P94B12200	FUEL PUMP       			SNIAS 	350   	AS350BA     	8680817	EU  	TMECA 	ARRIEL	ARRIEL1B    	6OO30	NE  					FUEL SYSTEM	MALAFUNCTIONED  	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	19	92MH	301  				2898	4524			REMOVED FUEL PUMP DUE TO NOT PRODUCING FUEL PRESSURE ALTHOUGH MOTOR CONTINUED TO OPERATE.						1	G	7	1 	3U	3	U	NC	H9EU    	E19EU				 
1999050700059	19990507	00059	EU  	1999	5	7	99ZZZX1889       	1	19990324	G	5101		STRUCTURE       			RHNFLU	EA300 	EA300S      	1130864	EU  										FUSELAGE	FAILED          	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03	9K					022				C/W EXTRA SB 300-2-95 ISSUE B.  INSTALLED REPAIR PER FACTORY DRAWINGS.  PERFORMED AT TT 856.3 HOURS.  INSPECTIONS NO LON	GER RECURRING IAW SB 300-2-95 ISSUE C.  AT 1,052.4 HOURS, UPPER LEFT LONGERON AT REPAIR BROKE IN TWO.  ALSO BROKE CROSS 	MEMBER IN TWO.  RECOMMEND AN AD BE ISSUED ON AIRCRAFT WITH THIS MODIFICATION.  SUBMITTER STATED FOURTH AIRCRAFT TO FAIL 	WITH THIS REPAIR.			1	M	7	1 	3O			NC	A67EU   					 
1999051400497	19990514	00497	WP  	1999	5	14	99ZZZX1890       	1	19990409	G	7714	369A45167	INDICATOR       			HUGHES	369   	369D        	4470706	WP  										COCKPIT	ERRATIC         	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	1097J		4321 		444D	900801D				N1 GAUGE GIVES ERRATIC READING.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999051400498	19990514	00498	WP  	1999	5	14	99ZZZX1891       	1	19990409	G	7400	369A45143	EPO ASSY        			HUGHES	369   	369D        	4470706	WP  										COCKPIT	ERRATIC         	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	1097J		1306 		430	900801D				EPO GIVES ERRATIC WARNINGS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999051400499	19990514	00499	WP  	1999	5	14	99ZZZX1892       	1	19990308	G	6710		T-BAR           			ROBSIN	R44   	R44         	7640120	WP  										CYCLIC	LOOSE           	H		A		O				OTHER                   				W			INADEQUATE Q C            			NR	NOT REPORTED   	1			EA	07	7037C	599  								T-BAR ON CYCLIC CONTROL IS RETAINED WITH A NUT AND COTTER PIN.  THE NUT, WASHER AND COTTER PIN WERE NEVER INSTALLED AT T	HE FACTORY.  THE THREADED PORTION STILL HAD MASKING TAPE ON THE THREADS.  THE T-BAR PULLED OUT OF THE CYCLIC IN-FLIGHT A	ND COULD VERY EASILY HAVE RESULTED IN CATASTROPHE.				1	G	7	1 	3O				H11NM   					 
1999051400500	19990514	00500	NE  	1999	5	14	99ZZZX1893       	1	19990415	G	3240	50075551	BRAKE ASSY      			SKRSKY	S76   	S76C        	8143008	NE  										MLG	LEAKING         	B			J2BR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			GL	15	1875P				AUG81819	760488				BRAKE ASSEMBLY WAS LEAKING AT THE 6 O'CLOCK AND 4 O'CLOCK POSITIONS, FROM THE BRAKE PADS.  NOTE:  LEAKING AT INSTALLATIO	N FROM INVENTORY.					1	G	7	2 	3U			NC	H1NE    					 
1999051400501	19990514	00501	EU  	1999	5	14	99ZZZX1894       	1	19990414	G	5102	BU11	SEAT CARRIER    		BU002001    	COLT  	77A   	77A         	2300102	EU  										BURNER	COMPRESSED      	B		A	R4BR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	05	372LB	118  			316	5014				RUBBER RING ON SEAT CARRIER COMPRESSED BEYOND LIMITS SUCH THAT WHEN BLAST-VALVE HANDLE WAS AT REST (NOT ACTIVATED), THE 	SEAT CARRIER WAS NOT ABLE TO PRODUCE A SEAL WITH MAIN VALVE BLOCK.  SUSPECT SEAT CARRIER WAS NOT THICK ENOUGH OR VALVE-W	EAR-PAD WAS TOO THICK.				1	B	0	0 					B3EU    					 
1999051400502	19990514	00502		1999	5	14	99ZZZX1895       	4	19990427	G	6113		BULKHEAD        			PIPER 	PA32  	PA32300     	7103212	SO  										SPINNER	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	2835W					327940148				DURING ROUTINE INSPECTION, NOTED A CRACK EXTENDING FROM THE TRAILING EDGE OF THE FORWARD SPINNER BULKHEAD TO ONE OF THE 	NUT PLATES AND CONTINUING ANOTHER .50 INCH FORWARD.  THIS IS THE SECOND BULKHEAD INSTALLED ON THIS AIRCRAFT IN LESS THAN	 8 HOURS DUE TO THIS SAME PROBLEM.  THE MOUNTING OF THE BULKHEAD AND SPINNER HAS BEEN CHECKED SEVERAL TIMES FOR PROPER F	IT AND ALIGNMENT AND CORRECT TORQUE ON THE SPINNER MOUNTING SCREWS.  TWO OTHER AIRCRAFT IN THE SAME FLEET HAVE ENCOUNTER	ED SIMILAR FAILURE TIMES.		1	L	7	1 	3O				A3SO    					 
1999051400503	19990514	00503	SO  	1999	5	14	99ZZZX1896       	1	19990427	G	2731		CONTROL CABLE   			PIPER 	PA32  	PA32300     	7103212	SO  										ELEVATOR TRIM	FRAYED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	2835W					327940148				DURING ROUTINE INSPECTION, THE FORWARD TRIM CABLE WAS FOUND FRAYED IN THE AREA THAT PASSES THROUGH THE ELECTRIC TRIM SER	VO. PIPER SB NR 669 HAD BEEN C/W BY INSTALLATION OF PIPER  ELECTRIC TRIM PULLEY ALIGNMENT KIT P/N 763-971 DURING THE LIF	E OF THE CABLE.  A CLOSE VISUAL INSPECTION OF THE TRIM SERVO REVEALED THAT INSTALLATION OF THE KIT DOES NOT PROPERLY ALI	GN THE CABLE.  THE SERVO MOUNT IS INCORRECTLY DESIGNED CAUSING THE ENTIRE SERVO TO BE OUT OF ALIGNMENT WITH THE CABLE. A	 NEW MOUNT SHOULD BE DESIGNED THAT ALIGNS THE SERVO.		1	L	7	1 	3O			 	A3SO    					 
1999051400504	19990514	00504	CE  	1999	5	14	99ZZZX1899       	1	19990415	G	5260	50430043865	FRAME           			BEECH 	100   	A100        	1152915	CE  										AIRSTAIR DOOR	CRACKED         	B	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	46BE	9247 				B214				FOUND CRACKS ORIGINATING FROM HOLE IN FRAMES WHERE THE UPPER LATCH BOLTS GO THROUGH.  THESE CRACKS WENT THROUGH THE TWO 	SCREW HOLES ADJACENT TO THE LATCH BOLT HOLE AND CONTINUED UP THE FRAMES.					1	L	7	2 	3T				A14CE   					 
1999051400505	19990514	00505	CE  	1999	5	14	99ZZZX1900       	1	19990415	G	5260	50430043867	FRAME           			BEECH 	100   	A100        	1152915	CE  										AIRSTAIR DOOR	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	46BE	9247 				B214				FOUND CRACKS ORIGINATING FROM HOLE IN FRAMES WHERE THE UPPER LATCH BOLTS GO THROUGH.  THESE CRACKS WENT THROUGH THE TWO 	SCREW HOLES ADJACENT TO THE LATCH BOLT HOLE AND CONTINUED UP THE FRAMES.					1	L	7	2 	3T				A14CE   					 
1999051400506	19990514	00506	SW  	1999	5	14	99ZZZX1901       	1	19990424	G	2910	5SS10083000A106Y	LINE            			SWRNGN	SA227 	SA227AC     	8780603	SW  										HYDRAULIC SYSTEM	FAILED          	B			R2JR	O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		NR	NOT REPORTED   	1			EA	21	685BR	23127				AC685				HYDRAULIC PRESSURE SENT TO ZERO IN-FLIGHT.  AIRCRAFT RETURNED TO AIRPORT SAFELY.  MAINTENANCE FOUND RESERVOIR EMPTY DUE 	TO MASSIVE LEAK AT RT FLAP ACTUATOR LINES.  NEW LINES INSTALLED.  RIGHT HYDRAULIC PUMP FAILED TO PRODUCE PRESSURE.  REPL	ACED PUMP AND FILTER.  OPS CHECK OK.  HOSES FAILED DUE TO AGE.  LOCATED IN AREA IMPOSSIBLE TO INSPECT PROPERLY.  PUMP FA	ILED DUE TO FLUID STARVATION.			2	L	7	2 	4T			RT	A8SW    					 
1999051400507	19990514	00507	CE  	1999	5	14	99ZZZX1902       	1	19990416	G	2400	5327111	SWITCH          			CESSNA	172   	172R        	2072401	CE  										COCKPIT	FAILED          	B			PRIR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	03	718EH	4    				17280061				WHEN SWITCH IS TURNED OFF HALF OF CONTACT STAYS IN CLOSED POSITION AND POWER SAYING ON.						1	H	7	1 	3O			NT	3A12    					 
1999051400508	19990514	00508	EA  	1999	5	14	99ZZZX1903       	1	19990420	G	7830	22850084801	BRACKET         		2285002D113 	CNDAIR	CL600 	CL6002B16   	1900305	EA  										THRUST REVERSER	LOOSE           	B			SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	914X	2132 			SBRJNACC0079	5185				THE BRACKETS ARE FASTENED BY SIX HL18PB-5 HI-LOKS TO THE INLET INNER RIB.  DURING REMOVAL OF THE LOOSE FASTENERS, THE HO	LE SIZES WERE BETWEEN .167 INCH TO .178 INCH.  THEY SHOULD BE .159 INCH TO .162 INCH.					2	L	7	2 	4F			RT	A21EA   					 
1999051400509	19990514	00509	EA  	1999	5	14	99ZZZX1904       	1	19990420	G	7830	22850071101	BRACKET         		22850020109 	CNDAIR	CL600 	CL6002B16   	1900305	EA  										THRUST REVERSER	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	611GS	3428 			110	5082				THE BRACKETS ARE FASTENED BY SIX HL18PB-5 HI-LOKS TO THE INLET INNER RIB.  DURING REMOVAL OF THE LOOSE FASTENERS, THE HO	LE SIZES WERE BETWEEN .165 INCH TO .178 INCH.  THEY SHOULD BE .159 INCH TO .162 INCH.					2	L	7	2 	4F			RT	A21EA   					 
1999051400510	19990514	00510	EA  	1999	5	14	99ZZZX1905       	1	19990420	G	7830	22850071102	BRACKET         		22850020109 	CNDAIR	CL600 	CL6002B16   	1900305	EA  										THRUST REVERSER	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	611GS	3428 			110	5082				THE BRACKETS ARE FASTENED BY SIX HL18PB-5 HI-LOKS TO THE INLET INNER RIB.  DURING REMOVAL OF THE LOOSE FASTENERS, THE HO	LE SIZES WERE BETWEEN .165 INCH TO .178 INCH.  THEY SHOULD BE .159 INCH TO .162 INCH.					2	L	7	2 	4F			RT	A21EA   					 
1999051400511	19990514	00511	EA  	1999	5	14	99ZZZX1906       	1	19990325	G	7830	22850055175	BRACKET         			CNDAIR	CL600 	CL6002B16   	1900305	EA  										THRUST REVERSER	LOOSE           	B			SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	893AC	3823 			039	501B				THE BALLSCREW ACTUATOR BRACKETS ARE FASTENED BY 6 EACH HI-LOKS TO THE INLET INNER RIB.  THE FASTENERS ARE WORKING LOOSE 	MAKING OVERSIZE HOLES AND PUTTING THE FASTENER HEAD IN TENSION.					2	L	7	2 	4F			RT	A21EA   					 
1999051400512	19990514	00512	EA  	1999	5	14	99ZZZX1907       	1	19990325	G	7830	22850055175	BRACKET         		2285002D109 	CNDAIR	CL600 	CL6002B16   	1900305	EA  										THRUST REVERSER	LOOSE           	B			SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	9700X	5580 			037	5186				THE BALLSCREW ACTUATOR BRACKETS ARE FASTENED BY 6 EACH HI-LOKS TO THE INLET INNER RIB.  THE FASTENERS ARE WORKING LOOSE 	MAKING OVERSIZE HOLES AND PUTTING THE FASTENER HEAD IN TENSION.					2	L	7	2 	4F			RT	A21EA   					 
1999051400516	19990514	00516	WP  	1999	5	14	99ZZZX1911       	1	19990301	G	2622	WKA89524001	FIRE EXTINGUISH 			DOUG  	DC10  	DC1030      	3023501	WP  										CABIN	MALFUNCTIONED   	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05					11565EH					DURING RECEIVNG INSPECTION OF FIRE EXTINGUISHER, PN 895240-01, THE INSPECTOR NOTED DAMAGE TO THE MAIN OUTLET DISC.  INSP	ECTION BY WALTER KIDDE ENGINEERING CONFIRMED A CARTRIDGE HAD BEEN FIRED, BUT FAILED TO RUPTURE DISC.  THE CARTRIDGE WAS 	NOT AVAILABLE FOR INSPECTION.  HOWEVER, IN DISCUSSION WITH THE AIRLINE, THEY INDICATED THE CARTRIDGE WAS NOT A WKA PRODU	CT, AND WAS NOT AVAILABLE.  INSPECTION OF THE DISC CONFIRMED IT WAS MANUFACTURED BY WKA AND A QUALITY REVIEW ALSO CONFIR	MED ALL LOT ACCEPTANCE TEST SAMPLES FROM LOT LN-067 WERE WITHIN DESIGN SPECIFICATIONS.		2	L	7	3 	4F				A22WE   					 
1999051400518	19990514	00518	NM  	1999	5	14	99ZZZX1913       	1	19990408	G	5347		SEAT TRACK      			DOUG  	MD11  	MD11F       	3023600	NM  										BS 635-755	CRACKED         	B			S3BR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01	274WA					48633				DURING C-CHECK, PER WORLD AIRWAYS 5901/SBA B0387-04R-00081 WORK CARD, FOUND 11 SEAT TRACKS FORWARD OF MAIN DECK CARGO DO	OR AREA CRACKED.  CRACKS WERE LOCATED AT FS 635 AND FS 755.  THE AIRPLANE HAS ACCUMULATED 18,385.32 HOURS AND 3,883 FLIG	HT CYLCES.  FIVE EACH SEAT TRACKS WERE FOUND CRACKED AT FS 635, RBL 10, RBL 28, RBL 48, LBL 28 AND LBL 48.  ALL SEAT TRA	CKS NOTED WERE CRACKED AT FLOOR BEAM ATTACH AREA.  ALSO, 5 EACH SEAT TRACKS WERE FOUND CRACKED AT FS 755 AT RBL 28, RBL 	48, LBL 28, LBL 48 AND LBL 76 RESPECTIVELY.  THESE WERE ALSO CRACKED AT THE FLOOR BEAM ATTACH POINT.  AT FS 735, ONE SEA	T TRACK WAS CRACKED AT LBL 10.  NOTE:  FS 635 IS JUST FWD OF MAIN CARGO DOOR AND FS 755 IS JUST AFT OF MAIN CARGO DOOR.	2	L	7	3 	4F			RT	A22WE   					 
1999051400519	19990514	00519	NE  	1999	5	14	99ZZZX1914       	2	19990427	G	7260	4B7320	SPACER          								IAE   	V2500 	V2500A1     		NE  					SCAVENGE PUMP	FAILED          	B			RA1D	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05							FAAAACW			VISUAL AND BINOCULAR INSPECTION OF THE SPACER REVEALED SOME ENTRAPPED COPPER-COLORED METALLIC DEBRIS IN  THE SLOTTED REC	ESS ON THE SIDE FACE FLAT.  FINE GRIT-LIKE PARTICLES WERE ALSO OBSERVED IN THE BORE ANNUAL RECESS.  THE ANODIZED SURFACE	S EXHIBITED A MOTTLED, CRAZE-CRACKED APPEARANCE WITH ISOLATED REGIONS WHERE PIECES OF THE COATING HAD SPALLED.  SPACER I	S STILL UNDER INVESTIGATION BY GEES-DALLAS ENGINEERING.								4	F			E311NE				 
1999051400520	19990514	00520	WP  	1999	5	14	99ZZZX1915       	1	19990414	G	7810	4215AB2025	CLAMP           		900635543   	CVAC  	440   	440         	2422902	WP  										LT NACELLE	MISINSTALLED    	B			TR1R	O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			SW	05	580HH				18	500				SUSPECTED THAT CLAMP HOLDING TAILPIPE TO THE REAR OF THE TURBINE WAS INSTALLED IMPROPERLY AND CAME LOOSE CAUSING THE TAI	LPIPE TO SLIDE BACK 6 INCHES AND ALLOWING HOT TURBINE EXHAUSTS ON NACELLE COWLS AND ENGINE FIRE DETECT LOOP.  THIS CAUSE	D AN ENGINE FIRE WARNING AND SUBSEQUENT IN-FLIGHT SHUT DOWN ON THE ENGINE.				2	L	7	2 	4R				6A6     					 
1999051400522	19990514	00522	EA  	1999	5	14	99ZZZX1917       	1	19990427	G	2840	601R623043	FUEL SENSOR     		604622501   	CNDAIR	CL600 	CL6002B16   	1900305	EA  										FUEL CELL	FAILED          	B			ROIR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	05	43R	663  				5334				TAIL FUEL TANK WOULD STOP AUTOMATIC FUEL TRANSFER AT APPROXIMATELY 800 POUNDS REMAINING IN TANK.  MANUAL TRANSFER WOULD 	PUMP OUT THE 800 POUNDS.  WOULD ALSO GET 'AUX AUTO XFR' EICAS MESSAGE.  REPLACED LOWER D-FUEL SENSOR IN TAIL TANK SUMP M	ANIFOLD.  SYSTEM NOW TRANSFERS 'ALL' FUEL OUT OF TAIL WITH NO EICAS MESSAGES AUTOMATICALLY.				2	L	7	2 	4F			RT	A21EA   					 
1999051400523	19990514	00523	CE  	1999	5	14	99ZZZX1918       	1	19990421	G	2612	875135	FIRE LOOP       			LEAR  	25    	25D         	5170514	CE  										NACELLE	MALFUNCTIONED   	E				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			GL	23	95CK					248				INTERMITTENT FIRE LIGHT RIGHT SIDE.  RE-POSITIONED FIRE DETECT LOOP, WAS MAKING CONTACT WITH COWLING.  DETECT SYSTEM OPE	RATIONALLY, CHECKS GOOD.					2	L	7	2 	4J				A10CE   					 
1999051400524	19990514	00524	NE  	1999	5	14	99ZZZX1919       	3	19990423	G	6111	57D0495	FORK            			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	PITCH CHANGE	CRACKED         	B			EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03			4322 		2032NR			HJ204A		FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS.  TSN:  IS UNKNOWN ON FORK.  PR	OPELLER TSN:  9,253.2 HOURS.					2	L	7	2 	4T			RT	A24CE   		5	C	P10N	 
1999051400525	19990514	00525	CE  	1999	5	14	99ZZZX1920       	1	19990329	G	5510		FASTENER        			CESSNA	340   	340CESSNA   	2076404	CE  										HORIZ STABILIZER	MISINSTALLED    	H		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	99	5151J					3400541				SEVERE VIBRATION.  SUBMITTER STATED WRONG HARDWARE INSTALLED AT FORWARD ATTACH POINTS OF HORIZONTAL STABILIZER.  REMOVED	 AN6-10A BOLTS, AN363-624 NUTS, AND AN960-616 WASHERS.  2 BOLTS, 2 NUTS, 4 WASHERS.  INSTALLED PROPER HARDWARE.  2 EACH 	AN6-7A BOLTS, 2 EACH MS21042L6 NUTS WITH AN960-616 WASHER UNDER NUTS.  CHECKED ALL ATTACH POINTS FOR CRACKS.  AIRCRAFT T	EST FLOWN.			1	L	7	2 	3O				3A25    					 
1999051400526	19990514	00526		1999	5	14	99ZZZX1921       	1	19990319	G	2435	EU10274	GEAR            	RROYCE      																START/GENERATOR	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05		3237 								ENGINE SUFFERED MULTIPLE AIR STARTER DRIVESHAFT FAILURES.  DETAIL STRIP OF HS GRBX DRIVING BEVEL GEAR ASSY REVEALED SEVE	RE WEAR OF LOCATION OF SPLINES ON SHAFT AND GEARWHEEL.  DURING STRIP OF SUB-ASSY, NOTED LITTLE OR NO TORQUE ON RETAINING	 NUT ALLOWING SHAFT TO SPIN IN RELATION TO THRUST BEARING.  EVIDENCE CAN BE SEEN WHERE THE END OF FACE OF THE THRUST BEA	RING DISPLAYS CONTACT WITNESS.  THE FIT BETWEEN SHAFT AND BEARING IS ONE OF INTERFERENCE AND NO RELATIVE MOVEMENT SHOULD	 OCCUR BETWEEN THE TWO.  HEAT WAS GENERATED IN THE SHAFT/GEAR AND SHAFT/BEARING INTERFACE AREAS.  REPLACED HS GEARBOX DR	IVING BEVEL GEAR, GEARSHAFT, THRUST BEARING AND ADJACENT WASHERS SPACERS WITH NEW.  ENG MDL NR TAYMK6118, ENG SN 16254.														 
1999051400527	19990514	00527	CE  	1999	5	14	99ZZZX1922       	1	19990415	G	5720	1014024	BOLT            			BEECH 	100   	B100        	1152919	CE  										WING	MISINSTALLED    	B			R2JR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	86FD					BE14				WHILE C/W 5 YEAR WING BOLT INSPECTION, FOUND FITTINGS DAMAGED DUE TO IMPROPER INSTALLATION OF RIGHT, LOWER, FORWARD AND 	LEFT, LOWER FORWARD WING BOLTS.  WASHERS WERE INSTALLED BACKWARDS WHICH DEFORMED THE WING FITTINGS.					1	L	7	2 	4T				A14CE   					 
1999051400528	19990514	00528	CE  	1999	5	14	99ZZZX1923       	1	19990302	G	3230	1004100133	FITTING         			BEECH 	90    	E90         	1152914	CE  										LT NLG	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	28MS					LW100				DURING ROUTINE INSPECTION, NOTICED ONE OF FOUR HUCK BOLTS, ON RT NLG DRAG LEG FITTING, BROKE AND ALL BUT ONE ON BOTH LT 	AND RT FITTINGS WERE LOOSE.  REMOVED ALL EIGHT HUCKBOLTS FROM FITTINGS AND INSTALLED NAS464-P3-LA4 AND NAS464-P3-LA5 BOL	TS WITH SELF-LOCKING NUTS.  WORK WAS DONE IAW BEECH TECHNICAL SUPPORT.  BEECH SERVICE COMMUNIQUE NR 52, DATED 1973, ADDR	ESSED THIS PROBLEM.			1	L	7	2 	3T				3A20    					 
1999051400529	19990514	00529	CE  	1999	5	14	99ZZZX1924       	1	19990302	G	3230	1004100134	FITTING         			BEECH 	90    	E90         	1152914	CE  										RT NLG	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	28MS					LW100				DURING ROUTINE INSPECTION, NOTICED ONE OF FOUR HUCK BOLTS, ON RT NLG DRAG LEG FITTING, BROKE AND ALL BUT ONE ON BOTH LT 	AND RT FITTINGS WERE LOOSE.  REMOVED ALL EIGHT HUCKBOLTS FROM FITTINGS AND INSTALLED NAS464-PE-LA4 AND NAS464-P3-LA5 BOL	TS WITH SELF-LOCKING NUTS.  WORK WAS DONE IAW BEECH TECHNICAL SUPPORT.  BEECH SERVICE COMMUNIQUE NR 52, DATED 1973, ADDR	ESSED THIS PROBLEM.			1	L	7	2 	3T				3A20    					 
1999051400115	19990514	00115	SW  	1999	5	14	99ZZZX1925       	1	19990423	G	6320	6898661	CAP             			BELL  	206   	206B        	1181511	SW  										GEARBOX	CRACKED         	B		A	DDZR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CE	03	600RP	2284 				3098				ONE MOUNTING EAR FOR ENGINE OIL FILTER HOUSING CAP BROKE ALLOWING ENGINE OIL PRESSURE TO PUSH CAP UP PASS O-RING.  THE E	NGINE OIL FILTER HOUSING IS MOUNTED ON TOP OF ENGINE.  LEAKING OIL RAN BACK ON TO TURBINE SECTION CATCHING ON FIRE.  HEL	ICOPTER LANDED UNDER ITS OWN POWER.  FIRE WENT OUT WHEN ENGINE WAS SHUT OFF.				1	G	7	1 	3U				H2SW    					 
1999051400116	19990514	00116	EU  	1999	5	14	99ZZZX1926       	1	19990426	G	5302	1053025151001	FRAME           			BOLKMS	117   	BK117B1     	5626012	EU  										TAIL BOOM	CRACKED         	B		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03	122SL	8421 				7207				FOUND CRACK IN FRAME 10L DURING ROUTINE INSPECTIONS.  CONTACTED AMERICAN EUROCOPTER.  TECH REP CAME TO ST LOUS, AND REMO	VED AND REPLACED FRAME 10L.					1	G	7	2 	3U				H13EU   					 
1999051400117	19990514	00117	GL  	1999	5	14	99ZZZX1927       	3	19990426	G	6114	C6447C23	HUB             			BEECH 	33    	35C33A      	1151410	CE  						MCAULY	2A36C	2A36C23     	GL  	PROPELLER	CRACKED         	B			EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03					66004			66004		HUB CRACKED IN THREAD AREA OF NR 2 BLADE SOCKET.  CRACK WAS FOUND WITH EDDY CURRENT INSPECTION ONLY.						1	L	7	1 	3O				3A15    		5	C	P880	 
1999051400118	19990514	00118	SO  	1999	5	14	99ZZZX1928       	1	19990426	G	3233	752726	SEAL            		3503002     	PIPER 	PA23  	PA23250     	7102308	SO  										MLG	LEAKING         	E				O				OTHER                   				J			WARNING INDICATION        			LD	LANDING        	1			GL	13	40599					277405345				WHEN LANDING GEAR HANDLE WAS SELECTED DOWN, PILOT DID NOT GET GREEN LIGHT.  CYCLED GEAR SEVERAL TIMES, UNABLE TO GET GRE	EN LIGHT.  TRIED TO HAND PUMP GEAR DOWN WITH SAME RESULTS.  THEN TRIED IT WHILE DOING NEGATIVE 'G'S', THEN NOSE LOCKED D	OWN WITH GREEN LIGHT.  FOUND LEFT MAIN GEAR RETRACT CYLINDER WITH A BLOWN SEAL.  LEAKING BAD WHEN PRESSURE PUT ON IT.  A	LL OF THE SYSTEM PRESSURE WENT TO THE BAD ACTUATOR.  AIRCRAFT LANDED WITHOUT FURTHER INCIDENT.			1	L	7	2 	3O				1A10    					 
1999051400120	19990514	00120	CE  	1999	5	14	99ZZZX1930       	1	19990427	G	3230	404188959	GEAR            		804188500613	BEECH 	18    	G18S        	1151010	CE  										MLG	WORN            	E				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CL	CLIMB          	1			GL	13	103AF	13524				BA526				PILOT TOOK OFF, SELECTED GEAR UP AND GEAR MADE LOUD RUMBLE SOUND.  MAIN CIRCUIT BREAKER TRIPPED.  GEAR WAS MANUALLY CRAC	KED DOWN.  UPON INSPECTION, FOUND BRASS GEAR IN GEARBOX WORN BAD; ALONG WITH SEVERAL TEETH BROKEN.					1	L	7	2 	3R				A765    					 
1999051400122	19990514	00122	CE  	1999	5	14	99ZZZX1932       	1	19990422	G	7120	9691001061	MOUNT           			BEECH 	58    	58          	1152740	CE  										LT/RT	CHAFED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	707PW	4779 				TH1106				CROSS MEMBER HAS HOLE AND WORN SPOT WHERE COOLING BLAST TUBE PASSES THROUGH MOUNT.  REPLACED MOUNT AND CLAMP COOLING BLA	ST TUBE TO MOUNT.  BEECH TECHS SAY ONLY 10 PERCENT THICKNESS LOSS.  TUBE THICKNESS .041 INCH.  SUBMITTER STATED THIRD MO	UNT FOUND.				1	L	7	2 	3O				3A16    					 
1999051400123	19990514	00123	CE  	1999	5	14	99ZZZX1933       	1	19990410	G	2731		CONTROL CABLE   			BEECH 	35    	V35         	1151538	CE  										ELEVATOR	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NE	01	6264V					D8596				FOUND LEFT ELEVATOR TRIM TAB CONTROL CABLE IMPROPERLY INSTALLED.  SUBMITTER STATED CABLE ENDS ARE NOT IDENTIFIED AND CAN	 BE EASILY INSTALLED IN WRONG POSITION CAUSING CABLE CHAFING AND INCORRECT TAB MOVEMENT.					1	L	7	1 	3O			 	3A15    					 
1999051400124	19990514	00124	CE  	1999	5	14	99ZZZX1934       	1	19990413	G	2910	LW12540	ADAPTER         	ARO         	21240       	BEECH 	65    	65          	1152802	CE  										HYDRAULIC PUMP	CRACKED         	G	P			K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			GL	15	5078U				769	LF32				OIL LEAK WAS FOUND AT THE REAR OF ENGINE.  AFTER INSPECTION, AN OBVIOUS CRACK WAS SEEN ON ADAPTER FLANGE.  ADAPTER FLANG	E SHOULD BE REINFORCED TO PREVENT FAILURE OF FLANGE.  THIS OPERATOR HAS HAD THIS FAILURE OCCUR BEFORE.					1	L	7	2 	3O				3A20    					 
1999051400125	19990514	00125	SW  	1999	5	14	99ZZZX1935       	1	19990329	G	5711		SPAR            			BBAVIA	8     	8GCBC       	1220803	SW  										LT/RT WING	CRACKED         	B			CXNR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	05	4109Y	2176 				23176				DURING AN INSPECTION OF THE LEFT AND RIGHT WING SPARS TO C/W AD 98-05-04, BOTH LEFT AND RIGHT SPARS WERE FOUND CRACKED I	N THE EXACT LOCATIONS AS LISTED IN THE AD.  THE CRACKS DID NOT GO CLEAR THROUGH THE SPAR.  SPARS WERE SENT TO CHAMPION A	CFT FOR FURTHER INSPECTION.				1	H	7	1 	3O				A21CE   					 
1999051400126	19990514	00126	SO  	1999	5	14	99ZZZX1936       	2	19990426	G	8530		CYLINDER        			BLANCA	17    	1730A       	1220433	GL  	CONT  	O520  	IO520K      	17032	SO  					ENGINE	LOOSE           	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	11	4058B	421  				7830861	557341			ENGINE LOG ENTRY JANUARY 3, 1991, FOR REMOVAL AND REPLACEMENT OF ALL 6 ENGINE CYLINDERS.  CYLINDERS INSTALLED WERE CERMI	CRON CYLINDERS, FLANGES WERE PAINTED ORANGE.  AIRCRAFT EXPERIENCED ENGINE FAILURE DUE TO NR 2 CYLINDER LOOSENED FOR THE 	ENGINE CASE.  THIS WAS DUE TO PAINTED NUT SEATS.  SB, TELEDYNE CONTINENTAL, NR SB 96-12, PAGE 5 OF 7, HAS WARNING OF PAI	NTING CYLINDER FLANGE IN NUT SEATS, SKIRT OR FLANGE.  SB WAS NOT IN EFFECT IN 1991, WHEN THE WORK WAS ACCOMPLISHED.  AIR	CRAFT HAD ONLY 400 HOURS SINCE OVERHAUL.		1	L	7	1 	3O	3	O		A18CE   	E5CE				 
1999051400129	19990514	00129	SO  	1999	5	14	99ZZZX1937       	1	19990428	G	5740		FITTING         			PIPER 	PA28  	PA28180     	7102808	SO  										WING	CORRODED        	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	11	7454W					281343				DURING EXECUTION OF PIPER SB NR 977 TITLED 'INSPECTION OF WING REAR ATTACH FITTING AND ADDITION OF INSPECTION ACCESS PAN	ELS', CORROSION DAMAGE WAS DISCOVERED ON THE FORWARD FACE OF THE WING REAR ATTACH FITTINGS NEAR THE FLOOR LINE.  (P/N 62	488-02 AND P/N 62488-03).  FURTHER INSPECTION REVEALED THE FRAME MEMBER BENEATH THE TWO FITTINGS (P/N 62695-03 AND STA 1	28.737) WAS ALSO DAMAGED.  ALL DAMAGED PARTS WERE REPLACED.			1	L	7	1 	3O				2A13    					 
1999051400130	19990514	00130	SO  	1999	5	14	99ZZZX1938       	1	19990118	G	3211	67054003	TRUNNION        			PIPER 	PA32  	PA32RT300   	7103215	SO  										MLG	FAILED          	B	P			O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	39921				11109P	32R7887167				LANDING GEAR TRUNNION FAILED.						1	L	7	1 	3O				A3SO    					 
1999051400131	19990514	00131	SO  	1999	5	14	99ZZZX1939       	1	19990428	G	2560	A883512	SEAT            			PIPER 	PA28  	PA28180     	7102808	SO  										COCKPIT	BENT            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	11	7454W					281343				FRONT ROLLERS OF THE RIGHT FRONT SEAT ASSY WERE BINDING ON THE TRACK FORCING THE SEAT AFT BY PUSHING ON THE SEAT BACK CA	USING THE TUBULAR FRAME BETWEEN THE LEGS TO BEND; GIVING THE SEAT A RECLINED POSTURE.  THE SEAT FRAME WAS STRAIGHTENED, 	AND REINFORCED IN THE WEAKENED AREA.				1	L	7	1 	3O				2A13    					 
1999051400132	19990514	00132	SO  	1999	5	14	99ZZZX1940       	1	19990428	G	5320		WEB             		6255704     	PIPER 	PA28  	PA28180     	7102808	SO  										SEAT TRACK	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	11	7454W					281343				INTERGRANULAR CORROSION WAS DISCOVERED ON THE WEB AND LOWER PORTIONS OF THE SEAT TRACKS.  ALL FOUR SEAT TRACKS WERE REPL	ACED.					1	L	7	1 	3O				2A13    					 
1999051400133	19990514	00133	CE  	1999	5	14	99ZZZX1941       	1	19990428	G	7160	CM321118A220	DUCT            			CESSNA	310   	310Q        	2074242	CE  										AIR INTAKE	FAILED          	B			GSTR	A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			SW	13	100TG	2296 				310Q1150				DURING TAKEOFF, EXPERIENCED LOSS OF POWER ON THE ELFT ENGINE.  WHEN THE POWER LEVER WAS REDUCED, THE ENGINE WANTED TO RU	N BETTER.  AN UNEVENTFUL LANDING WAS MADE.  THE 4.25 INCH DUCT FROM THE WING LEADING EDGE TO THE ENGINE COMPARTMENT WAS 	DETERIORATED AND ONE PLY OF THE DUCT WAS BLOCKING AIR FLOW TO THE INDUCTION SYSTEM MAKING THE ENGINE RUN EXTREMELY RICH.				1	L	7	2 	3O				3A10    					 
1999051400134	19990514	00134	SW  	1999	5	14	99ZZZX1942       	1	19990322	G	3221	14534117	FORK            			TMPSON	NAVION	NAVIONH     	6150122	SW  										NLG	SEPARATED       	G				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			GL	15	2549T	3115 				NAV42549				ON LANDING AT RED WING MUNICIPLE AIRPORT, THE NOSE GEAR FORK BROKE, DEPARTED AIRCRAFT, AND NOSE STRUT COLLAPSED.  FOUND 	WEAR MARKS ON FORK ATTACH POINT.  PILOT REPORTED NOSE WHEEL SHIMMY PRIOR TO INCIDENT.					1	L	7	1 	3O				A782    					 
1999051400135	19990514	00135	SO  	1999	5	14	99ZZZX1943       	1	19990415	G	2560	MDA2732	SEAT BELT       			PIPER 	PA28  	PA28140     	7102802	SO  										COCKPIT	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	1689J	30   				2824092				WHEN C/W AD 98-25-10, THREE OF THE FOUR BELT LATCHES FAILED THE INSPECTION REQUIRED BY THE AD.  THIS AD PERTAINS TO CERT	AIN MODELS OF BELTS MADE BY AIRCRAFT BELT INC.  BELTS WERE RETURNED TO MANUFACTURER FOR RE-WORK OR REPLACEMENT.					1	L	7	1 	3O				2A13    					 
1999051400136	19990514	00136	EA  	1999	5	14	99ZZZX1944       	2	19990308	G	7314	5006050	COUPLING        								PWA   	PT6   	PT6A20      	52043	EA  					FUEL PUMP	CRACKED         	B	S		XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01										FATIGUE CRACKS DETECTED IN MAGNETIC INSPECTION.											3	T			E4EA				 
1999051400138	19990514	00138	CE  	1999	5	14	99ZZZX1946       	1	19990318	G	2820	050011831	LINE            			CESSNA	172   	172P        	2072436	CE  	LYC   	O320  	O320D2J     	41508	EA  					FUEL SYSTEM	MISINSTALLED    	H				K				NONE                    				K	W		FLUID LOSS                	INADEQUATE Q C            		IN	INSP/MAINT     	1			EA	07	66717	2400 				17275991				THE MAIN FUEL SUPPLY LINE WAS IMPROPERLY INSTALLED.  THE RUDDER CONTROL CABLE WAS ROUTED BENEATH THE FUEL LINE IN SUCH A	 WAY TO BE RUBBING DIRECTLY ON THE LINE.  WHEN DISCOVERED, THE LINE WAS CUT MORE THAN HALFWAY THROUGH, BUT ONLY SLIGHTLY	 LEAKING.				1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999051400139	19990514	00139	SO  	1999	5	14	99ZZZX1947       	2	19990412	G	8550	CH48109	FILTER          			CESSNA	310   	310Q        	2074242	CE  	CONT  	O520  	TSIO520E    	17040	SO  					ENGINE OIL	LEAKING         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	17	69622				F03J261	310Q0904				ROUTINE OIL CHANGE, FILTER STARTED LEAKING AT BASE.  LOOKS LIKE CRACK OR SMALL PERFORATIONS WHERE HOUSING IS CRIMPED/WEL	DED TO END PLATE.  INSPECTED INVENTORY, NONE OTHERS FOUND.  (KEYSTONE AERIAL SURVEYS).					1	L	7	2 	3O	3	O		3A10    	E8CE				 
1999051400140	19990514	00140	CE  	1999	5	14	99ZZZX1948       	1	19990311	G	3230	98820022	SECTOR GEAR     		98820152    	CESSNA	172   	172RG       	2072438	CE  										RT MLG	CRACKED         	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	07	5255U	7480 			5637	172RG0304				RIGHT MAIN GEAR FAILED TO RETRACT IN-FLIGHT.  UPON INSPECTION, THE MAIN GEAR ACTUATOR WAS FOUND CRACKED.  THE PINION GEA	R WITHIN THE HOUSING WAS DRIVEN OUT BY THE SECTOR GEAR.  THE SECTOR GEAR TEETH WERE WORN, POSSIBLY ENOUGH TO CAUSE THE G	EARS TO SKIP.  SUBMITTER STATED, IF SO, IT WOULD BE DRIVEN OUT THROUGH THE HOUSING.				1	H	7	1 	3O				3A17    					 
1999051400184	19990514	00184	SW  	1999	5	14	99ZZZX1950       	1	19990219	G	6210	206015001107	BLADE           			BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	DEBONDED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	362AL	2353 			A1641	51471				DURING DAILY INSPECTION FOUND CORROSION AND DEBONDING AT SKIN/SPAR BENEATH LOWER GRIP FINGER DOUBLER.						1	G	7	1 	3U				H2SW    					 
1999051400185	19990514	00185	SW  	1999	5	14	99ZZZX1951       	1	19990412	G	6230	206040535105	MAST            		20604004105 	BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2025G	2491 			N2450	45690				MAST REMOVED FOR OVERHAUL.  FOUND UPPER SPLINES CORRODED AND WORN BEYOND LIMITS.  RETIREMENT LIFE 5,000 HOURS.						1	G	7	1 	3U				H2SW    					 
1999051400186	19990514	00186	SW  	1999	5	14	99ZZZX1952       	1	19990404	G	6210	206015001107	BLADE           			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	206SL	1530 			A2728	45245				DURING DAILY INSPECTION FOUND TRAILING EDGE EXTRUSION HEAVILY CORRODED.						1	G	7	1 	3U				H2SW    					 
1999051400187	19990514	00187	SW  	1999	5	14	99ZZZX1953       	1	19990412	G	6220	206011120103	TRUNNION        		206011100159	BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3184P	538  			A3417	45774				MAIN ROTOR REMOVED FOR INSPECTION, FOUND CORROSION ON SPLINES.  PITTING CORROSION IN SPLINES.  TRUNNION SCRAP 538.4 HOUR	S.					1	G	7	1 	3U				H2SW    					 
1999051400188	19990514	00188	EU  	1999	5	14	99ZZZX1954       	1	19990217	G	7921		COOLER          		308J81      	BOLKMS	105   	BO105S      	5626006	EU  										OIL SYSTEM	MISOVERHAULED   	B		A	AC2R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	5366Y					S782				INSTALLED OIL COOLER AT ZERO TSO TO REPLACE A LEAKING COOLER.  DURING FIRST RUN-UP, TRANSMISSION OIL PRESSURE IMMEDIATEL	Y EXCEEDED MAXIMUM ALLOWABLE LIMITS.  BY PERFORMING A BORESCOPE INSPECTION, LOOSE AND BUILT UP CARBON WAS DISCOVERED IN 	THE COOLER.  RELEASED CARBON ALSO CONTAMINATED THE TRANSMISSION CLOGGING UP THE OIL JETS AND DRIVING UP THE PRESSURE.  F	URTHER INVESTIGATION REVEALED ALL ENGINE AND TRANSMISSION FITTINGS AND LINES WERE CONTAMINATED WITH CARBON PARTICLES.  T	RANSMISSION WAS SUBSEQUENTLY TORN DOWN, CLEANED AND INSPECTED, AND ALL LINES.  FILTERS AND OIL TANKS HAD TO BE CLEANED, 	FLUSHED, INSPECTED AND RE-INSTALLED.	1	G	7	2 	3U				H3EU    					 
1999051400195	19990514	00195	SO  	1999	5	14	99ZZZX1956       	1	19990318	G	2820	1159P201377	VENT            			GULSTM	G1159 	G1159A      	3970109	SO  										RT WING	CRACKED         	B			COZR	J				DUMP FUEL               				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	27	684AT	7754 				339				AFTER TAKING ON A FULL LOAD OF FUEL, FUEL WAS LEAKING FROM THE RIGHT HAND VENT.  INSPECTION REVEALED A CRACK RUNNING 2.5	0 INCHES ALONG THE WELD THAT ATTACHES THE VENT TUBE TO THE VENT CASTING WITH UPWARD CRACKS APPROXIMATELY 1 INCH LONG ON 	EITHER SIDE.  THE CRACK IS BELIEVED TO HAVE BEEN INDUCED DUE TO LACK OF CLEARANCE BETWEEN THE VENT TUBE AND WS 16.  THE 	REPLACEMENT VENT ASSY HAD TO BE COLD RE-WORKED IN THAT AREA TO CLEAR THE INTERFERENCE.			2	L	7	2 	4F				A12EA   					 
1999051400363	19990514	00363		1999	5	14	99ZZZX1960       	1	19990322	G	5320	6785234	SUPPORT         																	FUSELAGE	CRACKED         	B	S		XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01					183					DETECTED DURING PENETRANT INSPECTION - CRACK IN FUSELAGE SUPPORT.  INSPECTED ON P.O. NR 26210 FROM PACIFIC SKY SUPPLY, I	NC.																		 
1999051400364	19990514	00364		1999	5	14	99ZZZX1961       	1	19990308	G	5320	49591941	BUSHING         																	FUSELAGE	CRACKED         	B	S		XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01										MAGNETIC INSPECTION DETECTED A FATIGUE CRACK ON INSIDE DIAMETER OF BUSHING.  PROCESSED ON THRUST AIR, INC., P.O. NR 1629	8.																		 
1999051400365	19990514	00365	CE  	1999	5	14	99ZZZX1962       	1	19990416	G	7602	646673	SHROUD          			BEECH 	58    	58          	1152740	CE  										MIXTURE CONTROL	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	7353R	67   				TH486				MIXTURE CONTROL COOLING SHROUD ASM MOUNTING TABS FAILED CAUSING SHROUD TO CUT INTO FUEL PRESSURE HOSE ASM (P/N 635218545	40.00).  THE DEFECT WAS FOUND DURING THE AIRCRAFT'S 100-HOUR INSPECTION.   THE ENGINE WAS ONLY IN SERVICE 67 HOURS AT TH	E TIME OF INSPECTION.				1	L	7	2 	3O				3A16    					 
1999051400366	19990514	00366	CE  	1999	5	14	99ZZZX1963       	1	19990423	G	2810	101120076601	FUEL CELL       			BEECH 	200   	B200        	1152922	CE  										FUSELAGE	MISMANUFACTURED 	D				K				NONE                    				W	K		INADEQUATE Q C            	FLUID LOSS                		IN	INSP/MAINT     	1			SO	14	975SC					BB806				FUEL CELL MANUFACTURED WITH MOUNTING HOLES MISALIGNED CAUSING FUEL LEAK.						1	L	7	2 	4T				A24CE   					 
1999051400367	19990514	00367	CE  	1999	5	14	99ZZZX1964       	1	19990430	G	2730	H64B6	HARNESS         			BEECH 	90    	C90         	1152913	CE  										FUSELAGE	CHAFED          	B	P	A		A				UNSCHED LANDING         				F			FLT CONT AFFECTED         			CL	CLIMB          	1			SW	01	94HB					LJ904				AIRCRAFT WAS ON A LOCAL TRAINING FLIGHT.  IMMEDIATELY AFTER TAKEOFF, PILOT TRAINEE REPORTED NO RESPONSE TO ELEVATOR INPU	TS.  ACFT APPROX 200 FEET AGL AND AIRSPEED WAS 120 KNOTS.  INSTRUCTOR PILOT ASSUMED COMMAND AND MADE AN IMMEDIATE LANDIN	G USING ELEVATOR TRIM.  ELEV DOWN CONTROL CABLE WAS BURNED IN TWO AND ELECTRICAL WIRE (PN H64B6) RUNNING FROM NORMAL ELE	CTRIC HEAT RELAY TO AIR CONDITIONER CHAFING.  FOUND ANOTHER ELEC WIRE (PN H64A6) LOCATED IN SAME AREA CHAFING ON BELLCRA	NK.  THESE ELECTRICAL WIRES AND RELAYS ARE LOCATED UNDER THE FLOORBOARD BENEATH PILOT'S SEAT.  NOTE:  SUBMITTER STATED T	HE ONLY TIME ONE CAN SEE INTERFERENCE BETWEEN BELLCRANK AND ELEC WIRE IS WHEN ELEVATOR IS IN THE FULL AFT POSITION.	1	L	7	2 	3T				3A20    					 
1999051400368	19990514	00368	CE  	1999	5	14	99ZZZX1965       	1	19990302	G	3222	998201005	STRUT           			BEECH 	90    	E90         	1152914	CE  										NLG	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	28MS					LW100				DURING REPLACEMENT OF WIPER RING AND SCRAPER RING ON NOSE LANDING GEAR, REMOVED PAD P/N 104036D3ZM0908 TO REPLACE.  SEVE	RE CORROSION NOTED INSIDE OF UPPER CYLINDER BEHIND PAD.  SUSPECT MOISTURE BEING TRAPPED IN PAD AS CAUSE OF CORROSION.					1	L	7	2 	3T				3A20    					 
1999051400370	19990514	00370	SO  	1999	5	14	99ZZZX1967       	1	19990414	G	5411	12003852001	FRAME           			EMB   	120   	EMB120RT    		SO  										LT/RT NACELLE	CRACKED         	B			WVER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	09	502AS					120274				DURING ROUTINE MAINTENANCE CHECKS, CRACKS WERE FOUND ON BOTH ENGINE NACELLE NR 1 FRAMES.  ON THE LT FRAME, THE CRACK IS 	LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB BETWEEN THE TOP OUTBOARD MOUNTING BOLT HOLE AND THE OUTBOARD EDGE OF THE	 FRAME.  ON THE RT FRAME, THE CRACK IS LOCATED IN BETWEEN THE TOP OUTBOARD MOUNTING BOLT HOLES ON THE STIFFENING WEB.  S	UBMITTER RECOMMENDED REPLACING BOTH FRAMES AND CONTINUE MONITORING IAW EXISTING MAINTENANCE CHECKS.			2	L	7	2 	4T			RT	A31SO   					 
1999051400371	19990514	00371	CE  	1999	5	14	99ZZZX1969       	1	19990312	G	5520	380210417005	SUPPORT         			RKWELL	NA265 	NA26580     	7630108	CE  										LT/RT ELEVATORS	CRACKED         	B	P	A	WK4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	424R	7888 				380015				DURING THE COURSE OF A ROUTINE ELEVATOR BALANCE INSPECTION, BOTH LEFT AND RIGHT ELEVATOR INBOARD HINGE BEARING SUPPORTS 	WERE FOUND CRACKED THROUGH THE BEARING SUPPORT RING AREA OF THE CASTING.  BOTH LEFT AND RIGHT SUPPORTS WERE REMOVED AND 	REPLACED WITH NEW PARTS.  THESE CASTINGS CANNOT BE INSPECTED WITHOUT REMOVING THE ELEVATOR.				2	L	7	2 	4F				A2WE    					 
1999051400373	19990514	00373	EU  	1999	5	14	99ZZZX1971       	1	19990416	G	2730		SEAL            	LUCAS       	614MK2      	BRAERO	DH125 	BAE125800A  	1500285	EU  										TE FLAP	FAILED          	B			PJYR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			GL	15	800PA	3416 			614C477	NA0438				DURING ROUTINE INSPECTION, THE FLAP CONTROL UNIT OIL RESERVOIR WAS FOUND DRY.   WHEN OIL (5606 HYDRAULIC FLUID) WAS ADDE	D IT IMMEDIATELY STARTED RUNNING OUT THE DRIVESHAFT SEAL.  THE FILLER CAP IS ALSO A VENT.  THE VENT WAS FOUND PLUGGED. A	T ALTITUDE, A PRESSURIZED OIL RESERVOIR COULD BLOW A SEAL.  THERE WAS NO INSTRUCTION IN THE INSPECTION PROCEDURE TO CHEC	K THE VENT.  LANDINGS, 2,604.			2	L	7	2 	4F			RT	A3EU    					 
1999051400376	19990514	00376	SO  	1999	5	14	99ZZZX1974       	1	19990424	G	5102		FLEX NET        			BALWKS	FIREFY	FIREFLY8B15 		SO  										BALLOON	MISMANUFACTURED 	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	01	3210R					F8B501				THE FLEX NET STRIP IS ABRADING THE ADJOINING BALLOON FABRIC IN  MANY AREAS.  IT APPEARS THE FLEX NET TAPE HAS BEEN CUT W	ITH A HOT KNIFE THAT IS LEAVING ROUGH EDGES.  TO REMEDY, CUT WITH SONIC CUTTER.  THIS CONDITION WAS FOUND DURING AN ANNU	AL INSPECTION.				1	B	0	0 	3O			RT	A14SO   					 
1999051400377	19990514	00377	SO  	1999	5	14	99ZZZX1975       	1	19990416	G	3230	4198300	HOOK            			PIPER 	PA31  	PA31350     	7103110	SO  										MLG HOOK ASSY	LACK OF LUBE    	D				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			SO	11	54307	10000				317405233				NO LEFT GREEN LIGHT, DOWN INDICATION.  LUBED DOWNLOCK HOOK ASSY.  ALSO, CLEANED AND LUBED.  HOOK DID NOT ENGAGE ALL THE 	WAY.  LACK OF LUBRICATION.  EXHAUST GASSES DRY UP LUBE.  ALSO, WASHING OF GEAR REMOVED LUBRICANT.					1	L	7	2 	3O				A20SO   					 
1999051400378	19990514	00378	CE  	1999	5	14	99ZZZX1976       	1	19990415	G	2823		SELECTOR VALVE  			CESSNA	172   	172L        	2072432	CE  	LYC   	O320  	O320E2D     	41508	EA  					COCKPIT	MALFUNCTIONED   	D				A				UNSCHED LANDING         				Y			ENGINE STOPPAGE           			NR	NOT REPORTED   	1			WP	27	3985Q					17260085	RL2469327A			FUEL SELECTOR VALVE INSTALLED.  APPROX 8 GALLONS OF FUEL WERE ADDED TO EACH TANK AND FUEL SELECTOR AND FUEL LINES WERE C	HECKED FOR LEAKS WITH SELECTOR IN ALL DETENTS.  DURING OPS CHECK, ENG WAS RUN APPROX 5 MINUTES WITH EACH LEFT, RIGHT,  A	ND BOTH DETENTS SELECTED.  NO DISCREPANCIES NOTED AND ACFT APPROVED FOR RETURN TO SERVICE.  ENG QUIT  FROM FUEL STARVATI	ON AFTER APPROX 2.5 HRS ON NEXT FLT, AND A DEADSTICK LANDING WAS SUCCESSFUL.  UPON INVEST, FND SELECTOR VALVE WAS NOT AL	LOWING FUEL FLOW FROM LT TANK, BUT WAS ALLOWING NORMAL FLOW FROM RT TANK WHEN IN THE 'BOTH' POSITION.  FUEL FLOWED NORMA	LLY FROM LT TANK WITH 'LEFT' POSTION SELECTED AND FROM RT TANK WITH 'RIGHT' POSITION SELECTED.	1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999051400379	19990514	00379	CE  	1999	5	14	99ZZZX1977       	1	19990106	G	2750	500000862	CONTROL CABLE   			CESSNA	421   	421C        	2076016	CE  										TE FLAP	BROKEN          	G	P	A		A				UNSCHED LANDING         				O			OTHER                     			NR	NOT REPORTED   	1			CE	01	265RG	7700 				421C0833				WHEN COMPLETING REPAIRS TO FLAP SYS AFTER PILOT ENCOUNTERED A FULL FLAP SPLIT WITH RT FLAP ALL THE WAY RETRACTED AND LT 	FLAP AT FULL EXTENSION, FOUND RT FLAP DOWN CABLE P/N 5000008-62 FRAYED AND BROKEN 2.5 INCHES INBD OF WHERE FLAP PRE-SELE	CT INSTALL CABLE CLAMP WAS INSTALLED.  CABLE FRAYED AND BROKE BETWEEN DETAIL B NR 39 PULLEY BRACKET AND DETAIL C NR 14 C	ABLE CLAMP.  WHEN THIS HAPPENED, FLAP WENT INTO FULL RETRACTION AND PULLED PRE-SELECT FLAP IND INTO FULL UP POSITION WHI	CH MADE FLAP SELECTOR USELESS.  PILOT WAS ON DESCENT FOR LANDING AND THIS PITCHED ACFT INTO A STEEP RT BANK.  PILOT REGA	INED CONTROL BY GIVING FULL LT AILERON RUNNING ENGINES TO FULL POWER AND RETRACTING LANDING GEAR.   UNEVENTFUL LANDING.	1	L	7	2 	3O			 	A7CE    					 
1999051400381	19990514	00381		1999	5	14	99ZZZX1979       	1	19990429	G	3244	226K084	TIRE            	GOODYEARAERO	31399       															MLG	MISMANUFACTURED 	B	L		G7CR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	05										EXPOSED WIRE STRANDS ON THE INNER-MOST BEAD OF THE TIRE HAS CAUSED DAMAGE TO THE WHEEL ASSY.  ON ONE INSTANCE THIS CAUSE	D REJECTION OF THE ENTIRE WHEEL ASSY.  SUBMITTER STATED WHEN TIRE PRODUCED, IT APPEARED THIS AREA WAS NOT CUT CLEAN LEAV	ING EXPOSED WIRE.																	 
1999051400382	19990514	00382	CE  	1999	5	14	99ZZZX1980       	1	19990101	G	7921	1E1884639171	OIL COOLER      			CESSNA	206   	206CESSNA   	2073302	CE  										OIL SYSTEM	LEAKING         	B			RF3R	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			WP	23					0979					PART RECEIVED PREVIOUS EPOXY REPAIRS.  THE EPOXY FAILED AFTER BEING INSTALLED IN UNIT DURING OVERHAUL IN 1996.  P.O.C.S.	 W/O NR 20712.  PREVIOUS O/H BY DRAKE AIR W/P NR 23220 8-29-96.					1	H	7	1 	3O				A4CE    					 
1999051400384	19990514	00384	GL  	1999	5	14	99ZZZX1982       	3	19990420	G	6111	A1983	GUIDE LUGS      			STOLAM	RC3   	RC3         	3080203	NM  						HARTZL	HCA3V	HCA3V203    	GL  	PROPELLER	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	27	5166B					1000		FCA57		THE A-1983 GUIDE LUGS (SHOULDER BUSHINGS) ARE INSTALLED BACKWARDS SO THAT 60 POUNDS OF SPRING PRESSURE IS INVERTED ON A 	SNAP RING.  THE FIX IS TO REVERSE IT LIKE THE FLANGED MODEL OF THIS PROPELLER.					1	H	7	1 	3O			RC	A769    		5	C	P6EA	 
1999051400385	19990514	00385	EU  	1999	5	14	99ZZZX1983       	3	19990427	G	6110		FERRULE         													CNPSL	AW2	AW2*        	EU  	PROPELLER	CRACKED         	B			NWOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05								W353130		FERRULE IS CRACKED IN THE FIRST THREAD.  N.E.A.S. W/O 5075.																6	C	P9EU	 
1999051400386	19990514	00386		1999	5	14	99ZZZX1984       	1	19990423	G	2560	KS9P0101	LIFE VEST       	EAAEROMARINE																CABIN	FAILED          	B			KQ1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	07					C07725					LIFE PRESERVER FAILED MANUFACTURER'S RECOMMENDED 2 PSI CELL PRESSURE TEST IAW MANUAL 25-60-1, PAGE 304, PARA C2.  DOM: S	EPT 1981.																		 
1999051400387	19990514	00387		1999	5	14	99ZZZX1985       	1	19990424	G	2560	KS9P010179	LIFE VEST       	EAAEROMARINE																CABIN	FAILED          	B			KO1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	25					A85953					LIFE PRESERVER FAILED MANUFACTURER'S RECOMMENDED 2 PSI CELL PRESSURE TEST IAW MANUAL 25-60-1, PAGE 304, PARA C2.  DOM: J	UN 1979.																		 
1999051400388	19990514	00388		1999	5	14	99ZZZX1986       	1	19990423	G	2560	KS9P0101	LIFE VEST       	EAAEROMARINE																CABIN	FAILED          	B			KO1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	25					C07609					LIFE PRESERVER FAILED MANUFACTURER'S RECOMMENDED 2 PSI CELL PRESSURE TEST IAW MANUAL 25-60-1, PAGE 304, PARA C2.  DOM: S	EP 1981.																		 
1999051400389	19990514	00389	CE  	1999	5	14	99ZZZX1987       	1	19990427	G	2897	746411	WIRE            			CESSNA	310   	310R        	2074245	CE  										FUEL PUMP	SHORTED         	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	11		220  				310R0071				PILOT DISCREPANCY:  LEFT LANDING LIGHT CIRCUIT BREAKER TRIPPED, RESET TO NO AVAIL.  INVESTIGATION REVEALED SHIELDED POWE	R WIRE SHORTED TO SHIELD AT CRIMP ENTERING PUMP, EVIDENCE OF EXCESSIVE HEAT.					1	L	7	2 	3O			 	3A10    					 
1999051400390	19990514	00390	CE  	1999	5	14	99ZZZX1988       	1	19990407	G	3230	582212715	SUPPORT         			CESSNA	441   	441         	2076020	CE  										LT MLG	CRACKED         	B	S		WTXR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	88834	5757 				4410269				DURING A PHASE INSPECTION, FOUND A CRACK IN THE OUTBOARD END OF THE LEFT MAIN GEAR UPLOCK HOOK SUPPORT BRACKET, ANGLE, W	HICH ATTACHES TO THE FORWARD SIDE OF THE FORWARD WING SPAR WEB.  CRACKS ORIGINATE AT THE OUTBOARD HILOK HOLE AND EXTENDS	 FOR APPROXIMATELY 1.1 INCH.  INSTALLED NEW ANGLE.				1	L	7	2 	3T			RT	A28CE   					 
1999051400391	19990514	00391	SO  	1999	5	14	99ZZZX1989       	2	19990222	G	8530		CYLINDER        								CONT  	O520  	IO520*      	17032	SO  					ENGINE	MISMANUFACTURED 	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05					09098762048					NATIONAL VENDOR SUPPLIED A NEW FACTORY IO520 CYLINDER.  INSPECTION OF CARTON, NO SIGNS OF DAMAGE.  INSPECTION OF CYLINDE	R SHOWS WHAT APPEARS TO BE A HAMMER BLOW TO THE INTAKE ROCKER BOSS MAKING A NEW CYLINDER SCRAP.  VENDOR SUPPLIED ANOTHER	 NEW CYLINDER AND INSPECTION SHOWED ROCKER ARMS WOULD NOT FIT INTO THE BOSSES.  UNFINISHED WORK.  VENDOR SUPPLIED A 3RD 	CYLINDER - (NEW).								3	O			E5CE				 
1999051400392	19990514	00392	SO  	1999	5	14	99ZZZX1990       	1	19990417	G	2810		FUEL CAP        			PIPER 	PA23  	PA23250     	7102308	SO  										FUEL CELL	FAILED          	B			CQVR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CE	01										SUBMITTER STATED THESE FUEL CAPS FAILED IN A TIME FRAME ANYWHERE FROM 2 WEEKS TO APPROXMATELY 2 MONTHS.						1	L	7	2 	3O				1A10    					 
1999051400393	19990514	00393	CE  	1999	5	14	99ZZZX1991       	1	19990426	G	2810	79C1	FUEL DRAIN      			CESSNA	441   	441         	2076020	CE  										LT WING	CORRODED        	D		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	25	15DB	4614 				4410278				FOUND FUEL DRAIN ON LEFT WING WITH CENTER PIECE, THAT PUSHES UP TO DRAIN FUEL, HANGING DOWN APPROXIMATELY .1250 INCH.  R	EMOVED VALVE AND FOUND SEVERELY CORRODED INSIDE ALLOWING CENTER PIECE WHICH IS SPRING LOADED TO GO BEYOND ITS INTERNAL S	TOPS.  IF NOT CORRECTED, DRAIN COULD CAUSE LARGE AMOUNTS OF FUEL TO LEAK OUT.  (NOTE:  CENTER PIECE WAS CORRODED ONE-FOU	RTH WAY THROUGH).			1	L	7	2 	3T			RT	A28CE   					 
1999051400394	19990514	00394	EA  	1999	5	14	99ZZZX1992       	2	19990326	G	8530		CYLINDER HEAD   			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	LTIO540J2BD 	41533	EA  					ENGINE	CRACKED         	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	35	4502L		193  			318052178	L43868A			ECI (ENGINE COMPONENTS INC) C/W CYLINDER RECONDITION.  NDT HEAD AND INSTALL NEW BARREL.  HEAD FAILED IN-FLIGHT.  POSSIBL	E CAUSE, UNDETECTED INTERNAL CRACK AT TIME OF RECONDITION.  CYLINDER IDENTIFIED AS CL 40/STF 405A.					1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999051400395	19990514	00395	SO  	1999	5	14	99ZZZX1993       	1	19990422	G	3230	9582900	LINK            			PIPER 	PA34  	PA34200T    	7103406	SO  										NLG	MISADJUSTED     	H				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			GL	21	9798C	500  				347870222				NOSE GEAR COLLAPSED DURING LANDING ROLL-OUT.  AIRCRAFT WAS PLACED ON JACKS AND NUMEROUS GEAR CYCLES WERE PERFORMED.  LAN	DING GEAR LOCKED UNDER NORMAL AND EMERGENCY EXTENSION CYCLES.  DOWNLOCK LINK APPEARED TO BE ADJUSTED TOO SHORT TO ENSURE	 DRAG BRACE REMAINED OVER CENTER IF PRESSURE WAS APPLIED TO OVER CENTER PIVOT AREA.  DRAG BRACE WOULD OVER CENTER WHEN H	AND PRESSURE WAS APPLIED.  BOLT ATTACHING UPPER END OF LINK WAS ALSO BENT.  IT IS NOT KNOW IF THIS HAPPENED DURING COLLA	PSE OR DURING INITIAL RIGGING APPROXIMATELY 500 HOURS EARLIER.		1	L	7	2 	3O				A7SO    					 
1999051400396	19990514	00396	WP  	1999	5	14	99ZZZX1994       	2	19990413	G	7261	31013201B	PUMP            			CASA  	C212  	C212CD      	2410209	EU  	GARRTT	TPE331	TPE33110    	01514	WP  					ENGINE OIL	CRACKED         	B			TUGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	7241E	10120	250  		P5815	318	P37540			SIGNS OF DEFECT:  LOW OIL PSI, HIGH TEMPERATURE, AND OIL TANK SPEWING OUT OIL (IT WAS BEING PRESSURIZED).  INSPECTION (D	ISASSEMBLY) REVEALED SCAVENGE PUMP WAS CRACKED.					2	H	7	2 	4T	4	T	RT	A43EU   	E4WE				 
1999051400476	19990514	00476	CE  	1999	5	14	99ZZZX1996       	1	19990318	G	7500	45A63517073	DUCT            			BEECH 	MU300 	400A        	1155402	CE  										BLEED AIR	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		997  								REPORTED DISCREPANCY STATED THAT DURING A PHASE INSPECTION, FOUND THE BLEED AIR TUBE BELLOWS WAS RUPTURED.  REPLACED THE	 DEFECTIVE TUBE.  (BEECHJET 400T - COMMERCIAL COUNTERPART BEECHJET 400A).					2	H	7	2 	4F			RT	A16SW   					 
1999051400477	19990514	00477	CE  	1999	5	14	99ZZZX1997       	1	19990316	G	7500	45A63517073	DUCT            			BEECH 	MU300 	400A        	1155402	CE  										BLEED AIR	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05										REPORTED DISCREPANCY STATED THAT THE BLEED AIR DUCT WIRE MESH HAS BLOWN.  FOUND DURING A PHASE INSPECTION.  REPLACED THE	 DEFECTIVE DUCT AND RETURNED THE AIRCRAFT TO SERVICE.   (BEECHJET 400T - COMMERCIAL COUNTERPART BEECHJET 400A).					2	H	7	2 	4F			RT	A16SW   					 
1999051400478	19990514	00478	CE  	1999	5	14	99ZZZX1998       	1	19990210	G	7500	45A63517075	DUCT            			BEECH 	MU300 	400A        	1155402	CE  										BLEED AIR	FAILED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05										REPORTED DISCREPANCY STATED THAT THE BELLOWS WAS FOUND BLOWN DURING A 1,200 HOURS INSPECTION.  THE DUCT THAT FAILED HAD 	P/N 45AS63024-13 AND P/N 00624-NH1007853-10 ON IT AND IS ONLY PART OF THE OVERALL ASSY.  REPLACED THE DEFECTIVE DUCT.  (	BEECHJET 400T - COMMERCIAL COUNTERPART BEECHJET 400A).				2	H	7	2 	4F			RT	A16SW   					 
1999051400483	19990514	00483	CE  	1999	5	14	99ZZZX2003       	1	19990407	G	5311		FRAME           			BEECH 	200   	C12F3       	1150422	CE  										BS 226/246	FAILED          	D	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01		9230 								TWO FRAME DOUBLERS WERE FOUND BROKEN AT RT AFT CABIN STA 226 AND STA 246 WL 117.  NO OTHER DAMAGE IN AREAS OF BREAKS WER	E FOUND.  NO SKIN DAMAGE WAS DETECTED.  ALL OTHER FRAMES AND DOUBLERS APPEARED NORMAL.  EACH DOUBLER HAS A PUCKER PARALL	EL TO THE BREAK.  BECAUSE OF THE PUCKER AND ABSENCE OF ANY OTHER DAMAGE, SUBMITTER SUSPECTED THE PART WAS STRESSED DURIN	G ASSY.  REPLACEMENT OF THE DOUBLERS SHOULD CORRECT THE PROBLEM.  DUE TO THE DOUBLER BEING AN INTEGRAL PART OF A PRESSUR	E VESSEL, ENGINEERING ANALYSIS MAY BE WARRANTED.		1	L	7	2 	4T			RT	A24CE   					 
1999051400484	19990514	00484	EU  	1999	5	14	99ZZZX2004       	1	19990427	G	3233	SA7670024004	HOSE            	AEROQUIP    		BRAERO	DH125 	HS125700A   	4230170	EU  										MLG ACTUATOR	MISMANUFACTURED 	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	17	564BR					NA0287				HOSES SHIPPED FROM U.K. FACILITY (AEROQUIP) SOLD TO RAYTHEON AIRCRAFT (VENDOR) ARE ONE INCH TOO SHORT.  THIS DEFECTIVE B	ATCH HAS BEEN DISTRIBUTED THROUGHOUT THE U.S.A. TO THE END USER.  IF ANY OF THSE HOSES ARE INSTALLED, INADVERTENT OPERAT	ION OF THE MLG WILL OCCUR.				2	L	7	2 	4F				A3EU    					 
1999051400490	19990514	00490	NM  	1999	5	14	99ZZZX2010       	1	19990401	G	7722	7732846	SENSOR          			BOEING	767   	7673T7      	1385201	NM  										RT ENGINE	MALFUNCTIONED   	H				A				UNSCHED LANDING         				M	J		OVER TEMP                 	WARNING INDICATION        		NR	NOT REPORTED   	1			WP	03	601EV				90117					PILOT REPORTED RIGHT ENGINE OVERHEATED.  RETURNED TO TAIPEI.  MAINTENANCE REPLACED FAN AIR TEMPERATURE SENSOR AND ZANAIR	 MODULATING VALVE PER MM 3-11-17 AND MM 36-11-16 AND PERFORMED ENGINE RUN PER MM 71-00-00.  FOUND ALL CONDITIONS NORMAL.					2	L	7	2 	4F			RT	A1NM    					 
1999051400491	19990514	00491	NM  	1999	5	14	99ZZZX2011       	1	19990401	G	7722	7738556	VALVE           			BOEING	767   	7673T7      	1385201	NM  										RT ENGINE	MALFUNCTIONED   	H				A				UNSCHED LANDING         				M	J		OVER TEMP                 	WARNING INDICATION        		NR	NOT REPORTED   	1			WP	03	601EV				890416					PILOT REPORTED RIGHT ENGINE OVERHEATED.  RETURNED TO TAIPEI.  MAINTENANCE REPLACED FAN AIR TEMPERATURE SENSOR AND ZANAIR	 MODULATING VALVE PER MM 3-11-17 AND MM 36-11-16 AND PERFORMED ENGINE RUN PER MM 71-00-00.  FOUND ALL CONDITIONS NORMAL.					2	L	7	2 	4F			RT	A1NM    					 
1999051400492	19990514	00492	NM  	1999	5	14	99ZZZX2012       	1	19990407	G	3230	65B904305	BRACE           			BOEING	747   	747132      	1384882	NM  										NR 2 MLG	CRACKED         	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	479EV					19898				DURING VISUAL INSPECTION OF NR 2 STRUT DIAGONAL BRACE, A CRACK OF .75 INCH LONG FOUND AT FORWARD LUG TOP SURFACE.  IT IS	 BELIEVED THE CRACK IS DUE TO FATIGUE.					2	L	7	4 	4F				A20WE   					 
1999051400493	19990514	00493	EU  	1999	5	14	99ZZZX2013       	1	19990427	G	3233	SA7670024004	HOSE            			BRAERO	DH125 	HS125700A   	4230170	EU  										MLG	MISMANUFACTURED 	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	17	945CE					NA0297				AEROQUIP U.K. DISTRIBUTED HIGH PRESSURE HOSES 1 INCH TOO SHORT.  HOSES SHIPPED ARE 21.6250 INCH.  CORRECT SIZE ACCORDING	 TO DRAWINGS SHOULD BE 22.6250 INCH.  RAYTHEON AIRCRAFT HAS BEEN NOTIFIED.					2	L	7	2 	4F				A3EU    					 
1999051400494	19990514	00494	SW  	1999	5	14	99ZZZX2014       	1	19990425	G	6710	A21810064603	SWITCH          			HUGHES	500N  	500N        	3027374	SW  										PILOT COLLECTIVE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	522FB	783  				LN002				PILOT TRIM SWITCH RUN-A-WAY AFT.						1	G	7	1 	3U			NC	H3WE    					 
1999051400495	19990514	00495	WP  	1999	5	14	99ZZZX2015       	1	19990504	G	6220	C1541	BEARING         			ROBSIN	R44   	R44         	7640120	WP  										M/R HUB	WORN            	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	13	7056H	814  			0519	0497				C106-5 AND C106-6 JOURNALS WORE INTO AND THROUGH THE C648-1 BEARING MATERIAL MAKING METAL-TO-METAL CONTACT.  HEAVY SHIP 	LOW FREQUENCY VIBRATION WAS NOTICED WHILE IN HOVER AND LOW COLLECTIVE INPUT.  SUBMITTER STATED POSSIBLE CAUSE IS CORROSI	ON ON JOURNALS, WORN OUT BEARING MATERIAL.				1	G	7	1 	3O				H11NM   					 
1999051400496	19990514	00496	WP  	1999	5	14	99ZZZX2016       	1	19990504	G	6220	C6481	BEARING         			ROBSIN	R44   	R44         	7640120	WP  										M/R HUB	WORN            	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	13	301AS	779  				0324				C106-5 AND C106-6 JOURNALS WORE INTO THE MAIN ROTOR HUB.  THE HUB WAS SCRAP.  SEVERE SHIP VIBRATIONS NOTICED WHEN LIGHT 	WEIGHT AND LOW COLLECTIVE INPUT.  SUBMITTER STATED POSSIBLE CAUSE AS CORROSION ON JOURNALS WORE THE C648-1 BEARING MATER	IAL AWAY UNTIL IT WORE INTO THE HUB.				1	G	7	1 	3O				H11NM   					 
1999052100049	19990521	00049	GL  	1999	5	21	99ZZZX2017       	2	19990505	G	7323	65A181	LINEAR ACTUATOR 			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28      	03013	GL  					GOVERNOR	MALFUNCTIONED   	H		A		O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			SW	99	57441		5    		380	45438	CAE860353			IN-FLIGHT RPM DECREASED TO 99 PERCENT.  WHEN GOVERNOR INCREASE BUTTON WAS PUSHED, RPM DECREASED TO 96 PERCENT.  PRIOR TO	 LANDING, RPM DECREASED TO 90 PERCENT.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999052100050	19990521	00050	CE  	1999	5	21	99ZZZX2018       	1	19990426	G	3230	24670036	BUNGEE          			CESSNA	172   	172RG       	2072438	CE  										MLG	MISMANUFACTURED 	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4802R	178  				172RG0035				BUNGEE MISSING ROLL CRIMP (ALLOWS EXCESSIVE PLAY OF BUSHING).						1	H	7	1 	3O				3A17    					 
1999052100051	19990521	00051	SO  	1999	5	21	99ZZZX2019       	1	19990505	G	5521		ELEVATOR        			PIPER 	PA31  	PA31350     	7103110	SO  										LEFT	MISREPAIRED     	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	05	4109D	6617 				318253012				NOTED THAT RIGHT AND LEFT ELEVATORS APPEARED TO BE MISALIGNED WITH EACH OTHER.  UPON FURTHER INSPECTION, FOUND LEFT ELEV	ATOR HAD BEEN IMPROPERLY REPAIRED IN THE PAST WITH A TWIST BEING BUILT IN.  UPON DISASSEMBLY, FOUND MAIN SPAR BROKEN AT 	TIP OF ATTACH POINT.  NOTE:  PIPER INSPECTION MODIFICATIONS HAD BEEN PREVIOUSLY ACCOMPLISHED, BUT DEFECTIVE SPAR STILL C	OULD NOT HAVE BEEN DETECTED.			1	L	7	2 	3O				A20SO   					 
1999052100052	19990521	00052	CE  	1999	5	21	99ZZZX2020       	1	19990411	G	3230	NAS56533	BOLT            		12416186    	CESSNA	210   	T210N       	2073456	CE  										MLG	LOOSE           	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	6506G	3977 				21064406				WHILE C/W ANNUAL, THE NAS 565-33 BOLTS THAT HOLD THE MAIN GEAR DOWNLOCK SUPPORTS LEFT 1241618-5 AND RIGHT 124618-6 IN PL	ACE, WERE FOUND LOOSE.  THIS IS THE SECOND TIME FOR THESE BOLTS.  THE FIRST TIME WAS 100 HOURS AND 145 LANDINGS AGO.  AT	 THAT TIME, THE BOLT HOLES AND BOLTS WERE CLEANED AND LOCK-TIGHTENED IN PLACE.				1	H	7	1 	3O				3A21    					 
1999052100053	19990521	00053	SO  	1999	5	21	99ZZZX2021       	1	19990503	G	2560	ELT10	ELT             	NARCO       		PIPER 	PA28  	PA28181     	7102807	SO  										TAIL CONE	FAILED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	1959H	6539 			11738	287790361				DURING ANNUAL INSPECTION, C/W FAR 91.207(D), MECHANIC NOTICED THAT ELT WAS VERY WEAK AND NOTICED AN ELECTRICAL SMELL.  D	IS-ASSEMBLY REVEALED VERY STRONG BURNT ELECTRICAL SMELL AND ELT WAS INOPERATIVE.  SIHPPED ELT TO MANUFACTURER FOR REPAIR	.				1	L	7	1 	3O				2A13    					 
1999052100054	19990521	00054	CE  	1999	5	21	99ZZZX2022       	1	19990420	G	7810	LW19296	GASKET          			CESSNA	182   	182S        	2072701	CE  										EXHAUST	FAILED          	B			MINR	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			NM	05	182EL	146  				18280009				AIRCRAFT TT:  145.7 HOURS.  PILOT NOTICED EXHAUST FUMES IN CABIN.  FOUND NR 1 EXHAUST GASKET BLOWN-OUT AND ATTACHING HAR	DWARE LOCATED IN BOTTOM OF COWLING.  RIGHT HEAT SHROUD HAD SLID DOWN EXHAUST MUFFLER ALLOWING FUMES TO ENTER CABIN THROU	GH HEATER.  HARDWARE ON HEAT SHROUD WAS TIGHT.  SB 97-78-01 WAS C/W AT 59.2 HOURS.  SB 98-78-03 WAS C/W AT 131.3 HOURS.				1	H	7	1 	3O			NT	3A13    					 
1999052100055	19990521	00055	CE  	1999	5	21	99ZZZX2023       	1	19990420	G	7810	STD1410	NUT             			CESSNA	182   	182S        	2072701	CE  										EXHAUST	FAILED          	B			MINR	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			NM	05	182EL	146  				18280009				SB 97-78-01 C/W AT 59.2 HOURS AND NUT WAS TORQUE CHECKED.  NUT AND 'STAR' TYPE LOCK WASHER FAILED TO HOLD WHEN GASKET BL	EW.  SUBMITTER RECOMMENDED UPGRADED GASKETS HAVE MANDATORY INSTALLATION (SB 97-78-01) AND SELF-LOCKING NUTS USED INSTEAD	 OF STAR-TYPE LOCK WASHERS.				1	H	7	1 	3O			NT	3A13    					 
1999052100056	19990521	00056	CE  	1999	5	21	99ZZZX2024       	1	19990420	G	7810	STD475	LOCK WASHER     			CESSNA	182   	182S        	2072701	CE  										EXHAUST	FAILED          	B			MINR	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			NM	05	182EL	146  				18280009				SB 97-78-01 C/W AT 59.2 HOURS AND NUT WAS TORQUE CHECKED.  NUT AND 'STAR' TYPE LOCK WASHER FAILED TO HOLD WHEN GASKET BL	EW.  SUBMITTER RECOMMENDED UPGRADED GASKETS HAVE MANDATORY INSTALLATION (SB 97-78-01) AND SELF-LOCKING NUTS USED INSTEAD	 OF STAR-TYPE LOCK WASHERS.				1	H	7	1 	3O			NT	3A13    					 
1999052100057	19990521	00057	SW  	1999	5	21	99ZZZX2025       	1	19990423	G	3250	72009517	FITTING         			MOONEY	M20   	M20J        	5870219	SW  										NLG STEERING	CRACKED         	G				C				ABORTED TAKEOFF         				E			VIBRATION/BUFFET          			TO	TAKEOFF        	1			GL	21	201BJ	5130 				240010				NOSE GEAR STARTED TO SHIMMY SEVERELY ON TAKEOFF ROLL.  FOUND STEERING T-FITTING BROKEN OFF.  FRACTURE OCCURRED NEXT TO W	ELD.					1	L	7	1 	3O				2A3     					 
1999052100058	19990521	00058	GL  	1999	5	21	99ZZZX2026       	1	19990208	G	8011		GEAR            			DIAMON	DA20  	DA20C1      	2990001	GL  										STARTER	SHEARED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	21	237ND	63   				C0022				PILOT REPORTED STARTER MADE GRINDING NOISE AND ENGINE WILL NOT START.  UPON REMOVAL OF STARTER, FOUND DRIVE GEAR SHEARED	.  THE GEAR HAD WORN AGAINST THE CRANKSHAFT GEAR, PN 641906, CAUSING METAL CONTAMINATION THROUGHOUT THE ENGINE.					1	L	7	1 	3O			NT	TA4CH   					 
1999052100059	19990521	00059	CE  	1999	5	21	99ZZZX2027       	1	19990401	G	2560	TR7013	ELT             			BEECH 	200   	200BEECH    	1152920	CE  										CABIN	MALFUNCTIONED   	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	23	944CL				33172	BB604				ELT ACTIVATED ITSELF AND COULD NOT BE DEACTIVATED UNTIL THE BATTERY WAS REMOVED.						1	L	7	2 	4T				A24CE   					 
1999052100061	19990521	00061	CE  	1999	5	21	99ZZZX2029       	1	19990416	G	3710		FILTER          	AIRBORNE    	D9181       	CESSNA	150   	A152        	2071836	CE  										VACUUM SYSTEM	BRITTLE         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	7332L	400  				A1520790				DURING ROUTINE INSPECTION, FOUND VACUUM FILTER END CRUMBLING.  FILTER WAS AT ITS 400 HOUR DUE TIME.  WHEN PIECES OF RUBB	ER WERE REMOVED AND ROLLED BETWEEN FINGERS, THEY CRUMBLED INTO SMALL PIECES.  HAVE FOUND SEVERAL LIKE THIS.					1	H	7	1 	3O				3A19    					 
1999052100062	19990521	00062	EA  	1999	5	21	99ZZZX2030       	2	19990301	G	7322	MA3PA105267	CARBURETOR      	FACET       		PIPER 	PA36  	PA36375     	7103620	SO  	LYC   	O235  	O235*       	41505	EA  					ENGINE	MISOVERHAULED   	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15	61940		23   		CM2198	368102025	L1876215			CARBURETOR LISTED IN NR 6 WAS REPAIRED AND TESTED.  23.1 HOURS AFTER INSTALLATION OF THIS CARBURETOR, ENGINE WOULD ONLY 	PRODUCE 2,000 RPM.  TEAR DOWN OF CARBURETOR REVEALED NEEDLE VALVE AND SEAT WORN, FLOAT LEVEL SET TOO HIGH, AND A THUMB S	IZED BALL OF LINE IN BOWL.				1	L	7	1 	3O	3	O		A10SO   	E223				 
1999052100065	19990521	00065	CE  	1999	5	21	99ZZZX2033       	1	19990427	G	3242		BRAKE           	PARKERHANFIN		CESSNA	414   	414A        	2075907	CE  										LEFT	WORN            	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	05	1245H	2100 				414A1204				PILOT COMPLAINED OF SOFT LEFT BRAKE.  INSPECTION REVEALED NO LEAK.  SMALL RESERVOIR DOES NOT ALLOW  MUCH BRAKE WEAR BEFO	RE REQUIRING SERVICE.  BLED BRAKES, OK.					1	L	7	2 	3O				A7CE    					 
1999052100066	19990521	00066	CE  	1999	5	21	99ZZZX2034       	1	19990424	G	2810		NUT             			CESSNA	177   	177         	2073704	CE  										CAP	LOOSE           	G				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	11	3270T				C1560010106	17700570				SELF-LOCKING NUT ON FUEL CAP LOCKING MECHANISM COULD BE TURNED BY HAND.  THE LOOSENING OF THE NUT ALLOWED THE LOCKING ME	CHANISM TO DISENGAGE FROM SHAFT.  THIS ALLOWED THE FUEL CAP TO COME OUT OF TANK OPENING AND ALLOWED FUEL TO BE SIPHONED 	OUT OF THE TANK.  THIS CAUSED A FUEL EXHAUSTION ACCIDENT.				1	H	7	1 	3O			NT	A13CE   					 
1999052100067	19990521	00067	EA  	1999	5	21	99ZZZX2035       	2	19990405	G	8520	LW14105	BEARING         			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					ENGINE	FAILED          	B			CBCR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	73764	1791 				17267661	L215776			DURING ROUTINE MAINTENANCE, THE OIL SCREEN WAS FOUND TO HAVE METAL PARTICLES IN IT.  THE ENGINE WAS 200 HOURS AWAY FROM 	TBO.  THE ENGINE WAS TORN DOWN TO DETERMINE THE SOURCE OF METAL.  DISCOVERED ONE OF THE MAIN BEARINGS TO THE CRANKSHAFT 	WAS FLAKING OFF.  THE DELAMINATION OF METAL ON THE BEARING FACE WAS TO A DEPTH OF APPROXIMATELY .015 INCH - .025 INCH.				1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999052100068	19990521	00068	SO  	1999	5	21	99ZZZX2036       	1	19990511	G	5510	1680000	NUTPLATE        			PIPER 	PA23  	PA23250     	7102308	SO  										STABILATOR	BROKEN          	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	54753				274720	277554065				UPON REMOVAL OF STABILATOR ATTACH FITTINGS, FOUND THE OUTBOARD NUTPLATES WERE BROKEN AND/OR CRACKED.  ONE NOT HOLDING AT	 ALL.					1	L	7	2 	3O				1A10    					 
1999052100069	19990521	00069	SO  	1999	5	21	99ZZZX2037       	2	19990329	G	7414	M3050	IMPULSE COUPLING	SLICK       	6310        	CESSNA	182   	182R        	2072731	CE  	CONT  	O470  	O470U       	17026	SO  					MAGNETO	CORRODED        	B	L	A	WXHR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	6594E	374  				18268375	809856R			IMPULSE COUPLING CORRODED ON MAGNETO.						1	L	7	1 	3O	3	O	NT	3A13    	E273				 
1999052100070	19990521	00070	CE  	1999	5	21	99ZZZX2038       	1	19990330	G	3220	071230916	BELLCRANK       			CESSNA	185   	A185F       	2072821	CE  										TAIL WHEEL	WORN            	B			CBCR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	9533H	2195 				18503446				DURING INSTALLATION OF TAILCONE ACCESS PANELS AT STA 198, DISCOVERED THE BELLCRANKS FOR TAIL WHEEL STEERING (WHERE THE S	PRING ATTACHES) WERE WORN EXTENSIVELY.  FURTHER INVESTIGATION REVEALED THE STEEL BUSHING WAS MISSING ON BOTH BELLCRANKS 	RESULTING IN EXCESSIVE WEAR.  WITHOUT THE INSTALLATION OF THESE SIDE INSPECTION PANELS, THE ONLY ACCESS IS DIRECTLY BELO	W THE BELLCRANKS.  THIS MAKES THE INSPECTION OF THESE ITEMS DIFFICULT AT BEST WITH A MIRROR.  BOTH BELLCRANKS WERE REPLA	CED.		1	H	7	1 	3O				3A24    					 
1999052100072	19990521	00072	EU  	1999	5	21	99ZZZX2040       	1	19990401	G	2910		LINE            	DUNLOP      		BRAERO	DH125 	HS125700A   	4230170	EU  										HYDRAULIC SYSTEM	CORRODED        	B		A	A83R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	17	564BR					257122				HEAVY CORROSION OF FLEX HYDRAULIC HOSES ON AIR FRAME.  THIS CORROSION IS NOT VISIBLE DUE TO PLASTIC INSULATION COVERING 	THE HOSE ASSY.					2	L	7	2 	4F				A3EU    					 
1999052100073	19990521	00073	EU  	1999	5	21	99ZZZX2041       	1	19990329	G	2910		LINE            	DUNLOP      		BRAERO	DH125 	HS125700A   	4230170	EU  										HYDRAULIC SYSTEM	CORRODED        	B		A	A83R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	17	947CE					257128				HYDRAULIC HOSE FAILURE DUE TO CORROSION OF METAL BRAID AND SWAGE.  THIS COVERED BY PLASTIC MATERIAL IN WHICH UNABLE TO S	EE UNLESS THE PLASTIC IS PEELED BACK.  NOTE:  SAME PART NUMBER HOSES ARE ON EARLY RAYTHEON MODELS HAVE A MANDATORY LIFE 	LIMIT.  THE HS 125-700 SERIES AIRCRAFT WAS NOT INCLUDED WITH THE CURRENT REVISION OF THE MAINTENANCE SCHEDULE.				2	L	7	2 	4F				A3EU    					 
1999052100074	19990521	00074	CE  	1999	5	21	99ZZZX2042       	1	19990405	G	2910		LINE            			LEAR  	25    	25D         	5170514	CE  										HYDRAULIC SYSTEM	CHAFED          	B	L		JGVR	A				UNSCHED LANDING         				K	J		FLUID LOSS                	WARNING INDICATION        		DE	DESCENT        	1			CE	09	510TP	2689 				353				AIRCRAFT EXPERIENCED LOSS OF HYDRAULIC PRESSURE DURING DESCENT INTO SALINA FOR ROUTINE FUEL STOP.  IMMEDIATELY RE-ROUTED	 TO LINCOLN FOR MAINTENANCE.  BLEW GEAR DOWN USING EMERGENCY SYSTEM.  WAS ABLE TO EXTEND FLAPS PARTIALLY.  USED EMERGENC	Y BRAKING FOR LANDING.  UPON INVESTIGATION, FOUND HYDRAULIC LINE IN AFT MAINTENANCE HOLE CHAFED THROUGH (REFERERENCE BUL	LETIN FIGURE 1 ITEM 3), BUT WAS NOT HOLDING TUBE PROPERLY AWAY FROM STRUCTURE ON LEFT SIDE OF AFT MAINTENANCE BAY.  RECO	MMEND INSPECTION OF THIS AREA FOR PROPER CLEARANCE.		2	L	7	2 	4J				A10CE   					 
1999052100075	19990521	00075	EU  	1999	5	21	99ZZZX2043       	1	19990416	G	3020	258KF35A	LINE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										FUSELAGE	MISROUTED       	B	P		PJYR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	800PA	3416 				NA0438				THIS LEADING EDGE SUPPLY LINE FOR TKS DE-ICE FLUID WAS FOUND CHAFED APROXIMATELY 90 PERCENT OF WALL THICKNESS BECAUSE OF	 IMPROPER ROUTING THROUGH A PROTECTIVE PLASTIC TUBE.  AS THE SUPPLY LINE EXITED THE PROTECTIVE TUBE IT WAS RUBBING ON TH	E AFT INBOARD EDGE.  THE CHAFING OCCURRED AT THAT POINT.				2	L	7	2 	4F			RT	A3EU    					 
1999052100076	19990521	00076	EU  	1999	5	21	99ZZZX2044       	1	19990413	G	5610	F50B268001110	FRAME           			AMD   	FALC50	FALCON50MYST	2730106	EU  										WINDSHIELD	CORRODED        	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	15TW					073				DURING CENTER WINDSHIELD FRAME CHANGE DUE TO INTERGRANULAR CORROSION, COPILOT WINDSHIELD WAS REMOVED, REVEALING SEVERE I	NTERGRANULAR CORROSION ON LOWER WINDSHIELD SEAL MATING SURFACE OF FRAME.  AFTER BLENDING CORROSION, SEVERAL AREAS MAPPED	 OUT TO PROTRUDE APPROXIMATELY 20-25 PERCENT INTO FRAME.  THIS CORROSION IS NOT VISIBLE WITHOUT REMOVING WINDSHIELD.  TH	E MANUFACTURER HAS APPROVED AN ULTRASONIC TEST PROCEDURE FOR THIS FRAME WHICH IS CURRENTLY IN THE FALCON 20 MAINTENANCE 	MANUAL TO CHECK FOR CORROSION IN THIS AREA WITHOUT REMOVING THE WINDSHIELD.		2	L	7	3 	4F				A46EU   					 
1999052100077	19990521	00077	EU  	1999	5	21	99ZZZX2045       	1	19990413	G	5610	F50B261001110	FRAME           			AMD   	FALC50	FALCON50MYST	2730106	EU  										WINDSHIELD	CORRODED        	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	15TW	6302 			990218012	073				AFTER REMOVAL OF CENTER COCKPIT WINDSHIELD, PN MY20261-10-4, WHICH WAS BEING REPLACED DUE TO EDGE DELAMINATION BY CUSTOM	ER REQUEST (NOTE:  EDGE DELAMINATION WAS WITHIN LIMITS PER MANUFACTURER'S MM), LOWER WINDSHIELD SEAL AREA OF FRAME HAD S	EVERE INTERGRANULAR CORROSION CAUSING EDGE OF FRAME TO FLAKE.  WHILE BLENDING OUT CORROSION, TRAILS, BLENDING PROTRUDED 	THROUGH FRAME AT LOWER SEAL AREA RADIUS TO UNPRESSURIZED SIDE OF FRAME.  (APPROXIMATELY 1 INCH LONG HOLE).  ALSO, SEVERA	L OTHER AREAS OF CORROSION BLENDED THROUGH APPROXIMATELY 50 PERCENT TO 65 PERCENT OF MATERIAL THICKNESS.  CORROSION CANN	OT BE VISUALLY SEEN WITHOUT REMOVAL OF WINDSHIELD.	2	L	7	3 	4F				A46EU   					 
1999052100078	19990521	00078	EU  	1999	5	21	99ZZZX2046       	1	19990413	G	5610	F50B267001110	FRAME           			AMD   	FALC50	FALCON50MYST	2730106	EU  										WINDSHIELD	CORRODED        	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	15TW	6302 				073				DURING CENTER WINDSHIELD FRAME CHANGE DUE TO INTERGRANULAR CORROSION, PILOT FORWARD WINDSHIELD WAS REMOVED REVEALING SEV	ERE INTERGRANULAR CORROSION ON LOWER WINDSHIELD SEAL MATING SURFACE OF FRAME.  AFTER BLENDING CORROSION, SEVERAL AREAS M	APPED OUT TO PROTRUDE APPROXIMATELY 10-15 PERCENT INTO FRAME.  MANUFACTURER PRESENTED A REPAIR SCHEME FOR THIS FRAME USI	NG PR1422 SEALANT TO FILL VOIDS.  THIS CORROSION IS NOT VISIBLE WITHOUT REMOVING WINDSHIELD.  MANUFACTURER HAS APPROVED 	AN ULTRASONIC TEST PROCEDURE FOR THIS FRAME WHICH IS CURRENTLY IN THE FALCON 20 MM TO CHECK FOR CORROSION IN THIS AREA W	ITHOUT REMOVING WINDSHIELD.	2	L	7	3 	4F				A46EU   					 
1999052100080	19990521	00080	CE  	1999	5	21	99ZZZX2048       	1	19990430	G	3250	99140807	STEERING UNIT   			CESSNA	650   	650         	2076802	CE  										NLG WW	FAILED          	C				A				UNSCHED LANDING         				O			OTHER                     			TO	TAKEOFF        	1			EA	21	2606	913  			141	6500194				AIRCRAFT EXPERIENCED A HARD LEFT YAW AT V1, FOLLOWED BY POSITIVE AIRCRAFT CONTROL TO ROTATION.  GEAR HANDLE WAS LOCKED I	N THE DOWN POSITION AFTER TAKEOFF.  DIVERTED AIRCRAFT TO CESSNA NY SERVICE CENTER.  APPROACH AND LANDING WAS NORMAL, HOW	EVER, NOSE TIRE WAS BADLY SCUFFED TO THE CORE.  TECHNICIANS FOUND THE NOSE POWER STEERING UNIT FAILED THE CENTERING SPRI	NG TEST AND BINDING ON THE UNIT.  REPLACED NOSE STEERING UNIT.			2	L	7	2 	4F				A9NM    					 
1999052100082	19990521	00082	CE  	1999	5	21	99ZZZX2050       	1	19990503	G	3231	55421022	TORQUE TUBE     			CESSNA	501   	501         	2076603	CE  										NLG	LOOSE           	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	17	41GT	6831 				5010297				DURING PHASE 2 INSPECTION, FOUND NOSE GEAR DOORS HANGING DOWN.  OPEN GEAR DOORS FOUND TORQUE TUBE FOR DOORS, THE ATTACH 	NUTPLATE HOLDER IS CRACKED ON WELD.  PART WAS REPLACED.  THE PART WAS INSTALLED NEW WHEN THE AIRCRAFT WAS DELIVERED NEW.					1	L	7	2 	4F				A27CE   					 
1999052100083	19990521	00083	CE  	1999	5	21	99ZZZX2051       	1	19990330	G	7602	07506134	SUPPORT         			CESSNA	185   	A185F       	2072821	CE  										ENGINE BAY	WORN            	B			CBCR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	03	9533H	2195 				18503446				PILOT REPORTED MIXTURE SETTING CONSISTANCY WAS ERRATIC.  INVESTIGATION INTO THE CONTROL MOUNT IN THE ENGINE COMPARTMENT 	REVEALED THE U-CHANNEL THAT SUPPORTS THE MIXTURE CONTROL HAD WORN TO AN EXTENT THAT THE CABLE HOUSING WAS SLIDING IN THE	 MOUNT.  THE OUTER CABLE NEEDS TO BE HELD FAST FOR PROPER OPERATION.  THE BRACKET SUPPORT HOLDS BOTH THE MIXTURE CONTROL	 AND THE THROTTLE CONTROL, ALTHOUGH THE THROTTLE WAS IN GOOD SHAPE.  THIS BRACKET, PN 0750613-4, WAS REPLACED AT THIS TI	ME.		1	H	7	1 	3O				3A24    					 
1999052100085	19990521	00085	NM  	1999	5	21	99ZZZX2053       	1	19990414	G	2435	03601018	BEARING         	LUCAS       	230650181   	ISRAEL	1125  	1125        		NM  										STARTER/GEN	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03	650GE				3824	064				THIS STARTER/GENERATOR, PN 23065-018-1, SN 3864, WAS MODIFIED TO MODS A-D BY LUCAS AEROSPACE FOR IMPROVED COOLING OF BEA	RINGS AND BEARING LIFE IMPROVEMENT.  THE BEARINGS ARE SUPPOSED TO LAST 1,000 HOURS.					2	L	7	2 	4F			RT	A16NM   					 
1999052100086	19990521	00086	EU  	1999	5	21	99ZZZX2054       	1	19990329	G	2910		LINE            			BRAERO	DH125 	HS125700A   	4230170	EU  										HYDRAULIC SYSTEM	CORRODED        	B		A	A83R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	17	945CE					257137				HYDRAULIC HOSE CORROSION OF SWAGE AT METAL BRAID.  EARLY SB 29-35 ADDRESSED THIS WITH A DIFFERENT HOSE MANUFACTURE.  SUB	MITTER STATED IT IS NOW HAPPENING WITH THE DUNLOP HOSES.					2	L	7	2 	4F				A3EU    					 
1999052100087	19990521	00087	EU  	1999	5	21	99ZZZX2055       	1	19990317	G	2820		VALVE           			BRAERO	DH125 	HS125700A   	4230170	EU  										MLG WW	LEAKING         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			GL	03	700BW	5577 			380VB241	257123				MASTER REFUEL VALVE LEAKED DURING REFUELING OF AIRCRAFT USING SINGLE POINT REFUEL SYSTEM.  THE VALVE IS LOCATED IN THE M	AIN GEAR WHEELWELL AND THE LEAKING FUEL TRAVELS ALONG THE WIRE BUNDLE FOR THE LOWER ROTATING BEACON AND INSIDE THE BEACO	N CAUSING BEACON FAILURE.  THE VALVE ONLY LEAKS DURING REFUELING MAKING IT HARDER TO FIND THE LEAK.				2	L	7	2 	4F				A3EU    					 
1999052800157	19990528	00157	SW  	1999	5	28	99ZZZX2056       	1	19990503	G	6510	206040328003	ADAPTER         		206040325017	BELL  	206   	206L1       	1182107	SW  										T/R DRIVESHAFT	LOOSE           	H		A		O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	165BH	7015 				45249				ONE BOLT AND NUT WERE FOUND SEPARATED FROM TAIL ROTOR DRIVESHAFT.  THE DRIVESHAFT DISCONNECTED AND BROKE A FITTING ON PO	WER TURBINE GOVERNOR.  THIS RESULTED IN LOSS OF TAIL ROTOR AUTHORITY AND ENGINE POWER.  PILOT PERFORMED AN EMERGENCY LAN	DING.				1	G	7	1 	3U				H2SW    					 
1999052800158	19990528	00158	EU  	1999	5	28	99ZZZX2057       	1	19990308	G	2410	109040307103	GEAR            		109040003105	AGUSTA	A109  	A109E       	0260119	EU  										TRANSMISSION	CRACKED         	B			DT1R	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			EA	17	109AH	369  			A21240	11040				GLEASON GEAR CRACKED.  PILOT REPORTED HAVING A CHIP LIGHT AND NOISE COMING FROM MAIN TRANSMISSION ASSY.  BORESCOPE INSPE	CTION OF TRANSMISSION YIELDED A CRACKED GEAR.  GEAR SENT TO AGUSTA S.P.A. FOR EVALUATION.  TB109K-16 AND AD 97-26-09 ADD	RESS THIS SITUATION ON A109K2 HELICOPTERS.				1	G	7	2 	3U			NC	H7EU    					 
1999052800159	19990528	00159		1999	5	28	99ZZZX2058       	1	19990510	G	7120	LK83060	BEARING         								RROYCE	RB211 	RB211535E4  	54555	NE  					ENGINE MOUNT	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07			12348				31053			CRACK INDICATIONS (AS MARKED) FOUND ON MAGNETIC PARTICLE INSPECTION.  DURING AN INSPECTION OF AN ENGINE RECEIVED FOR MAI	NTENANCE, THE INSPECTION PERSONNEL NOTICED THE FORWARD MOUNT WAS BADLY CORRODED.  THE MOUNT WAS SENT TO NDT FOR FURTHER 	EVALUATION WHEN IT WAS DISCOVERED TO BE CRACKED.  A POSSIBLE CAUSE HAS NOT BEEN DETERMINED, BUT PREVIOUS MOUNTS HAVE BEE	N DAMAGED OR BADLY CORRODED.								4	F			E12EU				 
1999052800160	19990528	00160	NM  	1999	5	28	99ZZZX2059       	1	19990414	G	2760	65445656	MANIFOLD        		654456115   	BOEING	737   	737*        		NM  										SPOILER	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		22654			8583					MANIFOLD IS CRACKED IN THE PASSAGE BETWEEN THE FILTER PORT AND EXTEND CHECK VALVE TEST PORT.  ALSO, THE EDGE OF THE PASS	AGE IN THE TRANSFER TUBE PORT IS CRACKED.  POSSIBLE CAUSE:  STRESS CRACKS.					2	L	7	2 	4F			RT	A16WE   					 
1999052800161	19990528	00161	NM  	1999	5	28	99ZZZX2060       	1	19990414	G	2760	65445656	MANIFOLD        		654456114   	BOEING	737   	737*        		NM  										SPOILER	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		16271			0283					MANIFOLD IS CRACKED IN THE PASSAGES BETWEEN THE FILTER PORT AND THE EXTEND CHECK VALVE AND RETRACT CHECK VALVE TEST PORT	S.  POSSIBLE CAUSE:  STRESS CRACKS.					2	L	7	2 	4F			RT	A16WE   					 
1999052800162	19990528	00162	NM  	1999	5	28	99ZZZX2061       	1	19990414	G	2760	65445656	MANIFOLD        		654456114   	BOEING	737   	737*        		NM  										SPOILER	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		11998			2480					MANIFOLD IS CRACKED IN THE PASSAGE BETWEEN THE FILTER PORT AND EXTEND CHECK VALVE TEST PORT.  ALSO, THE APEX BETWEEN THE	 EXTEND PORT PASSAGE AND RETRACT PORT PASSAGE IS CRACKED ALONG THE UPPER EDGE.  POSSIBLE CAUSE:  STRESS CRACKS.					2	L	7	2 	4F			RT	A16WE   					 
1999052800163	19990528	00163	NM  	1999	5	28	99ZZZX2062       	1	19990329	G	2720	69356071	SEGMENT         		65C370529   	BOEING	737   	737*        		NM  										RUDDER	MISMANUFACTURED 	B	P	A	IU6R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	01					01220A					BALL END IS UNDERSIZED.  MOVEMENT INSIDE YAW DAMPENER SLIDE.						2	L	7	2 	4F			RT	A16WE   					 
1999052800164	19990528	00164	NM  	1999	5	28	99ZZZX2063       	1	19990423	G	2742	69778551	SPRING          		65C347512   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		21860			00660					SPRINGS, PN 69-77855-1, ARE BROKEN, IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SP	RINGS.  SPRINGS, PN 69-77855-1, SHOULD BE REPLACED WITH, PN 69-77855-2, SPRINGS PER BOEING TELEX AEO-AUB-94-0195RR.					2	L	7	2 	4F			RT	A16WE   					 
1999052800165	19990528	00165	NM  	1999	5	28	99ZZZX2064       	1	19990423	G	2760	65C268636	HOUSING         		65C268642   	BOEING	737   	7373Y0      	1384671	NM  										SPOILER	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	682SW	40503	13423		0495	23496				HOUSING ASSY IS CRACKED AT RETAINER NUT BOSS JUST BELOW THREADS RUNNING HALF WAY AROUND CIRCUMFERENCE OF BORE.  POSSIBLE	 CAUSE, EXCESSIVE STRESS, FORCE AND/OR PRESSURE.  RE:  SOUTHWEST A/L, OPER CONTROL NR 0270131-63R.					2	L	7	2 	4F			RT	A16WE   					 
1999052800166	19990528	00166	WP  	1999	5	28	99ZZZX2065       	2	19990427	G	7270	30721631	BLADE           		30735703    						GARRTT	TFE731	TFE73122B   	01518	WP  					COMPRESSOR	MISMANUFACTURED 	B			IY2R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15					970322900659		P74124			FAN BLADES REMOVED FROM ENGINE DUE TO EXCESSIVE AMOUNTS OF THRUST (FN) FOLLOWING COMPRESSOR CORE ZONE INSPECTION (CZI). 	 FAN BLADES (30 EACH), PN 3072613-1 WERE REMOVED AND SENT FOR THRUST REDUCTION.  MECHANICAL BEND TO REDUCE THRUST, PENET	RANT INSP ONLY.  UPON RETURN, BLADES WERE INSTALLED AND ENGINE RUN IN TEST CELL.  UNABLE TO ADVANCE POWER LEVER MUCH BEY	OND IDLE DUE TO A SEVERED FAN VIBRATION >1.0 INCH PER SECOND (IPS).  FAN ASSY REMOVED AND A VECTOR SUMMATION BALANCE ACC	OMPLISHED PER 72-IR-02 INSP REPAIR MANUAL.  FAN REINSTALLED ON ENG WITH SAME SEVERE FAN VIBRATION.  FAN REBLADED WITH A 	DIFFERENT (NOT REWORKED) SET OF BLADES.   ENG WAS RUN IN TEST CELL.  FAN RAN SMOOTH AND QUIET.  REF:  W.O. GR2323.						4	F			E6WE				 
1999052800167	19990528	00167	NE  	1999	5	28	99ZZZX2066       	2	19990413	G	7230	1B3198	SHAFT           								PWA   	2037  	PW2040      		NE  					COMPRESSOR	CRACKED         	B			WA2D	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03					P32233		P717920			SUBJECT ENGINE RECEIVED FOR MAINTENANCE DUE TO PERFORMANCE DETERIORATION.  INSPECTION OF SHAFT THREADS BY ULTRASONIC MEA	NS IAW SB 72-510 REVEALED CRACK INDICATIONS.  CRACK CONFIRMED BY P&W AS BEING INTERMITTENT 2 INCH CRACK TYPICAL OF THE T	YPE ADDRESSED BY THE SB.  ENG TT:  9,563 HOURS.  ENG TC:  6,631.									4	F			E17NE				 
1999052800168	19990528	00168	NE  	1999	5	28	99ZZZX2067       	2	19990413	G	7230	1B7806REF	BLADE           								PWA   	2037  	PW2037      		NE  					COMPRESSOR	FRACTURED       	B			WA2D	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		7264 					P727222			ENGINE RECEIVED FOR REPLACEMENT OF SUSPECT NR 1 MAIN BEARING.  DISASSEMBLY INSPECTION REVEALED ONE EACH 6TH STAGE BLADE 	FRACTURE AT APPROX 60 PERCENT SPAN WITH SUBSEQUENT DOWNSTREAM DAMAGE.  THE BLADE WAS OF THE INCREASE L/E THICKNESS CONFI	GURATION PER SB 72-460.  THE FRACTURED BLADE HAS BEEN FORWARDED TO P&W FOR INVESTIGATION.									4	F			E17NE				 
1999052800169	19990528	00169	NE  	1999	5	28	99ZZZX2068       	2	19990304	G	7230	1B5129	BEARING         								PWA   	2037  	PW2037      		NE  					ENGINE	SPALLED         	B			WA2D	E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			J			WARNING INDICATION        			NR	NOT REPORTED   	1			NE	03		5249 			0441		P727243			ENGINE WAS IN FLIGHT SHUTDOWN DUE TO ZERO OIL PRESSURE AND OIL PRESSURE WARNING LIGHT.  ENGINE WINDMILLED OVER TWO HOURS	 WITH ZERO OIL PRESSURE.  DISASSEMBLY INSPECTION REVEALED FAILED NR 1 MAIN BEARING.  BEARING CONDITION AS RECEIVED:  OUT	ER RACE SPALLED OVER 90 DEGREE ARC.  CAGE BROKEN IN HALF (CIRCUMFERENTIALLY).  BALL SPALLING.  BEARING IS NOT PART OF SU	SPECT LOT.  BEARING TURNED OVER TO P&W  FOR INVESTIGATION.  ENGINE TT:  5,249 HOURS.  ENGINE TC:  1,784.								4	F			E17NE				 
1999052800170	19990528	00170	NE  	1999	5	28	99ZZZX2069       	2	19990414	G	7250	JR27207	SEAL            		M05100AA    	FOKKER	F27   	F27MK100    	4990617	EU  	RROYCE	TAY   	TAY62015    	04564	NE  					LP TURBINE	FAILED          	B	P		YRRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	GUKFI	16803			TM4026					THE LP ROTOR WAS FREE TO ROTATE AND THE HP ROTOR WAS CONFIRMED AS BEING SEIZED.  THERE WAS NO APPRECIABLE BACKLASH NOTED	 WHILE ATTEMPTING TO ROTATE THE HP ROTOR.  THE HIGH SPEED GEARBOX MOUNTED ACCESSORIES WERE REMOVED AND ON COMPLETION, TH	E ROTOR WAS STILL NOTED TO BE SEIZED.  THE GEARBOX MODULE ITSELF WAS THEN REMOVED AND THE HP ROTOR STILL REMAINED LOCKED	.			2	H	7	2 	4T	4	F		A817    	E25NE				 
1999060900009	19990609	00009	EA  	1999	6	9	99ZZZX2070       	3	19990424	G	6110	76EM855	PROPELLER ASSY  			MAULE 	MX7   	MX7180A     	5460185	SO  						SNSNCH	76E	76EM8S5     	EA  	FORWARD	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	27	10481	80   			31977K			31977K		PROPELLER INCORRECTLY TORQUED.  PROPELLER SPACER FRETTED .007 INCH.  FORWARD SPINNER BULKHEAD CRACKED.  FLAPS WERE RIGGE	D WRONG OUT 5 DEGREES (3 INCHES ON TRAILING EDGE).  GASCOLATOR SEALS SWELL IN FUEL.					1	H	7	1 	3O			NC	3A23    		5	N	P4EA	 
1999052800171	19990528	00171	SO  	1999	5	28	99ZZZX2071       	2	19990401	G	8510		GEAR            			DIAMON	DA20  	DA20C1      	2990001	GL  	CONT  	O240  	IO240B      	17030	SO  					STARTER	FAILED          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	01	212CS	16   				C0048				OPERATOR REPORTED BIG DROP IN OIL PRESSURE.  REMOVED OIL FILTER AND FOUND STEEL AND ALUMINUM CHUNKS (LARGE).  SOURCE OF 	METAL WAS FOUND TO BE CAUSED BY A FAILURE OF THE STARTER DRIVE GEAR AND THE ACCESSORY DRIVE GEARS.  ALL THE ABOVE GEARS 	WERE MISSING TEETH AND/OR HEAVILY DAMAGED.  THIS AIRCRAFT HAS A TOTAL TIME OF 16 HOURS.				1	L	7	1 	3O	3	O	NT	TA4CH   	E7SO				 
1999052800172	19990528	00172	GL  	1999	5	28	99ZZZX2072       	1	19990401	G	6720	28163511	CONTROL CABLE   			ENSTRM	F28   	F28C        	3300407	GL  										TAIL ROTOR	BROKEN          	B		A	GNER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	01	635H	1492 				386				AT APPROXIMATELY 12 INCHES FORWARD OF THE TAIL ROTOR, THE LEFT TAIL ROTOR CONTROL CABLE BROKE.  NO EVIDENCE OF RUBBING O	R CHAFING.					1	G	7	1 	3O			 	H1CE    					 
1999052800317	19990528	00317	EU  	1999	5	28	99ZZZX2073       	3	19990308	G	6111		FERREL          													CNPSL	AW2	AW2*        	EU  	PROPELLER	CRACKED         	B	S		NWOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05								2202		LOWER FERREL HAS CRACK.																6	C	P9EU	 
1999052800318	19990528	00318	EU  	1999	5	28	99ZZZX2074       	3	19990308	G	6111		SLEEVE          													CNPSL	AW2	AW2*        	EU  	PROPELLER	CRACKED         	B	S		NWOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05								W332144		OUTER AREA OF SLEEVE CRACKED.																6	C	P9EU	 
1999052800319	19990528	00319	SO  	1999	5	28	99ZZZX2075       	1	19990427	G	2497		WIRE            			PIPER 	PA46  	PA46350P    	       	SO  										ELECTRICAL SYS	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	01	9160X					4622046				CABIN HEAT AND BUS TIE FEED WIRES WERE ON INCORRECT CURRENT LIMITERS.  CABIN HEAT WAS ON 35 AMP LIMITER, BUS TIE FEED WA	S ON 100 AMP LIMITER.					1	L	7	1 	3O			RT	A25SO   					 
1999052800320	19990528	00320	SO  	1999	5	28	99ZZZX2076       	1	19990304	G	7160	638873	AIR BOX         			PIPER 	PA28  	PA28181     	7102807	SO  										ENGINE	MISMANUFACTURED 	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	03	9279J					2843068				IN C/W PIPER SB NR 1022 ON FACET INDUCTION AIR FILTERS PN 638873 FOR PLASTISOL DETERIORATION, MOLD WAS FOUND INSIDE FILT	ER ELEMENT PLEATS.  FURTHER INSPECTION REVEALED 8 TO 12 OUNCES OF WATER IN AIR BOX THAT IS FORMED INTO LOWER COWL.  NO D	RAIN HOLE WAS INSTALLED TO FACILITATE DRAINING DRILLED DRAIN HOLE.				1	L	7	1 	3O				2A13    					 
1999052800321	19990528	00321	SO  	1999	5	28	99ZZZX2077       	1	19990503	G	5510	9980303	BALANCE WEIGHT  			PIPER 	PA28  	PA28181     	7102807	SO  										HORIZ STABILIZER	LOOSE           	B			DPOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	234EM	2249 				287990183				DURING AN ANNUAL INSPECTION, THE BALANCE WEIGHT ASSEMBLY (99803-03) WAS FOUND LOOSE ON THE TUBE (69624-02).  WHEN THE BA	LANCE WEIGHT WAS REMOVED, THE BOLT HOLE THROUGH THE TUBE WAS FOUND ELONGATED ALTHOUGH THE BOLT WAS TIGHT.  THERE IS ONLY	 ONE BOLT THROUGH THE WEIGHT AND TUBE, AND OVER A PERIOD OF TIME AS THE WEIGHT DID NOT FIT TIGHTLY OVER THE TUBE, ALLOWE	D THE WEIGHT TO EVENTUALLY ELONGATE THE HOLE.			1	L	7	1 	3O				2A13    					 
1999052800328	19990528	00328	CE  	1999	5	28	99ZZZX2084       	1	19990420	G	3230	08411066	BELLCRANK       			CESSNA	340   	340A        	2076405	CE  										MLG	BROKEN          	B			BIGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	114BH	5011 				340A1230				AFTER LANDING, PILOT NOTICED RIGHT INBOARD GEAR DOOR HANGING OPEN.  INVESTIGATION FOUND BELLCRANK, PN 0841106-6, HAD BRO	KEN.  NEW PART WAS INSTALLED AND GEAR RIGGING WAS CHECKED.  OPERATION WAS NORMAL.					1	L	7	2 	3O				3A25    					 
1999052800329	19990528	00329	CE  	1999	5	28	99ZZZX2085       	1	19990421	G	3230	08411066	BELLCRANK       			CESSNA	340   	340A        	2076405	CE  										MLG	FAILED          	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	04	115BH	5954 				340A1531				POST-FLIGHT INSPECTION REVEALED RIGHT INBOARD DOOR HANGING DOWN.  INVESTIGATION FOUND RETRACT BELLCRANK BROKEN WHICH ALL	OWED DOOR TO HANG FREE.  PART SUBMITTED TO CESSNA FOR EVALUATION.					1	L	7	2 	3O				3A25    					 
1999052800330	19990528	00330	CE  	1999	5	28	99ZZZX2086       	1	19990507	G	7602	363800845	CONTROL CABLE   			BEECH 	36    	A36         	1151604	CE  										MIXTURE	LOOSE           	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	07	616JA	2827 				E2285				WHILE INSPECTING MIXTURE CONTROL DURING ANNUAL INSPECTION, LOOSENESS WAS NOTED IN MIXTURE CONTROL CABLE.  UPON FURTHER I	NSPECTION, DETERMINED THE SWAGED PORTION OF CONTROL CABLE WAS SLIPPING.  THE SWAGED PORTION CAME OFF WITHOUT TOO MUCH PR	ESSURE.				1	L	7	1 	3O			 	3A15    					 
1999052800331	19990528	00331	GL  	1999	5	28	99ZZZX2087       	3	19990406	G	6114	D6608C88	HUB             													MCAULY	3A32C	D3A32C88    	GL  	PROPELLER	CRACKED         	B			ME4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19								727906		PROPELLER RECEIVED FOR 5-YEAR OVERHAUL.  DURING HUB INSPECTION, DISCOVERED CRACK IN NR 2 BLADE SOCKET 4 THREADS IN AT 2 	DEGREE TO 3 DEGREE POSITION ABOUT 1 INCH LONG.  CRACK DISCOVERED USING A 10X POWER MICROSCOPE.															5	C	P21E	 
1999052800339	19990528	00339	GL  	1999	5	28	99ZZZX2095       	3	19990310	G	6114		HUB             													MCAULY	2A34C	D2A34C98    	GL  	PROPELLER	CRACKED         	B			NWOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05								781702		PROPELLER HUB CRACKED IN THREAD AREA.																5	C	P3EA	 
1999052800340	19990528	00340	SO  	1999	5	28	99ZZZX2096       	1	19990429	G	2700		FLIGHT CONTROL  			PIPER 	PA44  	PA44180     	7104402	SO  										COCKPIT	FOD             	B			R2JR	K				NONE                    				C			F.O.D.                    			IN	INSP/MAINT     	1			EA	21	39471					447995009				PRIOR TO TRAINING FLIGHT, AIRCRAFT PRE-FLIGHT INSPECTION REVEALED ELEVATOR CONTROLS WERE FOUND JAMMED NOSE DOWN WITH VER	Y LITTLE NOSE UP TRAVEL AVAILABLE.  MAINTENANCE INSPECTION FOUND LARGE SCREWDRIVER WEDGED IN COCKPIT FLIGHT CONTROLS UND	ER COCKPIT FLOORBOARDS.  SUBMITTER STATED UNABLE TO DETERMINE HOW LONG TOOL HAD BEEN UNDER FLOOR.  AIRCRAFT TT:  29,089 	HOURS.			1	L	7	2 	3O				A19S0   					 
1999052800341	19990528	00341	CE  	1999	5	28	99ZZZX2097       	1	19990314	G	3242	C163030011	BRAKE           			CESSNA	172   	172R        	2072401	CE  										RT MLG	FAILED          	B			WIWR	O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			WP	07	9581G	226  				17280530				PILOT REPORTED THAT ON LANDING ROLL-OUT, THE RIGHT BRAKE HAD FAILED AND REQUIRED CONSTANT PUMPING TO MAINTAIN ANY PRESSU	RE.  UPON INSPECTION, THE CALIPER WAS FOUND CRACKED IN TWO PLACES.					1	H	7	1 	3O			NT	3A12    					 
1999052800344	19990528	00344	CE  	1999	5	28	99ZZZX2100       	1	19990323	G	2820	AN9292	CAP             			CESSNA	402   	402C        	207590R	CE  										COCKPIT	LEAKING         	H				A				UNSCHED LANDING         				O			OTHER                     			NR	NOT REPORTED   	1			EA	01	618CA	78   				402C0620				CREW REPORTED FUEL/FUEL PUDDLE ON COCKPIT FLOOR ON THE FIRST OFFICER'S SIDE.  DIVERTED TO HYA EN ROUTE FROM BOS TO ACK. 	 MAINTENANCE COULD NOT CONFIRM PUDDLING OF FUEL.  FOUND FUEL STAIN (BLUE DYE) ON FUEL FLOW BLEEDER LINE ASSY.  TIGHTENED	 AN 929-2 CAP.  C/W FULL POWER GROUND RUN.  NO LEAKS NOTED.				1	L	7	2 	3O				A7CE    					 
1999052800345	19990528	00345	CE  	1999	5	28	99ZZZX2101       	1	19990421	G	3246	16210200	WHEEL           	PARKERHANFIN		CESSNA	425   	425         	2076018	CE  										MLG	CRACKED         	B	S		EIPR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	402NG	6100 				4250035				MAIN WHEEL CRACKED IN SPOKE AREA.						1	L	7	2 	3T			RT	A7CE    					 
1999052800346	19990528	00346	CE  	1999	5	28	99ZZZX2102       	1	19990405	G	5751		RIB             			BEECH 	76    	76          	1153005	CE  										AILERON	CRACKED         	D	S	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	6717Y	4033 				ME331				DURING THE NORMAL INSPECTION INTERVAL, CRACKS WERE FOUND IN THE WING RIBS WHERE THE INBOARD AILERON HINGE PLATES (PN 105	-100011-51) AND THE OUTBOARD AILERON HINGE PLATES (P/N 105-100011-51) ATTACH.  THE SAME PROBLEM HAS BEEN FOUND ON OTHER 	AIRCRAFT OF SAME MODEL.  REPAIRS WERE MADE BY FABRICATING A DOUBLER FOR EACH RIB.  ON A PREVIOUS AIRCRAFT, ALL FOUR RIBS	 WERE REPAIRED WITH DOUBLERS EVEN THOUGH ONLY THREE WERE DETERMINED TO BE CRACKED.  THE UNCRACKED RIB NEVER CRACKED WITH	 THE DOUBLER INSTALLED.		1	L	7	2 	3O				A29CE   					 
1999052800347	19990528	00347	EA  	1999	5	28	99ZZZX2103       	2	19990317	G	7414	437198120973	IMPULSE COUPLING	SLICK       	4371        	PIPER 	PA28  	PA28151     	7102805	SO  	LYC   	O320  	O320E3D     	41508	EA  					MAGNETO	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	41896	2    			9820973	287415349				IMPULSE COUPLING FAILS TO RETURN TO NORMAL LOADED POSITION.						1	L	7	1 	3O	3	O		2A13    	E274				 
1999052800348	19990528	00348	SO  	1999	5	28	99ZZZX2104       	1	19990503	G	5410	12003852001	FRAME           			EMB   	120   	EMB120RT    		SO  										LT & RT NACELLES	CRACKED         	B			WVER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	09	244AS					120073				DURING ROUTINE MAINTENANCE CHECKS, CRACKS WERE FOUND ON BOTH ENGINE NACELLE NR 1 FRAMES.  ON THE LT FRAME, THE CRACK IS 	LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB BETWEEN THE TOP OUTBOARD MOUNTING BOLT HOLE AND THE OUTBOARD EDGE OF THE	 FRAME.  ON THE RT FRAME, THE CRACK IS LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB BETWEEN THE TOP OUTBOARD MOUNTING	 BOLT HOLE AND THE OUTBOARD EDGE OF THE FRAME.  RECOMMEND REPLACING BOTH FRAMES AND CONTINUE MONITORING IAW EXISTING MAI	NTENANCE CHECKS.		2	L	7	2 	4T			RT	A31SO   					 
1999052800349	19990528	00349	WP  	1999	5	28	99ZZZX2105       	2	19990430	G	7240	31070531	COMBUSTOR       			BAG   	JETSTM	JETSTM3101  	1500215	EU  	GARRTT	TPE331	TPE33110U   	01514	WP  					COMBUSTION SECT	CRACKED         	B			R2JR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	10UP	12667	1371 		P42077C	635	P42077C			ONE ENGINE START, CREW NOTICED SLOW START ON NR 2 ENGINE AND 100 DEGREE CELCIUS EGT SPLIT DURING FLIGHT.  UPON ARRIVAL A	T DESTINATION, MAINTENANCE WAS NOTIFIED, INSPECTOR FOUND A 6 INCH CRACK ON COMBUSTOR CAN WHICH ALLOWED HOT BLEED AIR TO 	LEAK INTO ENGINE NACELLE CAUSING ENGINE POWER LOSS.  ALSO, FOUND DENTS ON EXTERNAL SURFACE OF COMBUSTOR.  ENGINE REPAIRE	D BY MANUFACTURER AND RETURNED TO SERVICE.			2	L	7	2 	4T	4	T	RT	A21EU   	E4WE				 
1999052800350	19990528	00350	CE  	1999	5	28	99ZZZX2106       	1	19990326	G	3000	738081	CAP             	WHITTAKER   	725673      	CESSNA	650   	650         	2076802	CE  										ANTI-ICE SYSTEM	SEIZED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	38WP				281	650032				WHILE PERFORMING OPERATION 8 INSPECTION WHEN REMOVING ANTI-ICE FILTER CAP, FOUND CAP FROZEN OR GALLED AND ON OTHER ANTI-	ICE VALVE, THE CAP FROZE OR GALLED UPON RE-INSTALLING CAP AFTER CLEANING AND INSPECTING FILTER.  RECOMMEND PROPER COMPOU	ND BE APPLIED BY OVERHAUL AND MANUFACTURING FACILITIES TO PREVENT THREAD SEIZURE.				2	L	7	2 	4F				A9NM    					 
1999052800351	19990528	00351	CE  	1999	5	28	99ZZZX2107       	1	19990326	G	3000	738081	CAP             	WHITTAKER   	725673      	CESSNA	650   	650         	2076802	CE  										ANTI-ICE SYSTEM	SEIZED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	38WP				292	650032				WHILE PERFOMRING OPERATION 8 INSPECTION WHEN REMOVING ANTI-ICE FILTER CAP, FOUND CAP FROZEN OR GALLED AND ON OTHER ANTI-	ICE VALVE, THE CAP FROZE OR GALLED UPON RE-INSTALLING CAP AFTER CLEANING AND INSPECTING FILTER.  RECOMMEND PROPER COMPOU	ND BE APPLIED BY OVERHAUL AND MANUFACTURING FACILITIES TO PREVENT THREAD SEIZURE.				2	L	7	2 	4F				A9NM    					 
1999052800354	19990528	00354	SW  	1999	5	28	99ZZZX2110       	1	19990409	G	5320		ANGLE           			AIRTRC	AT500 	AT502A      	0390306	SW  										MAIN SPAR	CRACKED         	B			Q2AR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	17	438RJ	1797 				50210345				LEFT MAIN SPAR WEB UPPER ANGLE CRACKED AT RIVIT HOLES.  THIS AREA APPEARS TO BE WEAK BY DESIGN.  INBOARD AND OUTBOARD PO	RTION OF SPAR REINFORCED WITH EXTRUDED ANGLE.  THIS PLUS OR MINUS 24 INCH SECTION NOT REINFORCED.					1	L	7	1 	3T			NC	A17SW   					 
1999052800356	19990528	00356		1999	5	28	99ZZZX2112       	4	19990406	G	3425	5040017901	INDICATOR       		5860B       	HUGHES	369   	369E        	4470707	WP  										ATTITUDE	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8330P					0330E				ATTITUDE GYRO FLOATING AND NOISY.  REMOVED AND REPLACED.  SENT FOR REPAIR.						1	G	7	1 	3U				H3WE    					 
1999052800359	19990528	00359	NM  	1999	5	28	99ZZZX2113       	1	19990401	G	5320		ANGLE           			BOEING	727   	727227      	1384078	NM  										BS 360-380	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON ANGLE BETWEEN STA 360 - STA 380, STR 28L - STR 28R.						2	L	7	3 	4F				A3WE    					 
1999052800360	19990528	00360	NM  	1999	5	28	99ZZZX2114       	1	19990401	G	5320		SPLICE          			BOEING	727   	727227      	1384078	NM  										BS 1010	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED AT STR SPLICE 29L, STA 1010.						2	L	7	3 	4F				A3WE    					 
1999052800362	19990528	00362	NM  	1999	5	28	99ZZZX2116       	1	19990401	G	5320		SUPPORT         			BOEING	727   	727227      	1384078	NM  										BS 620-720D	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON SEVERAL FLOOR SUPPORTS STA 620 - STA 720D, STR 27L - STR 27R.						2	L	7	3 	4F				A3WE    					 
1999052800364	19990528	00364	NM  	1999	5	28	99ZZZX2118       	1	19990401	G	5320		SUPPORT         			BOEING	727   	727227      	1384078	NM  										BS 540	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON FLOOR SUPPORT STA 540 ABOVE STR 27R.						2	L	7	3 	4F				A3WE    					 
1999052800365	19990528	00365	NM  	1999	5	28	99ZZZX2119       	1	19990325	G	5330		SKIN            			BOEING	727   	727227      	1384078	NM  	RROYCE	DART  	DART5327R   	54509	NE  					BS 1050-1070	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON EXTERIOR SKIN STA 1050 - STA 1070, STR 29R.						2	L	7	3 	4F	4	T		A3WE    	E297				 
1999061100099	19990611	00099	EA  	1999	6	11	99ZZZX2123       	2	19990514	G	8530	76097	CAMSHAFT        			CESSNA	172   	172P        	2072436	CE  	LYC   	O320  	O320D2J     	41508	EA  					ENGINE	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	54844		1550 		5743322	17275065	L1103539A			CAM LOBE WORN OUT CAUSING INTAKE VALVES ON NR 1 AND NR 2 CYLINDERS TO NOT FULLY OPEN.  SYMPTOMS WERE LOW TAKEOFF POWER (	2,000 RPM) AND WOULD NOT IDLE.					1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999061100100	19990611	00100	SO  	1999	6	11	99ZZZX2124       	1	19990511	G	5511	101121805	SPAR            			PIPER 	PA31  	PA31325     	7103105	SO  										HORIZ STABILIZER	CRACKED         	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CE	01	600LB					317812089				WHEN INSTALLING KIT PB 766-646 TO C/W AD 99-06-01 AND PIPER SB 1007, FOUND CRACK IN OUTBOARD SPAR FLANGE RADIUS IN ONE O	F KIT STUB SPARS PN 101121805.  SUBMITTER STATED CRACK APPEARED TO HAVE OCCURRED DURING MANUFACTURE.					1	L	7	2 	3O				A20SO   					 
1999061100102	19990611	00102	SO  	1999	6	11	99ZZZX2126       	1	19990426	G	5102	2230	GORE TAPE       			BALWKS	FIREFY	FIREFLY8B15 		SO  										ENVELOPE	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	01	3287X	47   				F8B553				THE GORE TAPES' STIFF, SHARP EDGES ABRAIDED SEVERAL .1250 INCH HOLES TO THE ENVELOPE PANEL FABRIC ATTACHED TO THE GORE T	APE.  THERE WERE CREASES AND THE EARLY STAGES OF ABRASION TO APPROXIMATELY 50 PERCENT OF THE ENVELOPE FABRIC PANELS.  DU	E TO THE LOW TIME ON THE ENVELOPE AND THE EARLY STAGE OF THE ABRASION, THE FABRIC CURRENTLY MEETS THE TENSILE STRENGTH R	EQUIREMENTS.  IT IS BELIEVED THAT AS THE ABRASION CAUSED BY THE EDGE OF THE GORE TAPE CONTINUES, THE PANELS WILL FAIL TO	 MEET THE TENSILE STRENGTH LIMITS.		1	B	0	0 				NC	A14SO   					 
1999061100103	19990611	00103	CE  	1999	6	11	99ZZZX2127       	1	19990429	G	5220		EXIT            			CESSNA	310   	310Q        	2074242	CE  										FUSELAGE	MISINSTALLED    	B			R2JR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	21	1562T					310Q0756				WHILE INSPECTING AIRCRAFT FOR FERRY FLIGHT, FOUND EMERGENCY EXIT WAS SEALED SHUT AND THERE WAS NO EVIDENCE, IT HAD EVER 	BEEN TESTED AS REQUIRED ON 100-HOUR/ANNUAL INSPECTIONS.  RETURNED AIRCRAFT TO CUSTOMER AS IS.  CUSTOMER/OPERATOR ADVISED	 EMERGENCY EXIT NEEDS TO BE TESTED BEFORE AIRCRAFT WOULD BE SAFE TO FLY ESPECIALLY FAR PART 135.				1	L	7	2 	3O				3A10    					 
1999061100105	19990611	00105	CE  	1999	6	11	99ZZZX2129       	1	19990503	G	8011	1108234	STARTER         			CESSNA	310   	310N        	2074234	CE  										RT ENGINE	MALFUNCTIONED   	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	09	4140Q		873  		A77329	310N0040				THE STARTER IN QUESTION WAS VERY WEAK/SLUGGISH AND WOULD BARELY SPIN ENGINE FAST ENOUGH TO START.  UPON REPLACEMENTS OF 	STARTER, ALL OPERATIONS RETURNED TO NORMAL.					1	L	7	2 	3O				3A10    					 
1999061100106	19990611	00106	SW  	1999	6	11	99ZZZX2130       	1	19990429	G	3232	4196001C	ACTUATOR        	DUKES       		MOONEY	M20   	M20C        	5870208	SW  										MLG	FAILED          	D	S			O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	7763M	3799 			1838	200016				WHEN GEAR WAS SELECTED DOWN, THE GEAR STARTED DOWN THEN TRIPPED THE LANDING GEAR CIRCUIT BREAKER.  REMOVAL OF THE GEAR M	OTOR REVEALED THE ARMATURE ARCED AND BURNED.  ONE OF THE BRUSH LEADS WAS WRAPPED AROUND THE STUD HOLDING THE LEAD.  THIS	 HELD THE BRUSH OFF OF THE ARMATURE CAUSING THE MOTOR TO FAIL.  THE BRUSHES WERE APPROXIMATELY ONE-HALF WORN.				1	L	7	1 	3O				2A3     					 
1999061100107	19990611	00107	SO  	1999	6	11	99ZZZX2131       	1	19990506	G	5320	2050027	ANGLE           			PIPER 	PA24  	PA24260     	7102406	SO  										BS 254-257	LOOSE           	D	L			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	13	9219P	4728 				244715				WHILE PERFORMING RECURRENT INSPECTION FOR AD 94-13-10, A CREAKING NOISE WAS HEARD COMING FROM THE ANGLES SUPPORTING THE 	STABILATOR TORQUE TUBE BEARING SUPPORT FITTINGS.  THE SOURCE OF THE  NOISE WAS NOT SPECIFIED IN THE AD.  LOOSE RIVETS WE	RE DISCOVERED AFTER DISASSEMBLY AT FS 254 TO FS 257 WHERE THE ANGLES, P/N'S 20500-27, DASH 28, AND DASH 29 ATTACH TO THE	 FUSELAGE.  WEAR MARKS WERE DISCOVERED BEHIND THESE ANGLES AND ON THE AFT BULKHEAD P/N 20479-15 WHERE THE LOWER ANGLE AS	SEMBLY MEETS THE BULKHEAD.		1	L	7	1 	3O				1A15    					 
1999061100108	19990611	00108		1999	6	11	99ZZZX2132       	1	19990505	G	2622	111155532412A	FIRE EXTINGUISH 	SEMCA       																CABIN	MISOVERHAULED   	B		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	23					21872					OWNER/OPERATOR SENT IN A FIRE EXTINGUISHER UNIT FOR HYDROSTATIC RETEST AND OVERHAUL.  AFTER THE RECEIVING PROCESS, THE U	NIT WAS ROUTED TO THE PRODUCTION DEPARTMENT.  AFTER UNIT HAD BEEN PROPERLY DUMPED OF ITS CONTENTS, THE TECH THEN PROCEED	ED TO TEAR DOWN UNIT.  DURING TEAR DOWN, TECH OBSERVED THE YELLOW OUTLET HAD BEEN FIRED, BUT UNIT WAS FULL PRIOR TO GEAR	 DOWN.  DISCHARGE PORT SHOULD HAVE HAD A DISC INSTALLED,  HAD A STEEL PLUG IN ITS PLACE.   SUPERVISOR NOTIFIED DIRECTOR 	OF QUALITY.  OWNER/OPERATOR NOTIFIED.  SUBMITTER SUGGESTED POSSIBLE CAUSE WAS FAILURE TO PROPERLY FOLLOW CMM DURING LAST	 OVERHAUL.														 
1999061100109	19990611	00109	CE  	1999	6	11	99ZZZX2133       	1	19990428	G	3246	C1630060102	WHEEL           			CESSNA	206   	TU206F      	2073353	CE  										MLG	FAILED          	D				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			NM	11	8482Q	6400 			760318	TU20603340				WHEEL FAILED WHILE TAXIING.  APPARENTLY, ONE OF THE 6 BOLTS ON OUTSIDE FLANGE LOOSENED TORQUE OVER TIME.  A FEW BOLTS BR	OKE AND CENTER HUB FRACTURED AT REMAINING BOLT LOCATION.  SUBMITTER RECOMMENDED EITHER A LIFE-LIMIT ON PART, OR THE OPTI	ON TO INSTALL BOLT THROUGH ASSEMBLY TO BRAKE SIDE OR INCREASE INSPECTION TIMES.				1	H	7	1 	3O				A4CE    					 
1999061100110	19990611	00110	NE  	1999	6	11	99ZZZX2134       	3	19990428	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			3842 					HJ203A		EROSION SHIELD DEBONDED.  DEBOND ON BLADE NR 1 IN DEICE BOOT AREA.  REPAIRED DEBOND AND INSTALLED NEW DEICE BOOT IAW MFG	 CMM.															5	C	P10N	 
1999061100111	19990611	00111	NE  	1999	6	11	99ZZZX2135       	3	19990428	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			2530 					H565		EROSION SHIELD DEBONDED.  DEBOND ON BLADE NR 4 IN DEICE BOOT AREA.  REPAIRED AND INSTALLED NEW DEICE BOOT IAW MFG CMM.																5	C	P10N	 
1999061100112	19990611	00112	NE  	1999	6	11	99ZZZX2136       	3	19990411	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3I     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			3169 					45568		NR 3 BLADE DEBONDED.  DISASSEMBLED PROPELLER.  OVERHAULED NR 3 BLADE AND REPLACED EROSION SHIELD.  ASSEMBLED PROPELLER, 	SET BLADE ANGLES REVERSE 14.5, FEATHER 79.0, AND LOW PITCH 18.6, AND STATIC BALANCED COMPONENT.															5	C	P10N	 
1999061100113	19990611	00113	NE  	1999	6	11	99ZZZX2137       	3	19990411	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			2597 					45621		EROSION SHIELD DEBOND ON NR 4 BLADE.  REPAIRED EROSION SHIELD DEBOND, AND INSTALLED NEW DEICE BOOT.																5	C	P10N	 
1999061100114	19990611	00114	NE  	1999	6	11	99ZZZX2138       	3	19990428	G	6111	D1533	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			1853 					H5601		EROSION SHIELD DEBONDED.  DEBOND ON BLADE NR 1 UNDER DEICE BOOT ABOUT 3 SQUARE INCHES TOTAL AT BUTT END, REPAIRED, AND I	NSTALLED NEW DEICE BOOT.															5	C	P10N	 
1999061100115	19990611	00115	NE  	1999	6	11	99ZZZX2139       	3	19990428	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			1421 					HJ988		EROSION SHIELD DEBONDED UNDER DEICE BOOT ON BLADE NR 3.  REPAIRED DEBONDED EROSION SHIELD AND INSTALLED NEW DEICE BOOT O	N BLADE NR 3.															5	C	P10N	 
1999061100116	19990611	00116	NE  	1999	6	11	99ZZZX2140       	3	19990401	G	6111	D5133	EROSION SHIELD  													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01								H51023		BLADE EROSION SHIELD DEBONDED.  FOUND DURING OVERHAUL.  REPLACED EROSION SHIELD ON BLADE 11743.																5	C	P10N	 
1999061100117	19990611	00117	SW  	1999	6	11	99ZZZX2141       	1	19990512	G	6510	406040340101	DISC PAC        			BELL  	407   	407         		SW  										TAIL ROTOR	OUT OF LIMITS   	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	407FC	13250				53050				TAIL ROTOR DISC PACKS OUT OF LIMITS.  REPLACED WITH NEW DISC PACS FROM BELL HELICOPTER.						1	G	7	1 	3U			O	H2SW    					 
1999061100118	19990611	00118		1999	6	11	99ZZZX2142       	4	19990426	G	3120	102149	HOUR METER      			HUGHES	369   	369D        	4470706	WP  										COCKPIT	INOPERATIVE     	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	369AW					470117D				HOUR METER INOPERATIVE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999061100119	19990611	00119	WP  	1999	6	11	99ZZZX2143       	1	19990426	G	7810	369A8230517	STACK           			HUGHES	369   	369D        	4470706	WP  										EXHAUST	CRACKED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	369AW					470117D				EXHAUST STACK CRACKED.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999061100120	19990611	00120	WP  	1999	6	11	99ZZZX2144       	1	19990426	G	7810	369A8230517	STACK           			HUGHES	369   	369D        	4470706	WP  										EXHAUST	CRACKED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	369AW					470117D				EXHAUST STACK CRACKED.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999061100121	19990611	00121	WP  	1999	6	11	99ZZZX2145       	1	19990426	G	7810	369A8230503	STACK           			HUGHES	369   	369D        	4470706	WP  										EXHAUST	CRACKED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	369AW		5    			470177D				STACK CRACKED.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999061100122	19990611	00122		1999	6	11	99ZZZX2146       	4	19990426	G	3422	RCA15BK2	GYRO            			BELL  	206   	206B3       	1181506	SW  										COCKPIT	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY		231  		4370	2871				DIRECTIONAL GYRO WILL NOT UNCAGE/UNFLAG.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999061100123	19990611	00123	SW  	1999	6	11	99ZZZX2147       	1	19990427	G	2435	23032027	STARTER         			BELL  	206   	206B        	1181511	SW  										STARTER/GEN	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BX		469  		5495	2872				STARTER WOULD NOT PRODUCE MORE THAN 13 PERCENT N1.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999061100125	19990611	00125	SO  	1999	6	11	99ZZZX2149       	1	19990322	G	3230	6760000	RESTRICTOR      		6774802     	PIPER 	PA32  	PA32R300    	7103213	SO  										MLG	MISINSTALLED    	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NE	01	5910V	2965 				32R7780377				DURING ANNUAL INSP, EMERGENCY GEAR EXTENSION SYSTEM WAS DEPLOYED.  THE RT MAIN GEAR CAME DOWN VIOLENTLY AND THE LT MAIN 	GEAR AND NOSE GEAR PARTIALLY DEPLOYED.  INVEST REVEALED THE RESTRICTOR PN 67600-00 THAT SHOULD HAVE BEEN INSTALLED IN TH	E RT MAIN GEAR RETURN LINE WAS INSTEAD INSTALLED IN THE RETURN LINE FOR THE NOSE GEAR AND LT MAIN GEAR.  THIS ALLOWED RT	 MAIN GEAR TO OPERATE WITHOUT RESTRICTION WHILE INTRODUCING A RESTRICTION IN THE NOSE GEAR LINE AND DOUBLING RESTRICTION	 IN LT MAIN GEAR LINE.  RESTRICTOR PROPERLY INSTALLED AND EMERG EXT SYS OPERATED NORMALLY.  IT IS NOT KNOWN  HOW LONG TH	E SYS WAS CONFIGURED INCORRECTLY, BUT ANY ANNUAL OR 100 HR INSP MUST INCLUDE A TEST OF THE EMERG GEAR EXTENSION SYS.	1	L	7	1 	3O				A3SO    					 
1999061100126	19990611	00126	SW  	1999	6	11	99ZZZX2150       	1	19990508	G	5711		SPAR            			MOONEY	M20   	M20E        	5870212	SW  										LT WING	CORRODED        	C				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	5636Q	3503 				0674				LOWER SPAR CAP ON STUB SPAR FROM STA 33 OUTBOARD SUFFERING FROM INTERGRANULAR CORROSION SO SEVERE THAT IT REQUIRED REPLA	CEMENT.  CORROSION FOUND WHILE REPLACING DAMAGED OUTBOARD WING ASSEMBLY, AND WAS NOT DETECTABLE FROM INSPECTIONS PERFORM	ED DURING ANNUAL INSPECTIONS.				1	L	7	1 	3O				2A3     					 
1999061100127	19990611	00127		1999	6	11	99ZZZX2151       	2	19990424	G	8520		CRANKSHAFT      			AMTR  		RV6         			CONT  		IO360A      							ENGINE	FAILED          	G				A				UNSCHED LANDING         				Y			ENGINE STOPPAGE           			CR	CRUISE         	1			GL	11	527RL	63   			77850	23426	L902051A			BROKEN CRANKSHAFT WHILE IN CRUISE FLIGHT.   ENGINE SEIZED.  LANDED ON ROAD WITHOUT COMPLICATIONS.  NO OTHER DAMAGE.									0 										 
1999061100128	19990611	00128	CE  	1999	6	11	99ZZZX2152       	1	19990510	G	5340	04310093	FITTING         			CESSNA	150   	152         	2071835	CE  										FUSELAGE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	49848	6900 				15281357				THERE ARE 2 OF THESE FITTINGS USED TO SECURE VERTICAL FIN TO FUSELAGE.  THE RIGHT FITTING WAS CRACKED AT THE BASE IN THE	 RADIUS.  THIS CRACK WAS FOUND DURING A 100-HOUR INSPECTION.  BOTH FITINGS WERE CHANGED AS PRECAUTION.  CAUSE UNKNOWN.					1	H	7	1 	3O			NT	3A19    					 
1999061100129	19990611	00129	CE  	1999	6	11	99ZZZX2153       	1	19990423	G	2820	1200406176	LINE            			CESSNA	206   	TU206F      	2073353	CE  										FUEL SYSTEM	LEAKING         	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NM	11	1002V	3072 				U20602387				FUEL LINE HAD A LEAK THAT SEEMED TO BE INTERMITTENT.  APPARENTLY, THE VARIED TENSION IN RELATION TO WING AND CABIN ALLOW	ED THE OPENING TO OPEN FURTHER.  INVESTIGATION REVEALED A PIN HOLE CAUSED BY CORROSION AS THE CAUSE.  THE CORROSION APPE	ARED TO BE CAUSED BY MOISTURE HELD AGAINST LINE AT THE UPPER CHAFE STRIP.  NOTE:  AIRCRAFT HAS MINIMAL SURFACE CORROSION	 ON REMAINDER OF AIRCRAFT.			1	H	7	1 	3O				A4CE    					 
1999061100130	19990611	00130	WP  	1999	6	11	99ZZZX2154       	1	19990426	G	6220	069D21400503	DAMPER          			HUGHES	369   	369D        	4470706	WP  										MAIN ROTOR	DAMAGED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	1097J		4912 			900801D				MAIN ROTOR VIBRATION.  WILL NOT ZERO, TOO MANY THREADS SHOWING WHEN ZERO ON TURNBUCKLE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999061100131	19990611	00131	SW  	1999	6	11	99ZZZX2155       	1	19990426	G	2460	A700ZC7	RELAY           			BELL  	206   	206B        	1181511	SW  										E/E BAY	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	9907K		3402 		CC61224	2040				RELAY INTERMITTENT.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999061100132	19990611	00132		1999	6	11	99ZZZX2156       	4	19990426	G	3455	KY196	RADIO           			BELL  	206   	OH58A       	1181579	SW  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	58AG		103  		11938	7221131				SOUNDS GARBLED IN PILOT HEADSET WHEN  TRANSMITTING.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999061100133	19990611	00133	SO  	1999	6	11	99ZZZX2157       	2	19990506	G	7414	M3050	IMPULSE COUPLING	SLICK       	6310        	CESSNA	182   	182Q        	2072732	CE  	CONT  	O470  	O470U       	17026	SO  					MAGNETO	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	9624E	505  				18268432				BOTH INMPULSE COUPLINGS ARE REJECTED DUE TO RUST ON AND AROUND THE PAWLS AND RIVETS.						1	H	7	1 	3O	3	O	NT	3A13    	E273				 
1999061100134	19990611	00134	EU  	1999	6	11	99ZZZX2158       	1	19990505	G	7931	DK040	TRANSMITTER     			BOLKMS	105   	BO105S      	5626006	EU  										ENGINE	MALFUNCTIONED   	D				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			CE	03	2784F	1    			8274	S621				PILOT OBSERVED LOW FUEL PRESSURE.  SENDING UNIT LAST 10 MINUTES TO 1 YEAR.  INSTALLED DK040 ON AIRCRAFT, PERFORMED GROUN	D RUN, OPERATIONAL CHECK, AND LEAK CHECK.  RAN AIRCRAFT 15 MINUTES.  PILOT REDUCED ENGINE RPM TO FLIGHT IDLE.  INSTRUMEN	T PEGGED HIGH SIDE.  THESE PARTS LAST 10 MINUTES TO 1 YEAR.				1	G	7	2 	3U				H3EU    					 
1999061100135	19990611	00135	NM  	1999	6	11	99ZZZX2159       	1	19990510	G	7920	369D2571213	LINE            			DOUG  	600N  	600N        	3027377	NM  										ENGINE	CHAFED          	H		A		O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		NR	NOT REPORTED   	1			WP	05	957SD	348  				RN011				THIS AIRCRAFT WAS ON POLICE PATROL IN THE MOUNTAINS.  JUST PRIOR TO LANDING, PILOT HAD A LOW OIL PRESSURE LIGHT COME ON 	FOR MIR TRANSMISSION.  PILOT LANDED AND FOUND THE ENGINE AND COMPARTMENT SOAKED IN OIL.  MECHANIC LATER FOUND, SAID OIL 	LINE, CHAFED THROUGH FROM RUBBING ON ENGINE AIR HARD LINE.  ALL MIR TRANMISSION OIL LEAKED OUT ON ENGINE.				1	G	7	1 	3U			NC	H3WE    					 
1999061200006	19990612	00006	WP  	1999	6	12	99ZZZX2160       	1	19990501	G	2410	ALUBAX1R	ALTERNATOR      			HUGHES	269   	269C        	4470504	WP  										ENGINE	DAMAGED         	D		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	25	9623F	71   			8111593	800031				ALTERNATOR PULLEY COOLING FINS BECAME DETACHED FROM PULLEY CAUSING ALTERNATOR TO VIBRATE OFF ENGINE SHEARING BRACKET BOL	TS.  INSTALLED NEW BOLTS AND ALTERNATOR.  PROBLEM HAS NOT RECURRED.  POSSIBLE CAUSE IS FATIGUE OF COOLING FINS.  SUGGEST	 INSPECTION OF FINS EACH 100 HOURS FOR CRACKS.				1	G	7	1 	3O				4H12    					 
1999061100136	19990611	00136	WP  	1999	6	11	99ZZZX2161       	1	19990505	G	6220	369A10053	DAMPER PIN      			HUGHES	369   	369D        	4470706	WP  										M/R HUB	LOOSE           	B		A	EOOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	5074R	59   				1151D				DURING A 100-HOUR INSPECTION, THE DAMPER PIN WAS FOUND UNCOUPLED FROM THE PIN ADJUSTMENT NUT.  INSPECTED, RE-TORQUED, AN	D RE-INSTALLED.					1	G	7	1 	3U				H3WE    					 
1999061100137	19990611	00137	WP  	1999	6	11	99ZZZX2162       	1	19990505	G	2821	RT170277	TIME DELAY      			HUGHES	369   	369D        	4470706	WP  										FUEL FILTER	MALFUNCTIONED   	B			EOOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	5074R					1151D				DURING A 100-HOUR INSPECTION OF ANTI-ICE FUEL FILTER ASSEMBLY, DISCOVERED THE TIME DELAY FOR THE BYPASS INDICATOR PRESS-	TO-TEST WAS NOT DELAYING THE SIGNAL.  REPLACED TIME DELAY.					1	G	7	1 	3U				H3WE    					 
1999061100138	19990611	00138	SW  	1999	6	11	99ZZZX2163       	1	19990423	G	6320	20404029001	RETAINER        		206040004101	BELL  	206   	206L1       	1182107	SW  										GEARBOX	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5000G	15804	4493 		BMC45252	45163				THE NYLON RETAINER FOR THE PLANATARY GEAR BEARING WAS FOUND IN THE TRANSMISSION OIL SCREEN IN SMALL PIECES.  SUBMITTER S	TATED THIS IS THE FOURTH TRANSMISSION IN THE LAST 6 MONTHS WITH THIS PROBLEM.					1	G	7	1 	3U				H2SW    					 
1999061100139	19990611	00139	SW  	1999	6	11	99ZZZX2164       	1	19990511	G	6220	222010403007	RING            			BELL  	222   	222U        	1182140	SW  										SWASHPLATE	DAMAGED         	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	111DS	2300 			EA37	47554				REPLACED WITH NEW OUTER RING FROM BELL HELICOPTER.						1	G	7	2 	3U				H9SW    					 
1999061100140	19990611	00140	NE  	1999	6	11	99ZZZX2165       	3	19990513	G	6111	57D0495	FORK            			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	PITCH CHANGE	CRACKED         	B			EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03			4633 		1490NR			HJ47A		FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS.  THREE CRACKS.						2	L	7	2 	4T			RT	A24CE   		5	C	P10N	 
1999061100141	19990611	00141	CE  	1999	6	11	99ZZZX2166       	1	19990513	G	2121	C209690C	MOTOR           			CESSNA	340   	340A        	2076405	CE  										RECIRC FAN	DAMAGED         	H				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			EA	11	339BE				229	340A044				FAN OVERHEATED, SMOKE IN CABIN.  THE TOP END BELL BEARING FAILED CAUSING THE ARMATURE TO RUB ON STATOR.						1	L	7	2 	3O				3A25    					 
1999061100142	19990611	00142	CE  	1999	6	11	99ZZZX2167       	1	19990508	G	2121	C209690C	MOTOR           			CESSNA	340   	340A        	2076405	CE  										RECIRC FAN	DAMAGED         	H				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			EA	11	338BE				105	340A034				FAN IS INOPERATIVE.  SMOKE IN CABIN.  MOTOR COVER DENTED CAUSING BRUSH LEADS TO SHORT ON MOTOR COVER.  SUBMITTER SUGGEST	ED INSULATION TAPE INSIDE MOTOR COVER MAY HELP TO PREVENT THIS TYPE OF FAILURE IN THE FUTURE.					1	L	7	2 	3O				3A25    					 
1999061100143	19990611	00143	CE  	1999	6	11	99ZZZX2168       	1	19990406	G	2121	C209690C	MOTOR           			CESSNA	340   	340A        	2076405	CE  										RECIRC FAN	DAMAGED         	H				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			EA	11	336BE				235	340A028				FAN IS INOPERATIVE.  SAW SPARKS COMING FROM MOTOR VENT.  MOTOR COVER DENTED CAUSING BRUSH LEADS TO SHORT ON MOTOR COVER.	  SUBMITTER SUGGESTED INSULATION TAPE INSIDE MOTOR COVER MAY HELP TO PREVENT THIS TYPE OF FAILURE IN THE FUTURE.					1	L	7	2 	3O				3A25    					 
1999061100144	19990611	00144	CE  	1999	6	11	99ZZZX2169       	1	19990312	G	3232	660402	BYPASS VALVE    			CESSNA	650   	650         	2076802	CE  										MLG	FAILED          	H				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			GL	11	475M					6500062				THE LANDING BYPASS VALVE FAILED AND CAUSED AN EMERGENCY LANDING.						2	L	7	2 	4F				A9NM    					 
1999061100145	19990611	00145	NM  	1999	6	11	99ZZZX2170       	1	19990412	G	2710	52119	BUSHING         			UNIVAR	415   	A2ALON      	0540102	NM  										CONTROL COLUMN	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01	6560Q	1760 				A60				OLD BUSHING IS PLASTIC MATERIAL.  WEARS AND BECOMES BRITTLE.  CAUSES EXCESS AILERON PLAY.   DIFFICULT TO INSPECT AND WOR	K ON.  LOCATION TOP OF CONTROL COLUMN FORWARD UNDER INSTRUMENT PANEL.  NEW BUSHING UNIVAR PN 52119 IS MADE OF METAL.  SU	BMITTER STATED PLASTIC BUSHING SHOULD BE REPLACED AT 800 HOURS TIS.				1	L	7	1 	3O				A787    					 
1999061100148	19990611	00148	NE  	1999	6	11	99ZZZX2173       	2	19990501	G	7230	2A0847	SEAL            								IAE   	V2500 	V2500A1     		NE  					NR 4 BEARING	CRACKED         	B			WNFR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03					0260					SUBMITTER STATED THIS IS AN ON-GOING PROBLEM WITH THIS PART.  FAIL F.P.I. FOR CRACKS ALMOST ALWAYS IN THE SAME GENERAL A	REA.										4	F			E311NE				 
1999061100149	19990611	00149	EU  	1999	6	11	99ZZZX2174       	1	19990513	G	3000		DUCT            			AMD   	FALC50	FALCON50MYST	2730106	EU  										ANTI-ICE SYSTEM	LOOSE           	B		A	VO2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01	96UT					192				INSPECTED S-DUCT ANTI-ICE DISTRIBUTION DUCT AND FOUND RIVETS MISSING.  INSPECTED 4 OTHER FALCON50 AIRCRAFT AND FOUND SAM	E PROBLEM.  RIVETS LOOSE OR MISSING FROM UPPER AIR DISTRIBUTION.  DUCT INSIDE OF AFT BAY AREA.					2	L	7	3 	4F				A46EU   					 
1999061100150	19990611	00150	CE  	1999	6	11	99ZZZX2175       	1	19990423	G	5610	10138402515	WINDSHIELD      			BEECH 	200   	200BEECH    	1152920	CE  										COCKPIT	CRACKED         	B			BONR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	19	94FG	2149 			95118H7197	BB433				PILOT'S WINDSHIELD CRACKED IN-FLIGHT.  CRACK STARTED IN LOWER INBOARD CORNER.  PILOT REPORTED NO SURFACE DISTORTION IN A	 SMALL SUSPICIOUS AREA PRIOR TO FLIGHT.  RECOMMEND A SECTION IN THE PILOT'S FLIGHT MANUAL THAT WILL GIVE A PILOT GUIDANC	E REGARDING WINDSHIELD DELAMINATION/CRACKS.				1	L	7	2 	4T				A24CE   					 
1999061100151	19990611	00151	CE  	1999	6	11	99ZZZX2176       	1	19990428	G	2910	2407003466	LINE            			LEAR  	25    	25D         	5170514	CE  										HYDRAULIC SYSTEM	RUPTURED        	B		A	FEHR	O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		NR	NOT REPORTED   	1			SO	13	531CW					231				HYDRAULIC PRESSURE LINE RUPTURED IN-FLIGHT DUE TO 'RUBBING' AGAINST ANOTHER HYDRAULIC LINE'S FITTINGS.  THE RUPTURE CAUS	ED A LOSS OF HYDRAULIC SYSTEM PRESSURE AND DEPLETION OF THE HYDRAULIC RESERVOIR.  THE LINE IS LOCATED AT THE AFT PRESSUR	E BULKHEAD AND IS DIFFICULT TO SEE DURING INSPECTION.				2	L	7	2 	4J				A10CE   					 
1999061100152	19990611	00152	CE  	1999	6	11	99ZZZX2177       	1	19990311	G	3233	99121201	ACTUATOR        			CESSNA	500   	550         	2076604	CE  										NLG	FAILED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	09	6846T				240	5500625				NLG ACTUATOR WAS REMOVED AND SENT TO CESSNA AFTER FAILING SLOW CYCLE TEST.  ACTUATOR WAS RE-INSTALLED AFTER REPAIR.  OPS	 CHECK SHOWED NO FAULTS.  ON FIRST FLIGHT, PILOTS WERE NOT ABLE TO GET AN 'UP AND LOCKED' LIGHT.  AIRCRAFT LANDED WITHOU	T INCIDENT.  POST-FLIGHT TROUBLESHOOTING DETERMINED ACTUATOR HAD FAILED INTERNALLY.  ACTUATOR WAS REMOVED AND SENT TO CE	SSNA FOR EVALUATION.  CYCLES, 2,067.			1	L	7	2 	4F				A22CE   					 
1999061100154	19990611	00154	CE  	1999	6	11	99ZZZX2179       	1	19990416	G	5610	10138402515	WINDSHIELD      	PPG         		BEECH 	200   	200BEECH    	1152920	CE  										COCKPIT	SHATTERED       	G				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			EA	23	200AP	2500 			94339H8966	BB277				PILOT'S WINDSHIELD INNER PANE SHATTERED DURING CRUISE FLIGHT.  WINDSHIELD APPEARED TO BE INSTALLED PROPERLY.  NO OBVIOUS	 DEFECTS.  REPLACED WINDSHIELD WITH NEW ONE.					1	L	7	2 	4T				A24CE   					 
1999061100155	19990611	00155	EA  	1999	6	11	99ZZZX2180       	2	19990430	G	8530		CYLINDER        			PIPER 	PA28  	PA28R201    	7102816	SO  	LYC   	O360  	IO360C1C6   	41514	EA  					ENGINE	FAILED          	D				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CL	CLIMB          	1			NE	01	173ND	1538 				2837025	L1870051A			AFTER NORMAL TAKEOFF, A BANG WAS HEARD AND THE AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.  AN INSPECTION REVEALED	 A CYLINDER BARREL TO CYLINDER HEAD SEPARATION.  ENGINE RETURNED TO FACTORY FOR INSPECTION.  NR 2 CYLINDER FAILED.  REF:	  INCIDENT NR BOS99017; EAST COAST AERO CLUB.				1	L	7	1 	3O	3	O		2A13    	1E10				 
1999061100156	19990611	00156	EA  	1999	6	11	99ZZZX2181       	2	19990501	G	7414	105136029	SHAFT           			PIPER 	PA28  	PA28150     	7102804	SO  	LYC   	O360  	O360A1A     	41514	EA  					MAGNETO	SHEARED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	5738W	625  				281434	L327736A			WHILE PERFORMING OPERATIONAL CHECK OF MAGNETO SYSTEM, NOTED THAT NORMAL DROP OCCURRED AT 1,800 RPM'S, BUT WAS ROUGH AT L	OWER RPM'S.  AFTER ELIMINATING PLUGS AND IGNITION HARNESS FOR DEFECTS, PULLED AND INSPECTED MAGNETO.  UPON OPENING THE P	OINT/CAPACITOR AREA, EVERYTHING APPEARED NORMAL UNTIL MULTIPLE REVOLUTIONS WERE APPLIED TO DRIVE GEAR.  ACCEPTABLE POINT	 GAP DIMINISHED TO NO POINT GAP.  UPON SPLITTING THE MAG CASE, IT WAS EVIDENT MAGNET SHAFT HAD SHEARED JUST BELOW THE WO	ODRUFF KEYWAY UNDER THE DRIVEN GEAR.  MODERATE BEARING AND RACE DISTRESS WERE NOTED.  NOTE:  UNIT STILL OPERATIONAL.  UN	IT REPLACED BY FACTORY O/H UNIT.  PART TIS:   625 HOURS SINCE NEW AND HAD NOT BEEN OPENED IN THE FIELD PRIOR TO FAILURE.	1	L	7	1 	3O	3	O		2A13    	E286				 
1999061100157	19990611	00157	CE  	1999	6	11	99ZZZX2182       	1	19990514	G	5511	043200159	SPAR            			CESSNA	150   	152         	2071835	CE  										HORIZ STABILIZER	MISDRILLED      	H			CB9T	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15					07088					STABILIZER APPEARS TO HAVE BEEN REPAIRED USING NEW SKINS AND USED P/N 0432001-56 SPARS AND USED P/N 0432001-15 REINFORCE	MENT.  THE RIVETS SECURING THE SKINS TO THE SPARS DO NOT ALIGN WITH THE EXISTING HOLES IN THE SPARS OR REINFORCEMENT.  T	HIS LEAVES UNFILLED HOLES IN SPARS AND REINFORCEMENT ALONG ENTIRE LENGTH ON TOP AND BOTTOM OF TRALING EDGE OF STABILIZER	.  THE UNFILLED HOLES ARE APPROXIMATELY ONE TO FOUR RIVET DIAMETERS FROM NEW RIVETS.  THIS IS EVIDENT IN APPROXIMATELY S	EVENTY-FIVE PLACES.		1	H	7	1 	3O			NT	3A19    					 
1999061100158	19990611	00158	SO  	1999	6	11	99ZZZX2183       	1	19990501	G	2720	82815023	CONTROL CABLE   			PIPER 	PA46  	PA46350P    	7104602	SO  										RUDDER	WORN            	B	P	A	AMYR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	05	321CR					4636124				DURING PRE-PURCHASE INSPECTION, DISCOVERED THE RT FWD RUDDER CABLE SHOWING SIGNS OF WEAR AT THE AILERON/RUDDER INTERCONN	ECT ASSY.  THE CABLE WAS STILL FOUND TO BE IN AN AIRWORTHY CONDITION, BUT WITH THE WEAR FOUND AT 406.0 HRS ACFT TT, IT W	OULD HAVE BEEN SOON AFTER THAT THE CABLE WOULD BECOME UNAIRWORTHY.  DETERMINED THE CAUSE OF THIS WEAR STEMS FROM THE INT	ERCONNECT ASSY CABLES ARE RIDING TOO HIGH ON THE CABLE GUIDE JUST AFT OF THE INTERCONNECT.  THIS CONDITION CAUSES THE BO	TTOM INTERCONNECT ARM TO RUB AGAINST  THE CABLE CAUSING WEAR.  TO RECTIFY THIS CONDITION, THE GROOVES FOR THE CABLES TO 	THE CABLE GUIDE MUST BE FILED DOWN TO ALLOW THE CABLE TO MOVE FREELY BETWEEN THE TWO ARMS.	1	L	7	1 	3O			RT	A25SO   					 
1999061100159	19990611	00159	SO  	1999	6	11	99ZZZX2184       	2	19990327	G	8540	Q6642	ADAPTER         			CESSNA	421   	421B        	2076014	CE  	CONT  	O520  	GTSIO520H   	17032	SO  					STARTER	MAKING METAL    	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	25	1942G					421B0842	267392R			FOUND RT ENGINE OIL FILTER CONTAMINATED WITH METAL.  METAL COMING FROM STARTER ADAPTER BEARING HOUSING.  KIT QE6642 INST	ALLED BY FACTORY, ALSO CSB 94.4 REPETITIVE INSPECTION N/A PER LOG BOOK.  INSPECTED LT ENGINE PER CSB 94-4.  OK AT THIS T	IME.				1	L	7	2 	3O	3	O		A7CE    	E7CE				 
1999061100160	19990611	00160	GL  	1999	6	11	99ZZZX2185       	3	19990504	G	6111	13012	CLAMP           			PIPER 	PA24  	PA24180     	7102402	CE  						HARTZL	HC92Z	HC92ZK8     	GL  	PROPELLER	CRACKED         	B			LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	6073P				T2153	241169		653F		INDICATION EXTENDED AROUND CORNER AT OUTBOARD BOLT HOLE.						1	L	7	1 	3O			NT	1A15    		5	C	P892	 
1999061100162	19990611	00162	SO  	1999	6	11	99ZZZX2187       	1	19990410	G	3230	9800400	CLAMP           			PIPER 	PA36  	PA36285     	7103610	SO  										MLG	BROKEN          	D		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	07	9942P	43   				367560053				LEFT MAIN GEAR TWISTED OUT OF MOUNT.  PILOT BRAKED HARD AND THE RESULTING TORSION BROKE THE RETENTION CLAMP.  THE CLAMP 	CASTING METAL LOOKS VERY GRAINEY.  THE BASIC DESIGN LOOKS WEAK AND THE QUALITY OF METAL IS DOUBTFUL.  SUBMITTER SUGGESTE	D .25 INCH 4130 STRAP BE USED TO REINFORCE THIS PRESSURE POINT.				1	L	7	1 	3O				A10SO   					 
1999061100163	19990611	00163	SO  	1999	6	11	99ZZZX2188       	1	19990505	G	5711		SPAR            			PIPER 	PA36  	PA36285     	7103610	SO  										LT WING	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	9942P	5308 				367560053				FOUND STRESS FRACTURE IN THE AFT SPAR ON THE LEFT WING.  THE BREAK WAS 10 INCHES OUTBOARD OF THE FUSELAGE/SPAR ATTACHMEN	T POINT.  SUBMITTER STATED THIS IS THE SECOND TIME TO OBSERVE A BREAK AT THIS POINT IN A PA36.  THIS AREA IS DIFFICULT T	O INSPECT AND NEEDS TO BE GIVEN SPECIAL ATTENTION; AD WOULD BE JUSTIFIED.				1	L	7	1 	3O				A10SO   					 
1999061100165	19990611	00165	CE  	1999	6	11	99ZZZX2190       	1	19990517	G	3710	442CW12	PUMP            			BEECH 	58    	58          	1152740	CE  										ENGINE	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05	99BM	421  			3AM124	TH1816				ENGINE PUMP FAILED AT 421 HOURS TT.						1	L	7	2 	3O				3A16    					 
1999061100166	19990611	00166	EA  	1999	6	11	99ZZZX2191       	2	19990513	G	8520	LW11625	PLUG            			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235N2C     	41505	EA  					;ISTON PIN	WORN            	B			BNZR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	95892		796  			15285979	L2336815			WHILE C/W LYC SI 1492B (PISTON PIN PLUG WEAR INSPECTION) AND FINDING METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMI	TS CONTAINED IN SI 1492B, FOUND THE FORWARD PISTON PIN PLUG EXCESSIVELY WORN DUE TO A PISTON RING WEAR STEP IN THE NR 1 	CYLINDER ON THE FORWARD SIDE WHICH WAS SHEARING OFF PIECES OF THE PISTON PIN PLUG ON EACH STROKE.  IT APPEARED THE PISTO	N WAS NOT RUNNING TRUE IN THE CYLINDER.			1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999061100167	19990611	00167	EA  	1999	6	11	99ZZZX2192       	2	19990514	G	8520	LW11625	PLUG            			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235N2C     	41505	EA  					PISTON PIN	WORN            	B			BNZR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	95617		889  			15285939	L2278415			WHILE C/W LYC SI 1492B (PISTON PIN PLUG WEAR INSPECTION) AND FINDING METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMI	TS CONTAINED IN SI 1492B, FOUND THE FORWARD PISTON PIN PLUG EXCESSIVELY WORN DUE TO A PISTON RING WEAR STEP IN THE NR 1 	CYINDER ON THE FORWARD SIDE WHICH WAS SHEARING OFF PIECES OF THE PISTON PIN PLUG ON EACH STROKE.  SUBMITTER STATED IT AP	PEARED THE PISTON WAS NOT RUNNING TRUE IN THE CYLINDER.			1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999061100168	19990611	00168	EA  	1999	6	11	99ZZZX2193       	2	19990514	G	8520	LW11625	PLUG            			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235N2C     	41505	EA  					PISTON PIN	WORN            	B			BNZR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	95670		1033 			15285957	L1677315			WHILE C/W LYC SI 1492B (PISTON PIN PLUG WEAR INSPECTION) AND FINDING METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMI	TS CONTAINED IN SI 1492B, FOUND THE FORWARD PISTON PIN PLUG EXCESSIVELY WORN DUE TO A PISTON RING WEAR STEP IN THE NR 1 	CYLINDER ON THE FORWARD SIDE WHICH WAS SHEARING OFF PIECES OF THE PISTON PIN PLUG ON EACH STROKE.  SUBMITTER STATED IT A	PPEARED THE PISTON WAS NOT RUNNING TRUE IN THE CYLINDER.			1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999061100169	19990611	00169	EA  	1999	6	11	99ZZZX2194       	2	19990505	G	7322		TUBE            	FACET       	MA45AA      	CESSNA	172   	172K        	2072430	CE  	LYC   	O320  	O320D2G     	41508	EA  					CARBURETOR	LOOSE           	D				E				ENGINE SHUTDOWN         				O			OTHER                     			NR	NOT REPORTED   	1			GL	13	84434				CK816851	17258469	L857039A			ACCELERATING PUMP DISCHARGE TUBE CAME OUT AND STRUCK THROTTLE OPEN, STOPPING ENGINE, THEN PART FELL DOWN INTO THE AIRBOX	.  (THIS OCCURRED IN-FLIGHT AT EFT).					1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999061100170	19990611	00170	CE  	1999	6	11	99ZZZX2195       	1	19990520	G	7921	8526T32	COOLER          			CESSNA	206   	206CESSNA   	2073302	CE  										OIL SYSTEM	LEAKING         	B			RF3R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	23										AFTER PREVIOUS EPOXY REPAIR, PART BEGAN LEAKING IN SERVICE DUE TO EPOXY REPAIR FAILURE.						1	H	7	1 	3O				A4CE    					 
1999061100172	19990611	00172	CE  	1999	6	11	99ZZZX2197       	1	19990514	G	7602	5038901223	CONTROL CABLE   			BEECH 	58    	58          	1152740	CE  										RT ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	7239R	83   				TH565				INSTALLED 3-19-99 AT 2,216.2 HOBBS.  END BROKE OFF 5-14-99 AT 2,299.4.  MIXTURE CONTROL CABLE FAILED ON RIGHT ENGINE.  8	3.2 HOURS/2 MONTHS.					1	L	7	2 	3O			 	3A16    					 
1999061100173	19990611	00173	SO  	1999	6	11	99ZZZX2198       	1	19990501	G	3213	2117400	STRAP           			PIPER 	PA24  	PA24250     	7102404	SO  										LT MLG STRUT	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	7001P					242146				LEFT GEAR STRAP CAME LOOSE AND TURNED AROUND CAUSING THE GEAR NOT TO EXTEND FULLY IN THE DOWN POSITION.  STRAP BRACKET A	SSEMBLY WAS MISSING THE NUT THAT HOLDS IT TOGETHER TO THE MAIN GEAR SPRING ATTACHMENT BRACKET.					1	L	7	1 	3O				1A15    					 
1999061100174	19990611	00174	EA  	1999	6	11	99ZZZX2199       	2	19990514	G	8520	LW11625	PLUG            			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235N2C     	41505	EA  					PISTON PIN	WORN            	B			BNZR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	6466L		1148 			15284404	L2359215			WHILE C/W LYC SI 1492B (PISTON PIN PLUG WEAR INSPECTION) AND FINDING METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMI	TS CONTAINED IN SI 1492B, FOUND THE FORWARD PISTON PIN PLUG EXCESSIVELY WORN DUE TO A PISTON RING WEAR STEP IN THE NR 1 	CYLINDER ON THE FORWARD SIDE WHICH WAS SHEARING OFF PIECES OF THE PISTON PIN PLUG ON EACH STROKE.  SUBMITTER STATED IT A	PPEARED THE PISTON IS NOT RUNNING TRUE IN THE CYLINDER.			1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999061100175	19990611	00175	EA  	1999	6	11	99ZZZX2200       	2	19990503	G	7314	LW15473	PUMP            			PIPER 	PA28  	PA28R201    	7102816	SO  	LYC   	O360  	IO360C1C6   	41514	EA  					FUEL SYSTEM	FOD             	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	630AC		671  		154739210	28R7837074	L1973351A			FOUND ONE-HALF OF WASHER IN OIL SUMP DURING OIL CHANGE.  INSPECTED ENGINE ACCESSORIES AND FOUND THE WASHER WAS MISSING F	ROM THE FUEL PUMP LIFT SHAFT.					1	L	7	1 	3O	3	O		2A13    	1E10				 
1999061100176	19990611	00176	EA  	1999	6	11	99ZZZX2201       	2	19990513	G	8520	LW11625	PLUG            			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235N2C     	41505	EA  					PISTO PIN	WORN            	B			BNZR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	5096L		597  			15284262	L2397115			WHILE C/W LYC SI 1492B (PISTON PIN PLUG WEAR INSPECTION) AND FINDING METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMI	TS CONTAINED IN SI 1492B, FOUND THE FORWARD PISTON PIN PLUG EXCESSIVELY WORN DUE TO A PISTON RING WEAR STEP IN THE NR 1 	CYLINDER ON THE FORWARD SIDE WHICH WAS SHEARING OFF PIECES OF THE PISTON PIN PLUG ON EACH STROKE.  SUBMITTER STATED IT A	PPEARED THE PISTON WAS NOT RUNNING TRUE IN THE CYLINDER.			1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999061100177	19990611	00177	CE  	1999	6	11	99ZZZX2202       	1	19990514	G	5753	232507918	BRACKET         			LEAR  	35    	31          	5170530	CE  										TE FLAP	CRACKED         	B		A	WIBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	11	5VG	5301 				014				FLAP ACTUATOR BRACKET CRACKED AT OPPOSITE END ACTUATOR ATTACHED TO.  RIVETS SHEARED ALSO.  SUBMITTER STATED THIS IS THE 	SECOND FOUND LIKE THIS WITHIN A 2-MONTH TIME FRAME.  BOTH AIRCRAFT HAVE SIMILAR TIMES.					2	L	7	2 	4F			RT	A10CE   					 
1999061100178	19990611	00178	CE  	1999	6	11	99ZZZX2203       	1	19990507	G	5330	12114005	SKIN            			CESSNA	210   	210J        	2073439	CE  										FUSELAGE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	3311S	3600 				21059111				A CRACK WAS FOUND IN THE FORWARD AREA OF THE RIGHT LANDING GEAR (MAIN CUT-OUT).  CESSNA ADVISED THIS WAS A COMMON PROBLE	M AND PROVIDED A LETTER WITH A METHOD OF REPAIR.  THE CRACK WAS APPROXIMATELY 1 INCH LONG AND RAN BENEATH A DOUBLER.					1	H	7	1 	3O				3A21    					 
1999061100179	19990611	00179	CE  	1999	6	11	99ZZZX2204       	1	19990518	G	5521		SPAR            			CESSNA	150   	152         	2071835	CE  										ELEVATOR	CRACKED         	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	17RR	8600 				15287134				RIGHT ELEVATOR OUTBOARD HINGE ATTACH POINT CRACKED AROUND RIVETS ON SPAR.  POSSIBLE CAUSE IS OIL CANNING OF ATTACH POINT	 ON SPAR.					1	H	7	1 	3O			NT	3A19    					 
1999061100180	19990611	00180	SO  	1999	6	11	99ZZZX2205       	1	19990518	G	3230	452729	BEARING         	PARKERHANFIN	3579702     	PIPER 	PA32  	PA32R300    	7103213	SO  										NLG	FAILED          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	05	1392H				23	32R7780156				PILOT REPORTED NOSE GEAR EXTENDED DURING FLIGHT.  INSPECTION REVEALED THE ROD END BEARING ON THE NOSE GEAR ACTUATOR BROK	E ALLOWING THE NOSE GEAR TO FREE FALL TO THE DOWN AND LOCKED POSITION.  THE BREAK IN THE ROD END BEARING SHOWED EVIDENCE	 OF A SMALL CRACK BEFORE THE FAILURE OCCURRED.  DETECTION OF THIS CRACK WOULD REQUIRE DISASSEMBLING THE CONNECTION OF TH	E ROD END BEARING FROM THE NOSE GEAR DOWNLOCK TO PERMIT VISUAL INSPECTION.  THE NOSE GEAR DOWNLOCK WAS NOT DAMAGED.			1	L	7	1 	3O				A3SO    					 
1999061100181	19990611	00181	CE  	1999	6	11	99ZZZX2206       	1	19990413	G	3232	08411044	BELLCRANK       			CESSNA	310   	310R        	2074245	CE  										RT MLG DOOR	FAILED          	C				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	05	1203W	7100 				310R2106				AFTER LANDING, PILOT NOTICED RIGHT INBOARD MAIN GEAR DOOR HANGING DOWN.						1	L	7	2 	3O				3A10    					 
1999061100182	19990611	00182		1999	6	11	99ZZZX2207       	4	19990520	G	6113	87325010	BULHEAD         			PIPER 	PA28  	PA28161     	7102803	SO  						SNSNCH	74D	74DM        	EA  	SPINNER	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	21	113ND	9277 				2841216		A56589		UPON REMOVAL OF SPINNER DURING PHASE INSPECTION, FOUND FORWARD SPINNER BULKHEAD CRACKED.  CRACK RADIATED FROM A SPINNER 	MOUNTING SCREW NUTPLATE RIVET, OUTBOARD TO EDGE AND INBOARD TOWARD PROPELLER BOLT HOLES.  EXAMINATION OF SPINNER SCREW W	ASHERS FOUND ONE TOTALLY DETERIORATED WHICH MAY HAVE BEEN A CONTRIBUTING FACTOR.				1	L	7	1 	3O				2A13    		5	N	P886	 
1999061100183	19990611	00183	EU  	1999	6	11	99ZZZX2208       	1	19990505	G	7931	DK040	TRANSMITTER     			BOLKMS	105   	BO105S      	5626006	EU  										ENGINE	MALFUNCTIONED   	D				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			CE	05	2784F	65   			13360	S621				PILOT OBSERVED LOW FUEL PRESSURE.  SENDING UNIT LAST 10 MINUTES TO 1 YEAR.  INSTALLED DK040 ON AIRCRAFT, PERFORMED GROUN	D RUN, OPERATIONAL CHECK, AND LEAK CHECK.  RAN AIRCRAFT 15 MINUTES.  PILOT REDUCED ENGINE RPM TO FLIGHT IDLE.  INSTRUMEN	T PEGGED HIGH SIDE.  THESE PARTS LAST 10 MINUTES TO 1 YEAR.				1	G	7	2 	3U				H3EU    					 
1999061100184	19990611	00184	GL  	1999	6	11	99ZZZX2209       	2	19990518	G	7230		SCROLL          			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					COMPRESSOR	CRACKED         	B			EOPR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	01	3194P					45788	860263			COMPRESSOR SCROLL P/N 23056109 DEVELOPED AN APPROXIMATELY 4 INCH CRACK ON THE RT SIDE JUST BELOW THE ANTI-ICE VALVE PAD.	  ENGINE POWER CHECKS INDICATED POWER LOSS.  REPLACED COMPRESSOR.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999061100185	19990611	00185	WP  	1999	6	11	99ZZZX2210       	1	19990512	G	2434	ALU8AZIR	PULLEY          			HUGHES	269   	269C        	4470504	WP  										ALTERNATOR	DAMAGED         	D		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	25	9623F	71   			8111593	800031				ALTERNATOR PULLEY COOLING FINS BECAME DETACHED FROM PULLEY CAUSING ALTERNATOR TO VIBRATE OFF ENGINE SHEARING BRACKET BOL	TS.  INSTALLED NEW BOLTS AND ALTERNATOR.  PROBLEM HAS NOT RECURRED.  POSSIBLE CAUSE IS FATIGUE OF COOLING FINS.  SUBMITT	ER SUGGESTED INSPECTION OF FINS EACH 100 HOURS FOR CRACKS.				1	G	7	1 	3O				4H12    					 
1999061100186	19990611	00186	NE  	1999	6	11	99ZZZX2211       	2	19990407	G	7314	02527730007	PUMP            			BELL  	212   	212         	1181420	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					NR 1 ENGINE	FAILED          	H		A		O				OTHER                   				O			OTHER                     			FF	FIRE FIGHTING  	1			WP	17	911HW		2168 		PE1290	31101	CPPS62032			AIRCRAFT WAS RETURNING FROM A FIRE FIGHTING MISSION IN THE STATE OF CHIAPUJ,MEXICO.  NR 1 ENGINE EXPERIENCED AN IN-FLIGH	T SHUT DOWN.  AIRCRAFT LANDED AT A REMOTE DIRT STRIP.  MAINTENANCE PERSONNEL ON BOARD AIRCRAFT FOUND NR 1 ENGINE DRIVEN 	FUEL PUMP HAD FAILED.  REMOVED AND REPLACED PUMP ASSEMBLY.  AIRCRAFT RETURNED TO BASE.  FUEL PUMP DRIVE FROM GEARBOX TO 	FUEL PUMP SPLINES HAD STRIPPED AT FUEL PUMP SIDE.  FUEL PUMP HAD 2,160.3 HOURS TSO.  TBO IS 4,500 HOURS.  FUEL PUMP GAVE	 NO WARNING OF IMPENDING FAILURE.		1	G	7	1 	4U	4	U		H4SW    	E22EA				 
1999061100187	19990611	00187	NM  	1999	6	11	99ZZZX2212       	1	19990514	G	3260	248036820	PROXIMITY SWITCH		VN10312     	AMD   	FALC50	FALCON2000  	2730170	NM  										RT MLG DOOR	MALFUNCTIONED   	B			CW1R	O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			EA	25	790L		450  			15				FLIGHT CREW SELECTED LANDING GEAR DOWN AND GOT THREE RED LIGHTS ON THE ANNUNCIATOR PANEL.  AFTER A DELAY, THE LEFT MAIN 	AND RIGHT MAIN GEAR EXTENDED, BUT NOT THE NOSE.  THE GEAR WAS EMERGENCY DEPLOYED AND THE AIRCRAFT LANDED WITHOUT INCIDEN	T.  THE AIRCRAFT WAS JACKED AND THE PROXIMITY SWITCH ON THE RIGHT MAIN DOOR ACTUATOR WAS CONFIRMED DEFECTIVE.  THE ACTUA	TOR ASSEMBLY WITH SWITCH WAS REPLACED AND THE AIRCRAFT DISPATCHED.			2	K	7	3 	4F			RT	A50NM   					 
1999061100188	19990611	00188	NE  	1999	6	11	99ZZZX2213       	3	19990426	G	6111	D60711	PITCH ROD       			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER	CRACKED         	B			LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	45AR	884  				UE12		HJ557		PITCH ROD CRACKED ON PROPELER.						2	L	7	2 	4T			RT	A24CE   		5	C	P10N	 
1999061100189	19990611	00189	EU  	1999	6	11	99ZZZX2214       	1	19990517	G	3233	AIR400390	SEAL            		AIR864141   	SAAB  	SF340 	340B        	7860101	EU  										NLG	FAILED          	B			FW1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NE	03	423XJ	4375 			LK9700484	340B423				PREMATURE FAILURE OF ACTUATOR RAMROD GLAND SEAL AFTER 4,987 HOURS OF 24,000 HOURS STANDARD OVERHAUL LIFE.  SURFACE FINIS	H OF RAMROD MEASURE ACCEPTABLE.					2	L	7	2 	4T			RT	A52EU   					 
1999061100195	19990611	00195	WP  	1999	6	11	99ZZZX2220       	1	19990305	G	5312		BULKHEAD        			DOUG  	DC10  	DC1030F     	3023504	WP  										BS 1841	CRACKED         	B			M8BB	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	33	10MB					47907				IN NARITA AFTER UNLOADING LC5 PALLET CENTER CARGO COMPT, CARGO HANDLER FOUND IMPACT DAMAGE (CRACK) AT BLKHD STA 1841 BET	WEEN CENTER CARGO AND AFT GARGO HOLD.  CRACKS OF APPROX 7-8 INCHES FROM IMPACT POINT ABOUT 2 INCHES FROM FLOORBOARD LEVE	L.  DAMAGE CAUSED BY A TETHERING DEVICE SHACKLE WHICH MAY HAVE SLIPPED OFF FROM ITS STORAGE BAG AND FALLEN ONTO THE FLOO	R NEAREST TO THE BULKHEAD.  CARGO HANDLERS POSSIBLY UNAWARE OF THIS, MOVED PALLET AGAINST SHACKLE AND IMPACT IT AGAINST 	BLKHD CAUSING CRACK.  REPAIR SPEC GENERATED BY JAL ENG WITH APPROVAL OF FAA 8110-3.  SUBMITTER STATED INSPECT TETHERING 	DEVICE FOR SECURITY PRIOR TO EVERY DEPARTURE.  PLANNING TO HAVE DEVICE REMOVED FROM ACFT.	2	L	7	3 	4F			RT	A22WE   					 
1999061100196	19990611	00196	EA  	1999	6	11	99ZZZX2221       	1	19990422	G	5415	6013704015	BOLT            			CNDAIR	CL600 	CL6002B16   	1900305	EA  										LT NACELLE	INADEQUATE      	B			SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	914X	2132 				5185				DURING INSPECTION, NOTED THERE WAS INSUFFICIENT CLEARANCE BETWEEN THE HEAD OF THE BOLT/PIN AND RETAINER PLATE AS REQUIRE	D (.013 INCH - .078 INCH) IAW PSP601-2 CH 71-00-00 PG 419 PARA(26).   NOTE:  THIS REQUIREMENT HAS JUST BEEN INITIATED IN	TO THIS LAST PROVISION DATED SEPT 4, 1998.				2	L	7	2 	4F			RT	A21EA   					 
1999061100197	19990611	00197	CE  	1999	6	11	99ZZZX2222       	1	19990521	G	3520	C3512000	OXYGEN MASK     	PURITANBENET		CESSNA	500   	550         	2076604	CE  										CABIN	DAMAGED         	B			AZNR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	53FP	8500 				5500434				WHILE INSPECTING OXYGEN MASKS PER AD 99-08-21, 5 MASKS WERE FOUND TORN WITH MFG DATES FROM 1979 TO 1983.  SAME DEFECT AS	 INDICATED IN THE AD/BULLETIN.  ANOTHER ACFT IN FLEET WAS CHECKED AND MORE DEFECTIVE MASKS WERE FOUND.  NONE HAD CURE DA	TES LISTED IN THE AD.				1	L	7	2 	4F				A22CE   					 
1999061100198	19990611	00198	NM  	1999	6	11	99ZZZX2223       	1	19990512	G	5510		BEAM            			BOEING	727   	727251      	138408H	NM  										HORIZ STABILIZER	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM ABOVE NR 7 ELEVATOR HINGE.						2	L	7	3 	4F				A3WE    					 
1999061100199	19990611	00199	NM  	1999	6	11	99ZZZX2224       	1	19990512	G	5510		BEAM            			BOEING	727   	727251      	138408H	NM  										HORIZ STABILIZER	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON THE LEFT HORIZ STABILIZER, LOWER T/E BEAM BETWEEN NR 5 AND NR 6 ELEVATOR HINGES	.					2	L	7	3 	4F				A3WE    					 
1999061100200	19990611	00200	NM  	1999	6	11	99ZZZX2225       	1	19990512	G	5753		SKIN            			BOEING	727   	727251      	138408H	NM  										TE FLAP	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON UPPER SURFACE AFT EDGE OF RT INBOARD AFT FLAP (ABOVE NR 5 CANOE).						2	L	7	3 	4F				A3WE    					 
1999061100201	19990611	00201	NM  	1999	6	11	99ZZZX2226       	1	19990512	G	5510		BEAM            			BOEING	727   	727251      	138408H	NM  										HORIZ STABILIZER	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, COROSION WAS NOTED ON RT HORIZONTAL STABILIZER, UPPER TRAILING EDGE BEAM.						2	L	7	3 	4F				A3WE    					 
1999061100202	19990611	00202	NM  	1999	6	11	99ZZZX2227       	1	19990512	G	5320		ANGLE           			BOEING	727   	727251      	138408H	NM  										BS 178	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED IN RADOME AREA FS 178 LOWER MOST Z-ANGLE LBL 18 TO RBL 18.						2	L	7	3 	4F				A3WE    					 
1999061100203	19990611	00203	NM  	1999	6	11	99ZZZX2228       	1	19990512	G	5330		SKIN            			BOEING	727   	727251      	138408H	NM  										BS 1283-1343	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON EXTERIOR AFT FUSELAGE LAMP SEAM FS 1283 - FS 1343 BELOW NR 1 ENGINE PYLON.						2	L	7	3 	4F				A3WE    					 
1999061100204	19990611	00204	CE  	1999	6	11	99ZZZX2229       	1	19990513	G	5210	5112358162	HINGE           			CESSNA	500   	550         	2076604	CE  										PASSENGER DOOR	BROKEN          	B	S	A	EWCR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	61CK	7599 				5500195				LOWER HINGE ARM BROKE COMPLETELY THROUGH WHEN DOOR OPENED TO STOP (WHICH IS LOCATED ON ARM).						1	L	7	2 	4F				A22CE   					 
1999061100207	19990611	00207	NE  	1999	6	11	99ZZZX2232       	2	19990519	G	7230	2A0851	SEAL            								IAE   	V2500 	V2500A1     		NE  					ENGINE	CRACKED         	B			KB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03							0215			PART REJECTED AT FLUORESCENT PENETRANT INSPECTION DUE TO CRACK ON OUTSIDE TOP FLAT, APPROXIMATELY 0.375 INCH IN LENGTH, 	AS MARKED ON PART.										4	F			E311NE				 
1999061100208	19990611	00208	CE  	1999	6	11	99ZZZX2233       	1	19990426	G	7603	08502638	CONTROL CABLE   		08502638    	CESSNA	310   	310L        	2074230	CE  										RT ENGINE	FAILED          	D				O				OTHER                   				O			OTHER                     			DE	DESCENT        	1			WP	23	2215F	4500 				310L0015				THROTTLE CABLE FAILED WHILE IN-FLIGHT.  DEFECT DISCOVERED AT FIRST ATTEMPT TO REDUCE POWER FOR DESCENT.  INNER CONTROL C	ABLE FAILED (SEPARATED) AT SWAGED TERMINAL END AT ENGINE.  UNABLE TO CONTROL POWER OUTPUT OF ENGINE. THIS ASSEMBLY CANNO	T BE VISUALLY INSPECTED DUE TO CONSTRUCTION OF THE CABLE.  DEFECT AREA IS INSIDE PROTECTIVE TUBE.  THIS IS NOT A LIFE LI	MITED PART NOR IS THERE ANY MANUFACTURER RECOMMENDATION FOR TIME IN SERVICE BEFORE RETIREMENT.  RECOMMEND REPLACEMENT AT	 3,500 HOURS TIME IN SERVICE FOR ANY MIXTURE, THROTTLE, OR PROPELLER CONTROL INSTALLED IN 310 AIRPLANES DUE TO INABILITY	 TO INSPECT PERIODICALLY.	1	L	7	2 	3O			 	3A10    					 
1999061100209	19990611	00209	CE  	1999	6	11	99ZZZX2234       	1	19990428	G	7800		SLIP JOINT      			ZINAIR	CH2000	CH2000      	9950100	CE  										EXHAUST SYSTEM	LEAKING         	D	L			K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	23	35ZA					200035				SLIP JOINT LEAKING ON ENGINE EXHAUST.						1	L	7	1 	3O			NT	TA5CH   					 
1999061100210	19990611	00210	SO  	1999	6	11	99ZZZX2235       	1	19990129	G	3230	2170400	TUBE            		2572000     	PIPER 	PA24  	PA24250     	7102404	SO  										TRANSMISSION	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	7697P	3338 			1010250	242908				P/N 25720-00 TUBE CORRODED TO P/N 21038-07 BUSHING, MOTOR RELEASE TUBE, CAUSING NO SLIDING ACTION FOR DISENGAGEMENT OF P	/N 26542-00 LOCK ASSY, LANDING GEAR SAFETY.					1	L	7	1 	3O				1A15    					 
1999061100211	19990611	00211	CE  	1999	6	11	99ZZZX2236       	1	19990519	G	3230	12801204	DOWNLOCK        			CESSNA	210   	T210N       	2073456	CE  										MLG	DAMAGED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	4620Y	4451 			4204	21063960				DOWNLOCK ACTUATORS COULD NOT BE RIGGED TO SPEC DURING ANNUAL INSPECTION CHECK.  FOUND ROD STICKING.  SENT IN FOR OVERHAU	L, FOUND INTERNAL P/N 1280246-1 CRACKED AND P/N 1280120-3 DEEP SCRATCH.  UNIT CONSIDERED B.B.R. (17 YRS OLD).  REPLACED 	WITH OVERHAULED EXCHANGE UNIT.  PART SHOULD HAVE LIFE/LIMIT OVERHAUL TIME.				1	H	7	1 	3O				3A21    					 
1999061100212	19990611	00212		1999	6	11	99ZZZX2237       	1	19990426	G	3700	V80500113	VALVE           	VALCOR      																VACUUM SYSTSEM	MISMANUFACTURED 	G				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	25										THE PISTON ASSEMBLY WITHIN THE SUSPECT VALVES MIGHT NOT HAVE BEEN ASSEMBLED TO PRINT AND TO ENSURE PARTS ARE LOCKHEED IN	 PLACE AS INTENDED.																		 
1999061100738	19990611	00738	SW  	1999	6	11	99ZZZX2238       	1	19990429	G	3340	G62504	SEARCH LIGHT    			BELL  	212   	212         	1181420	SW  										FUSELAGE	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530F					30920				SEARCH LIGHT WILL NOT MOVE.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999061100739	19990611	00739	GL  	1999	6	11	99ZZZX2239       	2	19990512	G	7412	6899093	EXCITER         			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20J     	03013	GL  					ENGINE	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	9907K					2040				EXCITER FAILED.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999061100740	19990611	00740	WP  	1999	6	11	99ZZZX2240       	1	19990512	G	6220	369D21800501	BEARING         			HUGHES	369   	369E        	4470707	WP  										T/R LINK	ROUGH           	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8330P				HT5210	0330E				TAIL ROTOR LINK HAS ROUGH, DRY BEARINGS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999061100741	19990611	00741	WP  	1999	6	11	99ZZZX2241       	1	19990512	G	7714	65011040	TACHOMETER      			HUGHES	369   	369E        	4470707	WP  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8330P		810  		1482	0330E				TACHOMETER SLUGGISH ON START-UP.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999061100742	19990611	00742	SW  	1999	6	11	99ZZZX2242       	1	19990512	G	7714	2060626273	TACHOMETER GEN  			BELL  	206   	OH58A       	1181579	SW  										N2 SYSTEM	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	58AG		148  		15222	7221131				N2 GAUGE FLUCTUATES.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999061100743	19990611	00743	SW  	1999	6	11	99ZZZX2243       	1	19990429	G	6220	204012101141	BEARING         			BELL  	204   	UH1H        	1181407	SW  										MAIN ROTOR	ROUGH           	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	53AG	4344 	100  		A2836	7221588				ROUGH GRIP BEARING.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999061100744	19990611	00744		1999	6	11	99ZZZX2244       	4	19990429	G	2330	C6533	AUDIO PANEL     			BELL  	204   	UH1H        	1181407	SW  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	51AG				411	7120178				AUDIO PANEL CAUSES STATIC IN PILOT'S HEAD SET.						1	G	7	1 	4U				EXPA1G71					 
1999061100745	19990611	00745		1999	6	11	99ZZZX2245       	4	19990512	G	3414	66108801591	ALTIMETER       			BELL  	204   	UH1H        	1181407	SW  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	51AG				416	7120178				ALTIMETER HAD EXCESSIVE FRICTION.  FAILED CERTIFICATION.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999061100746	19990611	00746	SW  	1999	6	11	99ZZZX2246       	1	19990429	G	7910	4362	CAP             			BELL  	206   	206B3       	1181506	SW  										OIL TANK	BROKEN          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY					2871				TAB BROKEN THAT LOCKS CAPS IN PLACE.						1	G	7	1 	3U				H2SW    					 
1999061100747	19990611	00747	SW  	1999	6	11	99ZZZX2247       	1	19990429	G	7700	12444412	INDICATOR       			BELL  	206   	206B3       	1181506	SW  										TOT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY		407  		780D0260B	2871				TOT GAUGE HANGS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999061100748	19990611	00748	WP  	1999	6	11	99ZZZX2248       	1	19990429	G	6720	369D2172311	LINK            			HUGHES	369   	369D        	4470706	WP  										TAIL ROTOR	WORN            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	1097J					906801D				TAIL ROTOR LINK HAS WORN BEARINGS.						1	G	7	1 	3U				H3WE    					 
1999061100749	19990611	00749	SW  	1999	6	11	99ZZZX2249       	1	19990512	G	6240	2060755451	SENSOR          		9787A       	BELL  	206   	206B3       	1181506	SW  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	49718					1917				RPM SENSOR WOULD NOT ACTIVATE AUDIO ALARM.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999061100750	19990611	00750	GL  	1999	6	11	99ZZZX2250       	2	19990512	G	7321	104900A5	FCU             			BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20      	03013	GL  					ENGINE	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	49718	3145 	1    			1917	CAE830523			FCU HARD TO START, TOO MUCH FUEL.  REMOVED AND SENT FOR REPAIR.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999061100751	19990611	00751		1999	6	11	99ZZZX2251       	4	19990512	G	2312	W18486E01	RADIO           			HUGHES	369   	369D        	4470706	WP  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	369AW		57   		0887009	470117D				PILOT REPORTED INTERCOM AND TRANSMISSION STATIC.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999061100752	19990611	00752	GL  	1999	6	11	99ZZZX2252       	2	19990512	G	7230		BLADE           		6890550     	HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20      	03013	GL  					COMPRESSOR	BENT            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	369AW	1108 			CAC35437	470117D	CAE833998			BLADES BENT  FOUND DURING INSPECTION.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999061100753	19990611	00753	WP  	1999	6	11	99ZZZX2253       	1	19990512	G	7714	369H45167	N1 TACHOMETER   			HUGHES	369   	369D        	4470706	WP  										COCKIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	369AW		869  		787D	470117D				N1 TACHOMETER HAD JERKY MOVEMENT, STICKY.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999061100754	19990611	00754		1999	6	11	99ZZZX2254       	4	19990512	G	2312	KY195B	RADIO           			HUGHES	369   	369D        	4470706	WP  										COCKPIT	MALFUNCTIONED   	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	369AW				5209	470117D				RADIO RECEIVES AND TRANSMITS WEAK.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999061100755	19990611	00755	WP  	1999	6	11	99ZZZX2255       	1	19990512	G	2425	369H452657	INDICATOR       			HUGHES	369   	369D        	4470706	WP  										TORQUE	MALFUNCTIONED   	B			LS1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	13	369AW				1109	470117D				TORQUE INDICATOR FAILED ACCURACY TEST.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999061100756	19990611	00756	GL  	1999	6	11	99ZZZX2256       	2	19990512	G	7314	6899253	PUMP            			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20      	03013	GL  					ENGINE	MALFUNCTIONED   	B			LS1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	13	369AW		3918 		T3393	470117D	CAE833998			FUEL PUMP ASSEMBLY FAILED BYPASS TEST.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999061100758	19990611	00758	SW  	1999	6	11	99ZZZX2258       	1	19990514	G	5210	205030220107	DOOR            			BELL  	212   	212         	1181420	SW  										CABIN	DAMAGED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	29AL					30569				WHEN AIRCRAFT WAS GETTING PREPPED FOR PAINT, FOUND LEFT AND RIGHT UPPER DOOR TRACKS HAD EXCESSIVE DAMAGE WHERE ROLLERS R	IDE WHEN DOOR IS CLOSED.  REPLACED WITH NEW TRACKS.					1	G	7	1 	4U				H4SW    					 
1999061100760	19990611	00760	CE  	1999	6	11	99ZZZX2260       	1	19990525	G	3260	444EN496	SWITCH          			BEECH 	100   	B100        	1152919	CE  										LT MLG	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	311CM	6618 				BE101				LEFT ENGINE STARTED, WOULD NOT ENGAGE.  TROUBLESHOT AND FOUND THE LEFT MLG SQUAT SWITCH CONTACTS  DEFECTIVE INTERRUPTING	 THE CONTROL CIRCUIT TO THE START RELAY CONTROL BOX.					1	L	7	2 	4T				A14CE   					 
1999061100761	19990611	00761	SO  	1999	6	11	99ZZZX2261       	1	19990516	G	3222	702057507	STRUT           			GULSTM	AA5   	AA5B        	3960105	SO  										NLG	BROKEN          	G				K				NONE                    				D			INFLIGHT SEPARATION       			NR	NOT REPORTED   	1			SO	14	211JA	7426 				AA5B1097				NOSE WHEEL, FORK, AND FAIRING DEPARTED THE AIRCRAFT IN-FLIGHT.  NOSE STRUT FAILED ON LANDING.  NO PARTS RECOVERED.  NOSE	 STRUT STUD, WHICH RETAINS NOSE FORK, FAILED ABOVE THREADED AREA.  CAUSE UNKNOWN.  SUBMITTER RECOMMENDED PERIODIC NDT FO	R CRACKS IN STUD.				1	L	7	1 	3O				A16EA   					 
1999061100762	19990611	00762	WP  	1999	6	11	99ZZZX2262       	2	19990519	G	7310	30743762	LINE            			CESSNA	650   	650         	2076802	CE  	GARRTT	TFE731	TFE7314R    	01518	WP  					FUEL SYSTEM	CHAFED          	E		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	795QS	22   				6507095				FUEL LINE IS CHAFING ON WIRING HARNESS THAT RUNS JUST AFT OF THE TRANSFER GEARBOX ON BOTH ENGINES.  INSTALL SPIRAL WRAP 	AROUND FUEL LINE OR SEPARATE WIRES AND LINE WITH ADEL CLAMPS.					2	L	7	2 	4F	4	F		A9NM    	E6WE				 
1999061100763	19990611	00763	EU  	1999	6	11	99ZZZX2263       	1	19990519	G	2932	51090	SWITCH          			ISRAEL	1125  	ASTRASPX    	4500205	EU  										HYDRAULIC SYSTEM	LEAKING         	B			QRRR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13	275RA				127	098				COMPLETE LOSS OF AUXILIARY HYDRAULIC SYSTEM PRESSURE DURING TAXI.  REPLACED SWITCH WITH MODIFIED UNIT.  REPLENISHED FLUI	D AND OPS TESTED.					2	L	7	2 	4F			RT	A16NM   					 
1999061100764	19990611	00764	EU  	1999	6	11	99ZZZX2264       	1	19990519	G	2932	51091	SWITCH          			ISRAEL	1125  	ASTRASPX    	4500205	EU  										HYDRAULIC SYSTEM	LEAKING         	B			QRRR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13	275RA				212	098				COMPLETE LOSS OF MAIN HYDRAULIC SYSTEM PRESSURE DURING TAXI.  REPLACED SWITCH WITH MODIFIED TYPE.  OPS TESTED NORMAL.						2	L	7	2 	4F			RT	A16NM   					 
1999061100765	19990611	00765	EU  	1999	6	11	99ZZZX2265       	1	19990519	G	2913	40183	PUMP            			ISRAEL	1125  	ASTRASPX    	4500205	EU  										RT ENGINE	LEAKING         	B			QRRR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13	275RA	508  			ML61AB	098				HYDRAULIC PUMP FOUND LEAKING OUT OF CASE SEAL DRAIN TUBE.  REPLACED PUMP.						2	L	7	2 	4F			RT	A16NM   					 
1999061100766	19990611	00766		1999	6	11	99ZZZX2266       	4	19990519	G	3445	6228971120	TCAS            		5866        	ISRAEL	1125  	ASTRASPX    	4500205	EU  										CARGO BAY	INOPERATIVE     	B			QRRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	273RA					097				'TCAS INOP' DISPLAYED.  INOPERABLE.						2	L	7	2 	4F			RT	A16NM   					 
1999061100767	19990611	00767	EU  	1999	6	11	99ZZZX2267       	1	19990519	G	2913	40183	PUMP            			ISRAEL	1125  	ASTRASPX    	4500205	EU  										LT ENGINE	LEAKING         	B			QRRR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13	273RA	365  			N025AB	097				DURING PRE-FLIGHT, FOUND LEFT HYDRAULIC PUMP LEAKING OUT BETWEEN CASE HALVES.   REPLACED PUMP.						2	L	7	2 	4F			RT	A16NM   					 
1999061100768	19990611	00768	EU  	1999	6	11	99ZZZX2268       	1	19990519	G	2430	S3092	CONTACTOR       			ISRAEL	1125  	ASTRASPX    	4500205	EU  										RT GENERATOR	INOPERATIVE     	B			QRRR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	273RA	365  			P109	097				RIGHT GENERATOR WOULD NOT LOAD SHED DURING TEST.  REPLACED GLC WITH NEW.  OPS TEST NORMAL.						2	L	7	2 	4F			RT	A16NM   					 
1999061100770	19990611	00770	SO  	1999	6	11	99ZZZX2270       	1	19990504	G	2437		AMMETER         			PIPER 	PA28  	PA28R200    	7102811	SO  										COCKPIT	MISMANUFACTURED 	B			VY2R	O				OTHER                   				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	23	46UT					7435068				PILOT REPORTS AMMETER INOPERABLE.  REMOVED STEWART WARNER 70-AMP METER AND FOUND ONE POST SHORTED TO THE MOUNT TRAY WHER	E IT PASSES THROUGH MOUNT HOLE.  IT MELTED THE TRAY IN THE AREA OF CONTACT.  INSTALLED NEW ROCHESTER 70-AMP GAUGE PER PI	PER KIT 765-186V AND PIPER SB 811A.  SUBMITTER STATED THIS  COULD HAVE LED TO AN IN-FLIGHT FIRE.				1	L	7	1 	3O				2A13    					 
1999061100772	19990611	00772	SO  	1999	6	11	99ZZZX2272       	1	19990525	G	2434	17T27596G	WIRE            			PIPER 	PA28  	PA28180     	7102808	SO  										ALTERNATOR	CHAFED          	B			TVMR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	05	6432J					284850				FOUND WIRE COMING OFF ALTERNATOR (BATTERY POST) TO MAIN BUSS AT CIRCUIT BREAKER PANEL CHAFED TO NR 1 CYLINDER PRIMER LIN	E AND WELDED ITSELF TO THE LINE.  THIS RESULTED IN A TOTAL ELECTRICAL FAILURE.					1	L	7	1 	3O			 	2A13    					 
1999061100774	19990611	00774		1999	6	11	99ZZZX2274       	4	19990517	G	3416	A30	ENCODER         	ACK         		CESSNA	182   	R182        	2072734	CE  										CABIN	MALFUNCTIONED   	B			FC6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	1675R					R18200509				FOUND ENCODER TO HAVE A2 CODE LINE SHORTED.  ALSO, FOUND TRANSPONER RT 350A SN 17101 TO HAVE A2 CODE LINE LOW.						1	H	7	1 	3O			RT	3A13    					 
1999061100775	19990611	00775	SO  	1999	6	11	99ZZZX2275       	2	19990501	G	8500		CRACK           			CESSNA	421   	421C        	2076016	CE  	CONT  	O520  	GTSIO520N   	17032	SO  					ENGINE	CRACKED         	B			AMYR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CE	05	421GF	689  				421C1110	276386R			PILOT REPORTED EXCESSIVE OIL LEAK ON RIGHT ENGINE   CAWLING PULLED AND 3 INCH - 4 INCH CRACK NOTED AT NR 5 CYLINDR BASE.	   IDENTIDAL PROBLEM OCCURRED.					1	L	7	2 	3O	3	O		A7CE    	E7CE				 
1999061800147	19990618	00147	EU  	1999	6	18	99ZZZX2276       	1	19990512	G	7500	E35893	LINE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										BLEED AIR SYSTEM	CHAFED          	B	P		G1FR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	85DW	4963 				258034				BLEED AIR PIPE PN E35893 HAS BEEN FOUND CHAFED BEYOND LIMITS BY THE INBOARD EDGE OF THE LEFT UPPER ENGINE COWL.   OPERAT	ING CLEARANCE BETWEEN THE COMPONENTS CANNOT BE VERIFIED.   CONTACT/DAMAGE APPEAR AS THE FIRST SYPTOMS OF INTERFERENCE. R	EF:  RAYTHEON  CORPORATE JETS OF CONDITION REPORT.   2.  RAYTHEON CORPORATE JETS IPC CH 21-10-05-05, PAGE  0.  3.  DRAWI	NG OF APROXIMATE DAMAGE TO PIPE PN E35893.			2	L	7	2 	4F			RT	A3EU    					 
1999061800148	19990618	00148	EU  	1999	6	18	99ZZZX2277       	1	19990112	G	2440	324056	TERMINAL        			AMD   	FALC20	FALCON20C5  	2730107	EU  										BS 39	DAMAGED         	H			G1FR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	400PC	9342 				113				INCOMING DISCREPANCY STATED 'CANNOT APPLY EXTERNAL POWER TO AIRCRAFT.'  DROPS OFF-LINE IN SEVERAL SECONDS.  TROUBLESHOOT	ING REVEALED THAT THE GROUND STUD OF THE GROUND POWER RECEPTABLE WAS 'OPEN' TO AIRCRAFT STRUCTURE.  FURTHER INVESTIGATIO	N REVEALED THE NUTPLATE AND STRUCTURE WERE DESTROYED AT THE POINT WHERE THE GROUND WIRE ATTACHES TO THE AIRFRAME.  AT FR	AME 39.  THIS POINT IS LOCATED BELOW THE BATTERY BOX FLOOR, APPROXIMATELY 1 INCH BELOW THE APU FUEL FEED LINE.  THE COMP	ARTMENT IS SEALED STRUCTURE AND ALSO CONTAINS THE APU SHUT-OFF VALVE AND APU.  FUEL BOOST PUMP  AREA WAS REPAIRED IAW FA	LCON 20 MRI CHAPTER 51-30-03 AND FALCON JET ENG RECOMMENDATIONS.  REPLACED TERMINAL P/N 324045 INSTALLING NEW UNIT.	2	L	7	2 	4F			RT	A7EU    					 
1999061800149	19990618	00149	EU  	1999	6	18	99ZZZX2278       	1	19990512	G	7500	E35893	LINE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										BLEED AIR SYSTEM	CHAFED          	B	P		G1FR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	255RB	3772 				258059				BLEED AIR PIPER PN E35893 HAS BEEN FOUND CHAFED BEYOND LIMITS BY THE INBOARD EDGE OF THE LT UPPER ENGINE COWL.  OPERATIN	G  CLEARANCE BETWEEN THE COMPONENTS CANNOT BE VERIFIED.  CONTACT/DAMAGE APPEAR AS THE FIRST SYMPTOMS OF THE INTERFERENCE	.  REF:  1.  RAYTHEON CORPORATION JETS CONDITION REPORT.  2.  RAYTHEON CORPORATION JETS IPC CH 21-10-05-05, PAGE 0.  DRA	WING OF APPROXIMATE DAMAGE TO PIPE PN E35893.			2	L	7	2 	4F			RT	A3EU    					 
1999061800150	19990618	00150	EU  	1999	6	18	99ZZZX2279       	1	19990512	G	7500	E35893	LINE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										LT PYLON	CHAFED          	B	P		G1FR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	800WH	5837 				258080				BLEED AIR PIPE P/N E35893 HAS BEEN FOUND CHAFED BEYOND LIMITS BY THE INBOARD EDGE OF THE LEFT UPPER ENGINE COWL.  OPERAT	ING CLEARANCE BETWEEN THE COMPONENTS CANNOT BE VERIFIED.  CONTACT/DAMAGE APPEAR AS THE FIRST SYMPTOMS OF INTERFERENCE. R	EF:  RAYTHEON CORPORATE JETS CONDITION REPORT.  RAYTHEON CORPORATE JETS IPC CH 21-10-05-05, PAGE 0.  DRAWING OF APPROXIM	ATE DAMAGE TO PIPE P/N E35893.			2	L	7	2 	4F			RT	A3EU    					 
1999061800151	19990618	00151	CE  	1999	6	18	99ZZZX2280       	1	19990512	G	7500	E35893	LINE            			RAYTHN	DH125 	HAWKER800XP 		CE  										BLEED AIR SYSTEM	CHAFED          	B	P		G1FR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	127KC	1138 				258255				BLEED AIR PIPE PN E35893 HAS BEEN FOUND CHAFED BEYOND LIMITS BY THE INBOARD EDGE OF THE LT UPPER ENGINE COWL.  OPERATING	 CLEARANCE BETWEEN THE COMPONENTS CANNOT BE VERIFIED.  CONTACT/DAMAGE APPEAR AS THE FIRST SYMPTOMS OF INTERFERENCE.  REF	:  RAYTHEON CORPORATE JETS CONDITION REPORT.  RAYTHEON CORPORATE JET IPC CH 21-10-05-05, PAGE 0.  DRAWING OF APPROX DAMA	GE TO PIPE PN E35893.			2	L	7	2 	4F			RT	A3EU    					 
1999061800152	19990618	00152	EU  	1999	6	18	99ZZZX2281       	1	19990512	G	7500	E35893	LINE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										BLEED AIR SYSTEM	CHAFED          	B	P		G1FR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	826CT	3624 				258117				BLEED AIR PIPE PN E35893 HAS BEEN FOUND CHAFED BEYOND LIMITS BY THE INBOARD EDGE OF THE LT UPPER ENGINE COWL.  OPERATING	 CLEARANCE BETWEEN THE COMPONENTS CANNOT BE VERIFIED.  CONTACT/DAMAGE APPEAR AS THE FIRST SYMPTOMS OF INTERFERENCE.  RE:	  RAYTHEON CORPORATE JETS CONDITION REPORT.  RAYTHEON CORPORATE JET IPC CH 21-10-05-05, PAGE 0.  DRAWING FOR APPROX DAMA	GE TO PIPE PN E35803.			2	L	7	2 	4F			RT	A3EU    					 
1999061800153	19990618	00153	EU  	1999	6	18	99ZZZX2282       	1	19990512	G	7500	E35893	LINE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										BEED AIR SYSTEM	CHAFED          	B	P		g1fr	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	74NP	3389 				258168				BLEED APR PIPE P/N E35893 HAS BEEN FOUND CHAFED BEYOND LIMITS BY THE INBOARD EDGE OF THE LT UPPER ORANGE.  RE:  RAYTHEON	 CORPORATE JETS CONDITION REPORT.  RAYTHEON CORPORATE JET IPC CH 21-10-05-05, PAGE 0.  DRAWING FOR APPROXIMATE DAMAGE TO	 PIPE PN E35893.				2	L	7	2 	4F			RT	A3EU    					 
1999061800154	19990618	00154	EU  	1999	6	18	99ZZZX2283       	1	19990512	G	7500	E35893	LINE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										BLEED AIR	CHAFED          	B	P		G1FR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	60PM	4283 				258187				BLEED AIR PIPE P/N E35893 HAS BEEN FOUND CHAFED BEYOND LIMITS BY THE INBOARD EDGE OF THE LT UPPER ENGINE COWL.  OPERATNG	 CLEARANCE BETWEEN THE COMPONENTS CANNOT BE VERIFIED.  CONTACT/DAMAGE APPEAR AS THE FIRST SYMPTOMS OF INTERFERENCE.  RE:	  RAYTHEON CORPORATE JETS CONDITION REPORT.  RAYTHEON CORPORATE JET IPC CH 21-10-05-05, PAGE 0.  DRAWING FOR APPROXIMATE	 DAMAGE TO PIPE PN E35893.			2	L	7	2 	4F			RT	A3EU    					 
1999061800155	19990618	00155	NM  	1999	6	18	99ZZZX2284       	1	19990606	G	6700		BEARING         			DOUG  	600N  	600N        	3027377	NM  										CRANK ASSY	LOOSE           	H	S	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	17	607BP	200  				RN036				DURING AN INSPECTION, FOUND THE FORWARD CRANK ASSY FOR LATERAL CONTROL HAD PLAY.  REMOVED THE PART AND FOUND THE BEARING	 WAS LOOSE INSIDE.					1	G	7	1 	3U			NC	H3WE    					 
1999061800156	19990618	00156	NM  	1999	6	18	99ZZZX2285       	1	19990606	G	6700		BEARING         			DOUG  	600N  	600N        	3027377	NM  										CRANK ASSY	LOOSE           	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	17	609BP	201  				RN038				DURING AN INSPECTION AND WORKING ON THE SAME TYPE OF HELICOPTER, INSPECTING THE FORWARD MAIN ROTOR CONTROL RODS AND BELL	 CRANKS.  THIS HELICOPTER ALSO HAD A BAD FORWARD LATERAL CRANK ASSY.  REMOVED THE CRANK AND ALSO FOUND THE BEARING WAS R	EADY TO FALL OFF.				1	G	7	1 	3U			NC	H3WE    					 
1999061800157	19990618	00157	EA  	1999	6	18	99ZZZX2286       	2	19990501	G	8530	74541	VALVE           			PIPER 	PA22  	PA22150     	7102210	SO  	LYC   	O320  	O320A1A     	41508	EA  					EXHAUST	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	7449D	802  				225214	L763827			EXHAUST VALVE NR 3 CYLINDER BROKE AT STEM CLOSE TO FACE OF VALVE.  COMPLETE HEAD OF VALVE GONE, NOT FOUND.  CAUSE UNKNOW	N.  NOTE:  LOG SHOWS PART AS NR 74541.  PART NUMBER ON VALVE STEM IS SL 74541 G 58.  ALSO, NR 3 CYLINDER WAS OVERHAULED 	BY CRS 202-87, W.O. NR 11840, BUT NO ENTRY OF VALVE CHANGE, ALSO, DONE 357 HOURS AGO.				1	H	7	1 	3O	3	O		1A6     	E274				 
1999061800158	19990618	00158	EA  	1999	6	18	99ZZZX2287       	2	19990521	G	8530	LW11625	PUG             			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235N2C     	41505	EA  					NR 1 CYLINDER	WORN            	B			BNZR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	6490L		496  			15284417	L2347615			FOUND METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN LYC ST 1492B. FOUND FORWARD PISTON PIN PLUG IN 	NR 1 CYLINDER EXCESSIVELY WORN DUE TO PISTON RING WEAR STEP SHAVING THE PLUG ON EACH STROKE.  FOUND GALLING ON UPWARD FA	CING PISTON SKIRT.  FOUND PISTON RING NEAR STOP TO BE GREATER ON FORWARD FACING SIDE OF CYLINDER GIVING THE APPEARANCE T	HE PISTON IS NOT RUNNING TRUE IN THE CYLINDER.			1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999061800159	19990618	00159	EA  	1999	6	18	99ZZZX2288       	2	19990521	G	8530	LW11625	PLUG            			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235N2C     	41505	EA  					NR 1 CYLINDER	WORN            	B			BNZR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	95843		595  			15285974	L1304515			FOUND METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN LYC SI 1492B.  FOUND FORWARD PISTON PIN PLUG IN	 NR 2 CYLINDER EXCESSIVELY WORN DUE TO PISTON RING WEAR STEP SHAVING THE PLUG ON EACH STROKE.  FOUND GALLING OF UPWARD F	ACING PISTON SHIRT.  FOUND PISTON RING WEAR STOP TO BE GREATER ON FORWARD FACING SIDE OF CYINDER, GIVING THE APPEARANCE 	THE PISTON IS NOT RUNNING TRUE IN THE CYLINDER.			1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999061800160	19990618	00160	EA  	1999	6	18	99ZZZX2289       	2	19990521	G	8530	LW11625	;PLUG           			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235N2C     	41505	EA  					NR 1 CYINDER	WORN            	B			BNZR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	93689		546  			15285535	L2498415			FOUND METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN LYC SI 1492B.  FOUND FORWARD PISTON PIN PLUG IN	 NR 1 CYLINDER EXCESSIVELY WORN DUE TO PISTON RING WEAR STEP SHAVING THE PLUG ON EACH STROKE.  FOUND GALLING ON UPWARD F	ACING PISTON SKIRTS.  FOUND PISTON RING WEAR STEP TO BE GREATER ON FOWARD FACING SIDE OF CYLINDER GIVING THE APPEARANCE 	THE PISTON IS NOT RUNNING TRUE IN THE CYLINDER.			1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999061800161	19990618	00161	EA  	1999	6	18	99ZZZX2290       	2	19990521	G	8530	LW11625	PLUG            			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235N2C     	41505	EA  					NR 1 CYLINDER	WORN            	B			BNZR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	5377B		865  			15283854	RL1696315			FOUND METAL CONTAMINATION OF OIL FILTER IN EXCESS OF LIMITS CONTAINED IN LYC SI 1492B.  FOUND FORWARD PISTON PIN PLUG IN	 NR 1 CYINDER EXCESSIVELY WORN DUE TO PISTON RING WEAR STEP SHAVING THE PLUG ON EACH STROKE.  FOUND GALLING ON UPWARD FA	CING PISTON SKIRT.  FOUND PISTON RING WEAR STEP TO BE GREATER ON FORWARD FACING SIDE OF CYLINDER GIVING APPEARANCE THAT 	PISTON IS NOT RUNNING TRUE IN THE CYLINDER.			1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999061800162	19990618	00162	CE  	1999	6	18	99ZZZX2291       	1	19990601	G	3244	GOODYEARAERO	TIRE            		505C661     	BEECH 	58    	58P         	1152744	CE  										MLG	FAILED          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	01	130Z					TJ314				TREAD SEPARATING, SPLITTING, AND BUMPS AT TOP OF SIDE WALL.						1	L	7	2 	3O				A23CE   					 
1999061800163	19990618	00163	EA  	1999	6	18	99ZZZX2292       	2	19990401	G	8530		STUD            			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					NR 1 CYLINDER	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	25	5171K					17073998	L29676			NR 1 CYLINDER INTAKE VALVE ROCKER ARM STUD BACKED OUT OF CYLINDER HEAD.						1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999061800164	19990618	00164	GL  	1999	6	18	99ZZZX2293       	3	19990525	G	6111	C83892L	CLAMP           													HARTZL	HCB4T	HCB4TN5     	GL  	PROPELLER	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99			1100 		DD1424			LT10282NB53R		FOUND EXTERNAL CRACK NEAR CLAMP BOLT HOLE.  CLAMP ASSY SENT TO HARTZELL.																6	C	P40E	 
1999061800165	19990618	00165	EU  	1999	6	18	99ZZZX2294       	1	19990512	G	7500	E35893	LINE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										BLEED AIR SYSTEM	CHAFED          	B	P		G1FR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	523WC	4169 				258086				BLEED AIR PIPE P/N E35893 HAS BEEN FOUND CHAFED BEYOND LIMITS BY THE INBOARD EDGE OF THE LEFT UPPER ENGINE COWL.  OPERAT	ING CLEARANCE BETWEEN THE COMPONENTS CANNOT BE VERIFIED.  CONTACT/DAMAGE APPEAR AS THE FIRST SYMPTOMS OF INTERFERENCE. R	EF:  RAYTHEON CORPORATE JETS CONDITION REPORT.  RAYTHEON CORPORATE JETS IPC CH 21-10-05-05, PG 0.  DRAWING OF APPROXIMAT	E DAMAGE TO PIPE P/N E35893.			2	L	7	2 	4F			RT	A3EU    					 
1999061800259	19990618	00259	EU  	1999	6	18	99ZZZX2296       	1	19990528	G	2612		DETECTOR WIRE   			AEROSP	AS355 	AS355F1     	8680810	EU  										ENGINE BAY	FAILED          	D				L	A			ABORTED APPROACH        	UNSCHED LANDING         			N			FALSE WARNING             			AP	APPROACH       	1			WP	03	510TG		17   			5168				ON APPROACH, 3 MILES SOUTH OF AIRPORT, PILOT EXPERIENCED A FIRE WARNING LIGHT TO RT ENGINE.  FLIGHT EN ROUTE FROM KAHOOL	AWE FOLLOWED BY ANOTHER HELICOPTER.  THE TWO AIRCRAFT WERE IN RADIO COMM WITH EACH OTHER.  PILOT OF ACFT FOLLOWING, ADVI	SED THERE WAS NO SMOKE OR UNUSUAL CONDITIONS WITH OTHER ACFT.  ALL COCKPIT INSTRUMENTATION INDICATIONS WERE NORMAL.  PIL	OT PROCEEDED WITH LANDING AT KAHULUI HELIPORT.  UPON LANDING, GROUND CREW , MECH FOUND A BROKEN WIRE ON THE RT HAND FIRE	 DETECTOR.  THE WIRE WAS REPAIRED AT THE CONNECTOR AND A LOG BOOK ENTRY MADE TO REFLECT MAINTENANCE.		1	G	7	2 	3U				H11EU   					 
1999061800260	19990618	00260	NM  	1999	6	18	99ZZZX2297       	1	19990606	G	6700		BEARING         		600N76051   	DOUG  	600N  	600N        	3027377	NM  										CRANK ASSY	LOOSE           	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	17	611BP	301  				RN041				BELLCRANK LOWER BEARING WAS LOOSE AND READY TO FALL OFF WHEN PART WAS REMOVED FROM BRACKET ASSY.						1	G	7	1 	3U			NC	H3WE    					 
1999061800261	19990618	00261	NM  	1999	6	18	99ZZZX2298       	1	19990512	G	5320		SHEAR TIE       			BOEING	727   	727256      		NM  										BS 720	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON STR 26R, FS 720B.						2	L	7	3 	4F				A3WE    					 
1999061800262	19990618	00262	NM  	1999	6	18	99ZZZX2299       	1	19990512	G	5313		STRINGER        			BOEING	727   	727256      		NM  										BS 740	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON STR 27R, STA 740.						2	L	7	3 	4F				A3WE    					 
1999061800263	19990618	00263	NM  	1999	6	18	99ZZZX2300       	1	19990512	G	5330		SKIN            			BOEING	727   	727256      		NM  										BS 990	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON SKIN UNDER PANELS AT BS 990L, STR 23L.						2	L	7	3 	4F				A3WE    					 
1999061800264	19990618	00264	NM  	1999	6	18	99ZZZX2301       	1	19990512	G	5320	651960624	CHANNEL         			BOEING	727   	727256      		NM  										AFT LAVATORY	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED IN LT AFT LAVATORY HAT CHANNEL LBL 24.75.						2	L	7	3 	4F				A3WE    					 
1999061800265	19990618	00265	NM  	1999	6	18	99ZZZX2302       	1	19990512	G	5311		FRAME           			BOEING	727   	727256      		NM  										BS 1166	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT STA 1166 BETWEEN STR 28 - STR 29, LEFT.						2	L	7	3 	4F				A3WE    					 
1999061800266	19990618	00266	NM  	1999	6	18	99ZZZX2303       	1	19990512	G	5313		STRINGER        			BOEING	727   	727256      		NM  										BS 990	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED AT STA 990 ON STR 30.						2	L	7	3 	4F				A3WE    					 
1999061800267	19990618	00267	NM  	1999	6	18	99ZZZX2304       	1	19990512	G	5313		STRINGER        			BOEING	727   	727256      		NM  										BS 950	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON STRINGER 28R AT STA 950E.						2	L	7	3 	4F				A3WE    					 
1999061800268	19990618	00268	NM  	1999	6	18	99ZZZX2305       	1	19990512	G	5313		FRAME           			BOEING	727   	727256      		NM  										BS 950	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON FRAME 950C ON STR 29L.						2	L	7	3 	4F				A3WE    					 
1999061800269	19990618	00269	NM  	1999	6	18	99ZZZX2306       	1	19990512	G	5313		STRINGER        			BOEING	727   	727256      		NM  										BS 420-440	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED STA 420 - STA 440 ON STR 28L.						2	L	7	3 	4F				A3WE    					 
1999061800270	19990618	00270	NM  	1999	6	18	99ZZZX2307       	1	19990512	G	5330		PANEL           			BOEING	727   	727256      		NM  										BS 480-560	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED AT STA 480 - STA 560 ON TRANSITION PANEL.						2	L	7	3 	4F				A3WE    					 
1999061800271	19990618	00271	NM  	1999	6	18	99ZZZX2308       	1	19990512	G	5320		SHEAR TIE       			BOEING	727   	727256      		NM  										BS 540	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED AT STA 540 AT STR 27R						2	L	7	3 	4F				A3WE    					 
1999061800272	19990618	00272	NM  	1999	6	18	99ZZZX2309       	1	19990512	G	5320		SHEAR TIE       			BOEING	727   	727256      		NM  										BS 500	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED AT STA 50 AT STR 26R.						2	L	7	3 	4F				A3WE    					 
1999061800273	19990618	00273	NM  	1999	6	18	99ZZZX2310       	1	19990512	G	5320		SHEAR TIE       			BOEING	727   	727256      		NM  										BS 660	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED AT STA 660 AT STR 26R.						2	L	7	3 	4F				A3WE    					 
1999061800274	19990618	00274	NM  	1999	6	18	99ZZZX2311       	1	19990512	G	5330		SKIN            			BOEING	727   	727256      		NM  										BS 680-700	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON STR 26R AND STR 27R AT STA 680 - STA 700.						2	L	7	3 	4F				A3WE    					 
1999061800276	19990618	00276	CE  	1999	6	18	99ZZZX2313       	1	19990409	G	2612	302158	DETECTOR        			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  					RT ENGINE	CORRODED        	E				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			GL	13	2883					BB144	PCE80042			FALSE FIRE WARNING, RT ENGINE.  POSSIBLY CAUSED BY AGE OF THE UNIT, OR MOISTURE AND SOAP CREEPING INSIDE.  SUBMITTER SUG	GESTED BETTER SEALING OF DETECTOR.					1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999061800277	19990618	00277	CE  	1999	6	18	99ZZZX2314       	1	19990426	G	3231	1153800025	ACTUATOR        		115811020613	BEECH 	200   	200BEECH    	1152920	CE  										MLG	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	13	2883				378080	BB144				LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF.  REPLACED MOTOR, SEVERAL CYCLES CARRIED OUT ON JACK, PROPER OPS NOTED.						1	L	7	2 	4T				A24CE   					 
1999061800278	19990618	00278	EU  	1999	6	18	99ZZZX2315       	1	19990415	G	3213	25UMR304	AXLE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										LT MLG	LACK OF LUBE    	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	317CC	4403 				258093				DURING HEAVY MAINTENANCE (SCHEDULED), THE MAXARETS (ANTI-SKID) UNITS WERE REMOVED.  NOTICED THE MAXARET HAD BEEN INSTALL	ED DRY AND NO LUBRICATION WAS PRESENT AS SHOULD HAVE BEEN IAW CHAPTER 32.  INSPECTION OF AXLE BORES FOUND EXCESSIVE PITT	ING.  PITTING COULD NOT BE REMOVED WITHIN THE DEPTHS REQUIRED.  UNIT REPLACED WITH A NEW UNIT.  SUBMITTER STATED LAST TI	ME THIS WAS ACCESSED, AIRCRAFT WAS AT AN APPROVED FACTORY SERVICE CENTER.			2	L	7	2 	4F			RT	A3EU    					 
1999061800279	19990618	00279	SO  	1999	6	18	99ZZZX2316       	1	19990513	G	2720		HINGE           		2070706     	PIPER 	PA30  	PA30        	7103002	SO  										RUDDER	CRACKED         	H	S	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	8329Y					301471				WITH RUDDER REMOVED AND V-FIN BEING STRIPPED FOR PAINTING, THE PAINTER DISCOVERED A CRACK IN THE TOP RUDDER HINGE BOSS U	NDER THE PAINT.  DURING INSPECTION OF THE V-FIN AND RUDDER, FOUND MAJOR REPAIRS HAD BEEN MADE TO BOTH.  SUBMITTER STATED	 IT IS POSSIBLE THE CRACK WAS OVERLOOKED, OR WAS HIDDEN BY PAINT.				1	L	7	2 	3O				A1EA    					 
1999061800280	19990618	00280	CE  	1999	6	18	99ZZZX2317       	1	19990416	G	3231	08411066	BELLCRANK       			CESSNA	310   	310R        	2074245	CE  										RT MLG DOOR	BROKE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	37256					310R0977				THE RIGHT MAIN GEAR IDLER BELLCRANK WAS FOUND BROKEN AT JUST AFTER THE WEBBING PORTION OF THE CASTING THAT SUPPORTS THE 	CURVED ARM OF THE BELLCRANK.  THIS SPECIFIC FAILURE IS THE THIRD ONE SEEN, AND THE SECOND ONE REPAIRED IN TWO MONTHS.  S	UBMITTER STATED ALL FAILURES HAVE BEEN TO THE RIGHT MAIN GEAR BELLCRANK.  ALL AIRPLANES THAT THIS HAPPENED TO ARE OF THE	 APPROXIMATE SAME AGE.			1	L	7	2 	3O				3A10    					 
1999061800281	19990618	00281		1999	6	18	99ZZZX2318       	4	19990525	G	3452	066106200	TRANSPONDER     			PIPER 	PA28  	PA28RT201   	7102818	SO  										E/E BAY	FAILED          	B			QS7R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	09	81897				1005918	28R8018063				KT76A TRANSPONDER FAILED IN-FLIGHT.  TRACED PROBLEM TO FAILED RESISTOR MODULE RM402 ON MAIN CIRCUIT BOARD.  ACCOMPLISHME	NT OF AD 98-14-03 (BENDIX/KING SB K7-76A-7).  REPLACED RM401 AND RM402 AND REPAIRED UNIT.  RE-INSTALLED UNIT AFTER REPAI	R/AD COMPLIANCE AND TESTED GOOD IN AIRCRAFT USING ATC-600 PUMP TESTER (FAR 91.413).  RM 401 AND RM402, P/N 015-00045-000	1.			1	L	7	1 	3O				2A13    					 
1999061800284	19990618	00284	EA  	1999	6	18	99ZZZX2321       	2	19990525	G	7322	30768	FLOAT           	PRECISION   	1060301     	HUGHES	269   	269C1       	8059504	SW  	LYC   	O360  	HO360C1A    	41514	EA  					CARBURETOR	LEAKING         	B				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			WP	03	6151L	408  			75049508	0087	C3624836A			THE PILOT OBSERVED FUEL DRAINING FROM THE CARBURETOR WHILE REFUELING.  THE CARBURETOR WAS REMOVED AND DISASSEMBLED.  THE	 FLOAT WAS FOUND TO HAVE A SMALL QUANTITY OF FUEL IN  IT WHICH CAUSED THE NEEDLE TO REMAIN UNSEATED.  A NEW FLOAT WAS IN	STALLED AND THE ENGINE RAN SATISFACTORY.				1	G	7	1 	3O	3	O	O	4H12    	E286				 
1999061800319	19990618	00319	WP  	1999	6	18	99ZZZX2327       	1	19990513	G	3340	A469B	BULB            			HUGHES	369   	369D        	4470706	WP  										STROBE	FAILED          	B			EOOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	5074R	48   				1151D				ON POST-FLIGHT, BOTH STROBES WERE FOUND INOPERABLE.  THIS IS THE SECOND SET IN 73.6 HOURS.  SUBSEQUENT INSPECTION FOUND 	THE WIRES AT THE LIGHT JUNCTIONS MIS-MARKED.  REWIRED AND REPLACED BULBS.					1	G	7	1 	3U				H3WE    					 
1999062500344	19990625	00344	EU  	1999	6	25	99ZZZX2338       	1	19990524	G	3320	AL12351097	BULB            			FOKKER	F28   	F28MK1000   	4990808	EU  										CABIN	FAILED          	B			K5SR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	43AE	86   				11016				AL-1235-1097 BULB FAILED AFTER 85.9 HOURS OF SERVICE.  BULB FAILED APPROXIMATELY 1 INCH FROM END THROUGH PIN HOLE MELTED	 IN GLASS.  ESCAPING HOT GAS BURNED A HOLE OF APPROXIMATELY .75 INCH IN AIRCRAFT INTERIOR BEFORE STOPPING.					2	L	7	2 	4F			RT	A20EU   					 
1999062500345	19990625	00345	EU  	1999	6	25	99ZZZX2339       	1	19990324	G	7697		WIRE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										ENGINE SYNC	CHAFED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	317CC					258093				DURING HEAVY MAINTENANCE, FOUND WIRE BUNDLE THAT CONNECTS TO THE ENGINE SYNC BOX CHAFED AT THE HYDRAULIC BOX.  THE WIRES	 HAD BEEN ROUTED BETWEEN TWO HYDRAULIC LINES.  THE BUNDLE IS REPAIRABLE.					2	L	7	2 	4F			RT	A3EU    					 
1999062500346	19990625	00346	CE  	1999	6	25	99ZZZX2340       	1	19990525	G	2140		DUCT            			BEECH 	100   	B100        	1152919	CE  										HEAT SYSTEM	SPLIT           	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	03	311CM	6417 				BE101				TAIL DE-ICE BOOTS WOULD NOT INFLATE.  FOUND DE-ICE SUPPLY LINE COLLAPSED AND PINCHED CLOSED DUE TO HEAT DUCT BELOW FLOOR	 TO HAVE A SPLIT SEAM ALLOWING HOT AIR TO HEAT PLASTIC DE-ICE HOSE, SOFTEN, THEN BE SUCKED CLOSED FROM THE NORMAL VACUUM	 SUPPLIED TO BOOTS.  REPAIRED BY REPLACING DE-ICE SUPPLY HOSE AND PERFORMING RED GREEN REPAIR TO THE HEAT DUCT.				1	L	7	2 	4T				A14CE   					 
1999062500347	19990625	00347	GL  	1999	6	25	99ZZZX2341       	2	19990527	G	7313	23031938NC	NOZZLE          		23D3233D    						ALLSN 	250C  	250C20R1    	03013	GL  					NR 2	CRACKED         	B			QD5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07		1414 			X56019		CAT15098			DIAPHRAGM CRACKED JUST UNDER INNER RIM, JUST OVER 2 INCHES LONG, AND LEFT VANE FILLET CRACKED AND BURNED.											3	U			E4CE				 
1999062500348	19990625	00348	GL  	1999	6	25	99ZZZX2342       	2	19990527	G	7313	23038219A	NOZZLE          		23032330    						ALLSN 	250C  	250C20R1    	03013	GL  					NR 1	CRACKED         	B	L		QD5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07		968  			ER183142		CHT15098			INNER AND OUTER BAND CRACKS, SADDLE CRACKS, MANY VANE TRAILING EDGE CRACKS, MULTIPLE IN SAME VANE, SOME OVER .3750 INCH 	LONG.										3	U			E4CE				 
1999062500349	19990625	00349	GL  	1999	6	25	99ZZZX2343       	2	19990527	G	7250	230374	SHAFT           								ALLSN 	250C  	250C20R1    	03013	GL  					ENGINE	CORRODED        	B			QD5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07					KV88295		CAT15098			POWER TURBINE OUTER SHAFT HAS SEVERE DEEP CORROSION AT DIMPLES AND CURVIC COUPLING.   CORROSION AT DIMPLES 360 DEGREES A	ROUND AND OVER HALF AS DEEP AS THE DIMPLE.  SEVERAL CURVIC CORRODED TOPS, INSIDE AND OUT.  PT INNER SHAFT - THE FIRST .2	5 INCH OF THREAD CORRODED AND NICKLE LIFTED AND MISSING FORWARD OF THREADS AND CORROSION PITTED.									3	U			E4CE				 
1999062500350	19990625	00350	GL  	1999	6	25	99ZZZX2344       	2	19990527	G	7250	230374	SHAFT           								ALLSN 	250C  	250C20R1    	03013	GL  					ENGINE	CORRODED        	B			QD5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07					KW94232		CAT15098			POWER TURBINE OUTER SHAFT HAS SEVERE DEEP CORROSION AT DIMPLES AND CURVIC COUPLING.   CORROSION AT DIMPLES 360 DEGREES A	ROUND AND OVER HALF AS DEEP AS THE DIMPLE.  SEVERAL CURVIC CORRODED TOPS, INSIDE AND OUT.  PT INNER SHAFT - THE FIRST .2	5 INCH OF THREAD CORRODED AND NICKLE LIFTED AND MISSING FORWARD OF THREADS AND CORROSION PITTED.									3	U			E4CE				 
1999062600033	19990626	00033		1999	6	26	99ZZZX2345       	1	19990414	G	7810		PIPE            			AMTR  		AVIDCATALINA												EXHAUST	CRACKED         	C				A				UNSCHED LANDING         				Y	E		ENGINE STOPPAGE           	VIBRATION/BUFFET          		CR	CRUISE         	1			SW	99	9224T					A5JAB				TAKE OFF AT AVON PARK 4-14-1999.  AFTER SOME WATERINGS ON LAKE JACKSON HEADING TOWARDS LAKE OKEECHOBEE, MAINTAINING 100 	FEET AGL.  AFTER ABOUT ONE HOUR OF FLIGHT TIME, A BIG BANG OCCURRED, SEVERE VIBRATION FOLLOWED , AND THE ENGINE STARVED.	  THE LET FRONT PIPE BROKE OFF AND WENT THROUGH THE PROPELLER.  IT WAS A STRAIGHT CRACK IN THE STAINLESS ROTAX PART THAT	 FITS INTO THE CYLINDER HEAD RIGHT AFTER THE BRAKES.  THE RT FRONT PIPE BUILT UP A CRACK ON 1 INCH LENGTH IN THE SAME PA	RT, BUT IN A DIFFERENT DIRECTION.  THE TWO PIPES ON THE BACK DID NOT HAVE ANY SINGE OF CRACKS OR OTHER DAMAGE.					0 										 
1999062500351	19990625	00351	EA  	1999	6	25	99ZZZX2346       	2	19990611	G	8530		CYLINDER        			CESSNA	177   	177B        	2073708	CE  	LYC   	O360  	O360A1F6    	41514	EA  					NR 2	CRACKED         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	27	67MM					17702269				NR 2 CYLINDER DEVELOPED AN OIL LEAK DIAGNOSED AS A CRACK THROUGH THE CYLINDER CASTING IN THE AREA OF THE INTAKE VALVE SE	AT.  UPON REMOVING THE CYLINDER FOR EXCHANGE UNDER WARRANTY, THE EXHAUST AND INTAKE ROCKER ARMS WERE DISCOVERED SWAPPED 	AS DELIVERED FROM THE FACTORY.  THE OTHER 3 CYLINDERS WERE CHECKED, AND THE ROCKER ARMS WERE IN THE CORRECT PLACES ON TH	OSE CYINDERS.			1	H	7	1 	3O	3	O		A13CE   	E286				 
1999062500352	19990625	00352	SO  	1999	6	25	99ZZZX2347       	1	19990611	G	3230	454630	CIRCUIT BREAKER 			PIPER 	PA31  	PA31350     	7103110	SO  										COCKPIT	FAILED          	H				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			SO	25	44AC					318052147				PILOT REPORTED THE LANDING GEAR HANDLE WOULD NOT RETURN TO NEUTRAL POSITION AFTER TAKEOFF.  THE LANDING GEAR WAS EXTENDE	D AND ALL THREE GEAR DOWN INDICATORS CAME ON, BUT THE GEAR HANDLE WOULD SITLL NOT RETURN TO NEUTRAL POSITION.  A PRECAUT	IONARY LANDING WAS MADE.  AFTER INSPECTION, IT WAS DETERMINED THE GEAR SAFETY CIRCUIT BREAKER HAD FAILED.  THE CIRCUIT B	REAKER WAS CHECKED FOR RESISTANCE IN THE CLOSED POSITION AND FOUND TO BE ABOVE 70,000 OHMS.  THIS CAUSED THE MAIN GEAR D	OOR ACTUATOR TO STAY OPEN WHICH INHIBITED THE HANDLE FROM RETURNING TO THE NEUTRAL POSITION.  THE CIRCUIT BREAKER WAS RE	PLACED.  THE SYSTEM WAS TESTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.	1	L	7	2 	3O				A20SO   					 
1999062500353	19990625	00353	CE  	1999	6	25	99ZZZX2348       	1	19990426	G	2710	NAS428K412	BOLT            			CESSNA	206   	206H        	2073301	CE  										LT AILERON	LOOSE           	B		A	PRIR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03	14122	12   			12600231	20608025				ON PRE-FLIGHT, PILOT COULD NOT MOVE AILERONS TO LEFT.  UPON INVESTIGATION, FOUND LT AILERON UPSTOP BOLT BACKED OUT LEAVI	NG ONLY A 4 DEGREE TRAVEL.  FOUND STOP NUT LOOSE, BUT HELD IN PLACE BY TORQUE PUTTY.   RE-ADJUSTED STOP TO OBTAIN PROPER	 TRAVEL PER SM AND CHECKED ALL OTHER STOP BOLTS.  FOUND SECOND JAM NUT ON LT BELLCRANK LOOSE AND UPSTOP ON RT BELLCRANK 	LOOSE.  RT DOWN WAS TIGHT.			1	H	7	1 	3O			RT	A4CE    					 
1999062500354	19990625	00354	GL  	1999	6	25	99ZZZX2349       	2	19990527	G	7250	23001967	WHEEL           		23032330    						ALLSN 	250C  	250C20R1    	03013	GL  					TURBINE	CRACKED         	B			QD5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07		1414 			HX20439		CAT15098			TURBINE WHEEL RIM CRACKED THROUGH KNIVES.											3	U			E4CE				 
1999062500358	19990625	00358	CE  	1999	6	25	99ZZZX2353       	1	19990602	G	3241	385814	VALVE           	HYDROAIRE   	385814      	CESSNA	500   	550         	2076604	CE  										BRAKE	MALFUNCTIONED   	G				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	01	CGDR		142  		634	0062				THE ANTI-SKID SERVO VALVE WIRES (POSITIVE AND NEGATIVE) WERE CROSSED ON THE REPLACEMENT OF THE POWER BRAKE VALVE.  THIS 	PREVENTED THE ANTI-SKID SYSTEM FROM ACTUATING THE VALVE TO UNLOAD THE BRAKE HYDRAULIC PRESSURE WHEN A SKID OCCURRED ON L	ANDING RESULTING IN A FLAT TIRE.  THE ANTI-SKID SYSTEM DOES NOT MONITOR THIS VALVE CONDITION, THEREFORE, IT DID NOT PROV	IDE A WARNING ANNUNCIATION TO THE CREW THAT THE SYSTEM WAS INOPERATIVE.  THE WIRE CONNECTORS ARE IDENTICAL AND THE WIRE 	NUMBERS ARE SIMILAR IN APPEARANCE (G111A22 AND G71A22) CONTRIBUTING TO THE PROBLEM OF CORRECTLY MATCHING THEM.  A FUNCTI	ON TEST OF THE SYSTEM WOULD HAVE REVEALED THE PROBLEM.	1	L	7	2 	4F				A22CE   					 
1999062500359	19990625	00359	SW  	1999	6	25	99ZZZX2354       	1	19990526	G	6510	106040316101	ADAPTER         			BELL  	407   	407         		SW  										T/R DRIVE	CORRODED        	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	113TV	579  			AFS1012	53242				ADAPTER HAD PITTED SPLINES.  REPLACED WITH NEW FROM BELL HELICOPTER. REF:  AD 97-24-17(F).						1	G	7	1 	3U			O	H2SW    					 
1999062500360	19990625	00360	SW  	1999	6	25	99ZZZX2355       	1	19990526	G	6510	407040316101	FLYWHEEL        			BELL  	407   	407         		SW  										T/R DRIVE	CORRODED        	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	113TV	579  				53242				FLYWHEEL HAS SPITTED SPLINES.  REPLACED WITH NEW FLYWHEEL FROM BELL HELICOPTER.  REF:  AD 97-24-17(F).						1	G	7	1 	3U			O	H2SW    					 
1999062500361	19990625	00361	SW  	1999	6	25	99ZZZX2356       	1	19990526	G	6510	407340339103	BEARING         			BELL  	407   	407         		SW  										T/R DRIVE	ROUGH           	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	113TV	579  			M9822032212	53242				BEARING HAD ROUGH SPOT, NOISEY.   REPLACED WITH NEW BEARINGS FROM BELL HELICOPTER.  REF:  AD 97-24-17(F).						1	G	7	1 	3U			O	H2SW    					 
1999062500362	19990625	00362	SW  	1999	6	25	99ZZZX2357       	1	19990526	G	6510	406040320101	SHAFT           			BELL  	407   	407         		SW  										T/R DRIVE	CORRODED        	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	113AT	579  			AFS1212	53242				SPLINES PITTED.  REPLACED WITH NEW SHAFT FORM BELL HELICOPTER.  REF:  AD 97-24-17(F).						1	G	7	1 	3U			O	H2SW    					 
1999062500363	19990625	00363	GL  	1999	6	25	99ZZZX2358       	2	19990201	G	7323		BEARING         			HUGHES	500N  	500N        	3027374	SW  	ALLSN 	250C  	250C20R1    	03013	GL  					GOVERNOR	FAILED          	D				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			WP	07	526FB		322  		87460059BR	2N006	CAE295398			PILOT FOUND GOVERNOR SWAGING ABOVE LIMITS FOR SAFE FLIGHT.  ENIGNE SURGING 20 PSI TORQUE AND 5 PERCENT N2.  UPON REMOVAL	 OF GOVERNOR, FOUND DRIVE SHAFT LOCKED-UP.  COMPONENT P/N ALAA123065123.					1	G	7	1 	3U	3	U	NC	H3WE    	E4CE				 
1999062500364	19990625	00364	EU  	1999	6	25	99ZZZX2359       	1	19990515	G	3252	20952253	DAMPENER        			BOLKMS	209   	BO209MONSUN 	5626007	EU  										NLG	DAMAGED         	G		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	23	209DB	774  				139				NOSE GEAR SHIMMY DAMPENER ALSO ALIGNS NOSE SEAL ON RETRACTION:  UNIT SHAFT CIRCLIP FAILED ALLOWING SHAFT TO EXIT BODY AN	D JAMMED NOSE.  GEAR AT ANGLE TO CENTERLINE OF AIRCRAFT.  GROOVE FOR CIRCLIP DOES NOT APPEAR DEEP ENOUGH.					1	L	7	1 	3O			RC	A27EU   					 
1999062500365	19990625	00365	CE  	1999	6	25	99ZZZX2360       	1	19990524	G	5210	05170392	BUSHING         			CESSNA	180   	180J        	2072622	CE  										DOOR HANDLE	LOOSE           	B		A	GJRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	183JP					18052620				P/N 0517039-2 - TWO DOOR HANDLES' SPLINED BUSHING SEPARATES FROM HANDLE CASTING.  SUBMITTER STATED THIS IS A CHRONIC PRO	BLEM WITH THIS PART NUMBER.  REPLACED MANY DOOR HANDLES THAT HAVE SEPARATED - THIS HAPPENS ALMOST EXCLUSIVELY TO NEW HAN	DLES.				1	H	7	1 	3O				5A6     					 
1999062500366	19990625	00366	CE  	1999	6	25	99ZZZX2361       	1	19990430	G	5330	041300427	SKIN            			CESSNA	150   	150M        	2071830	CE  										FUSELAGE	CRACKED         	B	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	05	7661U	8572 				15077787				THE WINDSHIELD HAD WORN THROUGH THE DECK SKIN IT RESTS ON AT THE 11: AND 1:00 O'CLOCK POSITIONS WHEN VIEWED FROM PILOT S	EAT.					1	H	7	1 	3O				3A19    					 
1999062500367	19990625	00367	GL  	1999	6	25	99ZZZX2362       	3	19990501	G	6114	C6447	HUB             			CESSNA	180   	180J        	2072622	CE  						MCAULY	2A36C	2A36C23     	GL  	PROPELLER	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	555BL					18052734		664383		PROPELLER IN SHOP FOR OVERHAUL.  FOUND CRACKS IN PROPELLER HUB THREAD SOCKET IN THREE AREAS ON THE NR 2 BLADE.  PROPELLE	R WAS OIL FILLED, BUT WAS NOT LEAKING.					1	H	7	1 	3O				5A6     		5	C	P880	 
1999062500368	19990625	00368	EU  	1999	6	25	99ZZZX2363       	1	19990525	G	3510		SWITCH          			SOCATA	TBM   	TBM700      	8682000	EU  										OXYGEN SYSTEM	MALFUNCTIONED   	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	01	56WF					8				RED CAUTION LIGHT COMES ON FOR OXYGEN SYSTEM - INTERMITTENT.  TROUBLESHOT SYSTEM TO COPILOT'S OXYGEN SYSTEM MICROSWITCH.	  WHEN COPILOT'S SEAT WAS RAISED , END OF A SCREW PUSHED SWITCH CAUSING SWITCH TO MAKE CONTACT.  REMOVED COPILOT'S SEAT,	 CUT END OF SCREW OFF.  CHECKED SWITCH FOR PROPER ADJUSTMENT.  CHECKS GOOD.  OPERATED SEAT, NO INTERFERENCE WITH SWITCH.	  RE-INSTALLED SEAT, RED LIGHT OUT.			1	L	7	1 	3T			RT	A60EU   					 
1999062500369	19990625	00369	CE  	1999	6	25	99ZZZX2364       	1	19990525	G	2822	8679523	VALVE           		8974005     	MTSBSI	MU2   	MU2B36      	5780412	CE  										FUEL PUMP	DAMAGED         	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	500PJ		56   		P182C	668				HIGH PRESSURE RELIEF VALVE BODY, P/N 867927-1, WAS STILL IN FUEL PUMP HOUSING, BUT THE WRENCHING FLATS AND CAP OF RELIEF	 VALVE WERE FOUND HANGING FROM SAFETY WIRE CAUSING FUEL TO BE SPRAYED ON ENGINE.  FUEL COULD ONLY BE STOPPED BY SHUTTING	 OFF AIRFRAME SUPPLY TO ENGINE.  FOUND DURING GROUND POWER-UP OF AIRCRAFT WITH ENGINES STOPPED AND AIRFRAME BOOST PUMPS 	AND AIRRAME FUEL SHUT-OFF VALVES ON.			1	H	7	2 	3T			RT	A10SW   					 
1999062500370	19990625	00370	NM  	1999	6	25	99ZZZX2365       	1	19990603	G	2730		CONTROL UNIT    			BOEING	727   	727         		NM  										ELEVATOR	DAMAGED         	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01										TWO TYPES OF HOUSING ASSY'S ARE INCORPORATED ON THE CONTROL UNIT, P/N 401-61155-7, WHICH IS MADE OF MAGNESIUM AND WEIGHS	 28.48 POUNDS, AND P/N 401-67675-01, WHICH IS MADE OF ALUMINUM ALLOY AND WEIGHS 36.0 POUNDS.  THE LINKAGE LUGS OF THE CO	NTROL UNIT'S HOUSING ARE BEING FOUND DAMAGED.				2	L	7	3 	4J			RT						 
1999062500371	19990625	00371	NM  	1999	6	25	99ZZZX2366       	1	19990527	G	2923	654468311	HOUSING         		654468117   	BOEING	737   	737300      	1384610	NM  										HYDRAULIC PUMP	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					2989					HOUSING ASSY CRACKED AT PRESSURE PORT.						2	L	7	2 	4F			RT	A16WE   					 
1999062500372	19990625	00372	NM  	1999	6	25	99ZZZX2367       	1	19990604	G	2740	69778552	SPRING          		654997025   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	BROKEN          	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		2261 			KE01066					HORIZONTAL STABILIZER SPRING, P/N 65-77855-2, WAS FOUND BROKEN.						2	L	7	2 	4F			RT	A16WE   					 
1999062500373	19990625	00373	NM  	1999	6	25	99ZZZX2368       	1	19990520	G	2740	69778552	SPRING          		654997025   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	BROKEN          	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		31728	18787		KE00785					ONE, PN 69-77855-2, SPRING WAS FOUND BROKEN IN THE AUXILIARY BRAKE SYSTEM.						2	L	7	2 	4F			RT	A16WE   					 
1999062500374	19990625	00374	NM  	1999	6	25	99ZZZX2369       	1	19990603	G	3230	5059	SHUTTLE VALVE   	PNEUDRAULICS		BOEING	737   	7373G7      	1384595	NM  										MLG	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	150AW	4548 			3391	23218				HAIR LINE CRACK LONG THE CASTING SEAM IN MOUNG BOLT HOLE.  WEAK OR FLAWED CASTING.						2	L	7	2 	4F			RT	A16WE   					 
1999062500375	19990625	00375	EU  	1999	6	25	99ZZZX2370       	1	19990430	G	3010	F50B258700A2	DUCT            			AMD   	FALC50	FALCON50MYST	2730106	EU  										ANTI-ICE SYSTEM	CRACKED         	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	508EJ					8				FOUND A 17 INCH LONGITUDINAL CRACK, AT THE 12 O'CLOCK POSITION, IN THE TOP SKIN OF SECT 3 OF THE AFT S-DUCT NEAR ANTI-IC	E PLENUM, FOUND NUMEROUS STIFFENER ANGLES CRACKED AROUND OUTER CIRCUMFERENCE OF AFT SECT OF DUCT.  FALCON JET SB NR 220 	ON THIS DUCT, WHICH IF INCORP, WOULD HAVE PREVENTED THIS CRACK FROM OCCURRING.  THE NEW REPLACEMENT DUCT, PN F50B258720A	2, HAS BEEN MANUFACTURED TO ADDRESS THE PROBLEM AND CONFORMS TO MODIFICATION 1667, WHILE SUPERSEDES MODIFICATION 1666/AN	D SB 220.		2	L	7	3 	4F				A46EU   					 
1999062500376	19990625	00376	CE  	1999	6	25	99ZZZX2371       	1	19990524	G	3213	244101115	STRUT           			LEAR  	55    	55LEAR      	5170702	CE  										MLG	DAMAGED         	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	553DJ	5770 				003				STRUT HITTING FORWARD WHEELWELL WING FASTENER NOT ALLOWING STRUT HOUSING TO FULLY EXTEND.  LEARJET RECOMMENDED BLENDING 	STRUT FOR CLEARANCE.					2	L	7	2 	4F				A10CE   					 
1999062500377	19990625	00377	CE  	1999	6	25	99ZZZX2372       	1	19990524	G	3213	244101116	STRUT           			LEAR  	55    	55LEAR      	5170702	CE  										MLG	DAMAGED         	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	553DJ	5770 				003				STRUT HITTING FORWARD WHEELWELL WING FASTENER NOT ALLOWING STRUT HOUSING TO FULLY EXTEND.  LEARJET RECOMMENDED BLENDING 	STRUT FOR CLEARANCE.					2	L	7	2 	4F				A10CE   					 
1999062500378	19990625	00378	SW  	1999	6	25	99ZZZX2373       	1	19990525	G	3213	54530031	PISTON          	OZONE       	0AS54535SA  	SWRNGN	SA226 	SA226AT     	8780405	SW  										MLG	PITTED          	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	55CE	197  			1923	AT004				CHROME PORTION OF PISTON IS POROUS ALLOWING HYDRAULIC FLUID TO WEEP OUT.  INSPECTION WITH 10X GLASS REVEALS TINY PORES A	ND CHECKS IN CHROME SURFACE.  PISTON WAS MAGNAFLUXED DYE PENERANT INSPECTION WITH NEGATIVE CRACK INDICATIONS.  SUBMITTER	 SUSPECTED DEFECT IN CHROMING PROCESS ALLOWING FLUID TO PASS BETWEEN STEEL BARREL AND CHROME SURFACE.  ASSEMBLY MFG DATE	 12-11-89.			2	L	7	2 	4T			RT	A5SW    					 
1999062500379	19990625	00379	EU  	1999	6	25	99ZZZX2374       	1	19990430	G	3220	ED2872501	TORSION SHAFT   			ISRAEL	1124  	1124        	4500102	EU  										NLG	CRCKED          	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	332DF	6824 				332				NO SPECIFIC INSTRUCTIONS TO INSPECT THE KEYWAY AREA ON INSPECTION GUIDE.  SUBMITTER SUGGESTED THIS SHOULD BE PLACED ON T	HE INSPECTION GUIDE.   FOUND OTHER TORSION SHAFTS CRACKED IN SAME AREA.					2	M	7	2 	4F				A2SW    					 
1999062500381	19990625	00381	CE  	1999	6	25	99ZZZX2376       	1	19990525	G	3213	07410016	AXLE            			CESSNA	185   	A185F       	2072821	CE  										RT MLG	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	4611E					18503813				AIRCRAFT ON WHEEL SKIS.  TURNING AIRCRAFT BY HAND APPLIED TORQUE LOAD TO LANDING GEAR.						1	H	7	1 	3O				3A24    					 
1999062500382	19990625	00382	EA  	1999	6	25	99ZZZX2377       	2	19990521	G	7414	M3163	IMPULSE COUPLING	SLICK       	4371        	BBAVIA	8     	8GCBC       	1220803	SW  	LYC   	O360  	O360C1E     	41514	EA  					MAGNEO	BENT            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	444AW	458  			95010464	37395				DURING C/W MAGNETO 500-HOUR INSPECTION AT AN ANNUAL, A BENT RIVET WAS FOUND ON LEFT MAGNETO IMPULSE COUPLING PAWL.  GAP 	EXCEEDED 0.150 INCH.					1	H	7	1 	3O	3	O		A21CE   	E286				 
1999062500383	19990625	00383	CE  	1999	6	25	99ZZZX2378       	1	19990526	G	5540	51310104	BEARING PLATE   			CESSNA	421   	421C        	2076016	CE  										RUDDER	MISINSTALLED    	B			UE3R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	13	81RD	3100 				421C0291				AFTER HAVING BEEN ALERTED TO THE POSSIBILITY BY PUBLISHED REPORTS, INSPECTED LOWER RUDDER PIVOT BEARING SUPPORT PLATE AN	D FOUND IT TO HAVE BEEN INSTALLED UPSIDE DOWN.  RECORDS INDICATE THIS IS THE ORIGINAL FACTORY INSTALLATION.					1	L	7	2 	3O				A7CE    					 
1999062500384	19990625	00384		1999	6	25	99ZZZX2379       	4	19990525	G	6113	075263717	BULKHEAD        	MCAULY      	C2A34C204   	CESSNA	182   	182Q        	2072732	CE  										SPINNER	DEFORMED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	5318N	15   			801012	18267642				SPINNER BULKHEAD WAS ASSEMBLED INCORRECTLY DURING PREVIOUS REPLACEMENT CAUSING BULKHEAD TO BECOME DEFORMED AND SPINNER T	O WOBBLE.					1	H	7	1 	3O			NT	3A13    					 
1999062500385	19990625	00385	CE  	1999	6	25	99ZZZX2380       	1	19990607	G	7910	20500111	TUBE            			CESSNA	177   	177RG       	2073709	CE  										ENGINE SUMP	MALFUNCTION     	D				A				UNSCHED LANDING         				R	K	J	PARTIAL RPM/PWR LOSS      	FLUID LOSS                	WARNING INDICATION        	NR	NOT REPORTED   	1			SW	01	2591V	4893 				177RG0627				AFTER 15 MINUTES FLIGHT TIME OF 1ST FLT AFTER ANNUAL, PILOT NOTICED PROP OVERSPEEDING AND ENG OIL PRESS DROPPING TO ZERO	.  PILOT ACCOMPLISHED SUCCESSFUL PARTIAL POWER, DOWNWIND, EMERG LANDING.  ENG STOPPED WHEN ACFT HAD CLEARED RUNWAY.  ENG	 COMPT AND BELLY COVERED WITH OIL, NO OIL SHOWED ON THE DIPSTICK.  NO LEAKS FOUND.  DRAIN VALVE FUNCTIONED PROPERLY.  WH	ILE CHECKING OIL QUICK DRAIN, NOTED ATTACHED OIL DRAIN TUBE, PN 2050011-1, HAD A DENT ON LOWER END AND THE NOSE GEAR TRU	NNION HAD FRESHLY CHIPPED PAINT ON UPPER LT PORTION.  OIL DRAIN TUBE BECAME LOOSE UNDER VIBRATION AND AIR LOAD,  FOULED 	NOSE GEAR TRUNNION.  WITH NOSE GEAR FULLY RETRACTED, OIL QUICK DRAIN FORCED OPEN ALLOWING ALL OIL TO VENT OVERBOARD.	1	H	7	1 	3O				A20CE   					 
1999062500386	19990625	00386	SW  	1999	6	25	99ZZZX2381       	1	19990507	G	5711		SPAR            			BBAVIA	7     	7ECA        	21101NN	SW  										WING	CRACKED         	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	2563F					137				WOOD SPAR (AFT) COMPRESSION CRACK, MID-SPAN AT COMPRESSION STRUT CRACKED FROM TOP SURFACE DOWN TO BOLT HOLE (COMPRESSION	 STRUT).					1	H	7	1 	3O				A759    					 
1999062500388	19990625	00388	EA  	1999	6	25	99ZZZX2383       	2	19990523	G	8530	15F1995713	PUSH ROD        								LYC   	O320  	O320B2C     	41508	EA  					ENGINE	WORN            	B			VI4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15							L1514039A			PUSH ROD BELOW BALL END SHOW SIGNS OF RUBBING AGAINST THE INSIDE RIDGE OF THE ROCKER ARM WHERE BALL AND SOCKET MEET.  IT	 APPEARS THE ROCKER ARM WAS NOT MACHINED OUT FOR CLEARANCE FOR WHEN THE ROCKER ARM IS PIVOTED TO ITS MAX OPENING WHICH W	OULD LEAD TO THE PUSH ROD RIDING ON THE INSIDE EDGE OF THE ROCKER ARM SOCKET.  ALL EIGHT PUSH RODS SHOW SIGNS OF THIS. S	UBMITTER RECOMMENDED THAT LATE MODEL ENGINES WITH 17F19353 ROCKER ARMS BE REMOVED FOR INSPECTION IN SOCKET END CLEARANCE	 FOR THE PUSH RODS.							3	O			E274				 
1999062500389	19990625	00389	NE  	1999	6	25	99ZZZX2384       	2	19990422	G	8550	RD4002	SCAVENGE PUMP   		735511A     						PWA   	JT8   	JT8*        	52044	NE  					OIL SYSTEM	SEIZED          	B			OB2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	07		71   			B1993					A PIECE OF METAL LODGED IN THE SCAVENGE PUMP CAUSED SEIZURE.  THE SCAVENGE PUMP SEIZURE CAUSED HIGH OIL TEMPERATURE.  TH	E PIECE OF METAL IN THE SCAVENGE PUMP WAS A GEAR TOOTH, WHICH HAD SEPARATED FROM THE CHARGE PUMP GEAR.  THIS GEAR HAS BE	EN SENT TO A LAB TO DETERMINE CAUSE OF FAILURE.  ONCE THE CAUSE HAD BEEN DETERMINED, WILL BE ABLE TO STATE POSSIBLE CAUS	E AND RECOMMENDATIONS TO PREVENT RECURRENCE.  THIS IS A PMA GEAR MANUFACTURED BY ROGERS-DIERKS INC., FOR REPLACEMENT OF 	SUNDSTRAND P/N 641833.							4	F			E2EA				 
1999062500390	19990625	00390	GL  	1999	6	25	99ZZZX2385       	2	19990409	G	7210	6821328	BEARING         								ALLSN 	501D  	501D13H     	03004	GL  					TORQUE SHAFT	CRACKED         	B	S		XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01					NDD536					BEARING DEFECTS ON TORQUE SHAFT DETECTED DURING MAGNETIC INSPECTION ON P. O. NR 26366 FROM PACIFIC SKY SUPPLY.											4	T			E282				 
1999062500391	19990625	00391	SW  	1999	6	25	99ZZZX2386       	1	19990601	G	7921	8542228	COOLER          	LORINORDAM  		MOONEY	M20   	M20         	5870202	SW  										OIL SYSTEM	LEAKING         	B			RF3R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	23					78C788					PART RECEIVED EPOXY REPAIRS THAT FAILED DURING NORMAL SERVICE.  EPOXY WAS USED OVER CRACKS WHICH WORKED THROUGH TO THE S	URFACE OF THE HARDENED EPOXY ALLOWING THE OIL COOLER TO LEAK AGAIN.  SUBMITTER STATED EPOXY FAILURE IS COMMON IN OIL COO	LERS AND RECOMMENDED ELIMINATING EPOXY USE IN OIL COOLERS.  REF:  P.O.C.S. W/O NR 21054.				1	L	7	1 	3O				2A3     					 
1999062500392	19990625	00392	SO  	1999	6	25	99ZZZX2387       	2	19990205	G	8530	654719	PISTON RING     								CONT  	O520  	IO520D      	17032	SO  					ENGINE	MISMANUFACTURED 	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	07										AT INSTALLATION, 5 OUT OF 6 SETS OF RINGS WERE DISCOVERED TO HAVE CHIPS IN THE CHROME ON THE OUTER CIRCUMFERENCE OF THE 	2ND COMPRESSION RING.  SUBMITTER SUGGESTED A POSSIBLE CAUSE AS LACK OF QUALITY CONTROL AT THE FACTORY.										3	O			E5CE				 
1999062500393	19990625	00393	GL  	1999	6	25	99ZZZX2388       	3	19990602	G	6114	D5904	HUB             													MCAULY	3A32C	D3A32C90    	GL  	PROPELLER	LEAKING         	B			DJFR	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			EA	23			105  		7710102			7710102		PILOT REPORTED RED DYE OIL LEAK.  DISASSEMBLED PROPELLER AND FOUND HUB CRACKED, NR 2 BLADE SOCKET.																5	C	P21E	 
1999062600034	19990626	00034	EA  	1999	6	26	99ZZZX2389       	2	19990603	G	7322	MA4SPA	CARBURETOR      			CESSNA	172   	172P        	2072436	CE  	LYC   	O320  	O320D2J     	41508	EA  					ENGINE	MALFUNCTIONED   	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	07	65058	289  			DC32266	17275678	L150139A			ENGINE WOULD NOT SHUT OFF WITH MIXTURE CONTROL.  FOUND CARBURETOR BOWL LOOSE, BUT MOUNTING BOLTS STILL HAD LOCK TABS IN 	PLACE.  BOLTS APPEARED TO BE LOOSE IN THREADS IN BOWL.  NEED TO HAVE A LOOK AT PAM MANUFACTURING PROCEDURES.					1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999062500394	19990625	00394	NE  	1999	6	25	99ZZZX2390       	2	19990428	G	8550	RD4002	SCAVENGE GEAR   		735511A     						PWA   	JT8   	JT8*        	52044	NE  					OIL SYSTEM	FAILED          	B			OB2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	07		204  			B3672					THE MPA RD4002 SCAVENGE PUMP GEAR FAILED.  A GEAR TOOTH CAME OFF AND LODGED IN THE PUMP CAUSING THE PUMP TO SEIZE WHICH,	 IN TURN, CAUSED THE OIL TEMP LIGHT TO ILUMINATE AND THE FREQS TO FLUCTUATE.  THE GEARS WERE REMOVED AND REPLACED.  SUBM	ITTER IS REQUESTING THE RETURN OF SEVEN CSD'S WHICH HAVE THE PMA GEARS INSTALLED.  UPON RECEIPT, WILL REMOVE AND REPLACE	 THE GEARS.								4	F			E2EA				 
1999062500395	19990625	00395	NE  	1999	6	25	99ZZZX2391       	2	19990422	G	8550	RD4002	SCAVENGE PUMP   		735511A     						PWA   	JT8   	JT8*        	52044	NE  					OIL SYSTEM	SEIZED          	B			OB2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	07		95   			B3757					A PIECE OF METAL LODGED IN THE SCAVENGE PUMP CAUSING SEIZURE.  THE SCAVENGE PUMP SEIZURE CAUSED HIGH OIL TEMPERATURE.  T	HE PIECE OF METAL IN THE SCAVENGE PUMP WAS A GEAR TOOTH WHICH HAD SEPARATED FROM THE CHARGE PUMP GEAR.  THIS GEAR HAS BE	EN SENT TO A LAB TO DETERMINE CAUSE OF FAILURE.  ONCE THE CAUSE HAD BEEN DETERMINED, WILL BE ABLE TO STATE POSSIBLE CAUS	E AND RECOMMENDATIONS TO PREVENT RECURRENCE.  THIS IS A PMA GEAR MANUFACTURED BY ROGERS - DIERKS INC., FOR REPLACEMENT O	F SUNDSTRAND, P/N 641833.							4	F			E2EA				 
1999062500396	19990625	00396	GL  	1999	6	25	99ZZZX2392       	2	19990415	G	7250	6890040	SHIELD          			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					ENGINE	CRACKED         	B	S		XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01					17860					CRACKS DETECTED DURING FLUORESCENT PENETRANT INSPECTION.  REF:  PACIFIC SKY SUPPLY, P. O. NR 26388.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999062500397	19990625	00397	SW  	1999	6	25	99ZZZX2393       	1	19990607	G	2910	70010H00012180	LINE            			BELL  	206   	206B        	1181511	SW  										HYDRAULIC SYSTEM	DAMAGED         	H				A				UNSCHED LANDING         				K	J		FLUID LOSS                	WARNING INDICATION        		NR	NOT REPORTED   	1			WP	13	801H	9    				3186				DURING IN-FLIGHT, PILOT NOTICED LOSS OF HYDRAULIC SYSTEMS.  PILOT MADE A PRECAUTIONARY LANDING.  AIRCRAFT INSPECTED, FOU	ND THE HYDRAULIC PRESSURE LINE WAS DEFECTIVE ONLY 9.0 HOURS SINCE INSTALLED.  REMOVED AND REPLACED HYDRAULIC LINE AND PE	RFORMED GROUND RUN AND OPERATION AND LEAK CHECK.  NO DEFECTS FOUND.  AIRCRAFT RETURNED TO SERVICE.				1	G	7	1 	3U				H2SW    					 
1999062500398	19990625	00398	CE  	1999	6	25	99ZZZX2394       	1	19990607	G	2140	K1250860M203	HEAT EXCHANGER  			CESSNA	206   	TU206G      	2073357	CE  										CABIN HEAT	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	6233Z	296  				U20606195				HEAT EXCHANGER IS PART OF COMPLETE KINLEY WELDING, INC., EXHAUST SYSTEM INSTALLED UNDER STC SA5010NM AND STC SE5009NM. T	HE HEAT EXCHANGER HAS HEAT TRANSFER STUBS WELDED TO ITS OUTER SURFACE FOR WARMING AIR FOR CABIN HEAT.  TWO OF THESE STUD	S WERE FOUND CRACKED LOOSE FROM THE EXCHANGER BODY DUE TO CRACKS IN THE BODY AROUND THE BASES OF THE STUDS.  THE CRACKS 	OPENED UP ALLOWING EXHAUST GAS TO BLEED INTO THE HEATED CABIN AIR.			1	H	7	1 	3O				A4CE    					 
1999062500399	19990625	00399	SO  	1999	6	25	99ZZZX2395       	2	19990501	G	8500		ENGINE          			CESSNA	421   	421C        	2076016	CE  	CONT  	O520  	GTSIO520L   	17032	SO  					FORWARD	FAILED          	D				A				UNSCHED LANDING         				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			GL	23	5488G	4670 	1504 			421C0235	239818R			OIL PRESSURE DROPPED, ENGINE PROPELLER STARTED SLOWING.  PILOT FEATHERED PROPELLER AND MADE SAFE, PRECAUTIONARY LANDING.	  APPEARS ENGINE HAD CATASTROPHIC FAILURE.  CRANK, ROD, OR COUNTERWEIGHT HAD COME APART.  SUBMITTER STATED TOO EARLY IN 	INVESTIGATION TO NAME SPECIFIC CAUSE.				1	L	7	2 	3O	3	O		A7CE    	E7CE				 
1999062500401	19990625	00401	CE  	1999	6	25	99ZZZX2397       	1	19990509	G	3230	08411304	TUBE            			CESSNA	310   	310         	2074202	CE  										LT FUSELAGE	FAILED          	C				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			GL	23	4846B	2681 				35146				UPON LANDING TOUCHDOWN AT YIP, THE LEFT MLG COLLAPSED.  INVESTIGATION SHOWED A FAILURE OF THE LT MAIN GEAR DRIVE TUBE AS	SY WHICH PREVENTED THE LEFT MAIN GEAR FROM LOCKING DOWN AFTER EXTENSION WAS SELECTED					1	L	7	2 	3O			RT	3A10    					 
1999062500402	19990625	00402	SO  	1999	6	25	99ZZZX2398       	1	19990607	G	2710	452860	ROD END         			PIPER 	PA38  	PA38112     	7103812	SO  										AILERON	BROKEN          	D				O				OTHER                   				F			FLT CONT AFFECTED         			NR	NOT REPORTED   	1			EA	17	2441A					3878A0691				DURING FLIGHT, LT AILERON WOULD NOT RESPOND TO CONTROLS.  FOUND AFT LT ROD END BROKEN AT AFT SIDE OF LOCKNUT AND BEARING	 END FROZEN AND IMMOVABLE, EVEN AFTER REMOVAL.  PILOT NOTICED AILERONS LOCKED ON GROUND WITH SEAT BELTS WITH LEFT AILERO	N DOWN POSITION WHEN TIED DOWN.  ALSO, ROD END LOWER HALF WAS CORRODED.  SUBMITTER RECOMMENDED NOT TO LOCK AILERONS IN T	HIS POSITION CAUSING OXYGEN TO BUILD-UP AROUND ROD END.			1	L	7	1 	3O				A18SO   					 
1999062500403	19990625	00403	EA  	1999	6	25	99ZZZX2399       	2	19990608	G	7414	K3822	DIST BLOCK      	SLICK       	4381        	CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  					RT MAGNETO	WORN            	H			CB9T	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	24708	551  			98010725	15280332	L1507615			DURING ROUTINE 500-HOUR INSPECTION OF BOTH MAGNETOS, OILITE BUSHING IN BOTH LT AND RT DISTRIBUTOR BLOCKS WERE FOUND WORN	 EXCESSIVELY.  REPLACED WITH NEW K3822 DISTRIBUTOR BLOCK AND GEAR ASSEMBLIES.  DUE TO LOW TIME ON MAGNETOS, SUBMITTER SU	GGESTED POSSIBLE CAUSE OF BUSHING FAILURE MAY BE IMPROPER LUBRICATION IN OILITE BUSHING WHEN INSTALLED AT FACTORY.				1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999062500404	19990625	00404	EA  	1999	6	25	99ZZZX2400       	2	19990608	G	7414	K3822	DIST BLOCK      	SLICK       	4381        	CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  					LT MAGNETO	WORN            	H			CB9T	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	24708	551  			98010724	15280332	L1507615			DURING ROUTINE 500-HOUR INSPECTION OF BOTH MAGNETOS, OILITE BUSHING IN BOTH LT AND RT DISTRIBUTOR BLOCKS WERE FOUND WORN	 EXCESSIVELY.  REPLACED WITH NEW K3822 DISTRIBUTOR BLOCK AND GEAR ASSEMBLIES.  DUE TO LOW TIME ON MAGNETOS, SUBMITTER SU	GGESTED POSSIBLE CAUSE OF BUSHING FAILURE MAY BE IMPROPER LUBRICATION IN OILITE BUSHING WHEN INSTALLED AT FACTORY.				1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999062500444	19990625	00444	EA  	1999	6	25	99ZZZX2402       	2	19990527	G	7414	1038255511	MAGNETO         	BENDIX      		MOONEY	M20   	M20J        	5870219	SW  	LYC   	O360  	IO360A3B6   	41514	EA  					ENGINE	LOOSE           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	34SA	171  			R1152270K	240428	L1817351A			FOUND MAGNETO SEPARATED FROM ENGINE.  HOLD DOWN BLOCKS WORE FLANGE DOWN.  NEW LOCKING HARDWARE WAS INSTALLED PREVIOUSLY.	  SUBMITTER STATED THIS HAS BEEN FOUND ON 3 OTHER INSTALLATIONS OVER PAST 2 YEARS.					1	L	7	1 	3O	3	O		2A3     	1E10				 
1999062500452	19990625	00452	GL  	1999	6	25	99ZZZX2410       	1	19990518	G	3211		SUPPORT         			BLANCA	17    	1730A       	1220433	GL  										MLG	FAILED          	D	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	179TW					7930957				LEFT MG UPPER STRUT HOUSING WELD FAILED CAUSING STRUT TO TEAR LOOSE FROM TRUNNION. REMOVED RIGHT MG UPPER STRUT HOUSING 	AND FOUND FAILED WELD.  APPEARED TO BE LACK OF PENETRATION AT MANUFACTURERS.  RE-WELDED TO REPAIR,BOTH UNITS.					1	L	7	1 	3O				A18CE   					 
1999062500453	19990625	00453	CE  	1999	6	25	99ZZZX2411       	1	19990412	G	3230	57422042	RAMP            			CESSNA	421   	421C        	2076016	CE  										NLG	BROKEN          	B			DXGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	5478G	90   				421C0225				DURING PRE-FLIGHT, RAMP ON REAR OF NOSE GEAR THAT CONTACTS ARM TO CLOSE NOSE GEAR DOORS WAS FOUND BROKEN.  SUBMITTER SUS	PECTED DAMAGE OCCURRED FROM TOWING WITH NOSE GEAR LIFTING CRADLE THAT HAS STRAP TO SECURE NOSE GEAR.  SUGGEST CAUTION PL	ACARD BE PLACED ON NOSE GEAR.				1	L	7	2 	3O				A7CE    					 
1999062500454	19990625	00454	GL  	1999	6	25	99ZZZX2412       	1	19990501	G	2434	DIN93LM10X60	MOUNT           			DIAMON	DA20  	DA20C1      	2990001	GL  										ALTERNATOR	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	954CT					00054				FOUND BOLT SHEARED BELOW HEAD.  SUBMITTER STATED THIS AIRCRAFT SERIAL NUMBER IS NOT INCLUDED IN THE RANGE OF THE DIAMOND	 SB ON THIS SUBJECT.					1	L	7	1 	3O			NT	TA4CH   					 
1999062500455	19990625	00455	GL  	1999	6	25	99ZZZX2413       	1	19990501	G	2434	2224111000	MOUNT           			DIAMON	DA20  	DA20C1      	2990001	GL  										ALTERNATOR	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	953CT	100  				C0053				FOUND ALTERNATOR BRACKET BROKE AT THE UPPER PIVOT.  APPEARED TO BE A BAD WELD, NO PENETRATION OF WELD BEAD INTO BASE MAT	ERIAL.					1	L	7	1 	3O			NT	TA4CH   					 
1999062500456	19990625	00456	SO  	1999	6	25	99ZZZX2414       	1	19990606	G	3230		VALVE           			PIPER 	PA23  	PA23250     	7102308	SO  										MLG	RUPTURED        	B			LG1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	40204	9516 				277305001				POST GEAR-UP LANDING INSP REVEALED FOLLOWING:  FOUND LT GEAR SEQUENCER VALVE HYD LINE, BEHIND LT UPHOLSTERY PANEL, CHAFE	D, RUPTURED.  LT RUDDER CABLE PASSES UNDER THIS LINE AND HAD CHAFED APPROX 2 INCHES OF THE LINE WHICH ALLOWED PRIMARY HY	D FLUID TO BE  DUMPED OVERBOARD.  WHEN PILOT ATTEMPTED TO USE AUX HAND PUMP, REMAINING BACKUP FLUID WAS DUMPED.  RECOMME	ND A ONE-TIME INSP OF AREA ON RT AND LT SIDES TO DETERMINE CLEARANCES BETWEEN CABLES, WIRES, HYD LINES.  WHEN EMERG CO2 	GEAR EXT SYS ACTIVATED, CABLE HOUSING TO PRIORITY VALVE SLIPPED WHICH ALLOWED CO2 BOTTLE TO BLOW, DID NOT PULL PIN ON PR	IORITY VALVE, CO2 NOT DIRECTED TO THE MAIN DOWN POSITION.  RECOMMEND BETTER SECURITY OF EMERG GEAR DOWN SYS CABLES.	1	L	7	2 	3O				1A10    					 
1999062500457	19990625	00457	SO  	1999	6	25	99ZZZX2415       	1	19990606	G	3232		VALVE           			PIPER 	PA23  	PA23250     	7102308	SO  										MLG	FAILED          	B			LG1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	40204	9516 				277305001				POST GEAR-UP LANDING INSP REVEALED FOLLOWING:  FOUND LT GEAR SEQUENCER VALVE HYD LINE, BEHIND LT UPHOLSTERY PANEL, CHAFE	D, RUPTURED.  LT RUDDER CABLE PASSES UNDER THIS LINE AND HAD CHAFED APPROX 2 INCHES OF THE LINE WHICH ALLOWED PRIMARY HY	D FLUID TO BE  DUMPED OVEBOARD.  WHEN PILOT ATTEMPTED TO USE AUX HAND PUMP, REMAINING BACKUP FLUID WAS DUMPED.  RECOMMEN	D A ONE-TIME INSP OF AREA ON RT AND LT SIDES TO DETERMINE CLEARANCES BETWEEN CABLES, WIRES, HYD LINES.  WHEN EMERG CO2 G	EAR EXT SYS ACTIVATED, CABLE HOUSING TO PRIORITY VALVE SLIPPED WHICH ALLOWED CO2 BOTTLE TO BLOW, DID NOT PULL PIN ON PRI	ORITY VALVE, CO2 NOT DIRECTED TO THE MAIN DOWN POSITION.  RECOMMEND BETTER SECURITY OF EMERG GEAR DOWN SYS CABLES.	1	L	7	2 	3O				1A10    					 
1999062500458	19990625	00458		1999	6	25	99ZZZX2416       	1	19990528	G	2460	SO1064001	RELAY           	LEACH       	58982       															E/E BAY	MISMANUFACTURED 	B	P	A	RO3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03										WHILE CONDUCTING A VISUAL INSPECTION PRIOR TO ASSEMBLY, NOTED THE TOP OF THE RELAY BASE IDENTIFIERS DID NOT MATCH THE BO	TTOM SECTION OF THE BASE.  THIS ITEM COULD BE ASSEMBLED AND ONCE INSTALLED IN THE AIRCRAFT, COULD CAUSE NUMEROUS MAN HOU	RS TRYING TO CORRECTLY RING OUT THE SYSTEM.  SUBMITTER RECOMMENDED ALL RELAY BASES BE INSPECTED TO ENSURE THE RELAY BASE	 HAS BEEN PROPERLY ASSEMBLED.																 
1999062500459	19990625	00459	SO  	1999	6	25	99ZZZX2417       	1	19990604	G	3320		RECEPTACLE      	BRUCE       	BC1004517   	GULSTM	G1159 	GIV         	3980115	SO  										CABIN	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	315GA	1114 				1315				DURING A 12-MONTH INSPECTION REQUIREMENT ON THE BRUCE LIGHTING SYSTEM, TWO LAMP ASSEMBLIES WERE FOUND TO HAVE CRACKED RE	CEPTACLES.  P/N BB 10020-03-94 CAGE 17023.  SUBMITTER BELIEVED THIS WAS CAUSED BY THE SPRING TENSION ON THE LAMP.  RE: C	USTOMER BULLETIN NR 98.				2	L	7	2 	4F			RT	A12EA   					 
1999062500460	19990625	00460		1999	6	25	99ZZZX2418       	4	19990409	G	2312	VHF20A	RADIO           	COLLINS     		LEAR  	25    	25D         	5170514	CE  										E/E BAY	MALFUNCTIONED   	E				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	23	95CK				2151	248				REPLACED NR 1 COMM ANTENNA WITH NEW UNIT, PN VF10-347, SN 414.  REPAIRED COAX END AT FRAME NR 5 FOR NR 2 COMM AND REPLAC	ED NR 2 COMM WITH SERVICEABLE UNIT MODEL VHF20A, SN 14386.  AIRCRAFT HAD LOST ALL COMMUNICATIONS UNTIL THEY WERE CLOSE T	O THE STATION.  COMM ANTENNA, P/N VJ10-347, S/N 3393.				2	L	7	2 	4J				A10CE   					 
1999062500461	19990625	00461	CE  	1999	6	25	99ZZZX2419       	1	19990113	G	2720	355241448	TUBE            		0024100343  	BEECH 	58    	58          	1152740	CE  										RUDDER PEDAL	CHAFED          	B			EKGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	3267N	239  				TH1767				THERE IS A SCREW HOLE DRILLED OUT IN THE PANEL DIRECTLY ABOVE ROD.  AN INSTALLATION OF A LONG SCREW IN THIS HOLE WILL RE	SULT IN THE SCREW CHAFING THE ROD.  SUBMITTER STATED THIS IS WHAT CAUSED THIS DAMAGE.					1	L	7	2 	3O				3A16    					 
1999062500462	19990625	00462	EU  	1999	6	25	99ZZZX2420       	1	19990526	G	3320	AL5112	POWER SUPPLY    			AMD   	FALCON	FALCON20    	2730103	EU  										CABIN	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	01	712ME				551	355				LEFT SIDE VALANCE LIGHTS INOPERATIVE.  TROUBLESHOT SYSTEM, FOUND LEFT SIDE AFT PROTECTED POWER UNIT AT FAULT.  REMOVED C	OVER FROM POWER UNIT AND FOUND BURNED INSIDE.  THIS UNIT IS MOUNTED IN THE OVERHEAD IN CABIN.					2	L	7	2 	4F			RT	A7EU    					 
1999062500463	19990625	00463		1999	6	25	99ZZZX2421       	4	19990601	G	6122	B41832	FLYWEIGHT       			PIPER 	PA31  	PA31350     	7103110	SO  						HARTZL	HCE3Y	HCE3YR2A    	GL  	GOVERNOR	CRACKED         	B			LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	59905		369  			317652135				PROPELLER GOVERNOR FLYWEIGHT CRACKED.						1	L	7	2 	3O				A20SO   		5	C	P33E	 
1999062500464	19990625	00464	NM  	1999	6	25	99ZZZX2422       	1	19990514	G	2820	25W653120570	LINE            			ISRAEL	1125  	1125        		NM  										FUEL SYSTEM	GOUGED          	B	P		JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	359VS					039				DURING MAINTENANCE ON AIRCRAFT, THE REAR BAGGAGE COMPARTMENT UPHOLSTERY PANELING WAS REMOVED AND A MAIN FUEL LINE PN 25W	653120-570 ON THE RT SIDE WAS DISCOVERED TO HAVE GOUGES IN THE LINE.  THE GOUGES APPEAR TO BE CREATED BY EXCESSIVE LENGT	H OF UPHOLSTERY SCREWS.				2	L	7	2 	4F			RT	A16NM   					 
1999062500465	19990625	00465	NM  	1999	6	25	99ZZZX2423       	1	19990607	G	5711		SPAR            			BOEING	727   	727         		NM  										RT WING	CORRODED        	B	L		OZRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	11	VPCJN					20371				WIDESPREAD LEVEL 3 CORROSION ON THE RT WING REAR SPAR UPPER CHORD AND WEB AT WBL-78.0.						2	L	7	3 	4J			RT						 
1999062500466	19990625	00466	GL  	1999	6	25	99ZZZX2424       	3	19990506	G	6111	A4577	LINK            			MOONEY	M20   	M20R        	5870225	SW  						MCAULY	3A32C	3A32C418G   	GL  	PROPELLER	CRACKED         	B			LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	323DM	114  				290155		971989		PROPELLER LINK CRACKED.						1	L	7	1 	3O			RT	2A3     		5	C	P21E	 
1999070200002	19990702	00002	NE  	1999	7	2	99ZZZX2425       	2	19990528	G	7200		RIVET           								PWA   	JT8   	JT8D219     	52053	NE  					ENGINE	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19							725884			ENGINE REPAIRED AND RETURNED TO SERVICE APPROX 2/3 WEEKS PRIOR TO BEING SENT TO REPAIR STATION FOR TURBINE FAILURE.  DUR	ING INVESTIGATION, DISCOVERED  REPAIR STATION HAD NOTICED LOOSE RIVETS ON ENGINES OF THIS TYPE APPROX 4,000 CYCLES AFTER	 COMPLETION OF P&W SB 6245.  THEY ELECTED TO REPLACE ALL SUBJECT RIVETS WHEN ENGINES HAD OVER 4,000 CYCLES FOR REPAIRS. 	 REPAIR STATION'S ENGINEERING DEPT STATED THERE IS A POSSIBILITY OF RIVETS FAILING DUE TO HEAT OR A POSSIBLE FAILURE OF 	LOCKING CAPABILITY OF THE ANCHOR NUT.							4	F			E9NE				 
1999071400001	19990714	00001	EA  	1999	7	14	99ZZZX2427       	2	19990519	G	7412	10176487121	VIBRATOR        	BENDIX      		MOONEY	M20   	M20F        	5870214	SW  	LYC   	O360  	IO360A1A    	41514	EA  					STARTER	MISMARKED       	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	13	4044N					680164	L470051A			PILOT REPORTED AIRCRAFT HARD TO START.  TROUBLESHOT PROBLEM TO INTERMITTENT STARTING VIBRATOR, TCM SYSTEM SUPPORT MANUAL	 INDICATOR, PN 10-176485-121, TO BE USED WITH S-200 SERIES MAGS.  HOWEVER, WHEN UNIT PULLED FROM STOCK PRINTED ON UNIT I	N 'RED', USE WITH 1200 AND 1400 SERIES MAGNETOS.  THE DEFECTIVE UNIT IS MARKED THE SAME WAY.  TCM CONFIRMED THE DASH 121	 IS CORRECT PN FOR 200 SERIES.  SUBMITTER STATED MARKINGS ARE NOT CORRECT.			1	L	7	1 	3O	3	O		2A3     	1E10				 
1999070200004	19990702	00004	CE  	1999	7	2	99ZZZX2428       	1	19990610	G	2810		FUEL TANK       			CESSNA	172   	172P        	2072436	CE  										WING	CONTAMINATED    	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03	52749					17274599				ACFT  MADE 4 FORCED LANDINGS INCLUDING 1 OFF-AIRPORT, NO DAMAGE.  LANDINGS DUE TO ENG STOPPAGE.  CARB ICE SUSPECTED AS E	NG WOULD FIRE UP ON THE GROUND.  AFTER OFF-AIRPORT LANDING, ACFT TAXIED FOR TAKEOFF WHEN ENG QUIT.  WINGS WERE SUMPED AN	D APPROX 20 OUNCES OF WATER WAS PRESENT.  ACFT FLOWN OUT TO HOME FIELD.  IN HANGAR, DYE WATER  INTRODUCED INTO TOP OF LT	 WING THRU ACCESS PANELS.  14 OUNCES OF WATER WAS PUT INTO TANK WITH ONLY 6 OUNCES DRAINING OUT OF SUMP AFTER ROCKING WI	NGS.  THIS IS A ONE-OWNER ACFT WITH NO REPAIRS MADE TO FUEL BAY AREA.   ACFT HAS BEEN FITTED WITH 4 ADD'L RETROFIT SUMPS	 IN EACH WING.  DURING EXPERIMENT, DRAINED NO WATER FROM ANY OF RETROFIT SUMPS.	1	H	7	1 	3O			NT	3A12    					 
1999070200005	19990702	00005	NE  	1999	7	2	99ZZZX2429       	2	19990501	G	7250	2A2221	TURBINE DISC    			AIRBUS	320   	A320212     		EU  	IAE   	V2500 	V2500A1     		NE  					ENGINE	CRACKED         	B			DQ5Y	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	35					P311AA0125					DURING INSPECTION OF PARTS FOR THIS ENGINE, FOUND THE HPI T/DISC HAD CRACKING FROM ITS AIR METERING HOLES AND BELLING OF	 THE FRONT SECTION.  THESE FEATURES HAVE BEEN CAUSED BY A FIRE WHICH WAS PRESENT IN THE NR 6 BEARING COMPARTMENT.					2	L	7	2 	4F	4	F	RT	A28NM   	E311NE				 
1999070200007	19990702	00007	CE  	1999	7	2	99ZZZX2431       	1	19990602	G	7810	K359500051	EXHAUST PIPE    			BEECH 	36    	A36         	1151604	CE  	CONT  	O550  	IO550B      		SO  					NR 4 CYLINDER	CRACKED         	B			W6NR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	25	903AT	2372 				E2627	296593R			DURING AN ANNUAL INSPECTION, A CRACK WAS FOUND ON THE LEFT OUTBOARD EXHAUST PIPE AT NR 4 CYLINDER.  THE CRACK SEEMS TO B	E ABOUT 1.25 INCHES LONG.  PILOT NOTICED NO ADVERSE EFFECTS.  EXHAUST PIPE WAS REPLACED AND NO OTHER DAMAGE FOUND.					1	L	7	1 	3O	3	O		3A15    	E3SO				 
1999070200008	19990702	00008	CE  	1999	7	2	99ZZZX2432       	1	19990526	G	5510	07326015	FITTING         		123260029   	CESSNA	210   	210M        	2073450	CE  										HORIZ STABILIZER	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	778VK					21062895				DURING ROUTINE PHASE INSPECTION, HEARD SQUEEKING NOISE FROM TAIL.  REMOVED PANELS, INSPECTED, FOUND TWO BRACKETS CRACKED	.  CAUSE UNKNOWN.					1	H	7	1 	3O				3A21    					 
1999070200009	19990702	00009	CE  	1999	7	2	99ZZZX2433       	1	19990526	G	5510	12324001	BRACKET         		123260029   	CESSNA	210   	210M        	2073450	CE  										HORIZ STABILIZER	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	778VK	9536 				21062895				DURING ROUTINE PHASE INSPECTION, HEARD SQUEEKING NOISE FROM TAIL.  REMOVED PANELS, INSPECTED, FOUND TWO BRACKETS CRACKED	.  CAUSE UNKNOWN.					1	H	7	1 	3O				3A21    					 
1999070200010	19990702	00010	EA  	1999	7	2	99ZZZX2434       	2	19990607	G	8530	LW15315	PUSHROD         			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					NR 2 CYLINDER	BROKEN          	B			AIHR	A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			GL	11	5435J		2145 			17273793	RL78576T			AIRCRAFT STARTED RUNNING ROUGH AND LOST POWER.  A LANDING WAS MADE WITH MINOR DAMAGE TO AIRCRAFT (RT WHEEL FAIRING).  UP	ON INSPECTION, FOUND NR 2 CYLINDER EXHAUST PUSHROD BROKEN AND INTAKE PUSHROD BENT.  (PUSHROD TUBES ALSO BENT).  SUBMITTE	R SUSPECTED EXHAUST ROD BREAKING CAUSED INTAKE PUSHROD TO BEND.  SUSPECT MOMENTARY EXHAUST VALVE STICKING CLOSED CAUSED 	ALL OF THIS.  SUBMITTER RECOMMENDED CHECKING/CLEANING EXHAUST VALVE GUIDE PERIODICALLY TO PREVENT THIS.			1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999070200011	19990702	00011	EA  	1999	7	2	99ZZZX2435       	2	19990527	G	8530	STD2090	NUT             			PIPER 	PA28  	PA28161     	7102803	SO  	LYC   	O320  	O320D3G     	41508	EA  					NR 1 CYLINDER	LOOSE           	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	21	108ND	60   				2841328	L1457039A			CYLINDER BASE NUT FOUND IN INNER CYLINDER BAFFLING BETWEEN NR 1 AND NR 3 CYLINDERS ON FIRST INSPECTION SINCE OVERHAUL. R	E-INSTALLED, CHECKED TORQUE ON REMAINING NUTS.  ALL FOUND WITHIN SPECS.					1	L	7	1 	3O	3	O		2A13    	E274				 
1999070200012	19990702	00012	SO  	1999	7	2	99ZZZX2436       	1	19990608	G	3243	M52874140110	LINE            			PIPER 	PA28  	PA28140     	7102802	SO  										RT BRAKE	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	02	6627W	3398 			MFD1264	2820724				DURING GROUND RUN-UP IN PREPARATION FOR AN ANNUAL INSPECTION, THE RIGHT BRAKE LINE BLEW OUT AT THE MASTER CYLINDER CONNE	CTION.  DATE CODE ON HOSE WAS 12-64.					1	L	7	1 	3O				2A13    					 
1999070200013	19990702	00013	SO  	1999	7	2	99ZZZX2437       	2	19990510	G	8520	653052	CAMSHAFT        			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520L      	17032	SO  					ENGINE	CHIPPED         	B			MK5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	23	961CC		1400 			21064620	294754R			DURING A ROUTINE 100-HOUR INSPECTION EXCESSIVE METAL WAS FOUND IN THE ENGINE OIL FILTER.  FURTHER INVESTIGATION REVEALED	 A CHIPPED CAM LOBE AND LIFTER.					1	H	7	1 	3O	3	O		3A21    	E5CE				 
1999070200014	19990702	00014		1999	7	2	99ZZZX2438       	4	19990525	G	6113		SPINNER         			CESSNA	172   	172N        	2072434	CE  										PROPELLER	MISREPAIRED     	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	27	1373E	6133 				17270975				PROPELLER WAS BALANCED PER PUB 1000-OM-01 REV 2.0 ACES SYTEM GUIDE AND INSTEAD OF ADDING WEIGHTS TO RING GEAR, THE WEIGH	TS WERE ADDED TO SPINNER.  SPINNER AND BACKPLATE FAILED DUE TO WEIGHTS ADDED.					1	H	7	1 	3O			NT	3A12    					 
1999070200015	19990702	00015	SO  	1999	7	2	99ZZZX2439       	1	19990316	G	3220	6710700	BRACKET         		6710010     	PIPER 	PA28  	PA28R200    	7102811	SO  										NLG	FAILED          	H	S		GO3S	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	15836					28R7335096				NOSE GEAR WOULD NOT EXTEND OR RETRACT.  (AFTER ACFT MADE A LANDING) THE STEERING ALIGNMENT CAM ASSY WAS FOUND OUTSIDE TO	 THE LEFT OF THE ALIGNER GUIDE BRACKET.  THIS CAUSED THE CAM ASSY TO HIT THE ALIGNER BRACKET EAR AND NOT LET IT FULLY EX	TEND BECAUSE THE NOSE TIRE WAS NOT STRAIGHT, IT WOULD NOT FULLY RETRACT INTO THE COWLING.  THIS CAUSED THE WHOLE ALIGNER	 GUIDE BRACKET ASSY TO BEND DOWN UNTIL THE LOWER PART OF THE ALIGNER BRACKET TRACK HITS THE TRUNNION HOUSING.  THIS LETS	 THE ALIGNMENT CAM ASSY OUT OF ITS TRACK WHEN THE GEAR IS FULLY RETRACTED.		1	L	7	1 	3O				2A13    					 
1999070200016	19990702	00016	SO  	1999	7	2	99ZZZX2440       	2	19990610	G	8530		BUSHING         			CESSNA	210   	T210N       	2073456	CE  	CONT  	O520  	TSIO520R    	17040	SO  					CONNECTING ROD	MISINSTALLED    	B			WTXR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	07	5360U		1569 			21064878	522557			WHEN NR 2 CYLINDER WAS REMOVED FOR REPAIR, NOTED THE CONNECTING ROD BUSHING HAD BEEN PUSHED OUT OF THE CONNECTING ROD FO	R A DISTANCE OF ABOUT .1250 INCH.  FURTHER EXAMINATION OF THE ENGINE REVEALED 2 MORE BUSHINGS THAT HAD BEEN SIMILARLY DI	SPLACED.  CLOSER EXAMINATION OF THE BUSHING REVEALED NO OBVIOUS REASON FOR ITS CONDITION BEYOND IMPROPER INSTALLATION OF	 THE PISTON PIN AT THE LAST CYLINDER REMOVAL AND RE-INSTALLING.  THE ENGINE HAD BEEN 'TOP OVERHAULED' AT 1,208 HOURS SIN	CE MAJOR OVERHAUL.  IT HAD BEEN OPERATED FOR 360.9 HOURS IN THIS CONDITION.		1	H	7	1 	3O	3	O		3A21    	E8CE				 
1999070200017	19990702	00017	NE  	1999	7	2	99ZZZX2441       	1	19990501	G	5302		SKIN            			SKRSKY	S76   	S76A        	8143006	NE  										TAIL BOOM	CORRODED        	B		A	H09R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	31211					760225				CORROSION.  SEVERE EXFOLIATION BETWEEN STA 250 - STA 300 AND STA 300 - STA 336, WITH ADDITIONAL CORROSION AT TAILBOOM, V	ERTICAL FIN ATTACHMENT.  CORROSION AREAS ARE BETWEEN ENGINE LONGERONS AND OUTER SKIN PANELS IN NEARLY INACCESSIBLE AREAS	.				1	G	7	2 	3U				H1NE    					 
1999071400002	19990714	00002	NE  	1999	7	14	99ZZZX2442       	1	19990501	G	5330		SKIN            			SKRSKY	S76   	S76A        	8143006	NE  										BS 300-336	CORRODED        	B		A	H09R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	917QS					76217				CORROSION REPAIRS.  SEVERE CORROSION FOUND BETWEEN UPPER ENGINE LONGERONS LEFT AND RIGHT, AND OUTER SKIN PANELS IN AN IN	ACCESSIBLE AREA.  STA 250 THROUGH STA 300.  CORROSION FOUND IN TAILBOOM STA 300 THROUGH STA 336 AND IN THE AREA WHERE VE	RTICAL FIN ATTACHES TO TAILBOOM.  SUBMITTER STATED BESIDES THE TWO THIS REPAIR STATION HAS REPAIRED, TWO OTHER SIMILAR 7	6'S ARE KNOWN TO HAVE THE SAME CORROSION.			1	G	7	2 	3U				H1NE    					 
1999070200018	19990702	00018	SW  	1999	7	2	99ZZZX2443       	1	19990512	G	5302	206033004143	SKIN            			BELL  	206   	206L3       	1182108	SW  										TAILBOOM	CRACKED         	B	S	A	H09R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09					51383					AD 99-02-01.  HORIZONTAL STABILIZER OPEN, LEFT SIDE HAS .75 INCH CRACK.						1	G	7	1 	3U				H2SW    					 
1999070200019	19990702	00019	SW  	1999	7	2	99ZZZX2444       	1	19990125	G	5302	206033004177	SKIN            			BELL  	206   	206L4       	1182110	SW  										TAILBOOM	CRACKED         	B	S	A	H09R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09					52120					AD 99-02-01.  HORIZONTAL STABILIZER OPENING, LEFT SIDE, HAS CRACK TO SEAM.						1	G	7	1 	3U			NC	H2SW    					 
1999070200020	19990702	00020	CE  	1999	7	2	99ZZZX2445       	1	19990607	G	3010		LINE            			BEECH 	95    	95B55       	1152729	CE  										RT WING	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	690DP	3368 				TC2347				RIGHT WING BOOT DE-ICE LINE RUBBED/MELTED THROUGH BECAUSE OF CONTACT WITH PNEUMATIC OUTPUT LINE FROM RIGHT ENGINE PUMP. 	 VERY DIFFICULT TO INSPECT.					1	L	7	2 	3O			RT	3A16    					 
1999070200021	19990702	00021	SO  	1999	7	2	99ZZZX2446       	1	19990518	G	5102		GORE TAPE       			BALWKS	FIREFY	FIREFLY10   	1050300	SO  										ENVELOPE	MISMANUFACTURED 	B			QLFR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	25	3288N	298  				F10025				REPAIRS WERE DONE ON 28 OUT OF 36 GORES DUE TO GORE TAPE ABRASION DAMAGE.  FABRIC DAMAGE IS CAUSED BY GORE TAPE THAT IS 	STIFF AND SHARP CAUSING PREMATURE FABRIC WEAR AND DEGRADATION.  GORE TAPE MATERIAL SHOULD BE CHANGED AS TO NOT WEAR THRO	UGH ADJACENT PANELS.				1	B	0	0 				NC	A14SO   					 
1999070200022	19990702	00022	CE  	1999	7	2	99ZZZX2447       	1	19990616	G	5711	951100224	SPAR            			BEECH 	55    	E55         	1152732	CE  										RT WING	CORRODED        	B			ERYR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	11	1619W	4137 				TE869				FOUND AFT UPPER SPAR CAP ON RIGHT WING TO BE EXFOLIATED AND CORRODED AT WS 70.340.  AFFECTED AREA IS APPROXIMATELY 6-8 I	NCHES IN LENGTH.  OUTBOARD END OF CORRODED AREA SEVERELY BLISTERED AND DISINTEGRATED THROUGH ENTIRE THICKNESS OF SPAR CA	P EXTRUSION.				1	L	7	2 	3O				3A16    					 
1999070200067	19990702	00067	SO  	1999	7	2	99ZZZX2452       	1	19990607	G	5751	12017933002	WEIGHT          		12008080002 	EMB   	120   	EMB120RT    		SO  										RT AILERON	CORRODED        	B	P		GOGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	11	454UE	17216				120155				DURING EXPORT CERTIFICATE OF AIRWORTHINESS COMPLIANCE, THE IMPORT COUNTRY REQUIRED C/W BRAZILIAN AD NR 98-01-02, DATED 1	-15-98.  INSPECTION OF THE AILERON MASS BALANCE WEIGHTS FOUND ALL WEIGHTS BROKEN AND CORRODED.  TWO OTHER EMB-120RT AIRC	RAFT WERE INSPECTED FOR SAFETY CONCERN, BOTH AIRCRAFT HAD ALL WEIGHTS CORRODED AND FOUR OF THE SIX WEIGHTS ON EACH AIRCR	AFT WERE BROKEN.  FOLLOWING ACFT S/N'S AND AILERON S/N'S WERE FOUND DEFECTIVE:  EMB-120RT, SN 120046, LT AILERON, SN 120	054, AND, RT AILERON, SN 120054.  EMB-120RT, SN 120045, LT AILERON, SN 120056, AND, RT AILERON, SN 120056.		2	L	7	2 	4T			RT	A31SO   					 
1999070200068	19990702	00068	NM  	1999	7	2	99ZZZX2453       	1	19990607	G	5313		STRINGER        			BOEING	727   	727256      		NM  										BS 360	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON STR 28R AND STR 28L AT STA 360.						2	L	7	3 	4F				A3WE    					 
1999070200069	19990702	00069	NM  	1999	7	2	99ZZZX2454       	1	19990607	G	5311		FRAME           			BOEING	727   	727256      		NM  										BS 380	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION NOTED ON FRAME AT STA 380 BETWEEN STR 28L AND STR 28R.						2	L	7	3 	4F				A3WE    					 
1999070200070	19990702	00070	NM  	1999	7	2	99ZZZX2455       	1	19990501	G	5311		FRAME           			BOEING	727   	727256      		NM  										BS 740	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AROUND AFT ADF LOOP ANTENNA FS 740 - BL ZERO.						2	L	7	3 	4F				A3WE    					 
1999070200071	19990702	00071	NM  	1999	7	2	99ZZZX2456       	1	19990501	G	5245	65261069	ROD ARM         			BOEING	727   	727256      		NM  										AC BAY	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON AC BAY  MECHANISMS.						2	L	7	3 	4F				A3WE    					 
1999070200072	19990702	00072	NM  	1999	7	2	99ZZZX2457       	1	19990501	G	5245	652610610	ROD ARM         			BOEING	727   	727256      		NM  										AC BAY	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON AC BAY EXTERNAL GROUND CONNECTION DOOR AND MECHANISMS.						2	L	7	3 	4F				A3WE    					 
1999070200073	19990702	00073	NM  	1999	7	2	99ZZZX2458       	1	19990501	G	5245	652555739	ROD ARM         			BOEING	727   	727256      		NM  										AC BAY	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON AC BAY EXTERNAL GROUND CONNECTION DOOR AND MECHANISMS.						2	L	7	3 	4F				A3WE    					 
1999070200074	19990702	00074	NM  	1999	7	2	99ZZZX2459       	1	19990501	G	5250	65183964	DOOR            			BOEING	727   	727251      	138408H	NM  										AFT LAVATORY	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON AFT LAVATORY SERVICE DOOR.						2	L	7	3 	4F				A3WE    					 
1999070200079	19990702	00079	CE  	1999	7	2	99ZZZX2463       	1	19990611	G	7921	10046A	OIL COOLER      	NIAGARA     		BEECH 	60    	B60         	1153605	CE  										OIL SYSTEM	LEAKING         	B			RF3R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	23					F88554496					PART FAILED DURING NORMAL SERVICE.  PART HAD PREVIOUSLY BEEN REPAIRED USING EPOXY.  THE EPOXY FAILED ALLOWING THE COOLER	 TO BEGIN LEAKING AT POINT OF ORIGINAL REPAIR.  RECOMMEND ELIMINATING USE OF EPOXY ON OIL COOLERS AS EPOXY FAILURE IS CO	MMON.				1	L	7	2 	3O				A12CE   					 
1999070200080	19990702	00080	SO  	1999	7	2	99ZZZX2464       	1	19990607	G	5751	23017933001	WEIGHT          		12008080001 	EMB   	120   	EMB120RT    		SO  										LT AILERON	CORRODED        	B	P		GOGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	11	454UE	17216			120056	120155				DURING EXPORT CERTIFICATE OF AIRWORTHINESS COMPLIANCE, THE IMPORT COUNTRY REQUIRED C/W BRAZILIAN AD NR 98-01-02, DATED 1	-15-98.  INSPECTION OF THE AILERON MASS BALANCE WEIGHTS FOUND ALL WEIGHTS BROKEN AND CORRODED.  TWO OTHER EMB-120RT AIRC	RAFT WERE INSPECTED FOR SAFETY CONCERN, BOTH AIRCRAFT HAD ALL WEIGHTS CORRODED AND FOUR OF THE SIX WEIGHTS ON EACH AIRCR	AFT WERE BROKEN.  THE FOLLOWING AIRCRAFT AND AILERON SERIAL NUMBERS WERE FOUND DEFECTIVE:  EMB-120RT, SN 120046, LT AILE	RON, SN 120054; RT AILERON, SN 120054.  EMB-120RT, SN 120045, LT AILERON, SN 120056; RT AILERON, SN 120056.		2	L	7	2 	4T			RT	A31SO   					 
1999070200265	19990702	00265	GL  	1999	7	2	99ZZZX2470       	3	19990528	G	6111		BLADE           			GULSTM	500   	500RKWELL   	0141102	SW  						HARTZL	HCA2	HCA2MVK2    	GL  	PROPELLER	DAMAGED         	B	P		LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	3824C		280  			697		H1393		ROLLED AREA OF SHANK OF BLADE HAS DAMAGE APPROXIMATELY .003 INCHES IN DEPTH.  APPEARS TO BE CAUSED BY CLAMP NOT MATCHING	 THE RADIUS OF THE BLADE.  CLAMP IS ALSO SHOTPEENED IN THIS AREA RESULTING IN A SHOTPEENED SURFACE IN CONTACT WITH THE R	OLLED AREA OF THE BLADE.				1	H	7	2 	3O				6A1     		5	C	P24EA	 
1999070200266	19990702	00266	SO  	1999	7	2	99ZZZX2471       	2	19990607	G	8520		COUNTERWEIGHT   			CESSNA	182   	182P        	2075816	CE  	CONT  	O550  	IO550F      	17042	SO  					CRANKSHAFT	LOOSE           	B			VH3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	7435Q	169  				18261075	284892R			DURING START-UP OF THE ENGINE, THE NR 1 CYLINDER TRAILING COUNTER WEIGHT ON THE CRANKSHAFT CAME LOOSE FROM CRANKSHAFT AN	D MADE A HOLE IN THE TOP OF THE CASE.  CSB99-3A HAD BEEN COMPLETED 1.7 HOURS PRIOR.  REASON FOR FAILURE UNKNOWN AT THIS 	TIME.				1	H	7	1 	3O	3	O	NT	TA13    	E3SO				 
1999070200267	19990702	00267		1999	7	2	99ZZZX2472       	4	19990614	G	3416	202	ENCODER         		202         	AMTR  		HARMONRCKTII												ALTIMETER	MALFUNCTIONED   	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	10	76HR				E755	74				ATC REPORTED ENCODER WAS INACCURATE.  REMOVED ENCODER AND SENT TO MANUFACTURER FOR REPAIRS.  RECEIVED, RE-INSTALLED, AND	 PERFORMED CORRELATION TEST IAW FAR 91:413.  ENCODER IS NOW REPORTING PROPERLY.								0 										 
1999070200268	19990702	00268		1999	7	2	99ZZZX2473       	1	19990612	G	2435	30E0221G	STARTER         	BENDIX      																STARTER/GEN	MISOVERHAULED   	B	P		MU4R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	19					1577					THE EQUIPMENT HAS BEEN HEAVILY DAMAGED DURING TEST PERFORMED IAW RELEVANT CMM.  AFTER 5 MINUTES OPERATION:   SHAFT BLOCK	ED.   INTERNAL PARTS APPEAR DESTROYED.																		 
1999070200269	19990702	00269		1999	7	2	99ZZZX2474       	1	19990501	G	2460	MS27497T	CONNECTOR       	BENDIX      																E/E BAY	MISMANUFACTURED 	B	P		RO3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03					12F35C					CONNECTOR PIN NUMBER REFERENCE ON FRONT OF CONNECTOR IS OPPOSITE OF PIN NUMBER REFERENCE ON REAR OF CONNECTOR.  FOUND PR	OBLEM WHILE CONDUCTING CONTINUITY CHECK OF WIRING HARNESS AND VISUAL INSPECTION.																		 
1999070200270	19990702	00270	EU  	1999	7	2	99ZZZX2475       	1	19990605	G	2810	PC01786	HOSE            			RHNFLU	EXT300	EA300L      	70218DG	EU  										FUEL TANK	LEAKING         	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	3FD					017				FUEL HOSE CONNECTS FUSELAGE FILLER NECK WITH MAIN FUSELAGE TANK.  HOSE SEPARATED FROM TOP OF TANK AT RANGE AND ALLOWED F	UEL TO ENTER COCKPIT.  HOSE WAS FOUND CUT TOO SHORT FROM FACTORY ALLOWING ENOUGH CLEARANCE AT TOP FOR IT TO BACK OFF OF 	TANK FLANGE.  FLEXING OF SKIN OF AIRCRAFT CONTRIBUTED TO THE PROBLEM.				1	M	7	1 	3O			NC	EA67U   					 
1999070200271	19990702	00271	SO  	1999	7	2	99ZZZX2476       	1	19990616	G	5710		STRUCTURE       			PIPER 	PA46  	PA46350P    		SO  										LT/RT WING	DAMAGED         	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	03	9255B	514  				4622197				AIRCRAFT ENCOUNTERED CLEAR AIR TURBULENCE AT 17,500 FEET WHICH CAUSED THE LEFT AND RIGHT INBOARD WING STRUCTURE TO BUCKL	E.					1	L	7	1 	3O			RT	A25SO   					 
1999070200272	19990702	00272	SO  	1999	7	2	99ZZZX2477       	1	19990528	G	3230	585220	SPRING          			PIPER 	PA46  	PA46310P    	7104605	SO  										NLG	WEAK            	B		A	EIPR	O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			WP	07	4391E	2236 				468508054				NOSE GEAR EMERGENCY EXTENSION SPRING UNABLE TO EXTEND NOSE GEAR AND LOCK IN-FLIGHT.  AFTER LANDING AND ROLL-OUT ON MAINS	 HOLDING NOSE OFF, NOSE GEAR LOCKED AT 30 KNOTS AIRSPEED.  NEW PART WAS 2 INCHES LONGER THAN OLD PART.  SUBMITTER RECOMM	ENDED TIME-LIFE CYCLE REPLACEMENT SCHEDULE.				1	L	7	1 	3O			RT	A25SO   					 
1999070200273	19990702	00273	SO  	1999	7	2	99ZZZX2478       	2	19990610	G	8540	632018	DRIVE GEAR      			CESSNA	340   	340A        	2076405	CE  	CONT  	O520  	TSIO520NB   	17040	SO  					ENGINE	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	01	340BA		123  		633620	340A0283	519790			DURING ROUTINE MAINTENANCE, A METALLIC CLUNK WAS DETECTED WHILE ROCKING THE PROPELLER.  FURTHER INVESTIATION REQUIRED RE	MOVAL OF THE ALTERNATOR.  NOISE DID NOT EXIT WITH ALTERNATOR REMOVED.  VISUAL INSPECTION OF THE RING GEAR ON THE CRANKSH	AFT SHOWED IRREGULAR WEAR PATTERN.  BACKLASH CHECK OF GEAR SHOWED .038 INCH BACKLASH.  TCM MAXIMUM SERVICEABLE LIMIT, 15	.012 INCH.			1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999070200331	19990702	00331	NM  	1999	7	2	99ZZZX2479       	1	19990607	G	2913	62983	PUMP            	VICKERS     		BOEING	727   	727251      	138408H	NM  										HYDRAULIC SYSTEM	FAILED          	H				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	99	109KM				MX289126G	21155				B-SYSTEM FAILURE WITH FLUID LOSS.  REPLACED NR 1 AND NR 2 B-SYSTEM HYDRAULIC PUMPS.  REPLACED NR 2 OUTPUT PRESSURE LINE.	  ACTT:  55,812.2 HOURS.  ACTC:  39,060.					2	L	7	3 	4F				A3WE    					 
1999070200332	19990702	00332	SW  	1999	7	2	99ZZZX2480       	1	19990617	G	3230	ED12758	CLEVIS          		210015      	GULSTM	690TP 	690C        	7630517	SW  										LT MLG	FAILED          	G	S			O				OTHER                   				O			OTHER                     			LD	LANDING        	1			EA	21	840V	2755 				11727				THE LEFT MAIN LANDING GEAR INBOARD RETRACT CYLINDER CLEVIS BROKE CAUSING THE LEFT MAIN GEAR TO COLLAPSE ON LANDING.  THE	 LEFT GEAR INBOARD EXTENSION/RETRACTION ACTUATOR IS CONNECTED TO THIS RETRACT CYLINDER CLEVIS.  THIS IS THE PHYSICAL CON	NECTION BETWEEN THE ACTUATOR AND THE STRUT TO EXTEND AND RETRACT THE LANDING GEAR.  THIS FORKED CLEVIS IS ATTACHED TO TH	E ACTUATOR AND IS INSERTED 2.250 INCHES INTO THE MAIN LANDING GEAR STRUT.  THE FRACTURE OF THIS CLEVIS STARTS .3750 INCH	 FROM THE BOTTOM OF THE SHAFT, IS PERPENDICULAR TO THE SHAFT COVERING 60 PERCENT OF THE CIRCUMFERENCE.  A SEPARATE FRACT	URE ORIGINATES FROM THIS FRACTURE UP DIAGONALLY .25 INCH FROM THE BOTTOM OF THE SHAFT CREATING A FLARED LIP.	1	H	7	2 	3T				2A4     					 
1999070200333	19990702	00333	NM  	1999	7	2	99ZZZX2481       	1	19990605	G	2913	40183	PUMP            			ISRAEL	1125  	1125        		NM  										LT ENGINE	LEAKING         	B			QRRR	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			EA	13	125AJ				CT26A	031				PUMP IS LEAKING FROM SHAFT SEAL.  UNIT LEAKS IN ANY CONDITION.  REPLACED UNIT WITH REPAIRED ONE.						2	L	7	2 	4F			RT	A16NM   					 
1999070200334	19990702	00334	NM  	1999	7	2	99ZZZX2482       	1	19990607	G	2910	3070C1S58D	COUPLING        			BOEING	727   	72761       	1384017	NM  										HYDRAULIC SYSTEM	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	530KF					19176				B-SYSTEM LOST HYDRAULIC FLUID AFTER LANDING.  FIELD TEMP REPAIR PERFORMED.  AIRCRAFT RETURNED TO HOME BASE WHERE NR 2 B-	PUMP PRESSURE LINE AND QUICK DISCONNECT FITTINGS WERE REPLACED.  ACTT:  34,099.3 HOURS.  ACTC:  72,838.					2	L	7	3 	4F				A3WE    					 
1999070200335	19990702	00335	EU  	1999	7	2	99ZZZX2483       	1	19990512	G	3213	AIR400390	GLAND SEAL      		AIR864101   	SAAB  	SF340 	340B        	7860101	EU  										NLG	FAILED          	B			FW1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	03			3190 		LK9700670					PREMATURE FAILURE OF GLAND SEAL UNIT HAD 3,789 CYCLES OF 24,000 CYCLE OVERHAUL.  MEASURED SURFACE FINISH OF RAMROD ACCEP	TABLE.  CSN:  3,789.					2	L	7	2 	4T			RT	A52EU   					 
1999070200336	19990702	00336	NM  	1999	7	2	99ZZZX2484       	1	19990501	G	5697	AMP36154	WIRE            			BOEING	727   	72761       	1384017	NM  										WINDSCREEN	SHORTED         	C				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	530KF					19176				DURING TEST FLIGHT FOLLOWING C-CHECK AND REMOVAL AND RE-INSTALLATION OF THE COCKPIT WINDOWS, THE CAPTAIN'S L-1 WINDOW PO	WER WIRE CAUGHT FIRE IN THE UPPER LEFT CORNER OF WINDSHIELD.  AFTER THE POWER AND CIRCUIT BREAKERS WERE PULLED, THE FLAM	ES QUICKLY SUBSIDED.  INSPECTION FOUND THE HEAT POWER TERMINAL INSULATION BOOT OUT OF PLACE AND THE TERMINAL SHORTED TO 	THE WASHER ON WINDOW RETAINING BOLT.  SUBMITTER RECOMMENDED CLOSE INSPECTION OF THIS AREA FOLLOWING WINDOW INSTALLATION.			2	L	7	3 	4F			 	A3WE    					 
1999070200337	19990702	00337	NM  	1999	7	2	99ZZZX2485       	1	19990617	G	2910		LINE            			BOEING	727   	72761       	1384017	NM  										HYDRAULIC SYSTEM	FAILED          	H	P			A				UNSCHED LANDING         				K	J		FLUID LOSS                	WARNING INDICATION        		CR	CRUISE         	1			SW	15	530KF					19176				DURING ROUTINE FLIGHT, FLIGHT CREW DISCOVERED LOSS OF HYDRAULIC FLUID, DECLARED EMERGENCY TO DIVERT TO OKC, LANDED WITHO	UT INCIDENT.  ACFT TOWED FROM RUNWAY AND PARKED IN HANGAR.   MAINTENANCE DISCOVERED THE RETURN HYD LINE FROM NR 2 SPOILE	R ACTUATOR (PN 6517840-118) HAD FRACTURED JUST BEHIND THE B-NUT AT THE ACTUATOR.  CLOSER INSPECTION DISCOVERED CHANNEL S	UPPORT (PN 65-21658-26) AT WS 521.53 FOR THE LOWER WING FAIRING CRACKED COMPLETELY AWAY FROM THE SUPPORT ROD.  ALSO, THE	 CHANNEL WAS MISSING THE PORTION WHICH THE CLAMP WAS MOUNTED THAT SECURES THE LOWER HYD LINE ASSY JUST OTBD OF T-FITTING	, DOWN-STREAM OF FRACTURED LINE.  INBD CHANNEL (PN 65-21658-27) FOUND CRACKED AROUND ROD SUPPORT ATTACH POINT.	2	L	7	3 	4F				A3WE    					 
1999070200338	19990702	00338	SO  	1999	7	2	99ZZZX2486       	1	19990528	G	7810		FLANGE          			PIPER 	PA18  	PA18180     	7101880	SO  										EXHAUST STACK	BROKEN          	G				O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			GL	03	32506					287505066				A LOUD KNOCKING SOUND EMANATED FROM THE ENGINE COMPARTMENT.  SHORTLY AFTER, ENGINE BEGAN TO EXPERIENCE SEVERE VIBRATION 	AND LOSS OF POWER.  THE RAM DROPPED TO 1,100 DEGREES, OIL AND FUEL PRESSURE REMAINED NORMAL.  BUT AIRCRAFT CONTINUED TO 	LOSE POWER AND ALITITUDE.  THE INSPECTION OF THE ENGINE REVEALED NR 3 EXHAUST STACK MOUNTING FLANGE AND SEVERAL STUDS WE	RE BROKEN.  EACH CYLINDER HAD NORMAL COMPRESSION AND THE ENGINE OIL SHOWED OBVIOUS SIGNS OF METALIC PARTICLES.			1	H	7	1 	3O				1A2     					 
1999070200339	19990702	00339		1999	7	2	99ZZZX2487       	4	19990530	G	3446	WX950	STORMSCOPE      	BFGOODRICH  		PIPER 	PA30  	PA30        	7103002	SO  										COCKPIT	RAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	09	8041Y	1    			JCP04902093	301151				ON FIRST START-UP, DISPLAY WAS NOT CLEAR.  WOULD NOT CHANGE FROM STRIKE MODE TO CELL MODE.  COMPLETE FAILURE IN LESS THA	N ONE HOUR'S TIME SINCE NEW.					1	L	7	2 	3O				A1EA    					 
1999070200340	19990702	00340	CE  	1999	7	2	99ZZZX2488       	1	19990624	G	3411		VALVE           			LEAR  	24    	24B         	5170306	CE  										STATIC SYSTEM	WRONG PART      	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	254JT					181				WHILE TROUBLESHOOTING PILOT'S SIDE STATIC SYSTEM FOR LEAKS, FOUND THE ALTERNATE STATIC SOURCE CONTROL VALVE WAS NOT THE 	PROPER LEARJET VALVE.  THE VALVE THAT WAS INSTALLED WAS A HARDWARE STORE VARIETY NATURAL GAS VALVE.  IT WAS FOUND THAT T	HIS VALVE LEAKED.  IT IS UNKNOWN WHY THIS VALVE WAS INSTALLED.  THE VALVE WAS REPLACED WITH THE CORRECT PART.				2	L	7	2 	4J				A10CE   					 
1999070200341	19990702	00341	WP  	1999	7	2	99ZZZX2489       	1	19990611	G	3244	72391451	TIRE            			DOUG  	DC10  	DC1030      	3023501	WP  										NLG	DAMAGED         	B			QBFR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	540AX				JUL76617	46595				WHEEL AND TIRE ASSEMBLY WAS RECEIVED AT REPAIR STATION NR QBFR289K ON 6-7-99.  UPON RECEIVING INSPECTION, NOTED THE TIRE	 ASSEMBLY RECEIVED TIRE DAMAGE WHILE INSTALLED ON THE AFFECTED AIRCRAFT.  THE DESCRIPTION OF THE DAMAGE FOUND WAS AS FOL	LOWS:  .1250 INCH DEPTH BY .1250 INCH WIDTH CUT WHICH COVERED THE ENTIRE CIRCUMFERENCE OF THE TIRE SIDEWALL AND TIRE RET	READ CAP MATING AREA.			2	L	7	3 	4F				A22WE   					 
1999070200342	19990702	00342	SW  	1999	7	2	99ZZZX2490       	1	19990610	G	6210	2120155015	BLADE           		2020155010  	BELL  	212   	212         	1181420	SW  										MAIN ROTOR	DISBONDED       	B			GURR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	9937K	1622 			A1137	30778				DURING DAILY INSPECTION, FOUND VOID AT UPPER AND LOWER SECTION OF TRIM TAB TRAILING EDGE.  AIRCRAFT TT:  4,967.8 HOURS. 	 M/R BLADE REMOVED AND SENT FOR REPAIR.					1	G	7	1 	4U				H4SW    					 
1999070200343	19990702	00343	SW  	1999	7	2	99ZZZX2491       	1	19990529	G	6210	2120155015	BLADE           			BELL  	212   	212         	1181420	SW  										MAIN ROTOR	DISBONDED       	B			GURR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	9937K	1298 			A262	30778				AIRCRAFT HAD VERTICAL VIBRATION ON SHORT FINAL TO LAND.  INSPECTED AIRCRAFT, FOUND LOWER TRIM TAB HAD DISBONDED ON M/R B	LADE PN 212-015-501-5, SN A262.  AFTER CLOSER INSPECTION, FOUND CORROSION UNDER TAB.  REMOVED M/R HUB AND BOTH M/R BLADE	S FOR CONVENIENCE.  INSTALLED SERVICEABLE M/R HUB AND BLADES.  COMPLETED GROUND RUN AND OPERATIONAL FLIGHT CHECK.  AIRCR	AFT RETURNED TO SERVICE.  AIRCRAF TT:  4,949.3 HOURS.			1	G	7	1 	4U				H4SW    					 
1999070200344	19990702	00344	SW  	1999	7	2	99ZZZX2492       	1	19990610	G	3212	412220116	SKID TUBE       			BELL  	204   	UH1H        	1181407	SW  										RT SKID	DENTED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	51AG					7120178				SKID TUBE DENTED.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999070200345	19990702	00345	SW  	1999	7	2	99ZZZX2493       	1	19990610	G	3212	412320115	SKID TUBE       			BELL  	204   	UH1H        	1181407	SW  										LT SKID	DENTED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	51AG					7120178				SKID TUBE DENTED.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999070200346	19990702	00346	GL  	1999	7	2	99ZZZX2494       	2	19990617	G	7230	6898607	BEARING         			BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					COMPRESSOR	FAILED          	B			C68R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	07	288JB				HAN1705	51288	CAE895354			DURING FLIGHT, THE 'ENGINE CHIP LIGHT' WARNING LIGHT ILLUMINATED.  DURING A 30-MINUTE GROUND RUN FOR TROUBLESHOOTING THE	 CHIP LIGHT AGAIN ILLUMINATED.  THE ENGINE WAS DISASSEMBLED AND THE NR 1 BEARING WAS FOUND TO HAVE FAILED CAUSING IMPELL	ER TO CONTACT THE SHROUD.  STRESS LOADING ON THIS BEARING UNDER NORMAL OPERATIONS COMBINED WTIH HEAT CYCLING CAUSES IT T	O FAIL.			1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999070200347	19990702	00347		1999	7	2	99ZZZX2495       	4	19990610	G	2312	KY196	TRANSCEIVER     			BELL  	206   	206B        	1181511	SW  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BX		529  		4168	2872				HAS NO TRANSMISSION OR SIDE TONE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999070200348	19990702	00348	SW  	1999	7	2	99ZZZX2496       	1	19990610	G	7722	12444412	INDICATOR       			BELL  	206   	206B        	1181511	SW  										TOT	FLUCTUATES      	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BX		140  		1403C	2872				TOT GAUGE FLUCTUATES.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999070200349	19990702	00349		1999	7	2	99ZZZX2497       	4	19990610	G	2312	KY196	TRANSCEIVER     			BELL  	204   	UH1H        	1181407	SW  										COCKPIT	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	51AG				8373	7120178				TRANSCEIVER WOULD NOT TRANSMIT.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999070200573	19990702	00573		1999	7	2	99ZZZX2499       	4	19990610	G	2340	18486G01	INTERPHONE      			HUGHES	369   	369D        	4470706	WP  										COCKPIT	MALFUNCTIONED   	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	369AW		57   		0887009	470117D				PILOT REPORTED INTERCOM, TRANSMITTED SCRATCHY.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999070200574	19990702	00574	NM  	1999	7	2	99ZZZX2500       	1	19990607	G	5510	65245712	BEAM            			BOEING	727   	727256      		NM  										HORIZ STABILIZER	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON RIGHT HORIZONTAL STABILIZER UPPER TIE BEAM (APROX STA 118).						2	L	7	3 	4F				A3WE    					 
1999070200575	19990702	00575	EU  	1999	7	2	99ZZZX2501       	1	19990512	G	3230	AIR130232	CYLINDER        			SAAB  	SF340 	340B        	7860101	EU  										MLG	CRACKED         	B			FW1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	369PX				QE987	340B295				SURFACE CRACK 1 INCH LONG BY .010 INCH WIDE DETECTED BY FLUORESCENT PENETRANT INSPECTION DURING NORMAL OVERHAUL CYCLE. C	SN:  13,573.					2	L	7	2 	4T			RT	A52EU   					 
1999070200576	19990702	00576	NM  	1999	7	2	99ZZZX2502       	1	19990617	G	7110	65825633	RING            		65196854539 	BOEING	727   	7272J0      	138407E	NM  	PWA   	JT8   	JT8D15A     	52051	NE  					COWL	CRACKED         	B			EB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	281KH				3090	21105	P708904B			PRIOR TO B-CHECK, ENGINE RUN, MECHANIC NOTICED SMALL PIECE OF METAL MISSING FROM NR 1 ENGINE NOSE COWL ASSEMBLY  MOUNT R	ING AT LOWER MOUNT BOLT.  UPON FURTHER INSPECTION, MOUNT RING WAS FOUND CRACKED OUT AROUND 10 OF 23 MOUNT BOLTS.  REMOVE	D NOSE COWL ASSY.  INSPECTED ENGINE, NO DEFECTS NOTED.  INSTALLED SERVICEABLE NOSE COWL ASSY.  RAN ENGINE, OPS AND LEAK 	CHECKS OK.  NOTIFIED AIRCRAFT OWNER/OPERATOR AND STC HOLDER FOR STAGE 3 NOSE COWL ASSY.			2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
1999070200577	19990702	00577		1999	7	2	99ZZZX2503       	1	19990423	G	6520	350A33215300	HINGE           																	T/R GEARBOX	CRACKED         	B			FF6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11		267  								RUBBER BLOCK IS CRACKED AND DISTORTED.																			 
1999070900001	19990709	00001	SO  	1999	7	9	99ZZZX2506       	1	19990617	G	2820	1621100	GASCOLATOR BOWL 			PIPER 	PA23  	PA23        	7102302	SO  										FUEL SYSTEM	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	08	64M					23534				CORROSION AT THE  BOTTOM OF GASCOLATOR BOWL.						1	L	7	2 	3O				1A10    					 
1999070900003	19990709	00003	GL  	1999	7	9	99ZZZX2508       	3	19990614	G	6114	D7292C201	HUB             			CESSNA	182   	182         	2072702	CE  						MCAULY	2A34C	2A34C201    	GL  	PROPELLER	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07								747273		SUBMITTER STATED PART SHOULD HAVE BEEN REJECTED AT OVERHAUL FOR CORROSION CAUSING METAL TO FLAKE OFF THE EXTERIOR HUB SE	RVICES.					1	H	7	1 	3O			NT	3A13    		5	C	P3EA	 
1999070900004	19990709	00004	CE  	1999	7	9	99ZZZX2509       	1	19990525	G	2720	03101965	SPRING          			CESSNA	172   	172R        	2072401	CE  										RUDDER	BROKEN          	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	03	392ES	804  				17280132				PILOT REPORTED RUDDER ALWAYS GOES TO RIGHT ON GROUND.  CABLES SLACK.  FOUND LEFT RUDDER RETURN SPRING BROKEN AT ONE END 	OTHER SIDE ALMOST BENT STRAIGHT.  REPLACED WITH NEW PART AND OPS CHECKED OK.					1	H	7	1 	3O			NT	3A12    					 
1999070900005	19990709	00005	GL  	1999	7	9	99ZZZX2510       	1	19990523	G	3250		BOLT            			AMTR  	SKYBLT	SKYBOLT     		GL  										TAILWHEEL ASSY	SHEARED         	G				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			WP	07	76GD					7476				ATTACHMENT BOLT SHEARED ON TAILWHEEL ASSEMBLY CAUSING PILOT TO LOSE STEERING WHILE TAXIING.  TAILWHEEL ASSY FAILED AND R	UDDER STRUCK PAVEMENT.					1	Q	7	1 	3O				EXPA1Q71					 
1999070900006	19990709	00006	CE  	1999	7	9	99ZZZX2511       	1	19990608	G	2421		HOUSING         	FORD        	C6115010102 	CESSNA	182   	182A        	2072704	CE  										ALERNATOR MOUNT	HOLE ELONGATED  	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	17	5129D	1027 				51229				BOLT HOLE ELONGATED ON DRIVE-END OF FRAME, CESSNA KIT, AK210-54D.  BOLT WAS NOT TIGHTENED ENOUGH AND ALLOWED MOVEMENT OF	 DRIVE-END FRAME.  ENGINE VIBRATION CAUSED FRAME TO MOVE AND ELONGATE HOLE BY .1250 INCH  PLUS.  DRIVE-END FRAME WAS WOR	N AWAY WEAKENING FRAME THAT SECURED ALTERNATOR TO MOUNTING BRACKET.				1	H	7	1 	3O			NT	3A13    					 
1999070900009	19990709	00009	WP  	1999	7	9	99ZZZX2514       	2	19990601	G	7321	89711014	FUEL CONTROL    			CESSNA	441   	441         	2076020	CE  	GARRTT	TPE331	TPE3318     	01514	WP  					RT ENGINE	MALFUNCTIONED   	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	4415A	5533 				4410172	31684			MANUAL MODE SOLENOID VALVE FAILED CAUSING AN UNCOMMANDED FUEL FLOW INCREASE TO THE RIGHT ENGINE.  THE RESULTANT TORQUE I	NCREASE CAUSED THE AIRCRAFT TO VEER SLIGHTLY.					1	L	7	2 	3T	4	T	RT	A28CE   	E4WE				 
1999070900010	19990709	00010	WP  	1999	7	9	99ZZZX2515       	2	19990611	G	7321	1390136	DIAPHRAGM       	WOODWARD    							GARRTT	TPE331	TPE331*     	01514	WP  					FCU	DEFECTIVE       	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	05		31   								FUEL CONTROL UNIT RETURNED WITH COMPLAINT OF 'LACK OF POWER LEVER RESPONSE AT ALTITUDE'.  AS RECEIVED, REVEALED HOLE INS	IDE OF DIAPHRAGM.  CAUSE UNKNOWN.										3	T			E2WE				 
1999070900012	19990709	00012	NE  	1999	7	9	99ZZZX2517       	2	19990615	G	7230	2A0851	SEAL            								IAE   	V2500 	V2500A1     		NE  					NR 4 BEARING	CRACKED         	B			KB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03					0079		0079			PART RECEIVED FROM WESTFIELD GAGE CO., INC., FOR FLUORESCENT PENETRANT INSPECTION PER SECTION 70-23-01, INSPECTION CHECK	-01, TASK 70-23-01-230-501, IAW INTERNATIONAL AERO ENGINE V2500 PROPULSION SYSTEM ENGINE MANUAL.  PART REJECTED AT FPI D	UE TO CRACK 9.0360 INCH, 1 PLACE ON TOP SURFACE (2ND TIME REJECTED).									4	F			E311NE				 
1999070900013	19990709	00013	NE  	1999	7	9	99ZZZX2518       	2	19990325	G	7210	7895781	TAB WASHER      		5074T51G10  	SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					GEARBOX	BROKEN          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		14790			IHI00034		GEE785328			DURING DISASSEMBLY OF GEARCASE, RIGHT IDLER FORWARD TAB WASHER WAS FOUND BROKEN.  OIL PUMP HOUSING HAS SOME DAMAGE.  HSS	 SO NR 251671 SO.  CUST:  SIMMONS A/L.  (X)					2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999070900014	19990709	00014	NE  	1999	7	9	99ZZZX2519       	2	19990325	G	7210	7757652	BEARING         		5074T51G10  	SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					GEARBOX	BROKEN          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		1891 			TB00499		GEE785757			DURING DISASSEMBLY OF GEARBOX, SLIDER BLOCK BEARING AND RIGHT IDLER FORWARD TAB WASHER WERE FOUND BROKEN WHICH CAUSED DA	MAGE TO BULKHEAD.  HSS SO NR 251975 SO.  CUST:  MESABA A/L.					2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999070900016	19990709	00016	CE  	1999	7	9	99ZZZX2520       	1	19990601	G	2497	P83A2	WIRE            			BEECH 	90    	B90         	1152912	CE  										COCKPIT	FAILED          	B		A	AZWR	K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			SO	01	901WL	10007				LJ410				AFTER RUNNING THE AIR CONDITIONER DURING A PHSE INSPECTION, SMOKE WAS SEEN AND AND ODOR WAS DETECTED IN THE COCKPIT.  FO	UND WIRE PB3A2 SMOULDERING UNDER THE CENTER PEDESTAL AT THE ISOLATION LIMITER BUS.  WIRES P83A2 AND P83B2 ARE ALUMINUM W	IRES RUNNING FROM THE STARTER RELAY BUS IN THE RIGHT WING TO THE ISOLATION LIMITERS IN THE COCKPIT.  THEY PROVIDE POWER 	TO THE ENTIRE AIRCRAFT EXCEPT FOR THE EMERGENCY BUS AND ARE UNPROTECTED WIRES.  THE ALUMINUM WIRING HAS CORRODED AND OVE	RHEATED, AND FAILED OVER TIME. WHILE REMOVING WIRE P83A2, FOR REPLACEMENT WIRE P83B2, IT SIMPLY SNAPPED AT THE STARTER R	ELAY.  WIRE WAS SEVERELY CORRODED AND THE INSULATION ALSO SHOWED OVERHEATING.	1	L	7	2 	3T			 	3A20    					 
1999070900017	19990709	00017	CE  	1999	7	9	99ZZZX2521       	1	19990602	G	2730	25CP221527	CONTROL CABLE   			RAYTHN	DH125 	HAWKER800XP 	7150012	CE  										ELEVATOR	MISMANUFACTURED 	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	1102U					258343				UPON COMPLIANCE OF INSPECTION, ELEVATOR CABLES WERE FOUND DAMAGED IN THE SAME AREA ON ALL FOUR AIRCRAFT.  THIS CABLE DAM	AGE APPEARED TO BE INCORRECT MANUFACTURING OR MISHANDLING OF CABLES.  CABLE SEGMENT AFT OF CABLE REINFORCEMENT APPEARS T	O BE UNRAVELING.				2	L	7	2 	4F			RT	A3EU    					 
1999070900018	19990709	00018	CE  	1999	7	9	99ZZZX2522       	1	19990602	G	2730	25CP221527	CONTROL CABLE   			RAYTHN	DH125 	HAWKER800XP 	7150012	CE  										ELEVATOR	MISMANUFACTURED 	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	23207					258350				UPON COMPLIANCE OF INSPECTION, ELEVATOR CABLES WERE FOUND DAMAGED IN THE SAME AREA ON ALL FOUR AIRCRAFT.  THIS CABLE DAM	AGE APPEARED TO BE INCORRECT MANUFACTURING OR MISHANDLING OF CABLES.  CABLE SEGMENT AFT OF CABLE REINFORCEMENT APPEARS T	O BE UNRAVELING.				2	L	7	2 	4F			RT	A3EU    					 
1999070900019	19990709	00019	CE  	1999	7	9	99ZZZX2523       	1	19990602	G	2730	25CP221527	CONTROL CABLE   			RAYTHN	DH125 	HAWKER800XP 	7150012	CE  										ELEVATOR	MISMANUFACTURED 	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	23204					258346				UPON COMPLIANCE OF INSPECTION, ELEVATOR CABLES WERE FOUND DAMAGED IN THE SAME AREA ON ALL FOUR AIRCRAFT.  THIS CABLE DAM	AGE APPEARED TO BE INCORRECT MANUFACTURING OR MISHANDLING OF CABLES.  CABLE SEGMENT AFT OF CABLE REINFORCEMENT APPEARS T	O BE UNRAVELING.				2	L	7	2 	4F			RT	A3EU    					 
1999070900020	19990709	00020	CE  	1999	7	9	99ZZZX2524       	1	19990302	G	2730	25CP221527	CONTROL CABLE   			RAYTHN	DH125 	HAWKER800XP 	7150012	CE  										ELEVATOR	MISMANUFACTURED 	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	2321V					258353				UPON COMPLIANCE OF INSPECTION, ELEVATOR CABLES WERE FOUND DAMAGED IN THE SAME AREA ON ALL FOUR AIRCRAFT.  THIS CABLE DAM	AGE APPEARED TO BE INCORRECT MANUFACTURING OR MISHANDLING OF CABLES.  CABLE SEGMENT AFT OF CABLE REINFORCEMENT APPEARS T	O BE UNRAVELING.				2	L	7	2 	4F			RT	A3EU    					 
1999072000001	19990720	00001	SO  	1999	7	20	99ZZZX2525       	1	19990607	G	2710		CABLES          			MAULE 	MX7   	MX7180A     	5460185	SO  										AILERON	CHAFED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	1055Z					21050C				WHILE PERFORMING A UNIFORMITY INSPECTION. FAA INSPECTORS DISCOVERED THE LT AND RT LOWER AILERON CABLES FRAYED WHERE THEY	 EXIT THE LOWER WING SKIN AT THE FAIRLEAD, APROXIMATELY 4 INCHES FROM THE THIMBLE EYE SPLICE.  FAA INSPECTORS DISCOVERED	 THE LT AND RT LOWER AILERON CABLES FRAYED WHERE THEY EXIT THE LOWER WING SKIN AT THE FAIRLEAD, APPROX 6 INCHES FROM THE	 THIMBLE EYE SPLICE.  APPEARED RT CABLE WORE THROUGH FAIRLEAD THEN BEGAN CHAFING ON THE WING SKIN ITSELF.  CAUSE OF LT C	ABLE FRAY IS UNDETERMINED, BUT IT APPEARS INSPECTION COVER ADJACENT TO FAIRLEAD CAN BE POSITIONED CAUSING CABLE TO 'RIDE	 HARD' AGAINST ONE EDGE OF THE FAIRLEAD.  ACFT AND PART TT:  88 HOURS.	1	H	7	1 	3O			NC	3A23    					 
1999070900021	19990709	00021		1999	7	9	99ZZZX2526       	1	19990426	G	2810	CCA1550	FUEL DRAIN      	CURTIS      																FUEL TANK	FAILED          	H	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09										AFTER INSTALLING NEW FUEL DRAIN, WAS UNABLE TO OPEN DRAIN.  THE SHAFT IN AREA JUST BELOW SEALS SEEMS TO BIND ON HOUSING.	  THIS IS EVIDENT BY USING A MAGNIFYING GLASS AND LOOKING AT THIS AREA.  THIS IS THE NEWER VALVE (WITH THE HEAVIER HEAD 	ABOVE THE SEAL.																	 
1999070900022	19990709	00022	CE  	1999	7	9	99ZZZX2527       	1	19990531	G	3230	03411091	SPRING          			CESSNA	195   	195B        	2073112	CE  										LT MLG	FAILED          	G		A		O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			SW	09	2151C					16136				UPON LANDING ROLL-OUT, AIRCRAFT SLOWED TO APPROXIMATELY 20 KNOTS.  THE LEFT MAIN GEAR SEPARATED THE AIRCRAFT.  THREE PAS	SENGERS ON BOARD THE AIRCRAFT STATED THE LANDING WAS VERY SMOOTH.  POST-ACCIDENT INVESTIGATION REVEALED WHAT COULD HAVE 	BEEN A SMALL FRACTURE IN THE LEFT MAIN GEAR SPRING WHERE IT ATTACHES TO THE AIRCRAFT.				1	H	7	1 	3R				A790    					 
1999070900023	19990709	00023	SO  	1999	7	9	99ZZZX2528       	1	19990601	G	3230	WTC22151	UPLOCK ACTUATOR 			PIPER 	PA42  	PA42720     	7104212	SO  										NLG	MISMANUFACTURED 	B	P			K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	21	9142B					425501038				EMERGENCY UPLOCK RELEASE ACTUATOR, PN WTC 2215-1, WAS ORIGINALLY REPLACED BECAUSE OF LEAK (HYD) AT ROD END.  WHEN 'NEW' 	PART WAS INSTALLED (SAME P/N), IT LEAKED FROM END CAP.  AFTER THIS, TWO OTHER ACTUATORS WERE TRIED WITH SAME RESULTS. TH	EY LEAKED WHILE PERFORMING MAIN/NOSE LANDING GEAR OPERATIONAL CHECKS.  PIPER P/N 551 968.  S/N'S AFFECTED:  WTC1072; WTC	1190; WTC1202; WTC1268; WTC1317; WTC1338.			1	L	7	2 	4T				A23SO   					 
1999070900024	19990709	00024	CE  	1999	7	9	99ZZZX2529       	1	19990310	G	2721	NAS56138	ROLL PIN        			CESSNA	208   	208B        	2073701	CE  										COCKPIT	LOOSE           	D		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	750PA	1284 				208B0628				ROLL PIN SECURING AILERON TRIM CHAIN SPROCKET TO AILERON TRIM WHEEL ASSY WORKED OUT OF SHAFT RENDERING AILERON TRIM INOP	ERABLE.  RE-INSTLALED ROLL PIN (ITEM 14 IN CESSNA 208 IPC CHAPTER 27-10-03 FIG 02).  SAFETY WIRED ROLL PIN WITH .020 INC	H SAFETY WIRE (ITEM 14) AND SAFETIED REMAINING ROLL PINS IN ASSY ITEMS 2, 12 (ITEM 12 IN TWO AREAS) TO PREVENT RECURRENC	E.			1	H	7	1 	3T				A37CE   					 
1999070900025	19990709	00025	SW  	1999	7	9	99ZZZX2530       	1	19990526	G	7110	206064819006	DOOR            			BELL  	407   	407         		SW  										INTAKE COWL	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03		1907 								DURING ROUTINE INSPECTION FOUND INTERGRANULAR CORROSION.						1	G	7	1 	3U			O	H2SW    					 
1999070900026	19990709	00026	NE  	1999	7	9	99ZZZX2531       	1	19990524	G	6210	7615009043050	TIP CAP         			SKRSKY	S76   	S76A        	8143006	NE  										M/R BLADE	MISINSTALLED    	B			ALGR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	S76A				A1750550					WHILE ATTEMPTING TO INSTALL TIP CAP ONTO MAIN ROTOR BLADE, DISCOVERED INSUFFICIENT CLEARANCE BETWEEN INNER DOUBLERS - WI	LL NOT FIT FORWARD END OF TIP PLATE.  COMPONENT P/N 76150-09100-952.					1	G	7	2 	3U				H1NE    					 
1999070900027	19990709	00027	GL  	1999	7	9	99ZZZX2532       	2	19990526	G	7230	230397911	SPLINE ADAPTER  		6890550     						ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	MISMANUFACTURED 	B			ALGR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03					69697					WHILE PERFORMING TOLERANCE INSPECTION PER OHM, FOUND INTERNAL SPLINES MANUFACTURED OVER LIMITS.											3	U			E4CE				 
1999070900515	19990709	00515	SW  	1999	7	9	99ZZZX2534       	1	19990526	G	6210	206015001107	BLADE           			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1075W	3297 			A2114	45377				DURING DAILY INSPECTION, FOUND TRAILING EDGE EXTRUSION WITH HEAVY INTERGRANULAR CORROSION, POSSIBLY CAUSED BY IMPROPERLY	 HEAT TREATED MATERIAL.					1	G	7	1 	3U				H2SW    					 
1999070900516	19990709	00516	NE  	1999	7	9	99ZZZX2535       	1	19990521	G	3220		LANDING GEAR    	BFGOODRICH  	1944E100A   	SKRSKY	S76   	S76         	8143010	NE  										NOSE	MALFUNCTIONED   	B			ALGR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	705AL				R7032	760267				DURING APPROACH, GEAR HANDLE WAS LOWER.  NOSE GEAR DID NOT EXTEND.						1	G	7	2 	3U				H1NE    					 
1999070900518	19990709	00518	EA  	1999	7	9	99ZZZX2538       	1	19990621	G	5610	6003303025	WINDSHIELD      			CNDAIR	CL600 	CL6002B16   	1900305	EA  										COCKPIT	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	05	43R	773  			2061	5334				SUBMITTER STATED WINDSHIELDS ARE HIGH FAILURE ITEMS.  CHANGED ANOTHER LEFT WINDSHIELD AT 1,100 TSN ON ANOTHER CHALLENGER	.  THIS ONE WAS CRACKED FROM BOTTOM TO TOP.  OTHER WINDSHIELD WAS CHANGED FOR 'NO HEAT' FAILURE.					2	L	7	2 	4F			RT	A21EA   					 
1999070900519	19990709	00519	CE  	1999	7	9	99ZZZX2539       	1	19990618	G	3520	C3512000	OXYGEN MASKS    	PURITANBENET		LEAR  	55    	55LEAR      	5170702	CE  										CABIN	FAILED          	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	273MC					119				INSPECTED CABIN OXYGEN MASKS IN C/W AD 99-08-21.  FOUND FIVE CABINS OXYGEN MASKS WITH CURE DATES FROM 1983 TO 1991 TO BE	 TORN.  AD 99-08-21 REFERS TO OXYGEN MASKS WITH CURE DATES FROM SEPTEMBER, 1993 TO MARCH, 1997.  THIS AD SHOULD REQUIRE 	THAT ALL OXYGEN MASKS BE INSPECTED FOR THIS DEFECT.				2	L	7	2 	4F				A10CE   					 
1999070900520	19990709	00520	SW  	1999	7	9	99ZZZX2540       	1	19990612	G	3230		VALVE           			GULSTM	500   	500S        	0141107	SW  										COCKPIT	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	03	33PG					17325				AFTER GEAR WAS RAISED, ON THE NEXT GEAR EXTENSION, THE VALVE MALFUNCTIONED AND GEAR DID NOT EXTEND.  REFERENCE ACCIDENT 	NR NYC99LA139.  PART S/N 12-6-84-407-14A 3126-1.					1	H	7	2 	3O				6A1     					 
1999070900521	19990709	00521	SO  	1999	7	9	99ZZZX2541       	2	19990620	G	8530		HEAD            			CESSNA	185   	A185F       	2072821	CE  	CONT  	O520  	IO520D      	17032	SO  					ENGINE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	4949E	1755 	55   		52785	18503917	572508H			CRACK DEVELOPED FROM SPARK PLUG HOLE TOWARD INTAKE VALVE.  COMPRESSION CHECK WAS GOOD BECAUSE CRACK WAS ABOVE COMBUSTION	 CHAMBER.					1	H	7	1 	3O	3	O		3A24    	E5CE				 
1999070900522	19990709	00522		1999	7	9	99ZZZX2542       	1	19990622	G	3350	AD4002P	BATTERY         	GRIMES      	60030451    															CABIN	MISMANUFACTURED 	B			JGVR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CE	09										FAA-PMA REPLACEMENT CELL IS PHYSICALLY SHORTER THAN ORIGINAL COMPONENT MANUFACTURER'S CELL.  (ORIGINAL CELL, P/N 41B004A	D07G3).  IN ADDITION, THE POSITIVE (TIP) TERMINAL IS OF LARGER DIAMETER THAN ORIGINAL COMPONENT MANUFACTURER'S BATTERY C	ELL.  THESE 2 DISCREPANCIES COMBINE TO CREATE A LOSS OF BATTERY OUTPUT CAUSED BY LACK OF PROPER CONTACT WITH EMERGENCY P	OWER SUPPLY BATTERY TERMINALS.  DEFECT FOUND AT TIME OF INSTALLATION OF REPLACEMENT CELLS.																 
1999070900523	19990709	00523	SO  	1999	7	9	99ZZZX2543       	1	19990608	G	3230	400692	CLEVIS BOLT     		9532900     	PIPER 	PA34  	PA34200     	7103405	SO  										NLG	BENT            	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	16	1519T	67   				347250337				THE HOSE GEAR FAILED DUE TO EXCESS PLAY IN OVERCENTER LINKAGE.  THE EXCESS PLAY WAS FROM A BENT CLEVIS BOLT WHICH INSTAL	LS THROUGH THE DOWNLOCK LINK ASSY AND THE OVERCENTER LINKAGE.  SUBMITTER STATED THE CLEVIS BOLT WAS MOST LIKELY BENT DUE	 TO A HARD LANDING WHICH WAS NOT REPORTED.				1	L	7	2 	3O				A7SO    					 
1999072000004	19990720	00004		1999	7	20	99ZZZX2545       	4	19990622	G	6113		BULKHEAD        			MAULE 	MX7   	MX7180A     	5460185	SO  										SPINNER	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	10421	100  				21017C				WHILE C/W A100-HOUR INSPECTION, THE SPINNER BULKHEAD WAS FOUND CRACKED AT ALL THE ATTACH BOLT HOLES.						1	H	7	1 	3O			NC	3A23    					 
1999070900525	19990709	00525	NE  	1999	7	9	99ZZZX2546       	1	19990622	G	7160		AIR BOX         			CONAER	LA4   	LA4200      	5110310	NE  										AIR INTAKE	CRACKED         	B	L		AW4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	11	2573P					872				PILOT REPORTED THAT WiTH FULL THROTTLE AND THE WASTEGATE CLOSED, ENGINE HAD EXCESSIVELY LOW BOOST.  (TURBO CHARGER INSTA	LLATION WAS AN AFTERMARKET INSTALLATION.  ALSO, RECORDS WERE UNAVAILABLE AS OF THIS DATE TO DETERMINE AIRCRAFT TIMES, TU	RBO CHARGER STC, ETC).				1	H	7	1 	3O				1A13    					 
1999070900526	19990709	00526	EA  	1999	7	9	99ZZZX2547       	2	19990618	G	7414	M3333	IMPULSE COUPLING	SLICK       	6351        	PIPER 	PA32  	PA32300     	7103212	SO  	LYC   	O540  	IO540K1A5   	41532	EA  					MAGNETO	CRACKED         	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	8908N	370  			98051437	3240695	L1417048A			WHILE CONDUCTING THE INSPECTION REQUIRED BY AD 99-04-04, CRACKS WERE DISCOVERED ON THE PAWL PLATE OF THE IMPULSE COUPLIN	G.  THE CRACKS WERE DIFFICULT TO SEE SINCE THE AREA IS HIDDEN BY THE PAWLS.  THE PAWL SPRINGS MUST BE REMOVED FROM THE S	PRING HOLES SO THE PAWL CAN BE ROTATED OUT OF THE WAY.				1	L	7	1 	3O	3	O		A3SO    	1E4				 
1999070900527	19990709	00527	GL  	1999	7	9	99ZZZX2548       	1	19990612	G	3213	670003	STRUT           	AIRIGHT     		AMTR  	300   	SX300       	05675EK	GL  										LT MLG	FRACTURED       	G				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			NM	11	120J	900  			153	60				AFTER LANDING AND DURING TAXI, 'LEFT TURN', THE LEFT MAIN GEAR COLLAPSED.  A SUBSEQUENT INSPECTION REVEALED THE STRUT'S 	OUTER LEFT TRUNNION FLANGE HAD CRACKED AND BROKE FREE FROM ITS ATTACHMENT BOLT.  THIS ACTION ALLOWED THE STRUT TO ROTATE	 FORWARD 'CLOCKWISE'.  WITH THIS ROTATION, THE ACTUATOR RAM THREADED ROD END BENT, THEN SNAPPED FREE FROM THE SELF-ALIGN	ING ANTI-FRICTION ROD END ASSY.  THE STRUT CONTINUED FORWARD AND IMPACTED THE FUSELAGE CAUSING DAMAGE.  THIS PILOT ADMIT	S TO MAKING THREE HARD LANDINGS WITHIN THE LAST THREE YEARS WHICH INCLUDED 50-KNOT CROSSWINDS IN MINUS 15 DEGREES FAHREN	HEIT TEMPS.	1	L	7	1 	3O			RT	EXPA1L71					 
1999070900530	19990709	00530	CE  	1999	7	9	99ZZZX2551       	1	19990618	G	3520		OXYGEN MASK     			CESSNA	650   	650         	2076802	CE  										CABIN	MISINSTALLED    	B			CWQR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	05	794QS	131  				6507094				DURING INSPECTION OF PASSENGER OXYGEN MASKS FOR AD 99-08-21, FOUND 2 SCOTT PASSENGER OXYGEN MASKS IN A PURITAN BENNETT C	ONTAINER ASSY.  CE650 IPC STATES PURITAN BENNETT MASK ASSEMBLIES ARE TO BE USED ONLY WITH PURITAN BENNETT CONTAINER ASSE	MBLY.				2	L	7	2 	4F				A9NM    					 
1999070900531	19990709	00531	CE  	1999	7	9	99ZZZX2552       	1	19990618	G	3520	17408005	OXYGEN MASK     			CESSNA	650   	650         	2076802	CE  										CABIN	DEFECTIVE       	B			CWQR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05	794QS	131  				6507094				INSPECTED AIRCRAFT FOR COMPLIANCE OF AD 99-08-21 PURITAN BENNETT PASSENGER OXYGEN MASKS.  OXYGEN MASK INSTALLED IN AIRCR	AFT WERE NOT FULLED LISTED.					2	L	7	2 	4F				A9NM    					 
1999070900532	19990709	00532	SW  	1999	7	9	99ZZZX2553       	1	19990621	G	6730	206076062107	ACTUATOR        			BELL  	407   	407         		SW  										SERVO PILOT WALL	FAILED          	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	407SD	10   				53330				ACTUATOR REPLACED WITH NEW FROM BELL HELICOPTER .						1	G	7	1 	3U			O	H2SW    					 
1999070900533	19990709	00533	NM  	1999	7	9	99ZZZX2554       	1	19990616	G	2710	69356881	RETAINER        		65447619    	BOEING	737   	737*        		NM  										AILERON	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					2641					UNIT RECEIVED WITH A BLOWN OUT FILTER CAP THAT APPARENTLY HAPPENED DURING FLIGHT.  P/N 69-36588-1 IS MADE OF ALUMINUM AL	LOY.  REPLACED FILTER CAP WITH P/N 69-35688-2 WHICH IS MADE OF FERROUS MATERIAL.					2	L	7	2 	4F			RT	A16WE   					 
1999070900534	19990709	00534	NM  	1999	7	9	99ZZZX2555       	1	19990617	G	3240	51161	PLUG            	PNEUDRAULICS	5059        	BOEING	737   	737*        		NM  										MLG	BROKEN          	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					3802					PLUG IS BROKEN BETWEEN THE TOP OF THE THREADS AND THE GRIP.  MADE OF ALUMINUM ALLOY.  REPLACED WITH STEEL PLUG.						2	L	7	2 	4F			RT	A16WE   					 
1999070900535	19990709	00535	SW  	1999	7	9	99ZZZX2556       	1	19990622	G	6220	222010415113	BEAM            			BELL  	222   	222B        	1182124	SW  										M/R HUB	DAMAGED         	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	4343H	2323 			EA144	47143				WALKING BEAM REPLACED WITH NEW FROM BELL HELICOPTER.						1	G	7	2 	3U				H9SW    					 
1999070900536	19990709	00536	SW  	1999	7	9	99ZZZX2557       	1	19990622	G	7714	407375008101	INDICATOR       			BELL  	407   	407         		SW  										DUAL TACHOMETER	FAILED          	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	407SD	10   			0408	53330				DUAL TACHOMETER REPLACED WITH NEW FROM BELL HELICOPTER.						1	G	7	1 	3U			O	H2SW    					 
1999070900537	19990709	00537	SW  	1999	7	9	99ZZZX2558       	1	19990610	G	2435	23032027	STARTER         			BELL  	206   	206B        	1181511	SW  										START/GENERATOR	FAILED          	B			EOPR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	01	27574	3004 				2562				SUSPECT BEARING FAILURE.  STARTER MAKES UNUSUAL NOISE AND WILL NOT SPIN ENGINE FAST ENOUGH TO START.  BEARINGS WERE REPL	ACED 611.9 HOURS PREVIOUSLY AT OVERHAUL.					1	G	7	1 	3U				H2SW    					 
1999070900538	19990709	00538	EU  	1999	7	9	99ZZZX2559       	1	19990503	G	2841		INDICATOR       			BOLKMS	BK117 	BK117C1     	5626025	EU  										FUEL QUANTITY	MALFUNCTIONED   	B			TI1R	A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			SW	05	317MC					7505				SHORTLY AFTER LEVEL-OFF, PILOT NOTICED 140 GALLONS IN MAIN FUEL TANK INDICATION.  SUDDENLY, DROPPED TO 40 GALLONS, THEN 	DECREASED TO ZERO INDICATION.  DISCUSSED SITUATION WITH CREW.  RETURNED TO HOME BASE WITH TECHNICIAN STANDING BY.  REFER	RED TO MEL FOR REJECT, BUT NO REJECT ON PROBLEMS FOR FUEL QUANTITY INDICATOR.				1	G	7	2 	3U			NC	H13EU   					 
1999070900539	19990709	00539	NE  	1999	7	9	99ZZZX2560       	2	19990520	G	7530		ACTUATOR        			BOLKMS	117   	BK117A3     	5626015	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					NR 2 ENGINE	MALFUNCTIONED   	B			TI1R	A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			SW	05	1140H					7078				WHILE AT CRUISE FLIGHT DURING A HOSPITAL TRANSPORT WITH A PATIENT ON BOARD, N1 INCREASED TO 102.5 DEGREES AT 60 PERCENT.	  TOT ALSO INCREASED APPROXIMATELY 70 PERCENT TO 680 DEGREES.  REDUCED POWER TO  MAINTAIN N1 LESS THAN 102 PERCENT.  NOT	IFIED THE CREW OF THE PROBLEM AND THAT WE WERE DIVERTING TO AN AIRPORT AND CORRDINATE FOR PATIENT TRANSPORT BY ANOTHER C	OMPANY HELICOPTER UPON ARRIVAL AT THE AIRPORT.  PERFORMED A SHALLOW APPROACH TO A RUNWAY LANDING WITHOUT ANOTHER INCIDEN	T.		1	G	7	2 	3U	3	U		H13EU   	E5NE				 
1999071600001	19990716	00001	NE  	1999	7	16	99ZZZX2561       	2	19990603	G	8530	M8324811904	O-RING          		430109902   	BOLKMS	117   	BK117A3     	5626015	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					T1 SENSOR	LEAKING         	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	911MZ	569  			16485	7098	45032			TROUBLESHOT SYSTEM PER ENGINE MM.  FOUND AIR LEAK ON TEMP COMPENSATOR.  REMOVED 5 O-RINGS, PN M8324811-904.  INSTALLED 5	 NEW O-RINGS, P/N SAME.  PERFORMED 7 GROUND RUNS ON NR 1 ENGINE.  PERFORMED MAXIMUM CONTINUOUS OE 1 ON NR 1 ENGINE.  TOP	PED NR 1 PER ACFT TECH REP.  ALL TEST RUNS AND FLIGHTS PERFORMED WITH NO DEFECTS NOTED.				1	G	7	2 	3U	3	U		H13EU   	E5NE				 
1999071600002	19990716	00002		1999	7	16	99ZZZX2562       	4	19990519	G	6113	10073805	BULKHEAD        			PIPER 	PA34  	PA34220T    	7103420	SO  										SPINNER	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	77FT	288  				3449018				CRACKS AT EACH MOUNTING BOLT HOLE (DOESN'T HAVE ANY DYNAMIC BALANCING WEIGHTS ATTACHED TO BULKHEAD).  SUBMITTER STATED N	EEDS RE-DESIGN TO HEAVIER METAL OR DOUBLER.					1	L	7	2 	3O				A7SO    					 
1999071600003	19990716	00003		1999	7	16	99ZZZX2563       	4	19990519	G	6113	10073805	BULKHEAD        			PIPER 	PA34  	PA34220T    	7103420	SO  										SPINNER	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	77FT	104  				3449018				CRACKS AT EACH MOUNTING BOLT HOLE (DOESN'T HAVE ANY DYNAMIC BALANCING WEIGHTS ATTACHED TO BULKHEAD).   SUBMITTER STATED 	NEEDS RE-DESIGN TO THICKER METAL OR DOUBLER.					1	L	7	2 	3O				A7SO    					 
1999071600004	19990716	00004	CE  	1999	7	16	99ZZZX2564       	1	19990519	G	3233	12801204	ACTUATOR        			CESSNA	210   	T210N       	2073456	CE  										MLG	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	4620Y	4451 			4204	21063960				DOWNLOCK ACTUATORS COULD NOT BE RIGGED TO SPECS.  DURING ANNUAL INSPECTION CHECK, FOUND ROD STICKEY.  SENT IN FOR OVERHA	UL.  FOUND INTERNAL PN 1280246-1 CRACKED AND PN 1280120-3 WITH DEEP SCRATCH.  UNIT CONSIDERED B.E.R. (17 YRS OLD).  REPL	ACED WITH OVERHAULED EXCHANGE UNIT.  SUBMITTER SUGGESTED PART SHOULD HAVE LIFE-LIMIT OVERHAUL TIME.				1	H	7	1 	3O				3A21    					 
1999071600005	19990716	00005	CE  	1999	7	16	99ZZZX2565       	1	19990519	G	3233	12801204	ACTUATOR        			CESSNA	210   	T210N       	2073456	CE  										MLG	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	4620Y	4451 			4208	21063960				DOWNLOCK ACTUATORS COULD NOT BE RIGGED TO SPECS.  DURING ANNUAL INSPECTION CHECK, FOUND ROD STICKING.  SENT IN FOR OVERH	AUL.  FOUND INTERNAL GUIDE DAMAGED, P/N 9851048-2. INSTALLED AFTER OVERHAUL (17 YRS OLD).  SUBMITTER SUGGESTED PART SHOU	LD HAVE LIFE-LIMIT OVERHAUL TIME.				1	H	7	1 	3O				3A21    					 
1999071600006	19990716	00006	CE  	1999	7	16	99ZZZX2566       	1	19990625	G	5310	05530313	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										FUSELAGE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	2745M	293  				17280586				C/W CESSNA SB 98-53-02.  FOUND FIREWALL CRACKED AT LOWER COWLING MOUNT BRACKET ADJACENT TO BATTERY BOX.  CRACK EXTENDED 	THROUGH INNER BRACKET RIVET HOLES APPROXIMATELY 1 INCH TO 2 INCHES IN LENGTH.  ALSO, FOUND LOWER COWL SHOCK MOUNTS, P/N 	J7444-36 TORN.  SUBMITTER STATED THIS AIRCRAFT SERIAL NUMBER DOES NOT FALL IN THE EFFECTIVITY RANGE OF THE SERVICE BULLE	TIN STATED ABOVE.			1	H	7	1 	3O			NT	3A12    					 
1999071600007	19990716	00007	CE  	1999	7	16	99ZZZX2567       	1	19990625	G	5310	0553031	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										FUSELAGE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	4118A	298  				17280629				C/W CESSNA SB 98-53-02.  FOUND FIREWALL CRACKED AT LOWER COWLING MOUNT BRACKET ADJACENT TO BATTERY BOX.  CRACK EXTENDED 	THROUGH INNER BRACKET RIVET HOLES APPROXIMATELY 2.75 INCHES IN LENGTH.  ALSO, FOUND LOWER COWL SHOCK MOUNTS, P/N J7444-3	6, TORN.  SUBMITTER STATED THIS AIRCRAFT SERIAL NUMBER DOES NOT FALL IN THE EFFECTIVITY RANGE OF THE SERVICE BULLETIN ST	ATED ABOVE.			1	H	7	1 	3O			NT	3A12    					 
1999071600009	19990716	00009	SO  	1999	7	16	99ZZZX2569       	1	19990608	G	5712		RIB             		5200004502  	GULSTM	AA5   	AA5A        	3960106	SO  										WS 66	BUCKLED         	B			AW4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	11	26076	4247 				AA5A0415				UPON OPENING LT WING FUEL TANK ACCESS PANELS FOR SEALANT INSPECTION, FOUND AFT PORTION OF THE WING RIB AT WS 66 BUCKLED.	  OWNER ADVISED THE PREVIOUS OWNER OF THE ACFT HAD TOLD HIM AT ONE TIME, UNKNOWN TO THE PILOT, THE LT FUEL TANK VENT HAD	 BECOME PLUGGED WITH AN INSECT NEST.  DURING FLIGHT, THE PILOT NOTED THE SKIN ON THE FUEL TANK OF THE LT FUEL TANK WAS D	ISTORTED.  AFTER LANDING, THE NEST WAS DISCOVERED AND CLEANED OUT.  APPARENTLY NO FURTHER CHECK FOR INTERIOR DAMAGE WAS 	CONDUCTED.  IT APPEARS THE ACFT HAS BEEN FLYING AROUND FOR AT LEAST 6-7 YEARS WITH THIS DAMAGED RIB.		1	L	7	1 	3O				A16EA   					 
1999071600010	19990716	00010		1999	7	16	99ZZZX2570       	4	19990625	G	3416	5934P3	ALTIMETER       			CESSNA	172   	172R        	2072401	CE  										COCKPIT	FAILED          	B			DVPR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03	2272H	10   			396337	17280688				ALTIMETER MANUFACTURED BY UNITED INSTRUMENTS, INC.  ALTIMETER FAILED BI-ANNUAL CERTIFICATION WHEN ONLY 10 HOURS TOTAL TI	ME.					1	H	7	1 	3O			NT	3A12    					 
1999071600011	19990716	00011	SO  	1999	7	16	99ZZZX2571       	1	19990626	G	5711		RIVET           			PIPER 	PA24  	PA24250     	7102404	SO  										SPAR	SHEARED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	7873P	4393 				243099				ALL RIVETS WERE FOUND SHEARED THAT ATTACH THE REAR WING SPAR ATTACHMENT BRACKETS TO THE REAR CENTER SECTION SPAR.  (BOTH	 LEFT AND RIGHT SIDES).  DISCOVERED DURING ANNUAL INSPECTION.					1	L	7	1 	3O				1A15    					 
1999071600012	19990716	00012	SW  	1999	7	16	99ZZZX2572       	1	19990625	G	2560	3000	ELT             			BBAVIA	7     	7AC         	2110102	SW  										CABIN	INOPERATIVE     	D				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SO	13	84729				300899	7AC3445				DURING ANNUAL INSPECTION AND C/W FAR 91.207(D) G-TEST FAILED WHILE IN THE ARM POSITION.  UNIT WAS OPENED AND SEVERAL LOO	SE PARTS WERE FOUND FLOATING AROUND.  AIRCRAFT TOTAL TIME:  2,382:7 HOURS.					1	H	7	1 	3O				A759    					 
1999071600013	19990716	00013	SW  	1999	7	16	99ZZZX2573       	1	19990622	G	7160	2849	AIR FILTER      			BBAVIA	7     	7AC         	2110102	SW  										INTAKE	ALTERED         	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	13	84729					7AC3445				DURING ANNUAL INSPECTION, THE ORIGINAL AIR FILTER ASSEMBLY WAS FOUND TO HAVE HAD THE GUTS REMOVED AND ALTERED TO ACCEPT 	A BRACKET AIR FILTER ELEMENT BA-4106 WHICH WAS CUT TO SIZE.  THIS IS NOT APPROVED AND NOT SAFE.  AIRCRAFT TT:  2,385.0 H	OURS.				1	H	7	1 	3O				A759    					 
1999071600014	19990716	00014	SO  	1999	7	16	99ZZZX2574       	1	19990622	G	3230	6705403	TRUNNION        			PIPER 	PA32  	PA32RT300T  	7103216	SO  										NLG	CRACKED         	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	2148B				9033P	32R7987030				DURING ANNUAL INSPECTION, SUBMITTER FOUND NUMEROUS CRACKS (7) IN MULTIPLE LOCATIONS ON NOSE GEAR TRUNNION.  UPON FURTHER	 DISASSEMBLY OF NOSE GEAR TRUNNION, MORE CRACKS WERE FOUND INSIDE TRUNNION.  THESE CRACKS COULD NOT BE SEEN UNLESS NOSE 	GEAR WAS DISASSEMBLED.  NO CAUSE OTHER THAN FATIGUE COULD BE ESTABLISHED.				1	L	7	1 	3O				A3SO    					 
1999071600015	19990716	00015	WP  	1999	7	16	99ZZZX2575       	1	19990617	G	7921		ENGINE          			DOUG  	DC3   	DC3C        	3021457	WP  	PWA   	R1830 	R183092     	52020	NE  					OIL COOLER	FAILED          	G				E				ENGINE SHUTDOWN         				K	J		FLUID LOSS                	WARNING INDICATION        		CL	CLIMB          	1			SW	11	5831B					AC4210082	CP358946			APPROXIMATELY 45 MINUTES AFTER TAKEOFF, PILOT NOTICED OIL PRESSURE DROPPING.  ENGINE WAS SECURED AND PROPELLER FEATHERED	 WHEN MINIMUM PRESSURE WAS OBTAINED.  MAINTENANCE FOUND THE ENGINE OIL OUT TO OIL COOLER IN LINE HAD BROKEN.  LINE WAS R	EPLACED AND OIL TANK REFILLED.  ENGINE GROUND RAN, NO LEAKS NOTED.  AIRCRAFT RETURNED TO SERVICE.				2	L	7	2 	4R	4	R		A669    	5E4				 
1999071600016	19990716	00016	CE  	1999	7	16	99ZZZX2576       	1	19990625	G	2820	AN9246D	B-NUT           		98510965    	CESSNA	172   	172R        	2072401	CE  										FUEL SYSTEM	LEAKING         	B			DVPR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	03	9886F	21   				17280151				B-NUT FEEDING THE FUEL SELECTOR FROM LEFT FUEL TANK WAS LEAKING.  APPARENT CAUSE WAS INSUFFICIENT TORQUE.						1	H	7	1 	3O			NT	3A12    					 
1999071600017	19990716	00017		1999	7	16	99ZZZX2577       	4	19990625	G	3416	5934P3	ALTIMETER       			CESSNA	172   	172R        	2072401	CE  										COCKPIT	FAILED          	B			DVPR	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SO	03	9886F	17   			393890	17280151				ALTIMETER MANUFACTURED BY UNITED INSTRUMENTS, INC.,  ALTIMETER FAILED AFTER EFFECT REQUIREMENTS FOR BI-ANNUAL CERTIFICAT	ION WHEN ONLY 20.7 HOURS TOTAL TIME.					1	H	7	1 	3O			NT	3A12    					 
1999071600018	19990716	00018	SO  	1999	7	16	99ZZZX2578       	1	19990707	G	5730	24100511	FABRIC          			PITTS 	S2B   	S2B         	2210006	SO  										WING	MISMANUFACTURED 	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	07	25TC					5222				ON TOP WING 1 INCH OUTSIDE THE CENTER SECTION, 10 INCHES AFT OF THE LEADING EDGE, THE DOPE COVERING PEALED OFF IN A SHEE	T DOWN TO THE FABRIC.  IT IS HAS BEEN SUBMITTER'S EXPERIENCE THAT THIS SITUATION OCCURS WHEN EITHER THERE IS NO NITRATE 	DOPE APPLIED TO THE FABRIC OR THERE IS CONTAMINATION ON THE FABRIC.  THE FAILURE POINTS TOWARD A MANUFACTURING DEFECT. T	HE WINGS WERE RECOVERED BY AVIAT INC., 2/94 DUE TO PREVIOUS SERVICE DIFFICULTIES.			1	Q	7	1 	3O			NC	A8SO    					 
1999071600019	19990716	00019	SO  	1999	7	16	99ZZZX2579       	1	19990628	G	5540	3839402	FITTING         			PIPER 	PA32  	PA32RT300T  	7103216	SO  										RUDDER	CORRODED        	D	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	633CB	2605 				32R7887158				UPON REMOVAL OF RUDDER FOR C/W AD 79-26-04 AND PIPER SL 882A, IT WAS NOTED THE LOWER RUDDER ATTACH BOLTS WERE APPROXIMAT	ELY 40 PERCENT CORRODED.  THIS WAS CAUSED BY WATER ENTRAPMENT IN THE LOWER RUDDER ATTACH TUBE.  THE TUBE CONTAINED WATER	 WITH NO DRAINS PROVIDED FOR THE DRAINAGE OF THE WATER ,THE CROSS RETENTION WAS CORRODED IN THE CENTER.  SUBMITTER SUGGE	STED THIS COULD EVENTUALLY CAUSE FAILURE OF THE ATTACH BOLTS AND LOSS OF RUDDER CONTROL.			1	L	7	1 	3O				A3SO    					 
1999071600020	19990716	00020	CE  	1999	7	16	99ZZZX2580       	1	19990628	G	2824	476411	PUMP            	FACET       		CESSNA	310   	310R        	2074245	CE  										FUEL SYSTEM	SHORTED         	D				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			SO	11	87239	132  			9A	310R0314				PILOT NOTED THE RIGHT LANDING LIGHT CIRCUIT BREAKER TRIPPED.  PILOT RESET BREAKER AND IT TRIPPED AGAIN.  INVESTIGATION R	EVEALED THE RIGHT MAIN FUEL TRANSFER PUMP WAS SHORTING THIS CIRCUIT.  (NOTE:  BOTH THE LANDING LIGHT AND TRANSFER PUMP A	RE ON THE SAME CIRCUIT).  THIS PUMP SHOWS SIGNS OF ARCING AND BURN MARKS AT THE POINT THE SHIELDED POWER WIRE ENTERS THE	 PUMP.			1	L	7	2 	3O				3A10    					 
1999071600021	19990716	00021	CE  	1999	7	16	99ZZZX2581       	1	19990625	G	5310	05530313	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										FUSELAGE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	9562P	297  				17280499				C/W CESSNA SB 98-53-02.  FOUND FIREWALL CRACKED AT LOWER COWLING MOUNT BRACKET ADJACENT TO BATTERY BOX.  CRACK EXTENDED 	THROUGH INNER BRACKET RIVET HOLES APPROXIMATELY 2 INCHES IN LENGTH.  ALSO FOUND LOWER COWL SHOCK MOUNTS, P/N J7444-36, T	ORN.  SUBMITTER STATED THE ACFT SERIAL NUMBER IS NOT INCLUDED IN THE SERVICE BULLETIN EFFECTIVITY.				1	H	7	1 	3O			NT	3A12    					 
1999071600022	19990716	00022	CE  	1999	7	16	99ZZZX2582       	1	19990625	G	5310	05530313	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										FUSELAGE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	870CP	296  				17280666				C/W CESSNA SB 98-53-02.  FOUND FIREWALL CRACKED AT LOWER COWLING MOUNT BRACKET ADJACENT TO BATTERY BOX.  CRACK EXTENDED 	THROUGH INNER BRACKET RIVET HOLES APPROXIMATELY 2 INCHES IN LENGTH.  ALSO, FOUND LOWER COWL SHOCK MOUNTS, P/N J7444-36, 	TORN.  THIS ACFT SERIAL NUMBER DOES NOT FALL IN THE EFFECTIVITY RANGE OF THE SERVICE BULLETIN STATED ABOVE.				1	H	7	1 	3O			NT	3A12    					 
1999071600023	19990716	00023	CE  	1999	7	16	99ZZZX2583       	1	19990625	G	5310	05530313	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										FUSELAGE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	869CP	199  				17280641				C/W CESSNA SB 98-53-02.  FOUND FIREWALL CRACKED AT LOWER COWLING MOUNT BRACKET ADJACENT TO BATTERY BOX.  CRACK EXTENDED 	THROUGH INNER BRACKET RIVET HOLES APPROXIMATELY 2 INCHES IN LENGTH.  ALSO, FOUND LOWER COWL SHOCK MOUNTS, P/N J7444-36, 	TORN.  THIS ACFT SERIAL NUMBER DOES NOT FALL IN THE EFFECTIVITY RANGE OF THE SERVICE BULLETIN STATED ABOVE.				1	H	7	1 	3O			NT	3A12    					 
1999071600332	19990716	00332	EU  	1999	7	16	99ZZZX2589       	1	19990623	G	5320	350A21136227	BEAM            			SNIAS 	350   	AS350BA     	8680817	EU  										FUSELAGE	CRACKED         	B		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	21	189ND	5529 				2152				DURING 100-HOUR INSPECTION, FOUND CRACKS AT THE AFT END IN THE RADIUS OF REINFORCEMENT ANGLES, PN 350A21-1362-27, DASH 2	8.  CRACK ON LEFT SIDE (DASH 27) WAS 2.25 INCHES LONG, CRACK ON RT SIDE (DASH 28) IS 1.0 INCH LONG.  MANUFACTURER WAS NO	TIFIED AND ANGLES WERE REPLACED.				1	G	7	1 	3U			NC	H9EU    					 
1999071600333	19990716	00333	EU  	1999	7	16	99ZZZX2590       	1	19990624	G	3233	D25W272005507	ACTUATOR        			ISRAEL	1125  	ASTRASPX    	4500205	EU  										NLG	LEAKING         	B			QRRR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13	273RA	7    			IL115	097				LEAKING FLUID OUT OF EMERGENCY GEAR EXTENSION VALVE.  SHUTTLE VALVE ON NLG ACTUATOR WAS FOUND BYPASSING OUT TO THE VENT 	LINE.  PURGED HYDRAULIC LINES AND RPELACED NLG ACTUATOR.					2	L	7	2 	4F			RT	A16NM   					 
1999071600334	19990716	00334	EU  	1999	7	16	99ZZZX2591       	1	19990624	G	3233	D25W272005507	ACTUATOR        			ISRAEL	1125  	ASTRASPX    	4500205	EU  										NLG	LEAKING         	B			QRRR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13	273RA	504  			IL101	097				LEAKING FROM AROUND PISTON SHAFT.  REPLACED WITH NEW UNIT.						2	L	7	2 	4F			RT	A16NM   					 
1999071600335	19990716	00335		1999	7	16	99ZZZX2592       	4	19990624	G	3445	6228971120	TCAS            			ISRAEL	1125  	ASTRASPX    	4500205	EU  										COCKPIT	MALFUNCTIONED   	B			QRRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	273RA		125  		6044	097				DURING HIGH TEMPERATURES, OUTSIDE UNIT WILL TRIP CIRCUIT BREAKER.  REPLACED AND TESTED IN 90 DEGREE FAHRENHEIT (NOT HOT 	ENOUGH IN MDT).  WILL TEST IN SDL, FOR A TRUE TEST.					2	L	7	2 	4F			RT	A16NM   					 
1999071600336	19990716	00336		1999	7	16	99ZZZX2593       	4	19990624	G	3442	6228440003	RADAR           			ISRAEL	1125  	ASTRASPX    	4500205	EU  										RADOME	INOPERATIVE     	B			QRRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	273RA		479  		3671	097				UNIT WILL NOT TEST OR PAINT.  INOPERABLE.  REPLACED.						2	L	7	2 	4F			RT	A16NM   					 
1999071600337	19990716	00337	CE  	1999	7	16	99ZZZX2594       	1	19990621	G	3710		HOSE            			CESSNA	182   	182R        	2072731	CE  										VACUUM SYSTEM	DETERIORATED    	D				K				NONE                    				O			OTHER                     			TX	TAXI/GRND HDL  	1			SO	11	6453H					18267890				ALL VACUUM HOSES INSTALLED IN THIS AIRCRAFT HAVE HEAVY DETERIORATION BOTH INSIDE AND OUTSIDE OF THE HOSE.  THE ONLY INDI	CATION OF A PROBLEM WAS A DROP IN THE VACUUM GAUGE PRESSURE WITH THE AIRCRAFT IN-FLIGHT. THIS AIRCRAFT HAS HAD TWO PREVI	OUS VACUUM PUMPS INSTALLED ALONG WITH GYRO INSTRUMENTS REPLACED.  THIS WAS IN 1989 AND 1990.  (2,547 AND 2,582 HOURS TT)	.  TOTAL TIME IN SERVICE AT THIS EVENT IS 4,273.9 TACH HOURS.  THESE HOSES APPEAR TO HAVE BEEN INSTALLED AT THE FACTORY.			1	L	7	1 	3O			NT	3A13    					 
1999071600338	19990716	00338	CE  	1999	7	16	99ZZZX2595       	1	19990608	G	3297	G102A22	WIRE            			BEECH 	MU300 	400A        	1155402	CE  										MLG	SHORTED         	B			JAVR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	01	866BB	1277 				RK98				PILOT REPORTS 2 AMP LANDING GEAR CIRCUIT BREAKER TRIPS WHEN GEAR SELECTED UP.  MAINTENANCE FOUND TWO WIRES FROM GEAR SEL	ECTOR CONTROL SWITCH CRUSHED AND SHORTED TOGETHER BETWEEN EFIS TUBE NR 3 AND CENTER PEDESTAL STRUCTURE.  REPAIRED WIRES 	AND REPOSITIONED WIRE BUNDLE TO CLEAR STRUCTURE.  PERFORMED NORMAL GEAR RETRACTION CHECK.  NO DEFECTS NOTED.				2	H	7	2 	4F			RT	A16SW   					 
1999071600339	19990716	00339	WP  	1999	7	16	99ZZZX2596       	1	19990625	G	7810	369A8230504	EXHAUST STACK   			HUGHES	369   	369D        	4470706	WP  										ENGINE	CRACKED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	369AW					470117D				EXHAUST STACK HAS SLIGHT CRACK.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999071600340	19990716	00340	WP  	1999	7	16	99ZZZX2597       	1	19990625	G	7810	369A8230503	EXHAUST STACK   			HUGHES	369   	369D        	4470706	WP  										ENGINE	CRACKED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	369AW					470117D				EXHAUST STACK HAD SLIGHT CRACK.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999071600341	19990716	00341	SW  	1999	7	16	99ZZZX2598       	1	19990621	G	2497		WIRE            			BELL  	412   	412         	1182202	SW  										FUSELAGE	DETERIORATED    	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	19	411DE	3369 				36030				DURING PERFORMANCE OF A 300 HOUR/180 DAY INSPECTION, NOTED NUMEROUS AREAS IN THE ENGINE COMPARTMENT AND IN THE MAIN TRAN	SMISSION AREA WHERE THE 'YELLOW' COLORED WIRING INSULATION WAS CRACKED, SPLIT, AND FALLING OFF THE WIRING.  FURTHER INVE	STIGATION REVEALED THIS WAS THE CASE THROUGHOUT ALL THE WIRE BUNDLES IN THE ENGINE BAYS AND TRANSMISSION AREA.  WHEN THE	 WIRES IN A BUNDLE WERE SEPARATED FOR INSP, THE INSULATION HAD LITERALLY DISINTEGRATED WITHIN THE BUNDLE LEAVING BARE WI	RES EXPOSED.  SUSPECT A SUBSTANDARD QUALITY OR DEFECTIVE LOT OF WIRE WAS INSTALLED BY BELL HELICOPTER DURING PRODUCTION 	OF THIS SHIP.  SUBMITTER RECOMMENDED A ONE-TIME INSP OF ALL BELL HELICOPTER PRODUCTS FOR SIMILAR HAZARDOUS CONDITION.	1	G	7	2 	4U			 	H4SW    					 
1999071600342	19990716	00342	EU  	1999	7	16	99ZZZX2599       	1	19990623	G	5302	L535A1501210	FLANGE          			UROCOP	EC135 	EC135P1     	8680990	EU  										TAIL BOOM	CRACKED         	B	S		BAQR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	135ME	1217 				0009				FOUND CRACK WHERE NR 1 TAIL ROTOR DRIVE SHAFT BEARING MOUNTS TO CONNECTING FLANGE.  CRACK FOUND DURING C/W ECA5B EC135-5	3A-010 INSPECTION OF CONNECTING FRAME FLANGES CAUSED BY TOO FLEXIBLE OF A TAIL BOOM.  MANUFACTURER IS WORKING ON A RESOL	UTION.  AIRCRAFT TOTAL TIME:  1,217.1 HOURS.				1	G	7	2 	3U			O	H88EU   					 
1999071600343	19990716	00343	EU  	1999	7	16	99ZZZX2600       	1	19990625	G	6210	L621M1010054	BLADE           			UROCOP	EC135 	EC135P1     	8680990	EU  										MAIN ROTOR	CRACKED         	B	S		BAQR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	135ME	783  			428	0009				FOUND HARILINE CRACKS (8 EACH) EXTENDING CHORDWISE ALL THE WAY AROUND THE NICKLE LEADING EDGE EROSION PROTECTION STRIP. 	 CRACKS COULD NOT BE SEEN UNTIL A THOROUGH CLEANING OF THE BLADE LEADING EDGE WAS PERFORMED (REMOVAL OF BUGS/CARBON).  S	UBMITTER RECOMMENDED CLEANING AND VISUAL INSPECTION OF MAIN ROTOR BLADES AT REGULAR INTERVALS.				1	G	7	2 	3U			O	H88EU   					 
1999071600344	19990716	00344	SW  	1999	7	16	99ZZZX2601       	1	19990625	G	2910	206076031015	SERVO           			BELL  	206   	OH58A       	1181579	SW  										HYDRAULIC SYSTEM	LEAKING         	B			LS1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13	58AG				3453A	7221131				SERVO LEAKING BEYOND LIMITS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999071600345	19990716	00345	GL  	1999	7	16	99ZZZX2602       	2	19990625	G	7323	252476913	GOVERNOR        			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	MALFUNCTIONED   	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	5027P		269  		22476	611002D	CAE822961			GOVERNOR SLOW TO RESPOND.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999071600346	19990716	00346	GL  	1999	7	16	99ZZZX2603       	2	19990528	G	8530		VALVE           			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	BROKEN          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03	881SP					1354				THE INSPECTION OF THE ENGINE REVEALED NR 3 EXHAUST STACK MOUNTING FLANGE AND SEVERAL OF THE CYLINDER STUDS WERE BROKEN. 	 THE CARBURETOR AIR FILTER BOX WAS BLOWN OPEN AT THE SEAMS.  IT APPEARS TO BE FROM ENGINE BACKFIRE.  ALL CYLINDERS HAD N	ORMAL COMPRESSION AND THE ENGINE OIL SHOWED OBVIOUS SIGNS OF METALLIC PARTICLES.  RUB MARKS WERE NOTICED ON THE RIGHT LO	WER RUBBER MOUNTS.  SUBMITTER STATED FROM EXCESSIVE VIBRATION, THE FACTS LEADS TO A STUCK CYLINDER EXHAUST VALVE.			1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999071600347	19990716	00347	SW  	1999	7	16	99ZZZX2604       	1	19990625	G	2435	23032023	COMMUTATOR      			BELL  	206   	206B3       	1181506	SW  										START/GENERATOR	WORN            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY		498  		23305	2871				COMMUTATOR ON ARMATURE GROUND BEYOND LIMITS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999071600348	19990716	00348	GL  	1999	7	16	99ZZZX2605       	2	19990625	G	7412	106149501E	EXCITER         		95365498    	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	FAILED          	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	7907K	63   				2040	CAE831608			EXCITER WILL NOT CREATE SPARK WITH INPUT VOLTAGE.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999071600349	19990716	00349	SW  	1999	7	16	99ZZZX2606       	1	19990625	G	2424	CSV115212AB	VOLT REGULATOR  			BELL  	204   	UH1H        	1181407	SW  										ENGINE	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	52AG				BR6229A	7015746				VOLTAGE REGULATOR WILL NOT PRODUCE POWER.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999071600350	19990716	00350	WP  	1999	7	16	99ZZZX2607       	1	19990625	G	7810	369A8230503	EXHAUST STACK   			HUGHES	369   	369D        	4470706	WP  										ENGINE	CRACKED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	500DC					290456D				EXHAUST STACK IS CRACKED.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999071600356	19990716	00356	EA  	1999	7	16	99ZZZX2613       	2	19990629	G	8530		CYLINDER        			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					ENGINE	FAILED          	E				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			CL	CLIMB          	1			NM	07	3035K	232  				317752120	L721261A			AIRCRAFT DEPARTED SALT LAKE CITY FOR ST GEORGE, UT.  DURING CLIMB, ENGINE BEGAN RUNNING VERY POORLY.  ENGINE WAS FEATHER	ED.  AIRCRAFT MADE UNEVENTFUL LANDING.  INSPECTION OF ENGINE FOUND NR 5 CYLINDER ASSY FAILED.  PISTON CONDITION VERY BAD	.  PRE-IGNITION ON VERY LEAN BURN SUSPECTED.  NO PREVIOUS REPORTS OF PROBLEMS OF THAT NATURE.				1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999071600357	19990716	00357	CE  	1999	7	16	99ZZZX2614       	1	19990601	G	2432		WIRE            			CESSNA	172   	172         	2072402	CE  										BATTERY	CORRODED        	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	23										NO CHARGING INDICATION.  FOUND BATTERY WIRE TO BUS BAR FROM REGULATOR PREVIOUSLY SPLICED.  SPLICE HEATED, CORRODED CAUSI	NG LARGE RESISTANCE.  NOTED POWER TO REGULATOR WHEN STATIC ON THIS WIRE WHEN RUNNING POWER, WOULD NOT RETURN THROUGH THI	S WIRE TO BUS.  WIRE ORIGINAL, SPLICED?				1	H	7	1 	3O			NT	3A12    					 
1999071600358	19990716	00358	CE  	1999	7	16	99ZZZX2615       	1	19990626	G	2824	C2915060101	PUMP            	FACET       		CESSNA	310   	310G        	2074218	CE  										FUEL TIP TANK	INOPERATIVE     	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	13	8934Z					310G0034				DISCREPANCY FROM PILOT.  RIGHT TRANSFER PUMP INOPERATIVE.  DURING INSPECTION, NOTED FUEL PUMP AND ASSOCIATED WIRING DAMA	GED DUE TO EXTREME HEAT OF FUEL PUMP OPERATION.  INSPECTED ALL WIRING AND ELECTRICAL CIRCUIT WITH NO DEFECTS NOTED.  PAR	T TOTAL TIME 357 HOURS.  THIS HAS BEEN THE THIRD PUMP INSTALLED WTHIN 2 YEARS WITH FAILURES OCCURRING WITHIN 400 HOURS. 	 CESSNA HAS BEEN INFORMED AND IS CURRENTLY RESEARCHING.			1	L	7	2 	3O				3A10    					 
1999071600359	19990716	00359	CE  	1999	7	16	99ZZZX2616       	1	19990630	G	7921	627392	OIL COOLER      			CESSNA	182   	182         	2072702	CE  										ENGINE	LEAKING         	B			AF3R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	23										PART WS REPAIRED USING EPOXY.  EPOXY FAILED DURING NORMAL SERVICE ALLOWING PART TO LEAK AT POINT OF ORIGINAL REPAIR.  EP	OXY FAILURE IS COMMON.  SUBMITTER RECOMMENDED ELIMINATING USE OF EPOXY IN OIL COOLERS.					1	H	7	1 	3O			NT	3A13    					 
1999071600360	19990716	00360	EA  	1999	7	16	99ZZZX2617       	1	19990626	G	7830	22860020113	THRUST REVERSER 		SBRJNACC0224	CNDAIR	CL600 	CL6002B19   		EA  										ENGINE	CHAFED          	B			WVER	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	09	77195					7195				THRUST REVERSER MAIN TRACKS AND MAIN TRACKS ATTACHMENT POINTS CHAFED AT THE FIVE AND SEVEN O-CLOCK POSITIONS.  REPAIRED 	MAIN TRACKS AND ATTACHMENT POINTS IAW CRJ REQ 601R-78-30-1190.  BLEND, ROTO-PEEN AND PROTECTIVE TREATED.					2	L	7	2 	4F			RT	A21EA   					 
1999071600361	19990716	00361	EA  	1999	7	16	99ZZZX2618       	1	19990626	G	5320	6003603032	DOUBLER         			CNDAIR	CL600 	CL6002B19   		EA  										BS 718	CRACKED         	B			WVER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	09	77195					7195				DOUBLER ON AFT SIDE OF BS 718.00 STRINGER 11 RIGHT HAND SIDE CRACKED IN RADIUS.  REMOVED DAMAGED DOUBLER, FABRICATED NEW	 DOUBLER AND INSTALLED IAW WVAC EO NR 601R-53-0080.					2	L	7	2 	4F			RT	A21EA   					 
1999071600362	19990716	00362	EA  	1999	7	16	99ZZZX2619       	1	19990624	G	5320		BRACKET         			CNDAIR	CL600 	CL6002B16   	1900305	EA  										BS 295	CHAFED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	237GA					5019				NR 2 GENERATOR WIRES CHAFED ON GALLEY SUPPORT BRACKET RESULTING IN SIGNIFICANT ARCING DAMAGE TO BRACKET AND GENERATOR WI	RES.					2	L	7	2 	4F			RT	A21EA   					 
1999071600363	19990716	00363	EU  	1999	7	16	99ZZZX2620       	1	19990621	G	7730	21188823003	DEEC            			ISRAEL	1125  	ASTRASPX    	4500205	EU  										LT ENGINE	MALFUNCTIONED   	B			QRRR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	275RA	612  			036K0024	098				LEFT ENGINE MANUAL MODE LIGHT BLINKING.  DOWNLOADED DEEC, FOUND FAULT CODE 076.  TROUBLESHOT TO DEEC.  REPLACED WITH SER	VICEABLE UNIT.  OPS TESTED NORMAL.					2	L	7	2 	4F			RT	A16NM   					 
1999071600389	19990716	00389	NE  	1999	7	16	99ZZZX2629       	2	19990126	G	7250	2A221	TURBINE DISC    			AIRBUS	320   	A320231     	3930325	EU  	IAE   	V2500 	V2500A1     		NE  					ENGINE	CRACKED         	B			DQ5Y	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	35	GCRPH				P311AA0125	424	V0292			DURING INSPECTION OF PARTS FROM THIS ENGINE, FOUND THE HPI TURBINE DISC HAD CRACKING FROM ITS AIR METERING HOLES AND BEL	LING OF THE FRONT SECTION.  THESE FEATURES HAVE BEEN CAUSED BY A FIRE WHICH WAS PRESENT IN THE NR 6 BEARING COMPARTMENT.					2	L	7	2 	4F	4	F	RT	A28NM   	E311NE				 
1999072300003	19990723	00003	CE  	1999	7	23	99ZZZX2632       	1	19990414	G	7920		FILTER          			CESSNA	414   	414A        	2075907	CE  										OIL SYSTEM	LEAKING         	B			DJFR	K				NONE                    				B	K		SMOKE/FUMES/ODORS/SPARKS  	FLUID LOSS                		IN	INSP/MAINT     	1			EA	23	555DG					414A0115				AFTER AN OIL CHANGE ON THIS AIRCRAFT WHICH IS MODIFIED WITH RAM , STC'D, REMOTE OIL FILTERS, THE ICE LIGHT WIRE CAME IN 	CONTACT WITH THE OIL FILTER AND ARCED A HOLE IN THE FILTER AND A LARGE QUANTITY OF OIL WAS PUMPED OVERBOARD.					1	L	7	2 	3O				A7CE    					 
1999072300004	19990723	00004	CE  	1999	7	23	99ZZZX2633       	1	19990601	G	2823		TORQUE TUBE     			CESSNA	310   	310         	2074202	CE  										FUEL SELECTOR	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	23	CGOXN					35074				UPON INSPECTION, FOUND BOTH FUEL SELECTOR TORQUE TUBE ASSEMBLIES, PN 0820000-5 AND PN 0812000-13, SUFFERED SEVERE WEAR. 	 TUBE, PN 082000-5, WORN AT FUSELAGE GROMMET AREA AND TUBE, PN 0812000-13, WORN AT BULKHEAD WL 557.50 DAMAGE TO TUBES, W	AS ONLY DETECTABLE UPON REMOVAL AND IMPOSSIBLE TO DETECT UNDER NORMAL INSPECTIONS.  EXTENT OF DAMAGE IS APPROXIMATELY 65	 PERCENT OF THE PERIMETER OF THE TUBE AND 50 PERCENT THROUGH THE TUBE.  SUBMITTER STATED FOUR SHIELDED BEARING BLOCKS, P	N 5-352, SHOULD BE REMOVED FOR INSPECTION ASAP.		1	L	7	2 	3O			RT	3A10    					 
1999072300005	19990723	00005	EA  	1999	7	23	99ZZZX2634       	2	19990630	G	7414	1068291013	MAGNETO         	BENDIX      		PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					ENGINE	FRACTURED       	D				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			NM	07	800SA		390  		J089203GR	318152012	L384161A			AIRCRAFT INBOARD TO SLC, UT.  OIL PRESSURE FLUCTUATION NOTICED.  ENGINE FEATHERED AS PRECAUTION.  OIL LEAK AT BACK OF EN	GINE.  INSPECTION FOUND MAGNETO BASE FRACTURED AT LOWER HOLD-DOWN AREA OF CONTACT, 1/4 MOON SHAPE CHUNK HAD BROKEN OFF. 	 SUBMITTER SUSPECTED EXCESSIVE TORQUE ON STUD OR HOLD-DOWN NOT PROPERLY SEATED.  AIRCRAFT MADE UNEVENTFUL LANDING.				1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999072300006	19990723	00006	SW  	1999	7	23	99ZZZX2635       	1	19990704	G	3230	14333153	PIVOT SHAFT     			TMPSON	NAVION	NAVIONB     	6150112	SW  										MLG	BROKEN          	D	L			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23		1200 								MLG ACTUATING STRUT SUPPORT.  THIS PIVOT SHAFT IS HELD IN PLACE BY 2 COTTER KEYS AT EACH END.   A NAVION B OWNER STATED 	THE LT MAIN GEAR WOULD NOT RETRACT.  UPON PLACING ACFT ON JACKS AND USING AUX HAND PUMP, A GRINDING SOUND WAS HEARD FROM	 LT HAND GEAR WELL.  ON REMOVING RECTANGLE INSP PLATE JUST AFT OF GEAR WELL.  PIVOT SHAFT WAS FOUND BROKEN AT INNER COTT	ER KEY JUST NEXT TO HYD CYL UNIVERAL.  AS IT BROKE, IT BENT THE 2 BLKHDS THE PIVOT SHAFT RIDES ON.  NOTED THE PIVOT SHAF	T WAS GROOVED AT THE RIDING POINTS ON BLKHDS.  TT 1,200 HRS.  PART ORIG INSTALL FROM FACTORY.		1	L	7	1 	3O				A782    					 
1999072300007	19990723	00007	SW  	1999	7	23	99ZZZX2636       	1	19990704	G	5710		BULKHEAD        			TMPSON	NAVION	NAVIONB     	6150112	SW  										WING	DAMAGED         	B	L			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23		1200 								MLG ACTUATING STRUT SUPPORT.  THIS PIVOT SHAFT IS HELD IN PLACE BY 2 COTTER KEYS AT EACH END.   A NAVION B OWNER STATED 	THE LT MAIN GEAR WOULD NOT RETRACT.  UPON PLACING ACFT ON JACKS AND USING AUX HAND PUMP, A GRINDING SOUND WAS HEARD FROM	 LT HAND GEAR WELL.  ON REMOVING RECTANGLE INSP PLATE JUST AFT OF GEAR WELL.  PIVOT SHAFT WAS FOUND BROKEN AT INNER COTT	ER KEY JUST NEXT TO HYD CYL UNIVERAL.  AS IT BROKE, IT BENT THE 2 BLKHDS THE PIVOT SHAFT RIDES ON.  NOTED THE PIVOT SHAF	T WAS GROOVED AT THE RIDING POINTS ON BLKHDS.  TT 1,200 HRS.  PART ORIG INSTALL FROM FACTORY.		1	L	7	1 	3O				A782    					 
1999072300008	19990723	00008	SO  	1999	7	23	99ZZZX2637       	1	19990628	G	6120	74711	PLUG            		LW11224     	PIPER 	PA28  	PA28R201    	7102816	SO  										CRANKSHAFT	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	03	3327M	6098 			123740	28R7837112				THIS ENGINE EXPERIENCED A PROPELLER OVERSPEED REQUIRING REDUCTION TO 18 INCHES OF MP TO RETURN TO MAXIMUM RPM.  INSTALLI	NG AN OVERHAULED GOVERNOR DID NOT CORRECT THE PROBLEM.  PRESSURIZING THE OIL PASSAGE TO THE PROPELLER IAW LYC SI 1462 GA	VE AN ACCEPTABLE DIFFERENTIAL PRESSURE OF 7/40.  BY SLIGHTLY PRESSURIZING THE CRANKCASE AND LOOKING DOWN THE CRANKSHAFT 	BORE, IT WAS OBSERVED THAT AIR WAS COMING THROUGH THE REAR CRANKSHAFT PLUG DUE TO ITS BEING CRACKED.  WHEN ATTEMPTING TO	 REMOVE THE PIPE PLUG IN THE CENTER OF THIS PLUG, IT TURNED IN THE CRANK BORE AND BROKE INTO SIX PIECES.		1	L	7	1 	3O				2A13    					 
1999072300009	19990723	00009	SO  	1999	7	23	99ZZZX2638       	1	19990701	G	5540	3839402	FITTING         		7898119     	PIPER 	PA32  	PA32RT300   	7103215	SO  										RUDDER	CORRODED        	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	89VG	3387 				32R7885112				INSPECTED RUDDER LOWER ATTACH BOLTS AT OWNER'S REQUEST.  FOUND LOWER BOLT MISSING AND THE REMAINING BOLT SHOWING SIGNS O	F CORROSION AND WEAR.  SUBMITTER SUGGESTED DUE POSSIBLY TO STRESS CAUSED BY THE ONE MISSING BOLT.					1	L	7	1 	3O				A3SO    					 
1999072300010	19990723	00010		1999	7	23	99ZZZX2639       	4	19990515	G	3416	A30	ENCODER         	ACK         		CESSNA	150   	150G        	2071816	CE  										COCKPIT	MALFUNCTIONED   	B			GA6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	2977J				54120	15065777				MODE C REPORTED AS INVALID.  RETURNED DEFECTIVE ENCODER TO MANUFACTURER FOR REPAIR.  PERFORMED BI-ANNUAL TESTS AND INSPE	CTIONS.					1	H	7	1 	3O				3A19    					 
1999072300014	19990723	00014	SO  	1999	7	23	99ZZZX2643       	1	19990629	G	7602	8930700	ROD END         			PIPER 	PA34  	PA34200     	7103405	SO  										THROTTLE	FAILED          	D	P	A		A	E			UNSCHED LANDING         	ENGINE SHUTDOWN         			O			OTHER                     			NR	NOT REPORTED   	1			WP	23	41298	35   				347450106				ROD END CONNECTS THROTTLE CABLE TO ARM AT SERVO.  BALL SEPARATED FROM SOCKET.  ENGINE WENT TO FULL POWER AND HAD TO BE F	EATHERED TO LAND.					1	L	7	2 	3O				A7SO    					 
1999072300015	19990723	00015	CE  	1999	7	23	99ZZZX2644       	1	19990709	G	7720	35380141163	BULB            			BEECH 	35    	V35A        	1151544	CE  										OIL TEMP	MISMANUFACTURED 	D	L			K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	03	7048N					D8636				THE OIL TEMPERATURE BULB WAS TO BE REPLACED DUE TO INACCURATE TEMPERATURE INDICATION.  THE REPLACEMENT PART WAS REJECTED	 BECAUSE THE WIRE STUD WAS LOOSE AND COULD BE ROTATED WITH FINGERS.  THE PART WAS SENT BACK TO THE VENDOR FOR REPLACEMEN	T.  THE VENDOR (KRN AVIATION SERVICES CHANDLER, AZ 85224) PULLED 2 OTHER BULBS FROM THEIR STOCK AND CHECKED THEM PRIOR T	O SHIPPING.  THE THREADED STUDS ON THESE ALSO WERE FOUND TO BE LOOSE.  A FOURTH TEMPERATURE BULB WAS PULLED FROM THE STO	CK OF THE VENDOR'S SUPPLIER; RAYTHEON.  THIS PART WAS REPORTED OK AND SHIPPED TO KRN WHERE IT WAS INSPECTED AND FOUND IN	 THE SAME CONDITION AS THE PREVIOUS 3.	1	L	7	1 	3O				3A15    					 
1999072300016	19990723	00016	CE  	1999	7	23	99ZZZX2645       	1	19990705	G	2916	511700712	SIGHT GAUGE     		511700726   	CESSNA	421   	421C        	2076016	CE  										HYD RESERVOIR	SPLIT           	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	01	421WT	50   				421C0620				HYDRAULIC LEAK IN NOSE COMPARTMENT.  INSPECTION REVEALED RESERVOIR SIGHT TUBE SPLIT AT TOP AND BOTTOM ATTACH TO RESERVOI	R.  TUBE WAS PURCHASED NEW AND INSTALLED APPROXIMATELY 50 HOURS BEFORE.  TUBE ALSO REPLACED ON SECOND AIRCRAFT, SN 421C0	236.  INSPECTION REVEALED TUBE ALSO SPLIT ON THIS AIRCRAFT.  COMPLETE FAILURE OF TUBE WILL RESULT IN LOSS OF HYDRAULIC F	LUID.			1	L	7	2 	3O				A7CE    					 
1999072300019	19990723	00019	SO  	1999	7	23	99ZZZX2648       	1	19990701	G	3222	65319004	STRUT           			PIPER 	PA28  	PA28161     	7102803	SO  										RT MLG	DETACHED        	B				O				OTHER                   				O			OTHER                     			AP	APPROACH       	1			WP	03	8166B	9478 				288216129				AIRCRAFT  BEING USED FOR FLIGHT INSTRUCTION UNDER PART 91.  AFTER LANDING DURING A TOUCH-AND-GO, PILOT FELT A SEVERE VIB	RATION.  WHILE EXECUTING GO-AROUND, BYSTANDERS NOTICED SOMETHING 'HANGING' UNDER RT WING.  THE RT MLG TRUNNION HAD BROKE	N AT THE UPPER TORQUE LINK ATTACH EARS AND THE LOWER STRUT AND WHEEL ASSY WERE ATTACHED TO THE ACFT ONLY BY THE BRAKE HO	SE.  THE PILOT LANDED ON WHAT REMAINED OF THE GEAR.  THE RT WING, RT FLAP, AND STABILATOR WERE DAMAGED BY THE LOWER STRU	T AND WHEEL ASSY.  THE ACFT IS AN '82 PIPER PA28161 WITH 9,477 TT HRS, ALMOST EXCLUSIVELY FLIGHT SCHOOL OPER.  RECORDS S	HOW NO ENTRIES OF LANDING GEAR TRUNNION REPLACEMENT.  SUBMITTER STATED PART TT BELIEVED TO BE 9,477 HRS.	1	L	7	1 	3O				2A13    					 
1999072300020	19990723	00020	CE  	1999	7	23	99ZZZX2649       	1	19990619	G	7920	0500118164	LINE            			CESSNA	172   	172P        	2072436	CE  										OIL PRESSURE	FAILED          	A				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			GL	31	177CB					17274204				OIL PRESSURE LINE FROM ENGINE TO THE FITTING ON THE AFT BAFFLE BROKE OFF AT THE FLARE.  CONSEQUENTLY, LOST OIL PRESSURE 	AND ALL BUT ONE-HALF QUART OF ENGINE OIL.  AFTER SAFE LANDING, OIL FILTER WAS CUT OPEN BY MECHANIC AND FOUND METAL CONTA	MINATION.  ENGINE DETERMINED UNAIRWORTHY.  ACFT TT:  8,434 HOURS.				1	H	7	1 	3O			NT	3A12    					 
1999072300021	19990723	00021	CE  	1999	7	23	99ZZZX2650       	1	19990623	G	3201	50420221	FENDER          			CESSNA	414   	414         	2075908	CE  										NLG	BROKE           	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	10	86VS					4140955				PILOT REPORTED HEARING A 'BANG' SHORTLY AFTER SELECTING GEAR DOWN.  NOSE GEAR DID NOT EXTEND.  INVEST REVEALED THE NOSE 	WHEEL FENDER LODGED ABOVE NOSE GEAR IN THE WHEELWELL.  THIS JAMMED THE UPLOCK MECHANISM.  THE NOISE WAS CAUSED BY THE RE	TRACT ROD FITTING BREAKING AS GEAR WAS EXTENDED.  EVIDENCE OF A PRE-EXISTING CRACK COULD BE SEEN IN THE FENDER WELDS AND	 IT EVIDENTLY FAILED WHEN THE GEAR WAS RETRACTED.  DAMAGE TO THE AIRCRAFT INCLUDED BOTH PROPELLERS.  NOSE TIRE, NOSE GEA	R RETRACT LINKAGE, NOSE GEAR DOORS, RADOME, AND NOSE STRUCTURE BETWEEN THE RADOME AND NOSE WHEELWELL.		1	L	7	2 	3O			RT	A7CE    					 
1999072300022	19990723	00022	GL  	1999	7	23	99ZZZX2651       	2	19990622	G	7310	6890581	TUBE            			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C30P     	03013	GL  					FUEL SYSTEM	CRACKED         	B			ZV1R	A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			SW	03	2611					45417	CAE890211			DURING CRUISE FLIGHT FROM OFFSHORE, PILOT NOTICED N2 DROPPING.  LANDING WAS MADE - NO DAMAGE TO AIRCRAFT.  DURING TROUBL	ESHOOTING, FOUND PC LINE FROM ACCUMULATOR TO FUEL CONTROL CRACKED AT FLARE ON POWER CONTROL SIDE CAUSING ENGINE TO SPOOL	 DOWN.  REPLACED LINE AND TEST FLEW AIRCRAFT.  OPS CHECK GOOD.  TROUBLESHOOTING DID SHOW .9 VIB IN ENG AREA - FOUND AFT 	ADAPTER ON DRIVESHAFT FROM ENGINE TO OIL COOLER BLOWER WORN.  REPLACED ADAPTER AND VIB LEVEL DROPPED TO .02.  CHECK OF A	DAPTER SHOWS PER MANUAL, IS STILL WITHIN LIMITS.  SUBMITTER STATED THEY ARE INSPECTING FLEET FOR QUESTIONABLE LINES AND 	ADAPTERS.	1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999072300023	19990723	00023	CE  	1999	7	23	99ZZZX2652       	1	19990621	G	2460	S20415016	RESISTOR        			CESSNA	177   	177RG       	2073709	CE  										COCKPIT	BURNED          	D				K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			NE	01	52926	3315 				177RG1311				DURING ANNUAL INSP, SMOKE NOTICED COMING OUT OF RADIO STACK.  INVEST SHOWED THE S2041-50-1.6 RESISTOR FOR THE CIGARETTE 	LIGHTER DAMAGED AND SMOKING.  SMOKE AND BURN MARKS NOTED ON BOTH SIDES OF GLOVE BOX SIDEWALL WHERE RESISTOR WAS MOUNTED.	  THE NYLON LOCKING PORTION OF MOUNTING NUTS WAS MELTED AWAY.  INSP SHOWED THE CERAMIC INSULATOR INSIDE THE BASE OF THE 	0513052-20 CIGARETTE LIGHTER WAS BROKEN.  NEITHER THE 7-AMP FUSE OR THE 10-AMP C/B ACTIVATED.			1	H	7	1 	3O				A20CE   					 
1999072300024	19990723	00024	EA  	1999	7	23	99ZZZX2653       	2	19990625	G	7310	AN9246D	B-NUT           		98510965    	CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FUEL SYSTEM	LEAKING         	B				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	03	2272H	10   				17280688				B-NUT FEEDING THE FUEL SELECTOR FROM LEFT FUEL TANK WAS LEAKING.  APPARENT CAUSE WAS INSUFFICIENT TORQUE.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999072300025	19990723	00025		1999	7	23	99ZZZX2654       	4	19990709	G	3452	066010620000	TRANSPONDER     	KING        		GULSTM	AA1   	AA1A        	0630710	SO  										COCKPIT	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03	9414L				122282	AA1A0219				THE SPECIFICATION FOR PULSE WIDTH IS 450 NS PLUS/MINUS 70 NS.  THE NEW UNIT HAD A PULSE WIDTH OF 545 NS.						1	L	7	1 	3O				A11EA   					 
1999072300026	19990723	00026	CE  	1999	7	23	99ZZZX2655       	1	19990707	G	3221		BOLT            			BEECH 	23    	C23         	1151242	CE  										MLG	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	17	180ED					M1622				FOUND AN 'AN' BOLT INSTALLED INSTEAD OF JO-BOLTS, NAS 699.667 IN LEFT LANDING GEAR STRUT.						1	L	7	1 	3O				A1CE    					 
1999072300027	19990723	00027	CE  	1999	7	23	99ZZZX2656       	1	19990707	G	5320	1694200091	CHANNEL         			BEECH 	23    	B24R        	1151253	CE  										BS 132	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	9206S					MC375				FOUND COROSION AT FORWARD ATTACH POINT OF CHANNEL 169, 520000-91, AT FS 132 WHERE AIR DUCT COMES THROUGH CHANNEL - ATTAC	H POINT COMPLETELY GONE.  ALSO, FOUND CORROSION AT VARIOUS POINTS ON FUSELAGE (WHERE FRESH AIR DUCT TOUCHES FUSELAGE).					1	L	7	1 	3O				A1CE    					 
1999072300028	19990723	00028		1999	7	23	99ZZZX2657       	4	19990701	G	6122	3019288	TUBE ASSY       			BEECH 	200   	A200        	1152921	CE  										PROP GOVERNOR	CRACKED         	B				C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			SW	03	1549					BC45				PRE-TAKEOFF ENGINE RUNS COMPLETED, PILOTS TAXIED OUT ONTO ACTIVE, APPLIED TAKEOFF POWER, NR 1 ENGINE NO RESPONSE.  RETUR	NED TO LINE, AND SHUT DOWN.  MAINTENANCE INSPECTED AND FOUND TUBE ASSY CRACKED AT B-NUT FITTING AT REAR OF ENGINE.  THIS	 TUBE IS STAINLESS STEEL AND THE SLEEVE FOR THE B-NUT IS BRAZED ON TO THE TUBE, AND THE CRACK DEVELOPED AT THE END OF TH	E SLEEVE.  THIS TUBE FEEDS P3 AIR TO THE PROP GOVERNOR AND ITS FAILURE CAUSED A LOSS OF P3 AIR TO THE FUEL CONTROL PREVE	NTING IT FROM SPOOLING UP PAST IDLE REGARDLESS OF THROTTLE POSITION.  ENGINE TSO:  1,731.8 HOURS.  CSO:  1,556.		1	L	7	2 	4T				A24CE   					 
1999072300029	19990723	00029		1999	7	23	99ZZZX2658       	4	19990625	G	3414	EA517517P12CES	INDICATOR       			CESSNA	172   	172R        	2072401	CE  										COCKPIT	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03	9886F	24   			135811	17280151				AIRSPEED INDICATOR MANUFACTURED BY SIGMA-TEK.  AIRSPEED INDICATOR WAS EXCESSIVELY SLUGGISH IN ALL MODES OF FLIGHT.  PROP	ER AIRSPEED WOULD ONLY BE INDICATED AFTER SEVERAL MINUTES (3-5) OF STABILIZED FLIGHT IN ANY PARTICULAR MODE.					1	H	7	1 	3O			NT	3A12    					 
1999072300030	19990723	00030	CE  	1999	7	23	99ZZZX2659       	1	19990611	G	7921	8526250	OIL COOLER      		APO7AU0603  	BEECH 	23    	B23         	1151240	CE  										OIL SYSTEM	RUPTURED        	G				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	01	6136N				73L271	M1219				OIL COOLER RUPTURED IN AIRCRAFT.						1	L	7	1 	3O			RT	A1CE    					 
1999072300031	19990723	00031	CE  	1999	7	23	99ZZZX2660       	1	19990629	G	5510		DOUBLER         			BEECH 	35    	C35BEECH    	1151508	CE  										RUDDERVATOR	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	13	654D	6005 				D2921				WHILE CHECKING AIRCRAFT FOR ANOTHER PROBLEM, FOUND BOTH RUDDERVATORS AND ONE AILERON TO HAVE BEEN PATCHED.  THEY WERE EX	CESSIVELY LOOSE AND A CONSIDERABLE AMOUNT OF CORROSION WAS OBSERVED ON THE SURFACES.  PILOT WAS NOTIFIED OF THIS SITUATI	ON AND PILOT AND SUBMITTER AGREED THIS AIRCRAFT WOULD NOT FLY UNTIL REPAIRS WERE MADE.  THIS AIRCRAFT AS 25 HOURS SINCE 	ANNUAL INSPECTION.			1	L	7	1 	3O				A777    					 
1999072300032	19990723	00032	CE  	1999	7	23	99ZZZX2661       	1	19990629	G	5751		DOUBLER         			BEECH 	35    	C35BEECH    	1151508	CE  										AILERON	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	13	654D	6005 				D2921				WHILE CHECKING AIRCRAFT FOR ANOTHER PROBLEM, FOUND BOTH RUDDERVATORS AND ONE AILERON TO HAVE BEEN PATCHED.  THEY WERE EX	CESSIVELY LOOSE AND A CONSIDERABLE AMOUNT OF CORROSION WAS OBSERVED ON THE SURFACES.  PILOT WAS NOTIFIED OF THIS SITUATI	ON AND PILOT AND SUBMITTER AGREED THIS AIRCRAFT WOULD NOT FLY UNTIL REPAIRS WERE MADE.  THIS AIRCRAFT AS 25 HOURS SINCE 	ANNUAL INSPECTION.			1	L	7	1 	3O				A777    					 
1999072300033	19990723	00033	SO  	1999	7	23	99ZZZX2662       	1	19990705	G	2520	IMM1110401	SEAT BELT       	INDIANAMILLS		GULSTM	AA5   	AA5B        	3960105	SO  										CABIN	WRONG PART      	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	14	74262	812  				AAB50177				SUBMITTER STATED THIS IS THE SECOND GRUMMAN AA5 SERIES AIRCRAFT THIS MECHANIC HAS FOUND IN THE LAST 6 MONTHS WITH THE SE	AT BELTS, EFFECTED BY AD 79-16-02, STILL INSTALLED.					1	L	7	1 	3O				A16EA   					 
1999072300519	19990723	00519	SW  	1999	7	23	99ZZZX2703       	1	19990708	G	7332	407375007103	INDICATOR       			BELL  	407   	407         		SW  										COCKPIT	MALFUNCTIONED   	B			GS1R	O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	175P	9    				53316				FUEL PRESSURE INDICATOR INTERMITTENT.  REPLACED WITH NEW INDICATOR FROM BELL HELICOPTER.						1	G	7	1 	3U			O	H2SW    					 
1999072300520	19990723	00520	CE  	1999	7	23	99ZZZX2704       	1	19990624	G	3320		BALLAST         	PRECISION   	00741626    	BEECH 	200   	200BEECH    	1152920	CE  										CABIN	FAILED          	D				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			SW	99	12CF				69000080	BB534				FRIED AND SHORTED BALLAST CAUSED SMOKE IN CABIN.  HEAT DAMAGED PLASTIC WINDOW HOLDING.						1	L	7	2 	4T				A24CE   					 
1999072300521	19990723	00521	NM  	1999	7	23	99ZZZX2705       	1	19990630	G	5210		FRAME           			BOEING	727   	727230      	1384080	NM  										PASSENGER DOOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON R01 DOOR FRAME.						2	L	7	3 	4F				A3WE    					 
1999072300522	19990723	00522	NM  	1999	7	23	99ZZZX2706       	1	19990630	G	5320	NAS670522	TIE BOLT        			BOEING	727   	727230      	1384080	NM  										BS 1183	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON TENSION TILE BOLT BS 1183, STR 12L.						2	L	7	3 	4F				A3WE    					 
1999072300523	19990723	00523	NM  	1999	7	23	99ZZZX2707       	1	19990628	G	5240	66157801	HINGE           			BOEING	727   	727230      	1384080	NM  										SERVICE DOOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON LOWER AFT LAVATORY SERVICE PANEL HINGE.						2	L	7	3 	4F				A3WE    					 
1999072300524	19990723	00524	NM  	1999	7	23	99ZZZX2708       	1	19990629	G	5320		ANGLE           			BOEING	727   	727230      	1384080	NM  										APU BAY	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON UPPER AND LOWER ANGLES OF APU INLET FOR SCREEN.						2	L	7	3 	4F				A3WE    					 
1999072300525	19990723	00525	EU  	1999	7	23	99ZZZX2709       	1	19990709	G	2497		WIRE            			AMD   	FALC50	FALCON50MYST	2730106	EU  										BS 10 & 11	SHORTED         	B			YL1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	11	198M					277				OPERATOR EXPERIENCED AN OVERHEATING CAUSED BY AN INCORRECT COFFEE MAKER GROUND WIRE CONNECTIONS.  THE GALLEY WAS REMOVED	 AND IT WAS NOTICED THE GROUND CABLES WERE IMPROPERLY TORQUED, BURNISHED, AND THE PROTECTION VARNISH SEEPED UNDER THE TE	RMINALS WHICH ISOLATED PROPER GROUND TO THE T1A COFEE MAKER.				2	L	7	3 	4F			 	A46EU   					 
1999072300526	19990723	00526	CE  	1999	7	23	99ZZZX2710       	1	19990719	G	5511		SPAR            			CESSNA	414   	414         	2075908	CE  										HORIZONTAL STAB	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	43TG					4140397				OPERATOR OF AIRCRAFT PERFORMED ROUTINE INSPECTION.  FOUND FRONT SPAR OF THE HORIZONTAL STABILIZER CRACKED APPROXIMATELY 	1 INCH OUTOARD OF EACH ATTACH POINT TO THE FUSELAGE.  SUBMITTER STATED CAUSE OF CRACKS IS UNKNOWN.					1	L	7	2 	3O			RT	A7CE    					 
1999072300527	19990723	00527		1999	7	23	99ZZZX2711       	4	19990402	G	6122	D20271	GOVERNOR        																	PROPELLLER	MISREPAIRED     	B			IC2R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15					840149					THE REFERENCED MCAULEY PROPELLER GOVERNOR, PN D20271 WAS SENT TO T-BIRD FOR TROUBLESHOOTING AND/OR REPAIR DUE TO OVERSPE	ED OF THE ENGINE (3,400 RPM).  ON TEAR DOWN, NO MAJOR DISCREPANCIES WERE NOTED EXCEPT THE PRESSURE RELIEF ADJUSTMENT DID	 NOT HAVE WASHERS AS PRESCRIBED, INSTEAD HAD BEEN SCREWED DOWN INTO THE BODY.  CLOSE INSPECTION SHOWED PREVIOUS OVERHAUL	 HAD PERFORMED AN UNAUTHORIZED BODY REPAIR BY SLEEVING THE GEAR SHAFT HOUSING RECESS.  THE SHAFT SHOWED ABOVE LIMITS ON 	WEAR TOLERANCE.  BODY REPLACED WITH USED SERVICEABLE HOUSING AND UNIT REBUILT AND BENCH TEST SATISFACTORY FOR RETURN TO 	SERVICE.														 
1999072300528	19990723	00528		1999	7	23	99ZZZX2712       	1	19990330	G	2434	ALV10125	BRUSH           	PRESTOLITE  	ALV9510     															ALTERNATOR	WORN            	B			IC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15			25   		AL1973					SUBMITTER STATED THIS IS THE SECOND INSTANCE OF FAILURE OF PMA'D BRUSHES FAILING TO GIVE SATISFACATORY TIME IN SERVICE. 	 ONE BRUSH WAS WORN DOWN, SO NO SPRING TENSION WAS EXERTED TO BRUSH.  LESS THAN 25 HOURS SINCE OVERHAUL.  PREVIOUS CASE 	BRUSHES LASTED APPROX 50 HOURS.  THE SLIP RINGS SHOWED NO BURNING AND WERE 200 PERCENT POLISHED PER OHM.  THOSE BRUSHES 	ARE CONTOURED AND RUN IN FOR 100 PERCENT CONTACT BEFORE RETURN TO SERVICE.																 
1999072300529	19990723	00529		1999	7	23	99ZZZX2713       	4	19990629	G	2561	P0701121KS35	LIFE PRESERVER  	EAAEROMARINE																CABIN	FAILED          	B			KQ1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	07					E02877					VEST FAILED MFG RECOMMENDED 2 PSI TEST.  DATE OF MFG JULY 1984 IAW MANUAL 6710.																			 
1999072300530	19990723	00530		1999	7	23	99ZZZX2714       	4	19990629	G	2561	P0701121KS35	LIFE PRESERVER  	EAAEROMARINE																CABIN	FAILED          	B			KQ1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	07					E03027					VEST FAILED MFG RECOMMENDED 2 PSI TEST.  DATE OF MG JULY 1984 IAW MANUAL 6710.																			 
1999090200006	19990902	00006		1999	9	2	99ZZZX2715       	4	19990729	G	2561	P0701121KS35	LIFE PRESERVER  																	CABIN	FAILED          	B			KQ1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	07										VEST FAILED MFG RECOMMENDED 2 PSI TEST.  DATE OF MFG JULY 1984 IAW MANUAL 6710.																			 
1999072300531	19990723	00531		1999	7	23	99ZZZX2716       	4	19990618	G	2561	KS9P0101	LIFE VEST       	EAAEROMARINE																CABIN	FAILED          	B			KQ1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	07					C93097					LIFE VEST CELL FAILED MFG RECOMMENDED 2 PSI TEST IAW 25-60-1.  DATE OF MFG JANUARY 1983.																			 
1999072300532	19990723	00532	GL  	1999	7	23	99ZZZX2717       	3	19990524	G	6114		HUB             			CESSNA	150   	152         	2071835	CE  						MCAULY	1A103	1A103TCM    	GL  	PROPELLER	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	757RF					15279938		R777001		PROPELLER CRACKED BEYOND LIMITS OF AD 97-06-16 SECTION III.  PROPELLER REMOVED FROM SERVICE.  TTP UNKNOWN.  TTA:  5,147.	8.					1	H	7	1 	3O			NT	3A19    		5	N	P50GL	 
1999072300533	19990723	00533	CE  	1999	7	23	99ZZZX2718       	1	19990630	G	7120	051313211	BRACKET         			CESSNA	175   	175         	2072502	CE  										ENGINE MOUNT	CRACKED         	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	6672E	2206 				56172				ALL FOUR ENGINE MOUNT ATTACH BRACKETS WERE DESTROYED AND 3 WERE CRACKED WHERE THE ENGINE MOUNT BOLTS PASS THROUGH THE FI	REWALL.  THIS IS AN ALUMINUM ANGLE THAT THE FIRWALL ATTACHES TO THAT IS .060 INCH THICK THAT COVERS PART OF THE FACE OF 	THE BRACKET.  THIS LEAVES AN OPEN GAP BETWEEN THE BRACKET AND THE ENGINE MOUNT.  WHEN THE BOLT IS TORQUED UP, IT PULLS T	HE BRACKET FORWARD TO TRY TO FILL THIS GAP.  FOUND THIS ONLY AFTER REMOVAL OF THE FIREWALL, BUT IT APPEARS TO BE A CONDI	TION PRESENT FROM THE FACTORY.		1	H	7	1 	3O			NT	3A17    					 
1999072300534	19990723	00534	CE  	1999	7	23	99ZZZX2719       	1	19990630	G	7120	051313210	BRACKET         			CESSNA	175   	175         	2072502	CE  										ENGINE MOUNT	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	6672E	2206 				56172				ALL FOUR ENGINE MOUNT ATTACH BRACKETS WERE DESTROYED AND 3 WERE CRACKED WHERE THE ENGINE MOUNT BOLTS PASS THROUGH THE FI	REWALL.  THIS IS AN ALUMINUM ANGLE THAT THE FIREWALL ATTACHES TO THAT IS .060 INCH THICK THAT COVERS PART OF THE FACE OF	 THE BRACKET.  THIS LEAVES AN OPEN GAP BETWEEN THE BRACKET AND THE ENGINE MOUNT.  WHEN THE BOLT IS TORQUED UP, IT PULLS 	THE BRACKET FORWARD TO TRY TO FILL THIS GAP.  FOUND THIS ONLY AFTER REMOVAL OF THE FIREWALL, BUT IT APPEARS TO BE A COND	ITION PRESENT FROM THE FACTORY.		1	H	7	1 	3O			NT	3A17    					 
1999072300544	19990723	00544	EA  	1999	7	23	99ZZZX272 9      	2	19990619	G	8520		TAPPET          			PIPER 	PA28  	PA28140     	7102802	SO  	LYC   	O320  	O320E2C     	41508	EA  					ENGINE	BROKEN          	G	L			A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			EA	23	39801	2135 				2823867	1834827A			THE ENGINE WAS REMOVED FROM THE AIRCRAFT COMPLETELY DISASSEMBLED FOR OVERHAUL.  THE NR 3 CYLINDER INTAKE TAPPET WAS FOUN	D BROKEN AT THE CAM LOBE IN 3 PIECES.  THE NR 4 PISTON SKIRT HAD A LARGE PIECE BROKEN FROM THE BOTTOM OF THE SKIRT.  ALL	 PIECES WERE FOUND IN THE SUMP.  ALL OTHER INTERNAL CONDITIONS WERE NORMAL.  TOTAL ENGINE TIME SINCE RE-MFG:  2,135 HRS.				1	L	7	1 	3O	3	O		2A13    	E274				 
1999072300535	19990723	00535	CE  	1999	7	23	99ZZZX2720       	1	19990630	G	7120	05131329	BRACKET         			CESSNA	175   	175         	2072502	CE  										ENGINE MOUNT	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	6672E	2206 				56172				ALL FOUR ENGINE MOUNT ATTACH BRACKETS WERE DESTROYED AND 3 WERE CRACKED WHERE THE ENGINE MOUNT BOLTS PASS THROUGH THE FI	REWALL.  THIS IS AN ALUMINUM ANGLE THAT THE FIREWALL ATTACHES TO THAT IS .060 INCH THICK THAT COVERS PART OF THE FACE OF	 THE BRACKET.  THIS LEAVES AN OPEN GAP BETWEEN THE BRACKET AND THE ENGINE MOUNT.  WHEN THE BOLT IS TORQUED UP, IT PULLS 	THE BRACKET FORWARD TO TRY TO FILL THIS GAP.  FOUND THIS ONLY AFTER REMOVAL OF THE FIREWALL, BUT IT APPEARS TO BE A COND	ITION PRESENT FROM THE FACTORY.		1	H	7	1 	3O			NT	3A17    					 
1999072300536	19990723	00536	SO  	1999	7	23	99ZZZX2721       	2	19990521	G	7322	6297032A3	FCU             			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520L      	17032	SO  					ENGINE	MALFUNCTIONED   	D				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			GL	23	961CC		10   		C189917AP	21064620	294996R			DURING FLIGHT, THE FUEL PRESSURE WAS NOTED TO FLUCTUATE ERRATICALLY.  REPLACING THE FUEL CONTROL UNIT RESOLVED THE PROBL	EM.					1	H	7	1 	3O	3	O		3A21    	E5CE				 
1999072300537	19990723	00537	SO  	1999	7	23	99ZZZX2722       	2	19990520	G	8530	654651A5	CYLINDER        			CESSNA	210   	210R        	2073458	CE  	CONT  	O520  	IO520L      	17032	SO  					ENGINE	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	23	962CC	949  				21064986	294785R			DURING A ROUTINE 50-HOUR OIL CHANGE COMPRESSION CHECK, EXCESSIVE LEAKAGE WAS FOUND LEAKING PAST THE INTAKE AND EXHAUST V	ALVE ON THE NR 1 CYLINDER. THE CYLINDER WAS REMOVED AND FOUND TO HAVE A WORN OUT EXHAUST VALVE AND GUIDE.  IT ALSO HAD A	 BROKEN OUTER SPRING ON THE INTAKE VALVE AND NO CHOKE LEFT IN THE CYLINDER.  POSSIBLE CAUSE; DEFECTIVE PARTS AND ASSY PR	OCECURES USED DURING REMANUFACTURING PROCESS.			1	H	7	1 	3O	3	O	RT	3A21    	E5CE				 
1999072300538	19990723	00538	CE  	1999	7	23	99ZZZX2723       	1	19990601	G	5541	12310233	BRACKET         			CESSNA	210   	210M        	2073450	CE  										RUDDER	CRACKED         	H	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	1781M					21061959				THE BRACKET IS THE RUDDER TOP ATTACH POINT.  CORROSION APPEARS TO HAVE STARTED BETWEEN THE ATTACH POINT BRACKET AND THE 	AFT SPAR.  EVENTUALLY CRACKING THE SPAR AND BRACKET.					1	H	7	1 	3O				3A21    					 
1999072300539	19990723	00539	CE  	1999	7	23	99ZZZX2724       	1	19990601	G	5541	12310231	BRACKET         			CESSNA	210   	210M        	2073450	CE  										RUDDER	CRACKED         	H	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	09	1781M	4193 				61959				THE BRACKET IS THE RUDDER BOTTOM ATTACH POINT.  INTERGRANULAR CORROSION EXTENDING THROUGH THE RIVETS AND SPLITTING THE S	EAM.  PICTURES PROVIDED.					1	H	7	1 	3O				3A21    					 
1999072300542	19990723	00542	EA  	1999	7	23	99ZZZX2727       	2	19990130	G	7414		BEARING         								LYC   	O540  	O540E4C5    	41532	EA  					LT/RT MAGNETO	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	23			1476 				L1533840A			OPERATORS OF AVCO LYCOMING O-540-E4C5 ENGINES FITTED TO BRITTEN NORMAN ISLANDER AIRCRAFT IN GUYANA HAVE BEEN EXPERIENCIN	G PREMATURE FAILURE OF THE MAGNETO DRIVE GEAR BEARINGS.  THERE HAVE BEEN INSTANCES OF REPORTED HARD STARTING.  ON INVEST	IGATION, THE BEARINGS ARE DISCOVERED DAMAGED.  THE ENGINES ARE THEN REMOVED FROM SERVICE.									3	O			E295				 
1999072300543	19990723	00543	EA  	1999	7	23	99ZZZX2728       	2	19990417	G	7414		BEARING         								LYC   	O540  	O540E4C5    	41532	EA  					LT MAGNETO	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	23			515  				RL1431240			OPERATORS OF AVCO LYCOMING O-540-E4C5 ENGINES FITTED TO BRITTEN NORMAN ISLANDER AIRCRAFT IN GUYANA HAVE BEEN EXPERIENCIN	G PREMATURE FAILURE OF THE MAGNETO DRIVE GEAR BEARINGS.  THERE HAVE BEEN INSTANCES OF REPORTED HARD STARTING.  ON INVEST	IGATION, THE BEARINGS ARE DISCOVERED DAMAGED.  THE ENGINES ARE THEN REMOVED FROM SERVICE.									3	O			E295				 
1999072300545	19990723	00545	EA  	1999	7	23	99ZZZX2730       	2	19990619	G	8520		PISTON          			PIPER 	PA28  	PA28140     	7102802	SO  	LYC   	O320  	O320E2C     	41508	EA  					ENGINE	BROKEN          	G				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			EA	23	39801	2135 				2823867	1834827A			THE ENGINE WAS REMOVED FROM THE AIRCRAFT COMPLETELY DISASSEMBLED FOR OVERHAUL.  THE NR 3 CYLINDER INTAKE TAPPET WAS FOUN	D BROKEN AT THE CAM LOBE IN 3 PIECES.  THE NR 4 PISTON SKIRT HAD A LARGE PIECE BROKEN FROM THE BOTTOM OF THE SKIRT.  ALL	 PIECES WERE FOUND IN THE SUMP.  ALL OTHER INTERNAL CONDITIONS WERE NORMAL.  TOTAL ENGINE TIME SINCE RE-MFG:  2,135 HRS.				1	L	7	1 	3O	3	O		2A13    	E274				 
1999072300546	19990723	00546	CE  	1999	7	23	99ZZZX2731       	1	19990709	G	5753		SKIN            		052390135   	CESSNA	172   	172S        	2072439	CE  										TE FLAP	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	789EP	96   				172S8135				NEW CESSNA DURING 1ST PHASE 2 INSPECTION, FOUND LEFT FLAP TRAILING EDGE, LOWER SKIN CRACKED AT 8 EACH RIVETS STARTING FR	OM INBOARD END TO OUTBOARD, 2 FEET.  REPLACED FLAP WITH NEW ASSY FURNISHED BY CESSNA.					1	H	7	1 	3O			NT	3A12    					 
1999072300547	19990723	00547	CE  	1999	7	23	99ZZZX2732       	1	19990709	G	2720	04113070	ARM             			CESSNA	172   	172S        	2072439	CE  										RUDDER PEDAL	MISDRILLED      	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	949SP	97   				172S8145				NEW CESSNA WITH 97.4 HOURS SINCE NEW.  DURING FIRST PHASE 2 INSPECTION, FOUND PILOT'S AND COPILOT'S RUDDER PEDALS WERE N	OT ALIGNED PARALLEL TO ONE ANOTHER.  THE PILOT'S 'R' AND COPILOT'S 'L' RUDDER PEDAL MOUNT ARMS WERE MISDRILLED WHERE THE	Y MOUNT TO THE RUDDER PEDAL CROSS-OVER SHAFT.  REPLACED BOTH ARMS WITH CORRECTELY DRILLED PARTS FROM CESSNA AND ALIGNMEN	T IS NOW CORRECT.			1	H	7	1 	3O			NT	3A12    					 
1999072300548	19990723	00548	CE  	1999	7	23	99ZZZX2733       	1	19990402	G	2510	05142158	FITTING         			CESSNA	172   	172S        	2072439	CE  										PILOT SEAT BACK	BENT            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP	51   				172S8035				PILOT'S SEAT BACK IN FULL UPRIGHT POSITION WAS RECLINED 3 INCHES FROM FULL UPRIGHT.  THE PILOT'S SEAT BACK SUPPORT FITTI	NG WAS BENT.  THIS IS THE SECOND DEFECTIVE SEAT BACK FITTING REPLACED ON THE PILOT'S SEAT BACK.  THE FIRST ONE WAS REPLA	CED AT 23.6 HOURS TOTAL TIME. TIS IS THE 4TH FAILURE OF THIS PART ON OUR NEW CESSNA FLEET.				1	H	7	1 	3O			NT	3A12    					 
1999072300549	19990723	00549	CE  	1999	7	23	99ZZZX2734       	1	19990709	G	5753		SKIN            			CESSNA	172   	172S        	2072439	CE  										TE FLAP	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	948SP	149  				172S8144				NEW CESSNA DURING PHASE 1 INSPECTION, FOUND LEFT FLAP TRAILING EDGE, LOWER SKIN, CRACKED AT 4 EACH RIVETS STARTING FROM 	INBOARD END TO OUTBOARD 2 FEET.  REPLACED FLAP WITH NEW ASSY FURNISHED BY CESSNA.					1	H	7	1 	3O			NT	3A12    					 
1999072300550	19990723	00550	CE  	1999	7	23	99ZZZX2735       	1	19990709	G	7160	05503647	AIRBOX          			CESSNA	172   	172S        	2072439	CE  										INLET	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	567JW	51   				172S8187				DURING FIRST PHASE 1 INSPECTION, FOUND AIRBOX ASSY HAD PIECE MISSING AROUND ALTERNATE AIR DOOR AND THE DOOR HAD A GAP WH	ERE THE PIECE WAS MISSING. A FILLER MATERIAL WAS USED TO FILL IN ONE EDGE AS THE AIR DOOR HINGE WAS MISALIGNED. THE FILL	ER MATERIAL BROKE OFF LEAVING A GAP AROUND 1 EDGE OF THE ALTERNATE AIR DOOR CUT-OUT APPROXIMATELY .50 INCH LONG AND THE 	OTHER .50 INCH OF FILLER MATERIAL WAS CRACKED AND LOOSE.  REPLACED AIRBOX.			1	H	7	1 	3O			NT	3A12    					 
1999072300551	19990723	00551	EA  	1999	7	23	99ZZZX2736       	2	19990709	G	7322	05503623	ELBOW           			CESSNA	172   	172S        	2072439	CE  	LYC   	IO360 	IO360L2A    		EA  					FCU	LEAKING         	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NM	03	567JW	50   				172S8187				DURING FIRST PHASE 1 INSPECTION, FOUND FUEL LEAKING OUT OF AIR INLET ELBOW TO FUEL CONTROL.  THE OVERBOARD DRAIN LINE AD	APTER WHICH IS RIVETED AND SEALED TO THE AIR INLET ELBOW WAS NOT SEALED PROPERLY ALLOWING LEAKAGE.  REPLACED AIR INLET E	LBOW.				1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999073000034	19990730	00034		1999	7	30	99ZZZX2747       	4	19990603	G	3416	KT78	TRANSPONDER     	BENDIX      		PIPER 	PA34  	PA34200     	7103405	SO  										COCKPIT	MALFUNCTIONED   	B			GPQR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	09	47GM				12298	347350224				FAULTY LOANER KT78 WAS REMOVED AND KT76 WAS INSTALLED ON 6-3-99 ER NR 22281.						1	L	7	2 	3O				A7SO    					 
1999073000035	19990730	00035		1999	7	30	99ZZZX2748       	4	19990601	G	3416	KT78	ENCODER         	KING        		CESSNA	150   	150E        	2071812	CE  										COCKPIT	BROKE           	B			GEDR	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			NM	09	3974U					15061374				TRANSPONDER MODE C REPORTED BY ATC AS BEING INVALID.  FOUND AND REPLACED BROKEN TEE CONNECTION IN SENSE LINE FOR ENCODER	.					1	H	7	1 	3O				3A19    					 
1999073000036	19990730	00036		1999	7	30	99ZZZX2749       	4	19990707	G	2561	AD8E25D212681	LIFE JACKET     	AIRCRUISERS 																CABIN	FAILED          	B			KQ1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	07					3011					LIFE VEST FAILED MFG RECOMMENED 2 PSI TEST IAW 25-60-05.  DOM:  JAN 1978.																			 
1999073000037	19990730	00037		1999	7	30	99ZZZX2750       	4	19990707	G	2561	AD8E25D212681	LIFE JACKET     	AIRCRUISERS 																CABIN	FAILED          	B			KQ1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	07					4037					LIFE VEST FAILED MFG RECOMMENDED 2 PSI TEST IAW 25-60-05.  DOM:  APRIL 1981.																			 
1999073000038	19990730	00038	SW  	1999	7	30	99ZZZX2751       	1	19990617	G	2822	2050606063	PUMP            			BELL  	204   	UH1H        	1181407	SW  										FUEL SYSTEM	DAMAGED         	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	53AG				6064	7221588				FUEL PUMP SOUNDS REAL ROUGH LIKE BEARINGS GROWLING.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999073000039	19990730	00039	CE  	1999	7	30	99ZZZX2752       	1	19990702	G	2822	1C610	DATA TAG        			CESSNA	402   	402B        	207590P	CE  										BOOST PUMP	LOOSE           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	910WT	193  				402B0392				PILOT REPORTED RIGHT ENGINE WOULD NOT PRIME.  TROUBLESHOT AND FOUND RIGHT BOOST PUMP NOT PRODUCING ENOUGH PRESSURE.  UPO	N OPENING THE FUEL TANK TO REPLACE PUMP, FOUND THE PUMP'S DATA TAG HAD COME UNGLUED AND WAS DIRECTLY UNDER THE PICK-UP T	UBE.  WHEN PUMP WAS ACTIVATED, IT WOULD SUCK UP THE DATA TAG AND REDUCE FLOW TO ALMOST ZERO-10 PSI.  DATA TAG MEASURED A	PPROX 2.50 INCHES BY 2.50 INCHES.  PUMP HAD BEEN OVERHAULED BY FLEET SUPPORT SERVICES, MONRO, WI.			1	L	7	2 	3O				A7CE    					 
1999073000040	19990730	00040	CE  	1999	7	30	99ZZZX2753       	1	19990610	G	3210	PT08421072	DRAG BRACE      			CESSNA	320   	320B        	2074508	CE  										MLG	BROKE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	9840L					320B0040				DRAG BRACE  BROKE AT BOLT HOLES.						1	L	7	2 	3O				3A25    					 
1999073000041	19990730	00041	CE  	1999	7	30	99ZZZX2754       	1	19990714	G	7714	S33291	INDICATOR       			CESSNA	172   	172R        	2072401	CE  										TACHOMETER	STUCK           	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	15	2369P	4    				17280657				TACHOMETER NEEDLE STUCK AT ZERO, THEN JUMPED TO 1,700 RPM AND STUCK.  NEEDLE WOULD DROP TO ZERO AGAIN IF GLASS WAS TAPPE	D.  NEW TACHOMETER, SN 0852, CORRECTED PROBLEM.					1	H	7	1 	3O			NT	3A12    					 
1999073000042	19990730	00042	SO  	1999	7	30	99ZZZX2755       	2	19990701	G	8530		CYLINDER        			BEECH 	58    	58          	1152740	CE  	CONT  	O520  	IO520CB     	17032	SO  					ENGINE	SEPARATED       	B			L9PR	O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			GL	23	9206Q		1300 			TH157	231703			CYLINDER HEAD SEPARATED FROM THE BARREL IN CRUISE.  THE PISTON AND RINGS REMAINED IN THE CYLINDER AND THE HEAD CAME OFF 	AT THE END OF THE BARREL.  THE HEAD CRACKED AROUND BETWEEN THE THIRD AND FOURTH COOLING FIN.					1	L	7	2 	3O	3	O		3A16    	E5CE				 
1999073000043	19990730	00043	EA  	1999	7	30	99ZZZX2756       	2	19990610	G	7322	105009	CARBURETOR      	FACET       		CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					ENGINE	SEPARATING      	D				O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			GL	25	737GV		25   		BL2010649	17269415				ONE FIRST FLIGHT OF DAY STUDENT PILOT REPORTED ENGINE WOULD NOT IDLE CUT OFF AND WHEN SHUT OFF WITH MAG SWITCH, PROP RAN	 BACKWARDS.  QUESTIONED INSTRUCTOR AND FOUND THAT ENGINE DID NOT IDLE WELL ON THE FLIGHT THE PREVIOUS EVENING WHICH HE A	TTRIBUTED TO HOT WEATHER.  ON EXAMINATION, FOUND THAT CARBURETOR UPPER AND LOWER HALVES HAD SEPARATED BY APPROXIMATELY .	125 INCH.  ATTACH BOLTS ARE SLOTTED/HEX HEAD WITH A TABBED LOCKING WASHER UNDER THE HEAD.  TABS HAD BEEN BENT AS REQUIRE	D BY OVERHAULER, BUT BOLTS STILL LOOSENED.  SUBMITTER WOULD RECOMMEND A MORE POSITIVE SAFETY DEVICE BE UTILIZED ON THESE	 ATTACH SCREWS.	1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999073000044	19990730	00044	CE  	1999	7	30	99ZZZX2757       	1	19990713	G	2822	476411	PUMP            			CESSNA	310   	310Q        	2074242	CE  										RT WING	FAILED          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	11	69980	57   			9A	310Q1053				MAIN FUEL TRANSFER PUMP IN RIGHT WING FAILED DUE TO SHORTING OF POSITIVE WIRE TO GROUNDING SHIELDED WIRE.  FAILURE OCCUR	RED IN FLIGHT.  SUBMITTER STATED CAUSE UNKNOWN.					1	L	7	2 	3O				3A10    					 
1999073000045	19990730	00045	GL  	1999	7	30	99ZZZX2758       	3	19990701	G	6111	V7363N2R	BLADE           			BEECH 	55    	95A55       	1152704	CE  						HARTZL	HCA3V	EHCA3VF2    	GL  	PROPELLER	CRACKED         	B			LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	9733Y				E5372	TC419		BR672		BLADE CRACKED IN THE V-SHANK AREA OF PROPELLER.						1	L	7	2 	3O				3A16    		5	C	P6EA	 
1999073000046	19990730	00046	GL  	1999	7	30	99ZZZX2759       	3	19990701	G	6114		HUB             			CESSNA	402   	402B        	207590P	CE  						MCAULY	3AF32C	3AF32C87    	GL  	PROPELLER	CRACKED         	B			LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	768WC					402B1066		739214		HUB CRACKED IN THREAD AREA ON PROPELLER						1	L	7	2 	3O				A7CE    		5	C	P22EA	 
1999073000047	19990730	00047	GL  	1999	7	30	99ZZZX2760       	3	19990701	G	6111	B3252L	FORK            			PIPER 	PA31  	PA31350     	7103110	SO  						HARTZL	HCE3Y	HCE3YR2A    	GL  	PROPELLER	CRACKED         	B			LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	216AS					317652087		DJ8511A		PITCH CHANGE FORK CRACKED ON PROPELLER						1	L	7	2 	3O				A20SO   		5	C	P33EA	 
1999073000048	19990730	00048	GL  	1999	7	30	99ZZZX2761       	3	19990701	G	6114		HUB             			CESSNA	411   	411         	2075902	CE  						MCAULY	3AF34C	3AF34C74    	GL  	PROPELLER	CRACKED         	B			LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17								695620		HUB CRACKED IN THE THREAD AREA OF PROPELLER ASSY.						1	L	7	2 	3O				A7CE    		5	C	P22EA	 
1999073000049	19990730	00049	GL  	1999	7	30	99ZZZX2762       	3	19990701	G	6111	8833	BLADE           			BEECH 	35    	35BEECH     	1151502	CE  						HARTZL	HCA2X	HCA2X204    	GL  	PROPELLER	CRACKED         	B			LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17					C63036			AK374		BLADE CRACKED IN THE V-SHANK OF THE PROPELLER.						1	L	7	1 	3O				A777    		5	C	P908	 
1999073000050	19990730	00050		1999	7	30	99ZZZX2763       	4	19990601	G	3416	8140B35	ALTIMETER       			FRCHLD	F27   	F27F        	3373008	EA  										COCKPIT	MALFUNCTIONED   	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	08	222DG				977	31				FOUND ENCODING ALTIMETER GRAY CODE INOPERATIVE.  REPLACED ENCODING ALTIMETER SYSTEM FUNCTION, TESTED GOOD.						2	H	7	2 	4T				7A1     					 
1999073000051	19990730	00051	SW  	1999	7	30	99ZZZX2764       	1	19990709	G	3150	2407570545	CAUTION PANEL   			BELL  	204   	UH1H        	1181407	SW  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	51AG				A3028	7120178				TRANSMISSION OIL HOT LIGHT CAME ON, TEMPERATURE GAUGE IS NORMAL.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999073000052	19990730	00052	SW  	1999	7	30	99ZZZX2765       	1	19990625	G	6730	206076031013	SERVO           			BELL  	206   	206B3       	1181506	SW  										FLIGHT CONTROL	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY		598  		3109	2871				FELT STIFFNESS IN MID-TRAVEL OF CYCLIC IN FORWARD/AFT SERVO.  REMOVED AND REPLACED.  SENT FOR TEAR-DOWN ANALYSIS TO FASC	O.  ANALYSIS REVEALED SIDE LOADING OF SERVO TO BE MALFUNCTIONING.					1	G	7	1 	3U				H2SW    					 
1999073000053	19990730	00053	SW  	1999	7	30	99ZZZX2766       	1	19990709	G	6220	2040109377	DAMPER          			BELL  	204   	UH1H        	1181407	SW  										MAIN ROTOR	CONTAMINATED    	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	52AG				C2416	7015746				SIGHT GLASS CLOUDY.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999073000054	19990730	00054	SW  	1999	7	30	99ZZZX2767       	1	19990716	G	7722	2060751901	INDICATOR       			BELL  	206   	206B        	1181511	SW  										TOT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	90322				238	1736				STAYS AT 200 DEGREES CELSIUS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999073000055	19990730	00055	SW  	1999	7	30	99ZZZX2768       	1	19990617	G	7714	32005	TACHOMETER      			BELL  	206   	OH58A       	1181579	SW  										ENGINE	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	58AG`				142674	7221131				TACHOMETER WOULD NOT REGISTER ON GAUGE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999073000056	19990730	00056	WP  	1999	7	30	99ZZZX2769       	1	19990709	G	6220	369D21400503	DAMPER          			HUGHES	369   	369D        	4470706	WP  										MAIN ROTOR	DEBONDED        	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	5211R	4276 				1161D				DEBONDED AT OUTBOARD CENTER.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999073000057	19990730	00057		1999	7	30	99ZZZX2770       	4	19990709	G	3457	GPS60	GPS             			HUGHES	369   	369D        	4470706	WP  										COCKPIT	DAMAGED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	5211R				AF11385	1161D				NO LIGHTS OR ANYTHING, SOMETHING LOOSE INSIDE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999073000060	19990730	00060	CE  	1999	7	30	99ZZZX2773       	1	19990714	G	7714		INDICATOR       			CESSNA	172   	172R        	2072401	CE  										COCKPIT	STUCK           	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	15	7275C	66   			881	17280503				NEEDLE STUCK AT SEVERAL RPM SETTINGS.  PROBLEM CORRECTED BY INSTALLATION OF NEW TACHOMETER, S/N 0896.						1	H	7	1 	3O			NT	3A12    					 
1999073000061	19990730	00061	CE  	1999	7	30	99ZZZX2774       	1	19990714	G	7714		INDICATOR       			CESSNA	172   	172R        	2072401	CE  										COCKPIT	STUCK           	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	15	7275C	17   			0896	17280503				TACHOMETER NEEDLE STUCK AT SEVERAL DIFFERENT PLACES ON FACE AND WOULD LAG RPM CHANGES.  THIS WAS THE SECOND TACHOMETER T	O BE INSTALLED IN THIS ACFT SINCE ACFT WAS NEW (82.5 HRS).  PROBLEM WAS CORRECTED BY REPLACEMENT OF TACHOMETER WITH S/N 	0798 AND TACHOMETER CABLE P/N S2550-2.  SUBMITTER SUSPECTED THE TACH CABLE WAS TOO LONG AND PRESSING THE TACH SHAFT TOWA	RD THE NEEDLE SHAFT BINDING THE NEEDLE SHAFT.			1	H	7	1 	3O			NT	3A12    					 
1999073000062	19990730	00062	WP  	1999	7	30	99ZZZX2775       	1	19990617	G	3310	369H64255C	DIMMER CONTROL  			HUGHES	369   	369E        	4470707	WP  										COCKPIT	FAILED          	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	8330P		611  		696	0330E				DIMMER CONTROL HAS A SHORTED DIODE. REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999073000064	19990730	00064	CE  	1999	7	30	99ZZZX2777       	1	19990709	G	2730		CONTROL CABLE   			CESSNA	182   	182B        	2072706	CE  										COCKPIT	MISINSTALLED    	G				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	11	2356G					51656				DURING RAMP INSPECTION BY THE FAA, IT WAS DISCOVERED THE ELEVATOR WOULD NOT MOVE TO THE DOWN POSITION.  IT WAS FOUND THA	T AN AVIONICS (COAX) CABLE WAS ROUTED IN FRONT OF THE FLIGHT CONTROLS TEE BEHIND THE INSTRUMENT PANEL AND WAS BLOCKING A	NY FORWARD MOVEMENT OF THE FLIGHT CONTROL YOKE.  THE MECHANIC FOR THE OPERATOR CUT THE TIE-WRAP THAT HELD THE CABLE BLOC	KING THE FLIGHT CONTROLS, RE-ROUTED THE CABLE (UP AND OUT OF THE WAY), AND RE-FASTENED THE CABLE BUNDLE.  THE AIRCRAFT W	AS APPROVED FOR RETURN TO SERVICE.		1	H	7	1 	3O			NT	3A13    					 
1999073000065	19990730	00065	CE  	1999	7	30	99ZZZX2778       	1	19990708	G	2120	99101135	BLOWER          			CESSNA	650   	650         	2076802	CE  										AIR DIST	MALFUNCTIONED   	H		A		G	A			O2 MASK DEPLOYED        	UNSCHED LANDING         			B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			EA	21	33UL	1739 				6500160				IN-FLIGHT, BLOWER MOTOR FAILED, CAUSED COCKPIT TO FILL WITH SMOKE.  PILOTS HAD TO PUT ON SMOKE GOGGLES AND OXYGEN MASKS 	AND DECLARE AN EMERGENCY TO LAND AT ACY AT APPROXIMATELY 15:45 7-7-99.  AFTER LANDING, OPS CHECKED BLOWER, IT RAN FOR AB	OUT 3 SECONDS AND STOPPED.  REMOVED FROM AIRCRAFT AND DISASSEMBLED UNIT.  SUBMITTER STATED BRUSHES AND BEARINGS SEEM TO 	BE OK.  THE COMMUTATOR LOOKS BURNED.			2	L	7	2 	4F				A9NM    					 
1999073000066	19990730	00066	EA  	1999	7	30	99ZZZX2779       	1	19990629	G	5711	A10087	SPAR            			SCWZER	G164  	G164B       	3952802	EA  										WING	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	8137K	5510 				580B				REMOVED UPPER WINGS TO FACILITATE HOPPER REMOVAL.  FOUND BOTH LEFT AND RIGHT UPPER WING REAR SPARS CRACKED AT ATTACH POI	NT IN UPPER RADIUS BETWEEN BOLT HOLE AND UPPER FLANGE OF SPAR.  CRACKS ARE APPROXIMATELY .25 INCH LONG AND RAN UNDER MIL	LED FITTINGS, P/N'S A1050-101 AND A3090-13.				1	Q	7	1 	3R				1A16    					 
1999073000067	19990730	00067	EA  	1999	7	30	99ZZZX2780       	1	19990629	G	5711	A10088	SPAR            			SCWZER	G164  	G164B       	3952802	EA  										WING	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	8137K	5510 				580B				REMOVED UPPER WINGS TO FACILITATE HOPPER REMOVAL.  FOUND BOTH LEFT AND RIGHT UPPER WING REAR SPARS CRACKED AT ATTACH POI	NT IN UPPER RADIUS BETWEEN BOLT HOLE AND UPPER FLANGE OF SPAR.  CRACKS ARE APPROXIMATELY .25 INCH LONG AND RAN UNDER MIL	LED FITTINGS, P/N'S A1050-101 AND A3090-13.				1	Q	7	1 	3R				1A16    					 
1999073000068	19990730	00068	CE  	1999	7	30	99ZZZX2781       	1	19990625	G	2730		TORQUE TUBE     			CESSNA	172   	172         	2072402	CE  										LT ELEVATOR	LOOSE           	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	15	6770A					28870				ALL RIVETS SHEARED IN-FLIGHT.  LEFT ELEVATOR TORQUE TUBE TO FLANGE ON BELLCRANK.  PILOT WAS ABLE TO LAND, BUT REPORTED L	OSS OF PITCH CONTROL EFFECTIVENESS.					1	H	7	1 	3O			NT	3A12    					 
1999073000407	19990730	00407	EA  	1999	7	30	99ZZZX2782       	2	19990712	G	7322	9984903	AIR HOSE        			PIPER 	PA28  	PA28151     	7102805	SO  	LYC   	O320  	O320E3D     	41508	EA  					CARBURETOR	MISINSTALLED    	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	11	43256					287415459				AIRCRAFT EXPERIENCED AN ENGINE COWL FIRE AFTER LANDING.  INSPECTION OF THE AIRCRAFT REVEALED THE CARBURETOR AIR INTAKE H	OSE FROM THE AIR FILTER WAS CONNECTED TO THE MUFFLER WHEN IT SHOULD HAVE BEEN CONNECTED TO THE CARB AIR BOX. THE CABIN H	EAT DUCT WAS FOUND CONNECTED TO THE CARB AIR BOX. THIS MAY HAVE LEAD TO A BACKFIRE WHICH IGNITED A LEAKING PRIMER FUEL F	LEX LINE.			1	L	7	1 	3O	3	O		2A13    	E274				 
1999073000408	19990730	00408	CE  	1999	7	30	99ZZZX2783       	1	19990707	G	2421	DOFF10300J	ALTERNATOR      			CESSNA	172   	172M        	2072418	CE  										ENGINE	SEPARATED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	172RJ	60   			4102380	17263314				ELECTRO SYSTEMS - AIRPORT COMPLEX FORT DEPOSIT AL 36032.  ALTERNATORS ARE SEPARATING AT CASE HALVES AND ARE NOT PROVIDIN	G SUFFICIENT ELECTRICAL POWER FOR AIRCRAFT CAUSING LOW VOLTAGE/HIGH VOLTAGE LIGHTS TO COME ON  AND OFF.  CIRCUMSTANCE IS	 NORMAL FLYING.				1	H	7	1 	3O			NT	3A12    					 
1999073000409	19990730	00409	SO  	1999	7	30	99ZZZX2784       	1	19990707	G	7603	3174700	JOINT ASSY      			PIPER 	PA34  	PA34200     	7103405	SO  										THROTTLE	BROKEN          	D				E				ENGINE SHUTDOWN         				J			WARNING INDICATION        			DE	DESCENT        	1			EA	11	1229T	5400 				347250267				IMMEDIATELY FOLLOWING A POWER REDUCTION FOR DESCENT, THE LEFT ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENTS.  AN UNEVEN	TFUL, LEFT ENGINE FEATHERED LANDING WAS MADE.  POST-FLIGHT INSPECTION REVEALED THE BALL AND SOCKET STYLE ROD END SEPARAT	ED.  ALL ENGINE CENTERED ROD ENDS REPLACED WITH SPHERICAL BALL TYPE ROD END.				1	L	7	2 	3O				A7SO    					 
1999073000410	19990730	00410	CE  	1999	7	30	99ZZZX2785       	1	19990720	G	3060	SMR11886	BOOTS           		BVA6682     	CESSNA	441   	441         	2076020	CE  										PROPELLER	FAILED          	B			ME4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		185  								HARTZELL PROPELLER NR HC-B3TN-5E/T10178NB-11, S/N BVA6682 WAS OVERHAULED AUGUST 27, 1998 WITH NEW FAA-PMA B/E AEROSPACE 	SMR TECHNOLOGIES BOOTS.  P/N SMR1188-6 INSTALLED.  BOOTS FAILED AFTER 184.9 HOURS TT, AND 11 MONTHS SINCE INSTALLATION. 	 OLD BOOT S/N'S 0156, 0157, AND 0158 HAVE A CURE DATE OF 2Q98.  BOOTS DETERMINED INOPERATIVE BY ELEMENT RESISTANCE CHECK	.  ALL BOOTS HAD SHORT OR OPEN CIRCUIT.  NO BURN HOLES NOTED.  NO DEFECT NOTED WITH THE INSTALLATION OR REMAINING DEICIN	G SYSTEM.  INSPECTION ACCOMPLISHED IAW BF GOODRICH INSTALLATION AND MM ATA 30-60-02.  BF GOODRICH P/N 4E1188-6 BOOTS INS	TALLED AND OPS CHECK GOOD.	1	L	7	2 	3T			RT	A28CE   					 
1999073000411	19990730	00411	NE  	1999	7	30	99ZZZX2786       	3	19990713	G	6111	57D04951	FORK            			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	PITCH CHANGE	CRACKED         	B			EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03			4645 		3740NR			HJ481		FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS.  FOUR CRACKS.						2	L	7	2 	4T			RT	A24CE   		5	C	P10NE	 
1999073000412	19990730	00412	NE  	1999	7	30	99ZZZX2787       	3	19990713	G	6111	57D0495	FORK            			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	PITCH CHANGE	CRACKED         	B			EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03			4004 		3750NR			HJ445		FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS.  FIVE CRACKS.						2	L	7	2 	4T			RT	A24CE   		5	C	P10NE	 
1999073000413	19990730	00413	CE  	1999	7	30	99ZZZX2788       	1	19990714	G	5312	05530313	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										ENGINE BAY	CRACKED         	D	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	9543P	299  				17280644				CW CESSNA SB 98-53-02.  FOUND FIREWALL CRACKED 1.25 INCHES AT LOWER COWLING MOUNT BRACKET ADJACENT TO FIREWALL.  CRACK E	XTENDED VERTICALLY BETWEEN TWO RIVET HOLES OF INNER BRACKET.  AIRCRAFT NOT AFECTED BY SERVICE BULLETIN BY S/N.					1	H	7	1 	3O			NT	3A12    					 
1999073000414	19990730	00414	SO  	1999	7	30	99ZZZX2789       	1	19990630	G	7921	76510	GASKET          		53E22144    	PIPER 	PA31  	PA31350     	7103110	SO  										BYPASS VALVE	MISMANUFACTURED 	G				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	25	728CA	100  				317952036				WHEN C/W LYCOMING MSB 518C ON INSPECTION OF THERMOSTATIC BYPASS VALVE, UPON RE-INSTALLING VALVE, NEW GASKET WOULD NOT SI	T ON VALVE CORRECTLY.  IT SITS ON TAPERED SECTION OF VALVE AND WHEN TORQUED DOWN, IT LEAKS.  IF THE INSIDE DIAMETER OF T	HE GASKET WAS CHAMFERED ON BOTH SIDES, GASKET WOULD FIT PROPERLY.				1	L	7	2 	3O				A20SO   					 
1999073000415	19990730	00415	CE  	1999	7	30	99ZZZX2790       	1	19990716	G	5312	05530313	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										ENGINE BAY	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	7275C	297  				17280503				FOUND FIREWALL CRACKED AT LOWER COWL MOUNT BRACKET ADJACENT TO BATTERY BOX WHILE C/W CESSNA SB 98-53-02, REV 1.   PATCHE	D CRACK IAW SB 98-53-02, REV 1.					1	H	7	1 	3O			NT	3A12    					 
1999073000416	19990730	00416	CE  	1999	7	30	99ZZZX2791       	1	19990712	G	8120	24540250	CLAMP           	AIRESRCH    	4656804     	CESSNA	210   	P210N       	2073454	CE  										ENGINE BAY	FAILED          	H		A		A				UNSCHED LANDING         				M	J		OVER TEMP                 	WARNING INDICATION        		CL	CLIMB          	1			WP	09	4753K				KG0101	P21000284				SHORTLY AFER NORMAL TAKEOFF ROLL AND ROTATION, PILOT NOTICED MANIFOLD PRESSURE REDUCTION TO ATMOSPHERIC.  PILOT REMAINED	 IN THE AIRPORT PATTERN AND EXECUTED A NORMAL LANDING.  INITIAL INSPECTION IDENTIFIED A BURNED LEFT FORWARD NOSE SKIN. U	PON COWLING REMOVAL, FURTHER HEAT DAMAGE TO THE NOSE GEAR TO TUNNEL ASSY AND LEFT NOSE CAP BULKHEAD ASSY.  CAUSE OF EXCE	SSVE HEAT WAS DETERMINED TO BE A FAILED TURBOCHARGER SYSTEM FWD LT CROSS-TUBE CLAMP.  CLAMP HAD FAILED AT THE ADJUSTING 	BOLT.		1	H	7	1 	3O				3A21    					 
1999073000417	19990730	00417	CE  	1999	7	30	99ZZZX2792       	1	19990714	G	5312	05530313	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										ENGINE BAY	CRACKED         	D	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	2369P	298  				17280657				FOUND FIREWALL CRACKED AT LOWER COWLING SHOCK MOUNT BRACKET ADJACENT TO BATTERY TRAY.  CRACK EXTENDED FROM BRACKET ATTAC	H RIVET HOLE VERTICALLY AND WAS APPROXIMATELY 1.75 INCHES LONG.  CRACK WAS STOP DRILLED AND PATCHED WITH DOUBLER IAW CES	SNA SBA 98-57-02.				1	H	7	1 	3O			NT	3A12    					 
1999073000418	19990730	00418	CE  	1999	7	30	99ZZZX2793       	1	19990715	G	5312	05530313	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										ENGINE BAY	CRACKED         	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	23675	298  				17280651				DURING 100-HOUR INSPECTION, FOUND FIREWALL CRACKED AT THE LEFT LOWER COWLING SHOCK MOUNT BRACKET ADJACENT TO THE BATTERY	 TRAY.  CRACK WAS PATCHED IAW CESSNA 5898-53-02.  IT EXTENDED VERTICALLY FROM SHOCK MOUNT BRACKET ATTACH RIVET HOLES.					1	H	7	1 	3O			NT	3A12    					 
1999073000419	19990730	00419	CE  	1999	7	30	99ZZZX2794       	1	19990719	G	5521	043200185	SPAR ASSY       			CESSNA	150   	152         	2071835	CE  										ELEVATOR	MISMANUFACTURED 	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15										RECEIVED ONE NEW SPAR ASSY ON OR ABOUT 7-15-99.  WHEN PART WAS INSPECTED PRIOR TO USE, IT WAS OBVIOUS THE HINGE BRACKET 	WAS CROOKED AS INSTALLED.  THIS PART IS RIVETED TO THE SPAR BY CESSNA.  THE PART WAS RETURNED TO KANSAS CITY AVIATION CE	NTER AND A NEW ONE WAS RECEIVED 7-19-99.  IT WAS ALSO REJECTED FOR THE SAME REASON.				1	H	7	1 	3O			NT	3A19    					 
1999073000420	19990730	00420	GL  	1999	7	30	99ZZZX2795       	3	19990714	G	6114	A2432	BOLT            													HARTZL	HCC2Y	HCC2YR4     	GL  	HUB	FAILED          	B			YX4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05								DN2422		PROPELLER CORNER BOLT FAILED IN THREAD AREA.  THIS BOLT WAS A SPINNER BULKHEAD ATTACHMENT BOLT.  THE OWNER COMMENTED THA	T THE SPINNER HAD CRACKED, THEN WELDED AND CRACKED AGAIN AND RE-WELDED.  THE SPINNER WAS CRACKED WHEN RECEIVED FOR REPAI	R.  THE OWNER ALSO COMMENTED THE AIRCRAFT GOES THROUGH A PERIOD OF SEVERE VIBRATION DURING ROLLOUT.  THE MAIN GEAR IS HA	RD MOUNTED DIRECTLY TO THE ENGINE MOUNT.													5	C	P920	 
1999073000421	19990730	00421	SW  	1999	7	30	99ZZZX2796       	1	19990714	G	5302	206033004045A	SKIN            			BELL  	206   	206L1       	1182107	SW  										TAIL BOOM	CRACKED         	B			KBTR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	2233F	9175 			A0KP01180	45739				TAIL BOOM CRACKED AT AFT UPPER VERTICAL FIN SUPPORT.						1	G	7	1 	3U				H2SW    					 
1999073000422	19990730	00422	SW  	1999	7	30	99ZZZX2797       	1	19990714	G	6300	406340102101	CARBON SEAL     			BELL  	206   	206L4       	1182110	SW  										M/R DRIVE	LEAKING         	B			KBTR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NM	07	722LM	1319 			A2383	52111				FORWARD FREEWHEEL SEAL LEAKING.						1	G	7	1 	3U			NC	H2SW    					 
1999073000424	19990730	00424	CE  	1999	7	30	99ZZZX2799       	1	19990715	G	7830	20200481	SUPPORT ASSY    			BEECH 	MU300 	400BEECH    		CE  										THRUST REVERSER	SHEARED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	455DW					RJ20				FOUND RIVETS THAT ATTACH SUPPORT ASSY TO OUTER FAN DUCT FLANGE SHEARED.  THIS CONDITION CANNOT BE DETECTED BY VISUAL INS	PECTION ALONE.  YOU MUST PHYSICALLY MOVE SUPPORT ASSY TO DETECT SHEARED RIVETS.					2	H	7	2 	4F			RT	A16SW   					 
1999073000425	19990730	00425	SO  	1999	7	30	99ZZZX2800       	2	19990720	G	8530	649166	CYLINDER        			BEECH 	55    	D55         	1152730	CE  	CONT  	O520  	IO520C      	17032	SO  					ENGINE	BROKEN          	D	P			A				UNSCHED LANDING         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CR	CRUISE         	1			GL	13	7725R		109  			TE644	1263728C			DURING CRUISE FLIGHT, LEFT ENGINE BEGAN TO RUN ROUGH.  PILOT FEATHERED ENGINE.  A NORMAL SINGLE ENGINE LANDING WAS MADE.	  FOUND NR 3 CYLINDER BROKEN HALF WAY BETWEEN FLANGE AND BOTTOM OF HEAD.  PISTON CAME OUT AND BROKE.  CASE BROKE ALSO, S	TEEL CYLINDER.				1	L	7	2 	3O	3	O		3A16    	E5CE				 
1999073000426	19990730	00426	SO  	1999	7	30	99ZZZX2801       	1	19990711	G	2710	764088V	RIVET           			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	MISINSTALLED    	H				O				OTHER                   				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	17	3063K					447995212				AIRCRAFT EXPERIENCED OBSTRUCTION IN AILERON OPERATION.  MAINTENANCE FOUND RIVETS FROM SB (PIPER) 702 STRIKING UPPPER WIN	G SKIN.  MAINTENANCE CORRECTED AND RETURNED AIRCRAFT TO SERVICE.  PROBLEM RESTRICTED TO LEFT AILERON.  KIT SUBJECT TO AD	 81-10-04.				1	L	7	2 	3O				A19S0   					 
1999073000427	19990730	00427	CE  	1999	7	30	99ZZZX2802       	1	19990713	G	5540	51310104	BEARING PLATE   			CESSNA	421   	421C        	2076016	CE  										RUDDER	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	09	6793V	3304 				421C1022				LOWER RUDDER BEARING PLATE INSTALLED BY MFG UPSIDE DOWN ALLOWING BEARINGS TO MOVE DOWN, FROM WEIGHT OF RUDDER, CAUSING R	UDDER INTERFERENCE WITH CLOSE-OUT FAIRING AT TOP SIDE OF HORIZONTAL.					1	L	7	2 	3O				A7CE    					 
1999073000428	19990730	00428	SO  	1999	7	30	99ZZZX2803       	1	19990621	G	2432	G35	BATTERY         			PIPER 	PA34  	PA34200     	7103405	SO  										BATTERY BOX	FAILED          	D				O				OTHER                   				A			FLAME/FIRE                			NR	NOT REPORTED   	1			SO	15	56880					347450038				THE BATTERY EXPERIENCED AN INTERNAL SHORT CAUSING THE TERMINAL POST TO MELT.  ONCE CONTACT WAS BROKEN, THERE MUST HAVE B	EEN A SPARK CAUSING A FIRE.  DAMAGE SUSTAINED WAS A BURNED BATTERY BOX LID.  NO RECOMMENDATIONS CAN BE MADE FOR PREVENTI	ON.  NO CAUSE COULD BE FOUND.  A NEW BATTERY WAS INSTALLED AND ALL SYSTEMS CHECKED NORMALLY AND FULLY FUNCTIONAL.				1	L	7	2 	3O				A7SO    					 
1999073000429	19990730	00429	CE  	1999	7	30	99ZZZX2804       	1	19990713	G	5540	51310104	BEARING PLATE   			CESSNA	421   	421C        	2076016	CE  										RUDDER	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	09	762CA	3664 				421C1214				LOWER RUDDER BEARING PLATE INSTALLED BY MANUFACTURER UPSIDE DOWN ALLOWING BEARINGS TO MOVE DOWN, FROM WEIGHT OF RUDDER, 	CAUSING RUDDER INTERFERENCE WITH CLOSE-OUT FAIRING AT TOP SIDE OF HORIZONTAL.					1	L	7	2 	3O				A7CE    					 
1999073000430	19990730	00430	CE  	1999	7	30	99ZZZX2805       	1	19990610	G	2810	260010159	FUEL VENT       			CESSNA	208   	208B        	2073701	CE  										WING	PLUGGED         	B		A		O				OTHER                   				J			WARNING INDICATION        			AP	APPROACH       	1			SW	01	765FE	4873 				2008B0259				AIRCRAFT WAS FLOWN FROM AUS TO HRL.  UPON APPROACH TO HRL, LOW FUEL PRESSURE WARNING LIGHT ILLUMINATED AND WOULD NOT GO 	OFF.  INSPECTION REVEALED THE FUEL TANKS WERE UNDER VACUUM.  WHAT APPEARED TO BE CAKED MUD WAS FOUND INSIDE BOTH LEFT AN	D RIGHT FUEL VENT LINES.  CLEARED VENTS, GROUND RAN, OPS CHECKED OK.  BOTH WINGS UPPER SKINS WERE DISTORTED AND TWO RIBS	 JUST INBD OF WS 214.3 APPEARED TO BE CRUSHED. AIRCRAFT WAS FERRIED TO ICT FOR REPAIR.  A COVER FOR THE WING TIP SIMILAR	 TO THE PITOT COVERS USED ON THESE AIRCRAFT MAY PREVENT THIS PROBLEM.		1	H	7	1 	3T				A37CE   					 
1999082100010	19990821	00010	CE  	1999	8	21	99ZZZX2806       	1	19990714	G	2820	MS20822660	ELBOW           		07560397    	CESSNA	172   	172R        	2072401	CE  										FUEL SYSTEM	LOOSE           	B				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SO	03	2272H	10   				17280688				ELBOW THAT COMES OUT OF THE STRAINER TO THE FUEL LINE FOR THE ENGINE DRIVEN FUEL PUMP WAS LEAKING.  APPEARS THAT IT WAS 	PUT IN DRY AND TIGHTENED EXCESSIVELY.					1	H	7	1 	3O			NT	3A12    					 
1999073000431	19990730	00431	CE  	1999	7	30	99ZZZX2807       	1	19990702	G	8010	643259A29R	ADAPTER         			CESSNA	185   	A185F       	2072821	CE  										STARTER	BROKEN          	B	P		J2SR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	05	369E	723  				18504000				FAILURE OF BEARING DUE TO CORROSION CAUSING SHAFT TO SHIFT AND DAMAGE CRANKCASE.  BEARING VERY ROUGH AND NEAR FAILURE DU	E TO CORROSION AND RUST.  TELEPHONE CONVERSATION WITH MFG, CONTINENTAL, SAYS THAT AFTER MARKET ENGINE HEATERS MAY CONTRI	BUTE TO MOISTURE IN THIS AREA CAUSING THE CORROSION PROBLEM ULTIMATELY RESULTING IN THIS FAILURE.				1	H	7	1 	3O				3A24    					 
1999073000433	19990730	00433	CE  	1999	7	30	99ZZZX2809       	1	19990701	G	8120		SEAL            			AYRES 	S2    	S2R         	7630202	CE  										TURBO CHARGER	WORN            	G				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			AG	AGRICULTURE    	1			GL	27	5013X	1775 				5046R				DURING AN AG OPERATION, ENGINE LOST POWER.  EMERGENCY OFF-AIRPORT LANDING ON ROAD.  AIRCRAFT RAN OFF ROAD, DAMAGE TO PRO	P AND ONE WING TIP.  FURTHER INVESTIGATION DETERMINED ENGINE WOULD RUN, BUT WOULD NOT DEVELOP MANIFOLD PRESSURE.  FOUND 	BLOWER SEAL BLOWN.				1	L	7	1 	3R			NC	A4SW    					 
1999073000434	19990730	00434		1999	7	30	99ZZZX2810       	4	19990728	G	3417	KDC481T	ADC             			BELL  	430   	430         	1182150	SW  										E/E BAY	DISONNECTED     	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03	430CH				10453	49037				AFTER 300-HOUR INSPECTION ON AIRCRAFT, TEMPERATURE SENSOR CONNECTION WAS LEFT DISCONNECTED.  THIS CAUSES KDC481T TO GO T	O A DEFAULT MODE AND LIMIT IAS FUNCTION TO 88 KNOTS.  NO ERROR CODES WERE GIVEN EXCEPT VMO LIMIT.  KDC481T WAS REPLACED 	TWICE BEFORE LOOSE CONNECTOR WAS FOUND.				1	G	7	2 	3U			RT	H9SW    					 
1999081400004	19990814	00004	EU  	1999	8	14	99ZZZX2837       	1	19990714	G	5320	1172213201	SPLICE          			BOLKMS	117   	BK117B1     	5626012	EU  										BS 5060	CRACKED         	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	214AE					7206				A CRACK WAS FOUND ON LT FORWARD TAILCONE SPLICE P/N 117-22132-01 DURING ROUTINE INSPECTION AT STA 5060MM, LBL 70MM, AND 	WL 2900.  THE CRACK STARTED AT A RELIEF HOLE IN AN INTERSECTION OF THE BEND RADIUS AND TRAVELED UPWARDS TO THE NEXT BOND	 RADIUS AND TERMINATED IN FREE AIR.				1	G	7	2 	3U				H13EU   					 
1999081400005	19990814	00005	NE  	1999	8	14	99ZZZX2838       	2	19990630	G	7210	408135008	IDLER GEAR      			BOLKMS	117   	BK117A3     	5626015	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					TRANSMISSION	LOOSE           	B		A	TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4493X				91C068	S7038	LE45387			DISASSEMBLY OF ENGINE REVEALED METAL IN BOTTOM OF GEARBOX ASSY.  INSPECTION REVEALED IDLER GEAR TO HAVE ONE EACH NUT MIS	SING FROM ASSY BOLTS AND 3 EACH NUTS EITHER DAMAGED OR PARTIALLY MISSING PIECES.  TORQUE ON SEVERAL REMAINING BOLTS WERE	 LOOSE.  SUBMITTER RECOMMENDED RE-TORQUE OF1,200 HOUR INTERVAL CHECKS.  REPLACED ANY LOOSE NUTS AND BOLTS.  NUT P/N: MS2	1043-5.  BOLT P/N:  4-081-119-04.  ENGINE TT:  2,943.8 HOURS.			1	G	7	2 	3U	3	U		H13EU   	E5NE				 
1999081400006	19990814	00006	EU  	1999	8	14	99ZZZX2839       	1	19990625	G	6210		DAMPENER        			BOLKMS	105   	BO105LSA3   	5626020	EU  										MAIN ROTOR	FAILED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	911SV					2033				THERE WAS AN APPARENT FAILURE WITHIN THE MAIN ROTOR BLADE CUFF THAT FIXES THE LEAD LAG DAMPENER, AND SPHERICAL BEARING S	UPPORT TO THE BLADE ASSEMBLY, AND IS CURRENTLY UNDER INVESTIGATION BY AEC TECHNICAL REPRESENTATIVES.					1	G	7	2 	3U				H3AU    					 
1999081400008	19990814	00008	EU  	1999	8	14	99ZZZX2841       	1	19990408	G	2430	117188001	WIRE            			BOLKMS	117   	BK117B2     	5626013	EU  										DC SYSTEM	BROKEN          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	117MK	164  				7196				CABLES BROKEN.  REF:  MCN 32.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400009	19990814	00009	SW  	1999	8	14	99ZZZX2842       	1	19990406	G	2932	205076044009	SWITCH          			BELL  	222   	222U        	1182140	SW  										HYD PRESSURE	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	222HX	482  			0057	47533				NEW PART DEFECTIVE.  ILLUMINATED NR 1 HYDRAULIC LIGHT.  REPLACEMENT OF SWITCH EXTINGUISHER.						1	G	7	2 	3U				H9SW    					 
1999081400010	19990814	00010	GL  	1999	8	14	99ZZZX2843       	2	19990405	G	7320	10593921	SERVOMOTOR      			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	2907T	33   			11458	S577				SERVOMOTOR DOES NOT OSCILLATE WHEN SWITCH IS IN ON POSITION.  REF: MCN NR 24.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999081400011	19990814	00011		1999	8	14	99ZZZX2844       	4	19990329	G	3452	066011410101	TRANSPONDER     		KT70        	BOLKMS	BK117 	BK117C1     	5626025	EU  										COCKPIT	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC				11119	7505				SOME SEGMENTS OF DISPLAY WILL NOT LIGHT,  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400012	19990814	00012	EU  	1999	8	14	99ZZZX2845       	1	19990316	G	6710	1174137801	SHAFT           			BOLKMS	BK117 	BK117C1     	5626025	EU  										MAIN ROTOR	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	3698 				7505				THREADED SHAFT WORN.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400013	19990814	00013	EU  	1999	8	14	99ZZZX2846       	1	19990316	G	6710	10513221	DRIVE LINK      			BOLKMS	BK117 	BK117C1     	5626025	EU  										MAIN ROTOR	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	3207 			2909	7505				DRIVE LINK BEARINGS WORN.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400014	19990814	00014	EU  	1999	8	14	99ZZZX2847       	1	19990320	G	7714	117902111	INDICATOR       			BOLKMS	BK117 	BK117C1     	5626025	EU  										TRIPLE TACH	READS HIGH      	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	747  			169	7505				ROTOR RPM READS 870, 10 PERCENT HIGH.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400015	19990814	00015		1999	8	14	99ZZZX2848       	4	19990402	G	2211	7008138903	COMPUTER        			BOLKMS	BK117 	BK117C1     	5626025	EU  										AUTOPILOT	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	3737 			94030235	7505				COMPUTER FLAGGED WITH CONSTANT ERROR CODES 2E5 2E17, AND 2E62.  REF:  NR R019493.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400016	19990814	00016		1999	8	14	99ZZZX2849       	4	19990322	G	2211	7004206901	COMPUTER        			BOLKMS	117   	BK117A4     	5626017	EU  										CSAS	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	117NG	84   			89020224	7083				INTERMITTENT ANNUNCIATOR LIGHT.  REF:  MCN NR 2.						1	G	7	2 	3U				H13EU   					 
1999081400017	19990814	00017		1999	8	14	99ZZZX2850       	4	19990305	G	2210	117986091	RELAY           			BOLKMS	BK117 	BK117C1     	5626025	EU  										AUTOPILOT	WRONG PART      	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC				060	7505				WRONG PART RECEIVED.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400018	19990814	00018		1999	8	14	99ZZZX2851       	4	19990221	G	3425	7002353913	SENSOR          			BOLKMS	BK117 	BK117C1     	5626025	EU  										AIR DATA	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	3617 			89050599	7505				AUTOPILOT TRIM FAILURE.  REF:  RMA NR R018967.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400019	19990814	00019	EU  	1999	8	14	99ZZZX2852       	1	19990227	G	3340	G62504	SEARCH LIGHT    		G62505      	BOLKMS	117   	BK117A3     	5626015	EU  										FUSELAGE	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	1140H	9    			67839	7078				SEARCH LIGHT EXTENDS ONLY OCCASIONALLY.  WILL EXTEND IF LAMP ASSY IF WIGGLED.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999081400020	19990814	00020	SW  	1999	8	14	99ZZZX2853       	1	19990309	G	6730	222382001105	SERVO           			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	BEARING WORN    	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	4UV	538  			0087A	23019				TOP BEARING WORN AND ACTUATOR LEAKING.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400021	19990814	00021	SW  	1999	8	14	99ZZZX2854       	1	19990309	G	6730		ACTUATOR        			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	LEAKING         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	4UV	538  				23019				TOP BEARING WORN AND ACTUATOR LEAKING.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400022	19990814	00022		1999	8	14	99ZZZX2855       	4	19990314	G	3421	06002600	GYRO            			BELL  	230   	230         	1182149	SW  										COCKPIT VG	NOISEY          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	934  			3104	23019				GYRO MAKING A SQUEALING NOISE.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400023	19990814	00023		1999	8	14	99ZZZX2856       	4	19990311	G	2211	117882921	SPAS COMPUTER   			BOLKMS	117   	BK117A1     	5626010	EU  										SPAS	FAILED          	B			TI1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	05	117LF				018803150	7013				COMPUTER FAILED SPAS TEST, PARA 4.2.1.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999081400025	19990814	00025		1999	8	14	99ZZZX2858       	4	19990211	G	3446	78806059008	DISPLAY         			BOLKMS	105   	BO105S      	5626006	EU  										STORMSCOPE	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	911LF	1    			JSD0550235	S663				AFTER STORMSCOPE UNIT USED FOR ONE FLIGHT AND WARMED UP, NEXT FLIGHT, UNIT WILL NOT DISPLAY.  REMOVED AND REPLACED.						1	G	7	2 	3U				H3EU    					 
1999081400026	19990814	00026		1999	8	14	99ZZZX2859       	4	19990308	G	3446	78806059412	COMPUTER        			BOLKMS	105   	BO105S      	5626006	EU  										STORMSCOPE	MALFUNCTION     	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	105NG				JEP06603035	S632				COMPUTER READS ERROR 001 WHEN TURNED ON, THEN READS, OPERATION NO LONGER POSSIBLE.  REMOVED AND REPLACED.						1	G	7	2 	3U				H3EU    					 
1999081400027	19990814	00027		1999	8	14	99ZZZX2860       	4	19990301	G	3425	5203137204	INDICATOR       			BOLKMS	117   	BK117A1     	5626010	EU  										RMI	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	117LF				5575	7013				FLAG ON RMI WILL NOT PULL.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999081400028	19990814	00028	EU  	1999	8	14	99ZZZX2861       	1	19990319	G	3340	G62504	SEARCH LIGHT    			BOLKMS	117   	BK117A3     	5626015	EU  										FUSELAGE	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	1140H	48   			67417	7078				SEARCH LIGHT STUCK IN FULL EXTEND POSITION, WILL NOT RETRACT.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999081400029	19990814	00029		1999	8	14	99ZZZX2862       	4	19990318	G	3421	5040045902	INDICATOR       			BELL  	230   	230         	1182149	SW  										COCKPIT ATTITUDE	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	2204 			1217913	23019				COCKPIT ATTITUDE INDICATOR WILL NOT STAY CAGED.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400030	19990814	00030		1999	8	14	99ZZZX2863       	4	19990224	G	2210	11798609	RELAY           			BOLKMS	BK117 	BK117C1     	5626025	EU  										AUTOPILOT	DAMAGED         	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	3624 				7505				AUTOPILOT TRIM LIGHT IN-FLIGHT.  REF:  RMA NR R019015.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400031	19990814	00031	EU  	1999	8	14	99ZZZX2864       	1	19990212	G	7714	1179405603	INDICATOR       			BOLKMS	117   	BK117A1     	5626010	EU  										ENGINE N1	INTERMITTENT    	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	117M	80   			735	S7023				ENGINE N1 INDICATOR NEEDLE DROPS OFF INTERMITTENTLY.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999081400032	19990814	00032		1999	8	14	99ZZZX2865       	4	19990223	G	3421	060002600	GYRO            		KVG350      	BELL  	230   	230         	1182149	SW  										COCKPIT VG	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	895  			2675	23019				VERTICAL GYRO SLOW TO SPIN UP.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400034	19990814	00034	SW  	1999	8	14	99ZZZX2867       	1	19990212	G	6720	222012715101	LEVER           			BELL  	230   	230         	1182149	SW  										TAIL ROTOR	BEARING WORN    	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	2139 				23019				LEVER BEARINGS WORN.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400035	19990814	00035	EU  	1999	8	14	99ZZZX2868       	1	19990125	G	6720	741C000005	ACTUATOR        			BOLKMS	BK117 	BK117C1     	5626025	EU  										TAIL ROTOR	LEAKING         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	317MC	1816 			00409	7505				ACTUATOR HAD EXCESSIVE LEAKAGE.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400036	19990814	00036	SW  	1999	8	14	99ZZZX2869       	1	19990522	G	6320	206040156101	MAGNETIC SEAL   			BELL  	206   	206L1       	1182107	SW  										TRANSMMISSION	LEAKING         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	721SP	635  			04171810151	45486				MAGNETIC SEAL LEAKING.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999081400037	19990814	00037	EU  	1999	8	14	99ZZZX2870       	1	19990521	G	7930	6607190A	SWITCH          			BOLKMS	105   	BO105LSA3   	5626020	EU  										OIL PRESSURE	INOPERATIVE     	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	8118Y	483  			V03451	2017				OIL PRESSURE SWITCH INOPERATIVE.  REMOVED AND REPLACED.						1	G	7	2 	3U				H3AU    					 
1999081400038	19990814	00038	EU  	1999	8	14	99ZZZX2871       	1	19990604	G	3340	G62504	SEARCH LIGHT    			BOLKMS	117   	BK117B1     	5626012	EU  										FUSELAGE	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	460H	21   			67412	7142				SEARCH LIGHT STAYS ON INTERMITTENTLY AFTER SWITCHED OFF.  REF:  MCN 101.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999081400039	19990814	00039	SW  	1999	8	14	99ZZZX2872       	1	19990531	G	2430	SM20ACD200A21	RELAY           			BELL  	222   	222U        	1182140	SW  										DC SYSTEM	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	219HM	377  			ABI505102	47573				RELAY STAYS PULLED AT ALL TIMES.  REMOVED AND REPLACED.						1	G	7	2 	3U				H9SW    					 
1999081400040	19990814	00040	EU  	1999	8	14	99ZZZX2873       	1	19990407	G	3246	117501031	SKID TUBE       			BOLKMS	BK117 	BK117C1     	5626025	EU  										MLG	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	3749 				7505				SIDE TUBE WORN THROUGH ON AFT ENG.  REF:  RMA NR R019614 MCN 95.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400041	19990814	00041	SW  	1999	8	14	99ZZZX2874       	1	19990519	G	6330	L633M2001105	MOUNT           		ZARIS       	BELL  	230   	230         	1182149	SW  										TRANSMISSION	LEAKING         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	4UV	113  			304	23019				NO GAP.  PISTON RETRACTED AND LEAKED FLUID.  REF:  RMA NR R020125 MCN 93.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400042	19990814	00042		1999	8	14	99ZZZX2875       	4	19990524	G	3421	RCA26BK3	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										COCKPIT ATTITUDE	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	206AZ	73   			7881	51007				GYRO FALLS OFF TO THE LEFT CONTINUALLY AND VERY SLOW TO CAGE.  REF:  MCN NR 84.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999081400043	19990814	00043	EU  	1999	8	14	99ZZZX2876       	1	19990517	G	6420	1053170023	BEARING         			BOLKMS	BK117 	BK117C1     	5626025	EU  										TAIL ROTOR	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	117NC	379  				7509				TAIL ROTOR BEARINGS WORN.  REF:  RMA NR R020377.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400044	19990814	00044		1999	8	14	99ZZZX2877       	4	19990521	G	2312	40001278500	TRANSCEIVER     		RT406F      	BOLKMS	105   	BO105LSA3   	5626020	EU  										COCKPIT	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	911SV	117  			1634	2033				TRANSCEIVER WILL NOT TRANSMIT OR RECEIVE. REF:  MCN 75.  REMOVED AND REPLACED.						1	G	7	2 	3U				H3AU    					 
1999081400045	19990814	00045	SW  	1999	8	14	99ZZZX2878       	1	19990511	G	3320	13AT402T2	SWITCH          			BELL  	230   	230         	1182149	SW  										CABIN	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	2304 				23019				SWITCH WILL NOT TURN LIGHT OFF.  REF:  MCN 71.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400046	19990814	00046	NE  	1999	8	14	99ZZZX2879       	2	19990525	G	7230	410106013	SHROUD          			BELL  	222   	222U        	1182140	SW  	LYC   	LTS101	LTS101750C1 	41560	NE  					IMPELLER	FLAKING         	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	219HM	92   			81J019	47573				COATING FLAKING OFF OF IMPELLER SHROUD PREMATURELY.  REF:  MCN 69.  REMOVED AND REPLACED.						1	G	7	2 	3U	3	U		H9SW    	E5NE				 
1999081400047	19990814	00047		1999	8	14	99ZZZX2880       	4	19990512	G	3421	222375033101	INDICATOR       			BELL  	222   	222         	1182122	SW  										COCKPIT	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	911LW	169  			0077	47520				OFF FLAG ON ATTITUDE INDICATOR PULLS CONTINUALLY DURING OPERATION.  REF:  MCH 68.  REMOVED AND REPLACED.						1	G	7	2 	3U				H9SW    					 
1999081400048	19990814	00048		1999	8	14	99ZZZX2881       	4	19990517	G	3420	5050010902	GYRO            			BELL  	206   	206L3       	1182108	SW  										COCKPIT	PRECESSING      	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	2210H	50   			21122	51006				GYRO PRECESSES.  REF:  MCN 67.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999081400049	19990814	00049		1999	8	14	99ZZZX2882       	4	19990428	G	2312	0502006	ANTENNA         			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	BROKEN          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	39112	102  				45652				FOUND ANTENNA BROKEN APPROXIMATELY 3 INCHES ABOVE BASE.  REF:  MCN 66.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999081400050	19990814	00050	EU  	1999	8	14	99ZZZX2883       	1	19990402	G	6321	20100	RELIEF VALVE    			BOLKMS	117   	BK117B1     	5626012	EU  										ROTOR BRAKE	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	117LU	8    			7145	7144				ROTOR BRAKE WILL NOT BUILD UP ANY PRESSURE.  REF:  RMA R020183 MCN 64.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999081400051	19990814	00051	EU  	1999	8	14	99ZZZX2884       	1	19990428	G	7714	1179405603	INDICATOR       			BOLKMS	117   	BK117A3     	5626015	EU  										N1 RPM	FLUCTUATES      	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	117CH	10   			191	7061				NG INDICATOR FLUCTUATES.  REF:  MCN 63.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999081400052	19990814	00052		1999	8	14	99ZZZX2885       	4	19990423	G	3452	066011410101	TRANSPONDER     		KT70        	BOLKMS	BK117 	BK117C1     	5626025	EU  										COCKPIT	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	30   			13736	7505				TRANSPONDER UNIT POWERS DOWN BY ITSELF AND REPOWERS UP.  REF:  RMA NR R019742 AND MCN 62.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400053	19990814	00053		1999	8	14	99ZZZX2886       	4	19990421	G	3425	7002353913	SENSOR          			BOLKMS	BK117 	BK117C1     	5626025	EU  										AIR DATA	CAN'T CALIBRATE 	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	169  			94030974	7505				CANNOT CALIBRATE JAS.  REF:  RMA NR R019743 MCN 57.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400054	19990814	00054	EU  	1999	8	14	99ZZZX2887       	1	19990504	G	2841	1179405403	INDICATOR       			BOLKMS	BK117 	BK117C1     	5626025	EU  										FUEL QUANTITY	INTERMITENT     	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	3829 			1157	7505				FUEL QUANTITY INDICATOR DROPS 'ON' AND 'OFF' LINE INTERMITTENTLY.  REF:  RMA NR R019924 MCN 56.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400055	19990814	00055	NE  	1999	8	14	99ZZZX2888       	2	19990422	G	7412	130036303	IGNITER         			BOLKMS	117   	BK117A3     	5626015	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					ENGINE	INOPERATIVE     	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	117MH	234  			97341602	7112				NO POWER OUTPUT TO IGNITERS.  EF:  MCN 55.  REMOVED AND REPLACED.						1	G	7	2 	3U	3	U		H13EU   	E5NE				 
1999081400056	19990814	00056	GL  	1999	8	14	99ZZZX2889       	2	19990421	G	7320	222360703101	SOLENOID        			BELL  	230   	230         	1182149	SW  	ALLSN 	250C  	250C30      	03013	GL  					ENGINE	INTERMITTENT    	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	789  			819	23019				SOLENOID OPERATES INTERMITTENTLY.  REF:  MCN 53.  REMOVED AND REPLACED.						1	G	7	2 	3U	3	U	NC	H9SW    	E1GL				 
1999081400057	19990814	00057	SW  	1999	8	14	99ZZZX2890       	1	19990430	G	7931	222060096103	SWITCH          			BELL  	230   	230         	1182149	SW  										COCKPIT	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	2287 				23019				WARNING LIGHT WOULD NOT GO OUT.  REF:  MCN 52.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400058	19990814	00058	SW  	1999	8	14	99ZZZX2891       	1	19990419	G	6720	230312001101	PITCH LINK      			BELL  	230   	230         	1182149	SW  										TAIL ROTOR	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	356  				23019				PITCH LINK HAS WORN BEARINGS.  REF:  MCN 51.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400059	19990814	00059	SW  	1999	8	14	99ZZZX2892       	1	19990419	G	6720	230312001101	PITCH LINK      			BELL  	230   	230         	1182149	SW  										TAIL ROTOR	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	356  				23019				PITCH LINK HAS WORN BEARINGS.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400060	19990814	00060		1999	8	14	99ZZZX2893       	4	19990430	G	3421	060002600	GYRO            			BELL  	230   	230         	1182149	SW  										COCKPIT VG	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	88   			2748	23019				GYRO SLOW TO COME UP AND EADI DISPLAY ATTITUDE FAIL LIGHT.  REF:  MCN 50.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400234	19990814	00234		1999	8	14	99ZZZX2895       	4	19990602	G	3421	4021541772	INDICATOR       			BELL  	222   	222U        	1182140	SW  										COCKPIT	PRECESSING      	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	222HX	248  			86111457	47533				ADI PRECESSING TO THE RIGHT 5 DEGREES CONSTANTLY.  REF:  MCN NR 81.  REMOVED AND REPLACED.						1	G	7	2 	3U				H9SW    					 
1999081400235	19990814	00235	EU  	1999	8	14	99ZZZX2896       	1	19990407	G	3340	G83857	SEARCH LIGHT    			BOLKMS	BK117 	BK117C1     	5626025	EU  										FUSELAGE	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	71   			1265130	7505				RELAY STICKS.  REF MCN NR 49.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400236	19990814	00236		1999	8	14	99ZZZX2897       	4	19990416	G	3425	066031231500	INDICATOR       			BELL  	230   	230         	1182149	SW  										COCKPIT HSI	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	314  			1723	23019				DARK SPOTS ON UPPER TWO CORNERS OF SCREEN.  REF:  MCN NR 45.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400237	19990814	00237	EU  	1999	8	14	99ZZZX2898       	1	19990429	G	2150	JBS8803	MIXING VALVE    			BOLKMS	105   	BO105LSA3   	5626020	EU  										HEATER	INPERATIVE      	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	911SV	14   			031	2033				VALVE WILL NOT OPEN.  REF:  RMA NR R019843 (MCN 44).  REMOVED AND REPLACED.						1	G	7	2 	3U				H3AU    					 
1999081400238	19990814	00238	EU  	1999	8	14	99ZZZX2899       	1	19990423	G	2150	JBS8803	MIXING VALVE    			BOLKMS	105   	BO105LSA3   	5626020	EU  										HEATER	INOPERATIVE     	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	911SV	71   			035	2033				MIXING VALVE WILL NOT OPERATE.  REF:  RMA NR R019777 (MCN 43).  REMOVED AND REPLACED.						1	G	7	2 	3U				H3AU    					 
1999081400239	19990814	00239	EU  	1999	8	14	99ZZZX2900       	1	19990418	G	7931	1179405807	INDICATOR       			BOLKMS	117   	BK117B2     	5626013	EU  										ENGINE OIL	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	117MK	4    			82120056	7196				OIL PRESSURE DROPPED TO ZERO.  REF:  MCN 39.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999081400240	19990814	00240	SW  	1999	8	14	99ZZZX2901       	1	19990401	G	2910	AE7013131J0134	HOSE            			BELL  	230   	230         	1182149	SW  										HYDRAULIC SYSTEM	LEAKING         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	4UV	2236 				23019				HOSE LEAKING.  REF:  MCN 37.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999081400344	19990814	00344		1999	8	14	99ZZZX2902       	4	19990329	G	3423	C2300DL4B	COMPASS         																	COCKPIT	LEAKING         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05					A6810					COMPASS FOUND TO BE LEAKING UPON RECEIPT.  HALF OF FLUID GONE.  REMOVED AND REPLACED.																			 
1999081400345	19990814	00345		1999	8	14	99ZZZX2903       	1	19990302	G	6220	1054190426	BOLT            																	MAIN ROTOR	MISMANUFACTURED 	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05					662					BOLT MACHINED INCORRECTLY.  WILL NOT FIT THROUGH LOWER BEARING AND BUSHING ON SWASHPLATE.  REMOVED AND REPLACED.																			 
1999081400346	19990814	00346		1999	8	14	99ZZZX2904       	1	19990128	G	7922	S3E1960	THERMO VALVE    																	ENGINE	DAMAGED         	B			NQ2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	05		1500 			32779					THERMOSTAT VERY NEAR FAILING WITH POSSIBLE SEVERE ENGINE DAMAGE RESULTING.  SEAT RETAINING NUT VERY LOOSE ON STEM.  NUT 	WAS 'JUMPED' 2 THREADS.  THIS PART NUMBER AND SERIAL NUMBER SUBJECT TO LYC BULLETIN SIBC AND SI'S 1, 2, AND 3.  SUBMITTE	R STATED THIS INSPECTION AND REWORK HAD NOT BEEN COMPLIED WITH.																	 
1999081400347	19990814	00347		1999	8	14	99ZZZX2905       	4	19990727	G	2297		WIRE            	HONEYWELL   	SH2222      	BELL  	222   	222         	1182122	SW  										AUTOPILOT	DAMAGED         	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	222TY					47081				PILOT REPORTED NO ALTITUDE FUNCTIONS ON AUTOPILOT.  TROUBLESHOOTING REVEALED SEVERAL KAPTON WIRES DISSOLVED UNDER FUEL P	UMP AND VENT.  REPLACED WIRES AND TESTED GOOD.  MAY CAUSE FIRE IF UNDETECTED.  SUBMITTER RECOMMENDED INSPECTING WIRE BUN	DLE FOR ANY DAMAGED WIRES DUE TO FUEL LEAKS.				1	G	7	2 	3U			 	H9SW    					 
1999081400348	19990814	00348	EA  	1999	8	14	99ZZZX2906       	2	19990708	G	7414	ES10361631	POINTS          	BENDIX      	S4LN204     	ROBSIN	R22   	R22BETA     		NM  	LYC   	O320  	O320B2C     	41508	EA  					MAGNETO	MISOVERHAULED   	H		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	09	461H				8137034	1460	L806039A			RECEIVED ENGINE FROM VAN BORTEL AIR POWER, LYC FACTORY OVERHAUL.  INSTALLED ENGINE IN HELICOPTER.  ON GROUND RUN, NO ENG	INE RPM INDICATION.  REMOVED RIGHT (ENGINE SIDE) MAGNETO.  FOUND TACH POINTS ASSEMBLED WRONG.					1	G	7	1 	3O	3	O		H10WE   	E274				 
1999082100051	19990821	00051	WP  	1999	8	21	99ZZZX2908       	2	19990721	G	7230	30740966	TURBINE WHEEL   								GARRTT	TFE731	TFE7313     	01518	WP  					COMPRESSOR	WORN            	B			XR1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09		1224 			3121721531		80250			THIRD STAGE LP TURBINE RUBBED AFT SIDE OF 3RD STAGE LPT STATOR SEAL.  ENGINE TSN:  5,402.6 HOURS.  CSN:  3,565.  PART TC	:  1,057.										4	F			E6WE				 
1999082100052	19990821	00052	WP  	1999	8	21	99ZZZX2909       	2	19990721	G	7230		STATOR          								GARRTT	TFE731	TFE7313     	01518	WP  					COMPRESSOR	WORN            	B			XR1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09		1224 					80250			THIRD STAGE LP TURBINE RUBBED AFT SIDE OF 3RD STAGE LPT STATOR SEAL.  ENGINE TSN:  5,402.6 HOURS.  CSN:  3,565.  PART TC	:  1,057.										4	F			E6WE				 
1999081400349	19990814	00349	CE  	1999	8	14	99ZZZX2910       	1	19990722	G	2752	5052119510	PISTON          		505212233   	BEECH 	200   	B200        	1152922	CE  										FLAP ACTUATOR	CRACKED         	E				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03	87JE	6243 				BE27				INSPECTION OF FLAP SYSTEM REVEALED DEFECTIVE LEFT OUTBOARD FLAP ACTUATOR DRIVE PISTON. DRIVE PISTON FOUND CRACKED AT FLA	P ROD END EXTENDING 1.5 INCHES LONGITUDINALLY, FORWARD WITH RESPECT TO AIRCRAFT INSTALLATION.					1	L	7	2 	4T				A24CE   					 
1999081400350	19990814	00350	EU  	1999	8	14	99ZZZX2911       	1	19990712	G	7330	59052444	INDICATOR       			ISRAEL	1125  	ASTRASPX    	4500205	EU  	GARRTT	TFE731	TFE7314R    	01518	WP  					COCKPIT	MALFUNCTIONED   	B			QRRR	O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			EA	13	275RA	656  			0443	098	113145			PILOTS OBSERVED A 'FUEL FILTER BYPASS' INDICATION.  FUEL FILTERS WERE CHANGED.  INDICATION WAS STILL THERE.  CHANGED LEF	T ENGINE FUEL DIFFERENTIAL PRESSURE INDICATOR.  PROBLEM FIXED.					2	L	7	2 	4F	4	F	RT	A16NM   	E6WE				 
1999081400351	19990814	00351	NM  	1999	8	14	99ZZZX2912       	1	19990618	G	5347		SEAT TRACK      			BOEING	727   	727251      	138408H	NM  										BS 1070-1130	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK BS 1070- BS 1130 LBL 48 AND LBL 25.						2	L	7	3 	4F				A3WE    					 
1999081400352	19990814	00352	NM  	1999	8	14	99ZZZX2913       	1	19990618	G	5347		SEAT TRACK      			BOEING	727   	727251      	138408H	NM  										BS 344-460	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK RT CENTER BS 344 - BS 460.  (ALSO ON LT INBOARD).						2	L	7	3 	4F				A3WE    					 
1999081400353	19990814	00353	NM  	1999	8	14	99ZZZX2914       	1	19990618	G	5320		WEB             			BOEING	727   	727251      	138408H	NM  										BS 1176	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON SHEAR WEB UNDER BS 1176 CHORD LBL 25 - RBL 25.						2	L	7	3 	4F				A3WE    					 
1999081400354	19990814	00354	NM  	1999	8	14	99ZZZX2915       	1	19990618	G	5315		FLOORBEAM       			BOEING	727   	727251      	138408H	NM  										BS 344	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM FS 344, LBL 24 OUTBOARD.						2	L	7	3 	4F				A3WE    					 
1999081400355	19990814	00355	NM  	1999	8	14	99ZZZX2916       	1	19990618	G	5320		CHANNEL         			BOEING	727   	727251      	138408H	NM  										FUSELAGE	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON FORWARD LAVATORY HAT CHANNEL.						2	L	7	3 	4F				A3WE    					 
1999081400356	19990814	00356	NM  	1999	8	14	99ZZZX2917       	1	19990618	G	5311		FRAME           			BOEING	727   	727251      	138408H	NM  										BS 1166	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT BS 1166 OUTBOARD OF MOP SILL AT FLOOR LEVEL.						2	L	7	3 	4F				A3WE    					 
1999081400357	19990814	00357		1999	8	14	99ZZZX2918       	4	19990618	G	3455	5221837000	ANTENNA         			BOEING	727   	727256      	1384062	NM  										ADF	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG				4372	22606				DURING A C-CHECK, CORROSION WAS NOTED ON ALL 4 SIDES OF ANTENNA (ADF).						2	L	7	3 	4F			RT	A3WE    					 
1999081400358	19990814	00358	NM  	1999	8	14	99ZZZX2919       	1	19990618	G	5347		SEAT TRACK      			BOEING	727   	727256      		NM  										BS 1070	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON RIGHT INBOARD SEAT TRACK, BS 1070.						2	L	7	3 	4F				A3WE    					 
1999081400359	19990814	00359	NM  	1999	8	14	99ZZZX2920       	1	19990618	G	5347		SEAT TRACK      			BOEING	727   	727256      		NM  										BS 460	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON RIGHT INBOARD SEAT TRACK FORWARD OF BS 460.						2	L	7	3 	4F				A3WE    					 
1999081400360	19990814	00360	NM  	1999	8	14	99ZZZX2921       	1	19990618	G	5711		SPAR            			BOEING	727   	727256      		NM  										WS 400 & 422	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	910PG					22606				DURING A C-CHECK, CORROSION WAS NOTED ON LEFT WING FRONT SPAR LOWER CHORD PLATE AT WS 400 AND WS 422.						2	L	7	3 	4F				A3WE    					 
1999081400361	19990814	00361	NM  	1999	8	14	99ZZZX2922       	1	19990618	G	5311		FRAME           			BOEING	727   	727230      	1384080	NM  										BS 1090	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT BS 1090 BETWEEN STR 28 AND STR 29R.						2	L	7	3 	4F				A3WE    					 
1999081400362	19990814	00362	NM  	1999	8	14	99ZZZX2923       	1	19990618	G	5313		STRINGER        			BOEING	727   	727230      	1384080	NM  										BS 1090	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON STR 29R, BS 1090.						2	L	7	3 	4F				A3WE    					 
1999081400363	19990814	00363	SO  	1999	8	14	99ZZZX2924       	1	19990712	G	5312	1156	BULKHEAD        			LUSCOM	8     	8F          	8190114	SO  										FUSELAGE	CRACKED         	B			FE4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	2129B	2772 				6556				DURING AN ANNUAL INSPECTION, FOUND MAIN BULKHEAD P/N 1156 CRACKED IN THE WING STRUT AREA.  CAUSE UNKNOWN.						1	H	7	1 	3O				A694    					 
1999081400364	19990814	00364	SW  	1999	8	14	99ZZZX2925       	1	19990721	G	3213	54001503	TRUSS           			MOONEY	M20   	M20J        	5870219	SW  										NLG	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05		3164 								CURING NLG INSPECTION, FOUND STEERING TRUSS BOLT HOLES ELONGATED WHERE OVERCENTER LINK BOLTS ONTO TRUSS; MFG SPECS FOR A	LLOWABLE WEAR AT THIS LOCATION IS .375 INCH - .379 INCH.  MEASURED WEAR WAS .392 INCH.  REPLACED TRUSS WITH SERVICEABLE 	UNIT.  SUSPECT WEAR WAS FROM THE BOLT BEING LOOSE.				1	L	7	1 	3O				2A3     					 
1999081400365	19990814	00365	EA  	1999	8	14	99ZZZX2926       	2	19990712	G	7414	M3333	IMPULSE COUPLING	SLICK       	6351        	BNORM 	BN2   	BN2A26      	1520226	EU  	LYC   	O540  	O540E4C5    	41532	EA  					MAGNETO	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	999SA	993  				897				DURING INSPECTION OF MAGNETO AND IMPULSE COUPLING, FOUND ONE OF THE PAWL PINS WAS WORKING LOOSE FROM IMPULSE BODY.  ALL 	OTHER WEAR APPEARED NORMAL.  IMPULSE HAD BEEN INSPECTED 190 HOURS PRIOR AND HAD BEEN FOUND TO BE NORMAL.					1	H	7	2 	3O	3	O		A17EU   	E295				 
1999081400366	19990814	00366	CE  	1999	8	14	99ZZZX2927       	1	19990703	G	3246		SKI             			CESSNA	185   	185         	2072802	CE  										TAIL	BROKE           	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	9890X	300  				1850090				FRONT EYE BOLT ATTACH BROKE AT FRONT SHOCK ABSORBER CAUSING SKI TO PITCH FORWARD DIGGING INTO SNOW.						1	H	7	1 	3O			NC	3A24    					 
1999081400367	19990814	00367	EA  	1999	8	14	99ZZZX2928       	2	19990624	G	7414	M3333	IMPULSE COUPLING	SLICK       	6531        	PIPER 	PA32  	PA32301     	7103207	SO  	LYC   	O540  	IO540K1G5   	41532	EA  					MAGNETO	FAILED          	E				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	8216T	305  				328206037				DURING 100-HOUR INPSECTION OF MAGNETO, IMPULSE WAS FOUND TO BE NEAR TOTAL FAILURE.  BOTH PAWL PINS WERE LOOSE IN BODY OF	 IMPULSE WITH ONE NEARLY READY TO PULL FREE.  THIS ASSY HAD BEEN INSPECTED 98 HOURS PRIOR AND FOUND TO HAVE NORMAL WEAR.					1	L	7	1 	3O	3	O		A3SO    	1E4				 
1999081400368	19990814	00368	EA  	1999	8	14	99ZZZX2929       	2	19990708	G	8530	CLASS12	CYLINDER        			CESSNA	172   	172N        	2072434	CE  	LYC   	O360  	O360A4A     	41514	EA  					ENGINE	CRACKED         	B			ZKGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	05	737YS		1039 			17269783	L1403736A			THIS NR 4 CYLINDER WAS REMOVED BECAUSE OF A  VERY LARGE CRACK AROUND THE TOP OF THE HEAD.  THIS AND 2 OTHER CYLINDERS WE	RE REMOVED AND REPAIRED AT 183.0 TSO BECAUSE OF LOOSE VALVE GUIDES AND SEAL TROUBLES.  NOW HAS 1,038.9 TSO HOURS AND A C	RACKED HEAD.				1	H	7	1 	3O	3	O	NT	3A12    	E286				 
1999081400369	19990814	00369		1999	8	14	99ZZZX2930       	4	19990601	G	3457	MD4065L	INDICATOR       			PIPER 	PA24  	PA24        	7102402	SO  										COCKPIT	MALFUNCTIONED   	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	5117P				3648	24130				FOUND BLACK AND WHITE LIGHTING WIRES SHORTED TOGETHER.  THIS OCCURRED AT THE BASE OF THE LIGHTING BAR, A POSITION THAT T	HE MANUFACTURER WOULD HAVE ASSEMBLED AT THE FACTORY.  THESE UNITS HAVE OPTIONAL LIGHTING CAPABILITIES. THE SHORT OCCURRE	D ON THE ASSEMBLY THAT CONNECTED THESE WIRES TO THE LIGHTS.				1	L	7	1 	3O				1A15    					 
1999081400370	19990814	00370	SO  	1999	8	14	99ZZZX2931       	1	19990722	G	3233	455987	ACTUATOR        			PIPER 	PA32  	PA32R301T   	7103220	SO  										NLG	LEAKING         	B			AMYR	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			CE	05	4134D	143  			1574	3257070				MALFUNCTION OCCURRED IN-FLIGHT.  PILOT REPORTED HYDRAULIC PUMP IN-FLIGHT.  TROUBLESHOT PROBLEM IN SHOP.  DETERMINED NOSE	 GEAR ACTUATOR WAS LEAKING INTERNALLY AND SUCKING IN AIR, AND LT MAIN GEAR ACTUATOR WAS LEAKING WHICH CAUSED PUMP TO CON	TINUALLY CYCLE AND FAIL CAUSING GEAR TO FREE FALL DOWN AND LOCKED.				1	L	7	1 	3O				A3SO    					 
1999081400371	19990814	00371	EA  	1999	8	14	99ZZZX2932       	2	19990624	G	8520	20736	PISTON          			MAULE 	M4    	M4220C      	5460114	SO  	FRNKLN	6AV350	6A350C1A    	27043	EA  					ENGINE	FAILED          	G				A				UNSCHED LANDING         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CL	CLIMB          	1			AL	03	40677	1046 				2181C	2611100014			APPROXIMATELY 15 MINUTES AFTER TAKEOFF, THE NR 4 PISTON SEPARATED FROM ITS CONNECTING ROD.  THIS CAUSED THE NR 4 CYLINDE	R TO FRACTURE RESULTING IN A COMPLETE LOSS OF OIL.  THE ENGINE STALLED FORCING AN EMERGENCY LANDING ON A RIVER BANK.  UP	ON LANDING, THE LEFT MAIN GEAR COLLAPSED WHICH FORCED THE AIRCRAFT INTO TREES LINING THE BANK.  AIRCRAFT SUFFERED SUBSTA	NTIAL DAMAGE.  PILOT WAS UNINJURED.			1	H	7	1 	3O	3	O		3A23    	E9EA				 
1999081400372	19990814	00372	CE  	1999	8	14	99ZZZX2933       	1	19990709	G	7120	56541111	BRACKET         			CESSNA	402   	402C        	207590R	CE  										ENGINE MOUNT	WRINKLED        	B			FE4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	402QA	4459 				402C0338				DURING A ROUTINE INSPECTION, MECHANIC FOUND THAT MOUNT BRACKET P/N'S 5654111-1 AND 5654111-2 WERE WRINKLED.  MOUNT ASSEM	BLY WAS DISASSEMBLED AND INSPECTED.  NO OTHER DAMAGE WAS FOUND.  DAMAGE CAUSE UNKNOWN.					1	L	7	2 	3O				A7CE    					 
1999081400373	19990814	00373	EA  	1999	8	14	99ZZZX2934       	2	19990719	G	8530		CYLINDER        			PIPER 	PA28  	PA28181     	7102807	SO  	LYC   	O360  	O360A4A     	41514	EA  					ENGINE	BURNED          	H				A				UNSCHED LANDING         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		NR	NOT REPORTED   	1			AL	05	2937X	1565 				287990567	L3050336A			PILOT REPORTED ROUGH ENGINE AND LOSS OF POWER AND BEING UNABLE TO CLIMB TO A SAFE ALTITUDE.  OPTED TO MAKE PRECAUTIONARY	 LANDING ON BEACH.  AIRCRAFT UNDAMAGED.  UPON INSPECTION, NR 3 CYLINDER HAD NO COMPRESSION.  SUBMITTER REMOVED CYLINDER 	AND FOUND A HOLE BURNED THROUGH CYLINDER HEAD BETWEEN THE SPARK PLUG AND THE EXHAUST VALVE.  UPON FURTHER EXAMINATION, N	OTED THE INTAKE TUBE WAS LOOSE IN THE SUMP HOUSING.			1	L	7	1 	3O	3	O		2A13    	E286				 
1999081400374	19990814	00374	CE  	1999	8	14	99ZZZX2935       	1	19990702	G	2120	05150892	BRACKET         			CESSNA	172   	172R        	2072401	CE  										AIR DISTRIBUTION	MISINSTALLED    	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15										WHILE C/W SB 99-21-01, FOUND NEW OUTLET DUCT P/N 0515089-2 HAD ATTACH BRACKETS INSTALLED. APPROXIMATELY 3 INCHES TOO FAR	 OUTBOARD PREVENTING DUCT FROM PROPERLY ENGAGING P/N 0522200-1 FITTING.					1	H	7	1 	3O			NT	3A12    					 
1999081400375	19990814	00375	EA  	1999	8	14	99ZZZX2936       	2	19990720	G	7324	63B22623	FLOW DIVIDER    			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE	STICKING        	B				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			CL	CLIMB          	1			SW	99	9559D	280  			0142845	17280488	L2757151A			FLOW DIVIDER STUCK AND WOULD NOT FULLY OPEN.  THIS HAPPENED ON TAKEOFF AT 700 - 800 FEET WHICH RESULTED IN A 1,100 - 1,2	00 RPM LOSS AND ENGINE SPUTTERED FOR ABOUT 10 SECONDS.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999082100053	19990821	00053	EA  	1999	8	21	99ZZZX2937       	2	19990720	G	7324	63B22623	FLOW DIVIDER    			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE	STICKING        	B				C				ABORTED TAKEOFF         				R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			SO	16	456ER	876  			0153134	17280667	L2787051A			FLOW DIVIDER STUCK AND WOULD NOT FULLY OPEN.  THIS HAPPENED ON TAKEOFF WHICH RESULTED IN A 1,000 RPM LOSS FOR ABOUT 3-4 	SECONDS.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999081400376	19990814	00376		1999	8	14	99ZZZX2938       	4	19990714	G	2561		ACTUATOR        	SWITLIK     	AV8A        															LIFE VEST	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07					841948					ACTUATOR SEVERELY RUSTED.  DATE OF MFG:  AUG 1984.																			 
1999081400377	19990814	00377	EA  	1999	8	14	99ZZZX2939       	2	19990617	G	7324	63B22623	FLOW DIVIDER    			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE	STICKING        	B				O				OTHER                   				R	Y		PARTIAL RPM/PWR LOSS      	ENGINE STOPPAGE           		NR	NOT REPORTED   	1			SO	16	434ER	116  			0146137	17280655	L2784651A			FLOW DIVIDER STUCK AND WOULD NOT FULLY OPEN.  THIS HAPPENED WHILE IN SLOW FLIGHT.  ENGINE SHUT OFF FOR ABOUT 10 - 15 SEC	ONDS.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999081400378	19990814	00378	CE  	1999	8	14	99ZZZX2940       	1	19990721	G	7931	S32791	CONNECTOR       			CESSNA	172   	172S        	2072439	CE  										COCKPIT	LOOSE           	D				A				UNSCHED LANDING         				N			FALSE WARNING             			NR	NOT REPORTED   	1			NM	03	494SP	294  				172S8035				NEW C-172S ON CROSS-COUNTRY FLIGHT, OIL PRESSURE STARTED FLUCTUATING.  OIL TEMP NORMAL AND NO LOW OIL PRESSURE LIGHT ILL	UMINATION.  OIL PRESSURE GAUGE STARTED FLUCTUATING OFF SCALE LOW.  PRECAUTIONARY LANDING MADE.  MAINTENANCE FOUND OIL PR	ESSURE GAUGE CONNECTOR PLUGGED INTO GAUGE, BUT NOT LOCKED OVER LOCKING TAB.  RE-CONNECTED AND OPERATIONAL CHECKED SATISF	ACTORY.			1	H	7	1 	3O			NT	3A12    					 
1999081400379	19990814	00379	CE  	1999	8	14	99ZZZX2941       	1	19990723	G	7160		GASKET          	BRACKETT    	BA8110      	CESSNA	182   	182H        	2072718	CE  										ENGINE COWL	DETERIORATED    	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	14	69995	2741 				18256289				REMOVED FILTER ASSY, P/N BA 8110, TO CHECK GASKET, 8 INCHES OF GASKET WAS MISSING.  SCREEN MESH COMING LOOSE FROM FILTER	 FRAME.					1	H	7	1 	3O			NT	3A13    					 
1999081400380	19990814	00380	CE  	1999	8	14	99ZZZX2942       	1	19990721	G	5312	05530313	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										FUSELAGE	CRACKED         	D	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	2663X	395  				17280643				DURING 100-HOUR INSPECTION, FOUND FIREWALL CRACKED AT LEFT LOWER COWLING SHOCK MOUNT BRACKET ADJACENT TO BATTERY BOX.  C	RACKS EXTENDED VERTICALLY FROM BRACKET ATTACH RIVET HOLES AND TOTALLED APPROXIMATELY 2.3750 INCHES IN LENGTH.  DOUBLER P	ATCH WAS INSTALLED ON INSIDE OF FIREWALL.				1	H	7	1 	3O			NT	3A12    					 
1999081400381	19990814	00381	GL  	1999	8	14	99ZZZX2943       	1	19990701	G	2421	ALX8421	ALTERNATOR      			ENSTRM	F28   	280C        	3300505	GL  										ENGINE	MISINSTALLED    	D				O				OTHER                   				W	K		INADEQUATE Q C            	FLUID LOSS                		NR	NOT REPORTED   	1			EA	25	5691W					1176				ALTERNATOR WAS INSTALLED ON THE AIRCRAFT WITHOUT REMOVING THE COOLING FAN FROM THE ALTERNATOR PER THE ENSTROM MM.  FAN T	HREW A BLADE WHICH PUNCTURED THE OIL COOLER CAUSING LOSS OF ENGINE OIL.  SUBMITTER SUGGESTED BULLETINS CALLING FOR INSPE	CTION OF INSTALLING OF COOLING FAN AND REMOVAL IF FOUND INSTALLED.  THIS PERTAINS TO ALL PISTON ENGINE MODEL ENSTROM HEL	ICOPTERS.			1	G	7	1 	3O				H1CE    					 
1999081400382	19990814	00382	GL  	1999	8	14	99ZZZX2944       	1	19990701	G	7921		OIL COOLER      			ENSTRM	F28   	280C        	3300505	GL  										ENGINE	DAMAGED         	D				O				OTHER                   				W	K		INADEQUATE Q C            	FLUID LOSS                		NR	NOT REPORTED   	1			EA	25	5691W					1176				ALTERNATOR WAS INSTALLED ON THE AIRCRAFT WITHOUT REMOVING THE COOLING FAN FROM THE ALTERNATOR PER THE ENSTROM MM.  FAN T	HREW A BLADE WHICH PUNCTURED THE OIL COOLER CAUSING LOSS OF ENGINE OIL.  SUBMITTER SUGGESTED BULLETINS CALLING FOR INSPE	CTION OF INSTALLING OF COOLING FAN AND REMOVAL IF FOUND INSTALLED.  THIS PERTAINS TO ALL PISTON ENGINE MODEL ENSTROM HEL	ICOPTERS.			1	G	7	1 	3O				H1CE    					 
1999081400383	19990814	00383	CE  	1999	8	14	99ZZZX2946       	1	19990706	G	3230	030A3876012	GEAR BOX        			MTSBSI	MU2   	MU2B36A     	5780413	CE  										RT MLG	BROKEN          	B			HMNR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	3UN	9151 			720	720SA				DURING MAINTENANCE INSPECTION, FOUND TOP AFT HOUSING FLANGE BROKEN ON RIGHT HAND MAIN LANDING GEAR THRUST GEAR BOX.  FAA	 INSP NOTE:  THIS PART HAS A S/B FOR LOOSE MOUNTING BOLTS.  A VISUAL INSPECTION CONDUCTED BY FAA SHOWS THAT THIS FLANGE 	HAD BEEN CRACKED FOR QUITE A WHILE AND WAS DISCOVERED BECAUSE OF A DAMAGED TIRE INCIDENT.				1	H	7	2 	3T				A10SW   					 
1999081400384	19990814	00384	NM  	1999	8	14	99ZZZX2947       	1	19990802	G	3234		HANDLE          			DOUG  	MD11  	MD11        	3023602	NM  										COCKPIT	MALFUNCTIONED   	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	489GX					48458				GEAR CONTROL HANDLE CANNOT MOVE TO UP POSITION AFTER AIRBORNE.  PERFORMED LANDING GEAR CONTROL CABLES TENSION CHECK AND 	RIGGING IAW AMM 32-31-00.  PERFORMED NOSE GEAR GROUND SENSING CONTROL CABLES TENSION CHECK AND RIGGING IAW AMM 32-50-00.	  PERFORMED LANDING GEAR OPERATIONAL TEST CONDITION NML.  REF:  CI-061.				2	L	7	3 	4F			RT	A22WE   					 
1999081400385	19990814	00385	NE  	1999	8	14	99ZZZX2948       	2	19990728	G	7230	772568QQ	BOLT            								PWA   	JT8   	JT8D15A     	52051	NE  					COMPRESSOR	MISMANUFACTURED 	B		A	WG4R	O				OTHER                   				W	C		INADEQUATE Q C            	F.O.D.                    		NR	NOT REPORTED   	1			SO	19							702904			PMA BOLT P/N 772568 QQ, REPLACEMENT FOR OEM BOLT P/N 772568, FAILED AFTER 7 HOURS AND 6 CYCLES IN SERVICE BOLT FRACTURED	 CAUSING HEAD TO BE INGESTED INTO THE N-2 COMPRESSOR DRIVE TURBINE WHERE EXTENSIVE DAMAGE WAS INFLICTED.  LABORATORY ANA	LYSIS HAVE REVEALED THE LACK OF NICKLE HAD CAUSED CADMIUM INBRITTLEMENT.  SUBMITTER RECOMMENDED REMOVING AND REPLACING A	LL PMA BOLTS P/N 772568QQ FROM BATCH NR'S 30246 AND 30248 FROM SERVICE WITH LESS THAN 300 HOURS/CYCLES AT OPERATOR'S EAR	LIEST CONVENIENCE.							4	F			E2EA				 
1999081400386	19990814	00386	NE  	1999	8	14	99ZZZX2949       	2	19990728	G	7230	772568QQ	BOLT            								PWA   	JT8   	JT8D9A      	52048	NE  					COMPRESSOR	MISMANUFACTURED 	B		A	WG4R	O				OTHER                   				C	W		F.O.D.                    	INADEQUATE Q C            		NR	NOT REPORTED   	1			SO	19							666726			PMA BOLT, P/N 772568 QQ, REPLACMENT FOR OEM BOLT P/N 772568 FAILED AFTER 176 HOURS AND 283 CYCLES IN SERVICE.  BOLT FRAC	TURED CAUSING THE HEAD TO BE INGESTED INTO THE N-2 COMPRESSOR DRIVE TURBINE WHERE EXTENSIVE DAMAGE WAS INFLICTED.  LABOR	ATORY ANALYSIS HAS REVEALED THE LACK OF NICKLE HAD CAUSED CADMIUM INBRITTLEMENT.  SUBMITTER RECOMMENDED REMOVING ALL BOL	TS FROM PMA BATCH NR'S 30246 AND 30248 FROM SERVICE WITH LESS THAN 200 HOURS AND 300 CYLCES AT THE OPERATOR'S EARLIEST C	ONVENIENCE.							4	F			E2EA				 
1999081400387	19990814	00387	NE  	1999	8	14	99ZZZX2950       	2	19990728	G	7230	772568QQ	BOLT            								PWA   	JT8   	JT8D7B      	52053	NE  					COMPRESSOR	MISMANUFACTURED 	B		A	WG4R	O				OTHER                   				W	C		INADEQUATE Q C            	F.O.D.                    		NR	NOT REPORTED   	1			SO	19							657135			PMA BOLT, P/N 772568 QQ, REPLACMENT FOR OEM BOLT P/N 772568, FAILED AFTER ZERO HOURS AND ZERO CYCLES IN SERVICE.  BOLT F	RACTURED CAUSING HEAD TO BE INGESTED INTO THE N-2 COMPRESSOR DRIVE TURBINE WHERE EXTENSIVE DAMAGE WAS INFLICTED.  LABORA	TORY ANALYSIS HAS REVEALED THE LACK OF NICKEL HAD CAUSED CADMIUM INBRITTLEMENT.  SUBMITTER RECOMMENDED REMOVING AND REPL	ACING ALL PMA BOLTS P/N 772568 QQ FROM BATCH NR'S 30246 AND 30248 FROM SERVICE WITH LESS THAN 300 HOURS/CYCLES AT OPERAT	OR'S EARLIEST CONVENIENCE.							4	F			E2EA				 
1999081400388	19990814	00388	EU  	1999	8	14	99ZZZX2951       	1	19990717	G	7714	54237138010	INDICATOR       			AMD   	FALC20	FALCONF     	2720306	EU  										COCKPIT	FAILED          	B			QL1R	A				UNSCHED LANDING         				O			OTHER                     			CR	CRUISE         	1			EA	13	520AW	697  			709	453				IN CRUISE FLIGHT, THE ENGINE INDICATOR  CB 1E2 POPPED OUT.  THE N1, N2, ITT, OIL PRESSURE, AND OIL TEMPERATURE INDICATOR	S LOST POWER.  THE CREW DIVERTED TO A MAINTENANCE FACILITY WHERE THEY FOUND THE N2 GAUGE SHORTED INTERNALLY.  (THIS FAIL	URE ALSO CAUSED THE DEEC BATTERY CB 92E2 TO OPEN.  REPLACED N2 INDICATOR P/N 5423-713-80-10.  OPS CHECKED OK.  697 HOURS	 TT ON N2 GAUGE.			2	L	7	2 	4F				A7EU    					 
1999081400389	19990814	00389	CE  	1999	8	14	99ZZZX2952       	1	19990702	G	2750	656517547	CONTROL CABLE   			CESSNA	500   	S550        	2076607	CE  										FLAP CONTROL	FRAYED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	09	200CV					S5500064				PILOT NOTED FLAP HYDRAULIC LIGHT WOULD STAY ILLUMINATED IN FLAP UP CONDITION UNLESS FLAP LEVER WAS PULLED BACK JUST OFF 	THE UP (ZERO DEGREES) STOP.  INVESTIGATION REVEALED CABLE FRAYED AT LOWER PULLEY/DRUM TO WITHIN 2 STRANDS OF BREAKING. F	AILURE TOOK MINIMAL TENSION ON CABLE ASSY.				1	L	7	2 	4F			RT	A22CE   					 
1999081400390	19990814	00390	CE  	1999	8	14	99ZZZX2953       	1	19990715	G	3246	16101901	WHEEL           	PARKERHANFIN		CESSNA	340   	340A        	2076405	CE  										LT MLG	CRACKED         	B			DPOR	O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			NM	07	1373G					340A0072				AFTER TAXI-OUT, PILOT CALLED BACK AND SAID HE WAS RETURNING BECAUSE HE HAD A  'FLAT SPOT' ON THE LEFT MLG TIRE.  AS THE 	AIRCRAFT TAXIED IN, MAINTENANCE NOTICED THE TIRE WAS FLAT AND STOPPED HIM.  WHEN THE WHEEL WAS REMOVED, A 4 INCH LONG CR	ACK WAS DISCOVERED IN THE BEAD AREA WHICH HAD EXPANDED OUTWARD AND BEGAN RUBBING ON A BRAKE BACKPLATE ASSEMBLY (064-0270	0) WHICH OVERHEATED AND CAUSED THE TIRE TO MELT AND DEFLATE.			1	L	7	2 	3O				3A25    					 
1999081400391	19990814	00391	CE  	1999	8	14	99ZZZX2954       	1	19990724	G	3232	528884082A	HOSE            			CESSNA	210   	T210M       	2073451	CE  										NLG DOOR	SEPARATED       	C				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	05	732YK	1055 				21061879				HOSE CLOSE TO GEAR DOOR DOUBLE-ACTING HYDRAULIC ACTUATOR SEPARATED AT SOCKET DURING LANDING GEAR LOWERING CYCLE.  HOSE W	AS FIVE YEARS OLD.					1	H	7	1 	3O				3A21    					 
1999081400392	19990814	00392	SO  	1999	8	14	99ZZZX2955       	1	19990723	G	7603	452606	ROD END         			PIPER 	PA34  	PA34200     	7103405	SO  										THROTLE	FAILED          	H				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			NE	03	88AG					347450093				PILOT REPORTED LEFT ENGINE NOT RESPONDING WITH THROTTLE LEVER.  FOUND BROKEN THROTTLE CONTROL ROD END.  REMOVED AND REPL	ACED WITH NEW STYLE ROD END.  OLD STYLE ROD END PART NUMBER NOT AVAILABLE.  KEPT OLD PARTS, CHANGED ALL PARTS ON BOTH EN	GINES INCLUDING MIXTURE, PROPELLER, AND ALTERNATE AIR CABLE ROD ENDS.				1	L	7	2 	3O				A7SO    					 
1999081400393	19990814	00393	CE  	1999	8	14	99ZZZX2956       	1	19990729	G	7921	1E1884	OIL COOLER      	MODINE      		CESSNA	206   	206CESSNA   	2073302	CE  										ENGINE OIL	LEAKING         	B			RF3R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	23					0375					PART BEGAN LEAKING DURING NORMAL SERVICE DUE TO EPOXY REPAIR FAILURE.  EPOXY REPAIRS COMMONLY FAIL.  SUBMITTER RECOMMEND	ED ELIMINATING USE OF EPOXY IN OIL COOLERS.					1	H	7	1 	3O				A4CE    					 
1999081400394	19990814	00394		1999	8	14	99ZZZX2957       	4	19990707	G	2562	AK450	ELT             	AMERIKING   		CESSNA	421   	421C        	2076016	CE  										CABIN	INOPERATABLE    	B			EKIR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	421RX	404  			453251	421C0264				UNIT WILL NOT TRANSMIT.  INSTALLED 5-7-98 AS A REPLACEMENT FOR ANOTHER AK-450 WITH SAME PROBLEM.						1	L	7	2 	3O				A7CE    					 
1999081400395	19990814	00395	SO  	1999	8	14	99ZZZX2958       	1	19990720	G	7810	78008	EXHAUST PIPE    			PIPER 	PA31  	PA31P       	7103120	SO  										LT ENGINE	WRONG PART      	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NE	01	12GF					31P7300134				PILOT REPORTED LOW MANIFOLD PRESSURE ON RIGHT ENGINE.  AFTER DETERMINING PROBLEM ON RIGHT ENGINE, CHECKED LEFT ENGINE AN	D FOUND P/N LW10798 ADAPTER WITH SLOTS CUT LENGTHWISE IN SLIP JOINT AREA.  SEVERAL CRACKS ENAMATE FROM THE END OF THESE 	SLOTS.  REPLACED ADAPTER AND FOUND INTERCONNECTING PIPE P/N 78008 WOULD NOT FIT WITHOUT GROSS DISTORTION.				1	L	7	2 	3O				A8EA    					 
1999081400485	19990814	00485	CE  	1999	8	14	99ZZZX2966       	1	19990706	G	3244		TIRE            	GOODYEAR    		MTSBSI	MU2   	MU2B36A     	5780413	CE  										MLG	FAILED          	B			HMNR	A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CL	CLIMB          	1			SW	15	3UN	168  			12731041	720SA				AT ROTATION (110 KNOTS), PILOT FELT BAD VIBRATION.  PILOT RETURNED TO AIRPORT, FOUND THAT RIGHT HAND RECAP CAME OFF.  RE	CAP DONE BY HAWKINS AIRCRAFT TIRE COMPANY.  LANDINGS:  98.					1	H	7	2 	3T				A10SW   					 
1999081400487	19990814	00487	CE  	1999	8	14	99ZZZX2968       	1	19990517	G	5210		SEAL            			CESSNA	525   	525         	2076601	CE  										PASSENGER DOOR	FAILED          	D				B				EMER. DESCENT           				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SW	05										AT FL 37, THE DOOR SEAL LIGHT CAME ON.  PRESSURIZATION WAS MAINTAINED AND A NORMAL DESCENT TO 15,000 FEET WAS REQUESTED.	  AT 15,000 FEET, THE DOOR SEAL LIGHT EXTINGUISHED.  FLIGHT WAS CONTINUED PER MEL AT OR BELOW 25,000 FEET.  SECONDARY DO	OR SEAL REPLACED AS A RESULT OF FAILURE.				1	L	7	2 	4F			RT	A1WI    					 
1999081400488	19990814	00488	CE  	1999	8	14	99ZZZX2969       	1	19990713	G	2520	6921004P3	BRACKET         			BEECH 	200   	B200        	1152922	CE  										RT PAX SEAT	BROKE           	D				O				OTHER                   				O			OTHER                     			TO	TAKEOFF        	1			SW	99	223HC	1933 				BB855				ON TAKEOFF, BOTH SEAT BACK SUPPORT ADJUSTER BRACKETS BROKEN ON NR 6 PASSENGER SEAT.  THIS IS THE THIRD OCCURRENCE WITH T	HIS PART.					1	L	7	2 	4T				A24CE   					 
1999081400489	19990814	00489	CE  	1999	8	14	99ZZZX2970       	1	19990713	G	2520	6921004R3	BRACKET         			BEECH 	200   	B200        	1152922	CE  										LT PAX SEAT	BROKE           	D				O				OTHER                   				O			OTHER                     			TO	TAKEOFF        	1			SW	99	223HC	1933 				BB855				ON TAKEOFF, BOTH SEAT BACK SUPPORT ADJUSTER BRACKETS BROKEN ON NR 6 PASSENGER SEAT.  THIS IS THE THIRD OCCURRENCE WITH T	HIS PART.					1	L	7	2 	4T				A24CE   					 
1999081400491	19990814	00491	NM  	1999	8	14	99ZZZX2972       	1	19990712	G	2740	69778551	SPRING          		654997025   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	BROKE           	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		18748			KE01633					SPRINGS, P/N 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SP	RINGS.  SPRINS, P/N 69-77855-1, SHOULD BE REPLACED WITH P/N 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB-94-0195RR.					2	L	7	2 	4F			RT	A16WE   					 
1999081400492	19990814	00492	NM  	1999	8	14	99ZZZX2973       	1	19990717	G	2740	69778551	SPRING          		65C347514   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	FAILED          	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		42216	24976		KE00064					SPRINGS, PN 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPR	INGS.  SPRINGS, PN 69-77855-1, SHOULD BE REPLACED WITH PN 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB-94-0195RR.					2	L	7	2 	4F			RT	A16WE   					 
1999081400493	19990814	00493	NM  	1999	8	14	99ZZZX2974       	1	19990712	G	2740	69778551	SPRING          		65C347514   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	BROKE           	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		36536	16911		KE00559					SPRINGS, PN 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPR	INGS.  SPRINGS, PN 69-77855-1, SHOULD BE REPLACED WITH PN 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB-94-0195RR.					2	L	7	2 	4F			RT	A16WE   					 
1999081400494	19990814	00494	CE  	1999	8	14	99ZZZX2975       	1	19990715	G	5610	5111604200	WINDOW          			CESSNA	421   	421B        	2076014	CE  										COCKPIT	SEPARATED       	B			DPOR	A				UNSCHED LANDING         				D			INFLIGHT SEPARATION       			NR	NOT REPORTED   	1			NM	07	7549Q					451B0341				PILOT PRESSURIZED AIRCRAFT AT 14,000 FEET WHEN THE COPILOT'S WINDSHIELD BLEW OUT.  AN UNEVENTFUL LANDING WAS MADE.  WHEN	 THE WINDSHIELD RETAINER WAS REMOVED, IT APPEARED THAT THERE WERE SEVERAL CRACKS EMANATING FROM SEVERAL SCREW HOLES.  IT	 ALSO APPEARED THAT THE LOWER WINDSHIELD AREA WHERE THE CRACKS WERE NOTED HAD BEEN RESEALED AT SOME POINT ALTHOUGH NO LO	G ENTRIES WERE NOTED.			1	L	7	2 	3O				A7CE    					 
1999081400495	19990814	00495	SO  	1999	8	14	99ZZZX2976       	1	19990720	G	7810	78008	EXHAUST PIPE    			PIPER 	PA31  	PA31P       	7103120	SO  										RT ENGINE	WRONG PART      	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	07	12GF					31P7300134				PILOT REPORTED LOW MANIFOLD PRESSURE IN-FLIGHT ON RIGHT ENGINE.  INVESTIGATION SHOWED THE LEFT EXHAUST ADAPTER P/N LW107	98 CRACKED AT MOUNTING FLANGE.  REPLACED WITH NEW PART AND FOUND INTERCONNECTING EXHAUST PIPE P/N 78008 WOULD NOT FIT WI	THOUT GROSS DISTORTION.				1	L	7	2 	3O				A8EA    					 
1999081400496	19990814	00496	CE  	1999	8	14	99ZZZX2977       	1	19990718	G	5720	04115341	BRACKET         			CESSNA	140   	140         	2071602	CE  										AILERON	BROKE           	H				A				UNSCHED LANDING         				D			INFLIGHT SEPARATION       			CL	CLIMB          	1			SW	99	77310	3657 				11752				UPPER RIGHT AILERON PULLEY BRACKET BROKEN IN-FLIGHT ABOUT 2 MINUTES AFTER TAKEOFF.  AIRPLANE WAS FLOWN RUDDER ONLY BACK 	TO AIRPORT.  NO DAMAGE OR INJURIES.					1	H	7	1 	3O			NC	A768    					 
1999081400497	19990814	00497	CE  	1999	8	14	99ZZZX2978       	1	19990701	G	5730		SKIN            			CESSNA	210   	T210L       	2073449	CE  										WING	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	10	4687Q				01577	21059587				THE TRAILING EDGE OF THE AIRCRAFT WING INBOARD OF THE SPEED BRAKE LOCATION.  THE DISTURBED AIR BEHIND THE EXTENDED SPEED	 BRAKES WAS WORKING THE TRAILING EDGE OF THE WING CAUSING CRACKS AROUND THE TRAILING EDGE ATTACHMENT RIVETS.					1	H	7	1 	3O				3A21    					 
1999081400499	19990814	00499	CE  	1999	8	14	99ZZZX2980       	1	19990720	G	2750	536000023	CONTROL CABLE   			CESSNA	340   	340CESSNA   	2076404	CE  										TE FLAP	LOOSE           	H	L			O				OTHER                   				F			FLT CONT AFFECTED         			AP	APPROACH       	1			NE	05	340MR					3400206				AIRCRAFT DEPARTED AT 3 PM 7-20-99, CLIMBED TO 9,500 FEET TO DO AIR WORK, RETURNED TO NASHUA AND COMPLETED A TOUCH-AND-GO	 AND ELECTED TO DO A NO FLAP TOUCH-AND-GO.  ON THE ROLL, CONFIRMED FLAPS WERE FULLY UP AND FLAP ACTUATOR HANDLE WAS FULL	Y UP.  ACFT ACCELERATED TO BLUE LINE AND GEAR RETRACTED AND STARTED TO CLIMB.   ACFT AT BLUE LINE WOULD NOT CLIMB BEYOND	 200 AGL AND WAS UNSTABLE IN PITCH.  FLAPS STILL INDICATED FULLY UP.  AIRCRAFT WAS TURNED THROUGH 180 DEGREES TO LAND ON	 OPPOSITE RUNWAY.  THE FOLLOW-UP CABLE FOR THE FLAPS HAD BECOME LOOSE AND DETACHED FROM THE FLAP CABLE.  ANY MOVEMENT OF	 THE ACTUATING SYSTEM (TURBULENCE, ETC) CAUSED THE FLAPS TO EXTEND AND THE PILOT HAD NO CONTROL OVER THE FLAP SYSTEM.	1	L	7	2 	3O			 	3A25    					 
1999081400500	19990814	00500	GL  	1999	8	14	99ZZZX2981       	3	19990720	G	6111		BLADE           			BEECH 	58    	58          	1152740	CE  						MCAULY	2A34C	D2AF34C30   	GL  	PROPELLER	CRACKED         	B			ME4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	619BE	6540 	49   			TH20		703815		DURING POST-FLIGHT INSPECTION, PROPELLER WAS FOUND LEAKING RED OIL DOWN THE BLADE.  PROPELLER WAS REMOVED AND SENT TO SH	OP FOR INSPECTION.  AFTER PROP WAS DISASSEMBLED, THE HUB WAS STRIPPED AND INSPECTED WITH A 10X MICROSCOPE AND A CRACK WA	S DISCOVERED IN NR 1 BLADE SOCKET, 7 O'CLOCK POSITION, 5 THREADS IN. 0.5 INCH LONG.  REPLACEMENT HUB INSTALLED AND PROPE	LLER CHECK GOOD.			1	L	7	2 	3O				3A16    		5	C	P5EA	 
1999081400502	19990814	00502	GL  	1999	8	14	99ZZZX2983       	1	19990708	G	5531		SPAR            			DIAMON	DA20  	DA20A1      		GL  										VERT STABILIZER	SEDPARATED      	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	44UV	1822 				10295				DURING A 100-HOUR INSPECTION, FOUND THE VERTICAL TAIL SPAR HAD DISBONDED WITH FUSELAGE AND THE AREA BELOW WHERE THE TAIL	 SKID IS FORMED HAS CRACKED.					1	L	7	1 	3O			NT	TA4CH   					 
1999081400503	19990814	00503	GL  	1999	8	14	99ZZZX2984       	1	19990708	G	5531		SPAR            			DIAMON	DA20  	DA20A1      		GL  										VERT STABILIZER	SEPARATED       	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	10UV	3979 				10037				DURING A 100-HOUR INSPECTION, FOUND THAT THE VERTICAL TAIL SPAR HAD DISBONDED WITH FUSELAGE AND THE AREA BELOW WHERE THE	 TAIL SKID IS FORMED HAS CRACKED.					1	L	7	1 	3O			NT	TA4CH   					 
1999081400504	19990814	00504	CE  	1999	8	14	99ZZZX2985       	1	19990721	G	5210	051502620	SHIELD          			CESSNA	172   	172S        	2072439	CE  										PASSENGER DOOR	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	676SP	95   				172S8083				THE RIGHT FORWARD CABIN DOOR POST SHIELD WAS FOUND BUCKLED.  UPON REMOVAL, FOUND THE FRESH AIR HOSE RUNNING DOWN THE DOO	R POST WAS NOT ALLOWING THE SHIELD TO SEAT FULLY IN ITS CORRECT POSITION.  THE AIR VENT HOSE WAS FLATENED TO PROVIDE SUF	FICIENT CLEARANCE FOR THE SHIELD TO FIT PROPERLY.				1	H	7	1 	3O			NT	3A12    					 
1999081400505	19990814	00505	EU  	1999	8	14	99ZZZX2986       	1	19990701	G	7120		MOUNT           			BNORM 	BN2   	BN2A26      	1520226	EU  										RT ENGINE	SEPARATED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	29884					847				AREA OF METAL BOX THAT ENGINE MOUNT ATTACHES TO TORE OUT AT MOUNT ATTACH HOLE, UPPER OUTBOARD ATTACH POINT.						1	H	7	2 	3O				A17EU   					 
1999081400506	19990814	00506	EA  	1999	8	14	99ZZZX2987       	2	19990712	G	8530	LW16586	CIRCLIP         			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					TAPPET	FAILED          	D				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			SW	01	6694E	1842 				17272050	L559276			IN CRUISE FLIGHT 2,400 RPM/10,000 FEET, CIRCLIP FAILED (BECAME DISCONNECTED) ON VALVE LIFTER TAPPET NR 3 CYLINDER ASSEMB	LY TAKING THE REST OF THAT CYLINDER'S UPPER VALVE TRAIN WITH IT.  A SAFE LANDING WAS MADE TO A ROAD.					1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999081400507	19990814	00507	SO  	1999	8	14	99ZZZX2988       	2	19990722	G	8530	631521	SPRING          			BEECH 	58    	58          	1152740	CE  	CONT  	O520  	IO520CB     	17032	SO  					INTAKE VALVE	BROKEN          	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	05	6058A	1570 				TH1017	282412R			NR 4 CYLINDER INTAKE SPRING FOUND BROKEN AT ANNUAL INSPECTION.						1	L	7	2 	3O	3	O		3A16    	E5CE				 
1999081400508	19990814	00508	SW  	1999	8	14	99ZZZX2989       	1	19990807	G	3411		TUBE            			MOONEY	M20   	M20J        	5870219	SW  										PITOT SYSTEM	MISINSTALLED    	H		A		O				OTHER                   				W			INADEQUATE Q C            			NR	NOT REPORTED   	1			SW	99	91381	397  				243237				THE PITOT TUBING IN THE CABIN WAS IMPROPERLY ROUTED CAUSING THE TUBING TO BE CRUSHED BETWEEN THE CABIN STEEL FRAME AND T	HE LEFT SIDE SKIN.  THIS CAUSED A RESTRICTION OF PRESSURE TO THE AIRSPEED INDICATOR RESULTING IN INCORRECT INDICATIONS T	O THE PILOT.  THIS AIRCRAFT WAS INVOLVED IN A LANDING ACCIDENT WHICH DAMAGED THE AIRCRAFT TO A TOTAL LOSS.  THE PITOT TU	BING CONDITION MAY HAVE HIGHER THAN WAS INDICATED TO THE PILOT.			1	L	7	1 	3O				2A3     					 
1999082000036	19990820	00036	SO  	1999	8	20	99ZZZX2990       	2	19990721	G	8530	EC649358	CYLINDER        			CESSNA	335   	335         	2075601	CE  	CONT  	O520  	TSIO520EB   	17040	SO  					LT ENGINE	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	6867C		490  		0443972	3350061	510405			CHOKE WORN OVERSIZE ON NR 3 CYLINDER.						1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999082000037	19990820	00037	SO  	1999	8	20	99ZZZX2991       	2	19990721	G	8530	EC649858	CYLINDER        		EC649358    	CESSNA	335   	335         	2075601	CE  	CONT  	O520  	TSIO520EB   	17040	SO  					RT ENGINE	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	6867C				0744350	3350061	0744350			CHOKE OVERSIZE.  COATING WORN AWAY ON NR 6 CYLINDER.						1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999082000038	19990820	00038	SO  	1999	8	20	99ZZZX2992       	2	19990721	G	8530	EC649358	CYLINDER        			CESSNA	335   	335         	2075601	CE  	CONT  	O520  	TSIO520EB   	17040	SO  					RT ENGINE	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	6867C		490  		0644259	3350061	182675			TOP CHOKE OVERSIZE.  COATING WORN AWAY ON NR 4 CYLINDER.						1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999082000039	19990820	00039	SO  	1999	8	20	99ZZZX2993       	2	19990721	G	8530	EC649350	CYLINDER        			CESSNA	335   	335         	2075601	CE  	CONT  	O520  	TSIO520EB   	17040	SO  					LT ENGINE	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	6867C		490  		0744335	3350061	510405			CHOKE WORN OVERSIZE ON NR 5 CYLINDER.						1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999082000040	19990820	00040	SO  	1999	8	20	99ZZZX2994       	2	19990721	G	8530	EC649358	CYLINDER        			CESSNA	335   	335         	2075601	CE  	CONT  	O520  	TSIO520EB   	17040	SO  					LT ENGINE	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	6867C		490  		0744334	3350061	182675			TOP OF TRAVEL OVERSIZE CHOKE.  CHROME WORN AWAY ON NR 5 CYLINDER.						1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999082000041	19990820	00041	SO  	1999	8	20	99ZZZX2995       	2	19990421	G	8530	DC649358	CYLINDER        			CESSNA	335   	335         	2075601	CE  	CONT  	O520  	TSIO520EB   	17040	SO  					LT ENGINE	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	6867C		490  		0744337	3350061	510405			CHOKE WORN OVERSIZE ON NR 6 CYLINDER.						1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999082000042	19990820	00042	SO  	1999	8	20	99ZZZX2996       	2	19990721	G	8530	ECL49358	CYLINDER        			CESSNA	335   	335         	2075601	CE  	CONT  	O520  	TSIO520EB   	17040	SO  					RT ENGINE	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	6867C		490  		0744319	3350061	182675			TOP OF PISTON TRAVEL, CHOKE OVERSIZE.  COATING WORN AWAY ON NR 1 CYLINDER.						1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999082000043	19990820	00043	SO  	1999	8	20	99ZZZX2997       	2	19990721	G	8530	EC649358	CYLINDER        			CESSNA	335   	335         	2075601	CE  	CONT  	O520  	TSIO520EB   	17040	SO  					LT ENGINE	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	6867C		490  		0744344	3350061	510405			CHOKE WORN OVERSIZE ON NR 4 CYLINDER.						1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999082000044	19990820	00044	SO  	1999	8	20	99ZZZX2998       	2	19990726	G	8530	EC649358	CYLINDER        			CESSNA	335   	335         	2075601	CE  	CONT  	O520  	TSIO520EB   	17040	SO  					RT ENGINE	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	6867C		490  		0744340	3350061	182675			TOP OF TRAVEL CHOKE OVERSIZE.  COATING WORN AWAY ON NR 3 CYLINDER.						1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999082000045	19990820	00045	SO  	1999	8	20	99ZZZX2999       	2	19990721	G	8530	EC649358	CYLINDER        			CESSNA	335   	335         	2075601	CE  	CONT  	O520  	TSIO520EB   	17040	SO  					LT ENGINE	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	6867C		490  		0444146	3350061	510405			CHOKE WORN OVERSIZE ON NR 2 CYLINDER.						1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999082000046	19990820	00046	SO  	1999	8	20	99ZZZX3000       	2	19990721	G	8530	EC649358	CYLINDER        			CESSNA	335   	335         	2075601	CE  	CONT  	O520  	TSIO520EB   	17040	SO  					RT ENGINE	WORN            	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	6867C		490  		0744358	3350061	182675			CHOKE OVERSIZE. COATING WORN AWAY ON NR 5 CYLINDER.						1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999082000048	19990820	00048		1999	8	20	99ZZZX3002       	4	19990701	G	3452	KT76A	TRANSPONDER     			PIPER 	PA60  	PA60601P    	7106012	NM  										COCKPIT	FAILED          	C				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	09	14NP					61P0521218				FIRST, FOUND TRANSPONDER HAD BROKEN WIRE.  THEN FOUND ENCODER WAS FAULTY, TESTED OK AFTER OVERHAUL, BUT DEFECTIVE AGAIN.	  REPLACED.  CHECKED OK.					1	M	7	2 	3O			RT	A17WE   					 
1999082000049	19990820	00049		1999	8	20	99ZZZX3003       	4	19990701	G	3416	10193509690	ENCODER         			PIPER 	PA60  	PA60601P    	7106012	NM  										COCKPIT	FAILED          	C				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	09	14NP				C115951	61P0521218				FIRST, FOUND TRANSPONDER HAD BROKEN WIRE.  THEN FOUND ENCODER WAS FAULTY, TESTED OK AFTER OVERHAUL, BUT DEFECTIVE AGAIN.	  REPLACED.  CHECKED OK.					1	M	7	2 	3O			RT	A17WE   					 
1999082000050	19990820	00050	EU  	1999	8	20	99ZZZX3004       	1	19990701	G	2720	NB45C965	BELLCRANK       			BNORM 	BN2   	BN2A26      	1520226	EU  										RUDDER	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	29884					847				HOLES ELONGATED IN LEVER (BELLCRANK) BOTH SIDES ALLOWING EXCESSIVE PLAY IN RUDDER.						1	H	7	2 	3O				A17EU   					 
1999082000053	19990820	00053	SO  	1999	8	20	99ZZZX3007       	1	19990802	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										NR 1 BRAKE	FAILED          	B			XC4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19		1365 			1638A					BRAKE ASSY, P/N 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN AND STATOR TANGS BINDING IN TORQUE TUBE KEY SLOTS.  THIS	 IS A CONTINUAL DISCREPANCY.  BRAKE ASSY SHOULD LAST 2,500 CYCLES.					2	L	7	2 	4T			RT	A31SO   					 
1999092100001	19990921	00001	WP  	1999	9	21	99ZZZX3008       	2	19990730	G	7230	30756332	CARBON SEAL     								GARRTT	TFE731	TFE7313     	01518	WP  					COMPRESSOR	FAILED          	B			XB1R	C				ABORTED TAKEOFF         				K	J		FLUID LOSS                	WARNING INDICATION        		TO	TAKEOFF        	1			SW	09		7371 					P76420			ENGINE LOST OIL PRESSURE ON TAKEOFF AND SAFELY ABORTED.  INVESTIGATION FOUND METAL IN OIL FILTER.  FURTHER DISASSEMBLY F	OUND NR 5 CARBON SEAL RUNNER BROKEN.  CONTAMINATED OIL SYSTEM.  PART S/N 970811401579.  ENG TSN:  7,329.8 HOURS.  ENG CS	N:  4,521.  PART CSN:  279.									4	F			E6WE				 
1999082000054	19990820	00054	WP  	1999	8	20	99ZZZX3009       	2	19990730	G	7230	30756332	CARBON SEAL     								GARRTT	TFE731	TFE7313R    	01518	WP  					COMPRESSOR	FAILED          	B			XB1R	O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		NR	NOT REPORTED   	1			SW	09		926  	547  				P84309			ENGINE LOST OIL PRESSURE IN-FLIGHT.  DISASSEMBLY FOUND NR 5 CARBON SEAL BROKEN. CONTAMINATED OIL SYSTEM.  PART S/N 96081	1401752.  ENG TSN:  7,666.3 HOURS.  ENG CSN:  5,701 HOURS.  PART CSN:  547.										4	F			E6WE				 
1999082000055	19990820	00055	CE  	1999	8	20	99ZZZX3010       	1	19990726	G	3250		CENTERING ARM   			BEECH 	1900  	1900D       	1154162	CE  										NLG	MISALIGNED      	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01										IT WAS DISCOVERED UPON OPS CHECK OF NEWLY INSTALLED NOSE GEAR JUST OUT OF OVERHAUL, THAT THE NOSE WHEEL WAS NOT CENTERIN	G PROPERLY.  AFTER FURTHER EXAMINATION, IT WAS DETERMINED THE CYLINDER ASSY (P/N 114-820022-17) CENTERING ARM ATTACHMENT	 HOLES (6) WERE ROTATIONALLY MISALIGNED BY APPROXIMATELY 4 DEGREES DURING MANUFACTURE.				2	L	7	2 	4T			RT	A24CE   					 
1999082000056	19990820	00056	WP  	1999	8	20	99ZZZX3011       	1	19990528	G	7120		MOUNT           			DOUG  	DC10  	DC1030F     	3023504	WP  										LT PYLON	LOOSE           	B			AAPY	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	33	600GC					46965				C-CHECK - PYLONS DURING ROUTINE INSPECTION.  REF:  J/C 0834, FOUND FORWARD ENGINE MOUNT BOLTS WITH LOCKWIRE BROKEN AND C	AP BETWEEN FORWARD PYLON ENGINE MOUNT AND FORWARD ENGINE MOUNT, LT SIDE 0.065 INCH.  RT SIDE 0.085 INCH.					2	L	7	3 	4F			RT	A22WE   					 
1999082000057	19990820	00057	WP  	1999	8	20	99ZZZX3012       	1	19990528	G	7120		MOUNT           			DOUG  	DC10  	DC1030F     	3023504	WP  										RT PYLON	LOOSE           	B			AAPY	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	33	600GC					46965				C-CHECK - PYLONS DURING ROUTINE INSPECTION.  REF:  J/C 0834, FOUND FORWARD ENGINE MOUNT BOLTS WITH LOCKWIRE BROKEN AND C	AP BETWEEN FORWARD PYLON ENGINE MOUNT AND FORWARD ENGINE MOUNT, LT SIDE 0.065 INCH.  RT SIDE 0.085 INCH.					2	L	7	3 	4F			RT	A22WE   					 
1999082000058	19990820	00058	NM  	1999	8	20	99ZZZX3013       	1	19990702	G	2761	65C311978	HOUSING         		65448517    	BOEING	737   	737*        		NM  										SPOILER ACTUATOR	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		3869 			3869					HOUSING IS BROKEN ACROSS THE BEARING MOUNTING LUG.  HOUSING OVERSTRESSED, HIGH TOTAL TIME HOURS.						2	L	7	2 	4F			RT	A16WE   					 
1999082000059	19990820	00059	NM  	1999	8	20	99ZZZX3015       	1	19990630	G	2760	65C268636	HOUSING         		65C268642   	BOEING	737   	737*        		NM  										SPOILER ACTUATOR	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		24300			WN0003					ACTUATOR WAS RECEIVED WITH HOUSING CRACKED ENTIRE CIRCUMFERENCE OF THE GLAND AREA ALONG THE BOTTOM OF THE THREADS.  OVER	PRESSURED OR HEAVY IMPACT.					2	L	7	2 	4F			RT	A16WE   					 
1999082000060	19990820	00060	NM  	1999	8	20	99ZZZX3016       	1	19990708	G	3210	65446924	MODULE PACKAGE  		65446915    	BOEING	737   	737*        		NM  										MLG	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01			47877		3095					HOUSING IS CRACKED AT BASE OF PORT 2.  FATIGUE, HIGH TSO.						2	L	7	2 	4F			RT	A16WE   					 
1999082000061	19990820	00061	NM  	1999	8	20	99ZZZX3017       	1	19990707	G	3210	65446925	MODULE PACKAGE  		65446916    	BOEING	737   	737*        		NM  										MLG	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01			42414		419					'D' PRIORITY PORT IS CRACKED.  OVERTORQUING AND/OR FATIGUE OF HOUSING.  HIGH TSO.						2	L	7	2 	4F			RT	A16WE   					 
1999082000062	19990820	00062	NM  	1999	8	20	99ZZZX3018       	1	19990706	G	3230	6F230925	RESTRICTOR VALVE	CRISSAIR    	6F23925     	BOEING	737   	737*        		NM  										MLG	BROKE           	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					548					BODY IS BROKEN AT PACKING GROOVE.  FATIGUE.  SUBMITTER SUGGESTED ADDING A REQUIREMENT FOR DYE PENETRANT INSPECTION.						2	L	7	2 	4F			RT	A16WE   					 
1999082000063	19990820	00063	CE  	1999	8	20	99ZZZX3019       	1	19990723	G	2510		SEAT            			CESSNA	210   	210B        	2073410	CE  										COCKPIT	BENT            	G	P	A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	05	9712X					21058012				THIS AIRCRAFT WAS INVOLVED IN AN ACCIDENT WHICH RESULTED IN THE PILOT'S SEAT COMING DISCONNECTED FROM THE SEAT TRACK.  T	HE LEFT SIDE SEAT BRACING WAS BENT.  THE PILOT RECEIVED SERIOUS HEAD INJURIES.  A SUPPORT BETWEEN THE LEFT AND RIGHT SEA	T VERTICAL BRACING MAY HAVE PREVENTED THIS.				1	H	7	1 	3O				3A21    					 
1999082000064	19990820	00064	EU  	1999	8	20	99ZZZX3020       	1	19990701	G	2720	NB45C966	BELLCRANK       			BNORM 	BN2   	BN2A26      	1520226	EU  										RUDDER	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	29884					847				HOLES ELONGATED IN LEVER (BELLCRANK) BOTH SIDES ALLOWING EXCESSIVE PLAY IN RUDDER.						1	H	7	2 	3O				A17EU   					 
1999082000080	19990820	00080	NE  	1999	8	20	99ZZZX3024       	1	19990614	G	5302		SKIN            			SKRSKY	S76   	S76A        	8143006	NE  										TAIL BOOM	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	164AG					760290				CORROSION OF TAIL PYLON ASSEMBLY AT VARIOUS NOSE RIBS, STRAP FITTINGS, AND STRINGERS.						1	G	7	2 	3U				H1NE    					 
1999082000081	19990820	00081	SW  	1999	8	20	99ZZZX3025       	1	19990603	G	6210	206010200133	BLADE           			BELL  	206   	206B        	1181511	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5008K	1323 			A3655	2524				DISCOVERED DURING DAILY INSPECTION, TRAILING EDGE EXTRUSION HEAVILY CORRODED (INTERGRANULAR CORROSION).						1	G	7	1 	3U				H2SW    					 
1999082000082	19990820	00082	SW  	1999	8	20	99ZZZX3026       	1	19990611	G	6210	206015001107	BLADE           			BELL  	206   	206L4       	1182110	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	171AL	3242 			A2163	52064				DISCOVERED DURING DAILY INSPECTION, HEAVY INTERGRANULAR CORROSION ON TRAILING EDGE.						1	G	7	1 	3U			NC	H2SW    					 
1999082000083	19990820	00083	SW  	1999	8	20	99ZZZX3027       	1	19990629	G	6210	206015001107	BLADE           			BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	343AL	1815 			A2151	51372				DURING DAILY INSPECTION, CORROSION AND DEBOND OF SKIN AND SPAR BENEATH GRIP FINGER DOUBLER ON LOWER SURFACE.  DAMAGE BEY	OND MANUFACTURER'S LIMITS, BLADE SCRAPPED.					1	G	7	1 	3U				H2SW    					 
1999082000090	19990820	00090	SW  	1999	8	20	99ZZZX3034       	1	19990422	G	7810	206064300005	PIPE            			BELL  	206   	206L3       	1182108	SW  										EXHAUST	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	17237	307  			971015	51478				WELD CRACKED OUT.						1	G	7	1 	3U				H2SW    					 
1999082000092	19990820	00092	SW  	1999	8	20	99ZZZX3036       	1	19990112	G	7810	206064300005	STACK           			BELL  	206   	206L3       	1182108	SW  										EXHAUST	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	715CC	749  			980216	51380				STACK CRACKED NEXT TO REAR ENTER SEAM.						1	G	7	1 	3U				H2SW    					 
1999082000093	19990820	00093	SW  	1999	8	20	99ZZZX3037       	1	19990429	G	7810	206064300005	PIPE            			BELL  	206   	206L3       	1182108	SW  										EXHAUST	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	53702	627  			980544	51249				EXHAUST PIPE CRACKED.						1	G	7	1 	3U				H2SW    					 
1999082000094	19990820	00094	SW  	1999	8	20	99ZZZX3038       	1	19990112	G	7810	206064300005	STACK           			BELL  	206   	206L3       	1182108	SW  										EXHAUST	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	715CC	575  			980116	51380				CRACK AT SEAM ON AFT SIDE OF DUCT ASSY.						1	G	7	1 	3U				H2SW    					 
1999082000095	19990820	00095	SW  	1999	8	20	99ZZZX3039       	1	19990203	G	7810	206064300005	STACK           			BELL  	206   	206L3       	1182108	SW  										EXHAUST	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	17592	306  			980713	51535				EXHAUST STACK CRACKED AT WELDED AREA ALONG SEAT SEAM.						1	G	7	1 	3U				H2SW    					 
1999082000098	19990820	00098	SW  	1999	8	20	99ZZZX3042       	1	19990623	G	6240	206075681109	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										DUAL TACHOMETER	STUCK           	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	39112				8405116	45652				ROTOR NEEDLE PEGGED AND STUCK AT 120.  REF:  MCN 116.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999082000099	19990820	00099		1999	8	20	99ZZZX3043       	4	19990607	G	3421	206075607103	GYRO            		5101A       	BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	206AZ	30   			91L2008	51007				GYRO BALL SPINS FREELY AND RESTS INVERTED AFTER BEING CAGED.  REF:  MCN 126.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999082000100	19990820	00100	SW  	1999	8	20	99ZZZX3044       	1	19990513	G	3340	900601	LIGHT           			BELL  	230   	230         	1182149	SW  										FUSELAGE	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	1157 			972277	23019				RELAY BAD, LIGHT WILL NOT GO OUT.  REF:  DMR 65440100.  MCN 127.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H9SW    					 
1999082000101	19990820	00101		1999	8	20	99ZZZX3045       	4	19990615	G	3421	4021541671	INDICATOR       			BOLKMS	117   	BK117A3     	5626015	EU  										COCKPIT	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	1140H	557  			88071674	7078				INDICATOR TUMBLES DURING 45 DEGREE BANK.  MCN 130.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999082000102	19990820	00102	NE  	1999	8	20	99ZZZX3046       	2	19990616	G	7412	103832251	EXCITER         		1300363     	BOLKMS	117   	BK117A3     	5626015	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					ENGINE	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	1140H	556  			98106311	7078				CIRCUIT BREAKER TRIPS WHEN ATTEMPTING TO START ENGINE.						1	G	7	2 	3U	3	U		H13EU   	E5NE				 
1999082000103	19990820	00103	EU  	1999	8	20	99ZZZX3047       	1	19990529	G	3340	G62504	SEARCH LIGHT    			BOLKMS	BK117 	BK117C1     	5626025	EU  										FUSELAGE	INOPERATIVE     	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	502  			558611	7505				SEARCH LIGHT WILL NOT EXTEND OR RETRACT. REF:  RMA NR R020259 MCN 132.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999082000104	19990820	00104	NE  	1999	8	20	99ZZZX3048       	2	19990621	G	7530	430110209	ACTUATOR        			BOLKMS	117   	BK117A3     	5626015	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					NR 2 ENGINE	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	117MH	269  			712	7112	LE45386			ACTUATOR WILL NOT OPEN WHEN 85 POUNDS SHOP AIR APPLIED.  LEVER FAILED TO MOVE  REF:  MCN 136.  REMOVED AND REPLACED.						1	G	7	2 	3U	3	U		H13EU   	E5NE				 
1999082000105	19990820	00105	EU  	1999	8	20	99ZZZX3049       	1	19990630	G	6210	L621M1010054	BOLT            			UROCOP	EC135 	EC135P1     	8680990	EU  										M/R BLADE	LOOSE           	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	911SV	183  			506	0070				EXPANSION BOLT LOOSE.  REF:  MCN 138.  REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999082000106	19990820	00106	EU  	1999	8	20	99ZZZX3050       	1	19990630	G	6210	L621M1010054	BOLT            			UROCOP	EC135 	EC135P1     	8680990	EU  										M/R BLADE	LOOSE           	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	911SV	183  			503	0070				EXPANSION BOLT LOOSE.  REMOVED PER AEC.  REF:  MCN:  139.  REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999082000107	19990820	00107	EU  	1999	8	20	99ZZZX3051       	1	19990630	G	6210	L621M1010054	BOLT            			UROCOP	EC135 	EC135P1     	8680990	EU  										M/R BLADE	LOOSE           	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	911SV	183  			502	0070				EXPANSION BOLT BACKED OUT OF BLADE.  REF:  MCN 140. REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999082700333	19990827	00333	NE  	1999	8	27	99ZZZX3065       	2	19990706	G	8520	6514	IMPELLER SHAFT  		126308      	SCWZER	G164  	G164A       	3952704	EA  	PWA   	R985  	R985AN14B   	52008	NE  					CRANKCASE	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	08	7869		480  		288934	1003	42111603			PRIOR TO DISASSEMBLY, A 'GRATING' OR 'RATCHETING' NOISE COULD BE HEARD AT A CONSTANT LOCATION DURING CRANKSHAFT ROTATION	 WITH THE NOSE OF THE ENGINE RACING DOWN.  THE ACCESSORY CASE AND COLLECTOR CASE WERE REMOVED AS A UNIT.  UPON REMOVAL, 	A SINGLE GEAR TOOTH WAS FOUND ON THE ENGINE CRANKCASE.  CLOSER EXAMINATION SHOWED THE TOOTH HAD BROKEN FROM THE IMPELLER	 DRIVE SHAFT (P/N 6514).  THE REMAINING TEETH WERE NOTED AS SEVERELY WORN.  DURING OIL SCREEN AND ENGINE SUMP OIL EXAMIN	ATION, NO METAL COULD BE NOTED VISUALLY.		1	Q	7	1 	3R	3	R		1A16    	5E1				 
1999082700334	19990827	00334	SO  	1999	8	27	99ZZZX3066       	2	19990701	G	8530	SA2000SC5293	PISTON RING     			CESSNA	140   	140         	2071602	CE  	CONT  	C85   	C8512F      	17008	SO  					ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	77310	311  				11752	25790612			REMOVED CYLINDERS BECAUSE LOWER COMPRESSION.  FOUND BROKEN RINGS ON NR 2, NR 3, AND NR 4 CYLINDERS.  CAUSE UNKNOWN.						1	H	7	1 	3O	3	O	NC	A768    	E233				 
1999082700341	19990827	00341	SO  	1999	8	27	99ZZZX3073       	1	19990805	G	2434		BRUSH           	FORD        	DOFF10300J  	GULSTM	AA5   	AA5B        	3960105	SO  										ALTERNATOR	WORN            	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	23	74608		672  		8040936	AA5B0282				ALTERNATOR FAILED TO CHARGE 672 HOURS AFTER OVERHAUL.  INSPECTION REVEALED THAT ALTHOUGH BOTH BRUSHES HAD BEEN REPLACED 	DURING OVERHAUL, ONE BRUSH WAS FULLY WORN OUT WHERE THE OTHER WAS ONLY 50 PERCENT WORN.  OVERHAULER SAID HE HAS SEEN THI	S BEORE AND ATTRIBUTES IT TO POOR MANUFACTURING AND/OR QUALITY CONTROL BY THE BRUSH VENDOR.  BOTH BRUSHES EXISTED IN THE	 SAME ENVIRONMENT AND RODE ON THE SAME ARMATURE AND THIS SHOULD HAVE WORN AT APPROXIMATELY THE SAME RATE.			1	L	7	1 	3O				A16EA   					 
1999082700342	19990827	00342	CE  	1999	8	27	99ZZZX3074       	1	19990701	G	8011	22735	SOLENOID        			CESSNA	172   	172H        	2072424	CE  										STARTER	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	2491L					17255691				VENDOR UNKNOWN.  IN JULY, APPROXIMATELY 40 CYCLES, THE SOLENOID WOULD NOT FUNCTION.  REMOVED/REPLACED WITH GOOD UNIT.  D	RILLED 4 RIVETS ON CAP AND FOUND THE ENTIRE INTERNAL PLUNGER/CONTACT DISC/STUDS COVERED WITH CORROSION.  SUBMITTER STATE	D WHATEVER IS USED PRIOR TO ASSEMBLY IS CAUSING SAME.				1	H	7	1 	3O			NT	3A12    					 
1999082700343	19990827	00343	EA  	1999	8	27	99ZZZX3075       	2	19990809	G	7414	IO382807F	CAPACITOR       								LYC   	O360  	HIO360E1AD  	41514	EA  					NR 1 MAGNETO	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99		15   			9847					DURING RUN-UP, CUSTOMER NOTED NO MAG DROP ON ONE MAGNETO.  MAINTENANCE PERSONNEL FOUND CAPACITOR WAS 'OPEN' INTERNALLY, 	SO MAG COULD NOT GROUND WHEN SELECTED.  NEW CAPACITOR WAS INSTALLED AND FUNCTION CHECKS WERE NORMAL.										3	O			1E10				 
1999082700344	19990827	00344	CE  	1999	8	27	99ZZZX3076       	1	19990803	G	2197		WIRE            			BEECH 	90    	65B90       	1152907	CE  										AIR CONDITIONER	SHORTED         	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	452TT					LJ452				PILOT REPORTED AIR CONDITIONER INOPERABLE.  MAINTENANCE INSPECTED AIR CONDITIONER SYSTEM AND FOUND GROUND TO COMPRESSOR 	MOTOR HAD BURNED A HOLE IN BEAM P/N 50-410012-249.  THIS BEAM HAS THE UPPER SUPPORT FOR THE DRAG BRACE ATTACHED TO IT. T	HE DIAMETER OF THE HOLE WAS APPROXIMATELY .75 INCH.  GROUND WIRE ATTACH BOLT APPEARED TO HAVE WORKED LOOSE CAUSING GROUN	D TO ARC.  SUBMITTER SUGGESTED RE-LOCATING GROUND ONTO A GROUND LUG AND NOT DIRECTLY ON THIS BEAM.			1	L	7	2 	3T			 	3A20    					 
1999082700345	19990827	00345	NE  	1999	8	27	99ZZZX3077       	3	19990729	G	6111	57D0495	FORK            			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	PITCH CHANGE	CRACKED         	B			EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03			4004 		3750NR			HJ445		FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS.  FIVE CRACKS.						2	L	7	2 	4T			RT	A24CE   		5	C	P10NE	 
1999082700346	19990827	00346	EU  	1999	8	27	99ZZZX3078       	1	19990728	G	3233	184811	CYLINDER        		1862K       	BAG   	JETSTM	JETSTM3201  	1500217	EU  										MLG	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	484UE	24954	2640 		LK8706352	899				RADIUS ROD, PN 1862/I, S/N LK-8706352, WAS RECEIVED WITH COMMENT 'CRACKED'.  INSPECTION REVEALED APPROXIMATELY A 10 INCH	 CRACK ORIENTED ALONG THE FORGING FLASH LINE, ON THE ONE-WAY RESTRICTOR MOUNTING LUG SIDE, RUNNING FROM THE 'OPEN' END O	F THE CYLINDER, PN 184811, SN PIP304.  COMPLETE RADIUS ROD HAS BEEN RETURNED TO APPH FOR INVESTIGATION.				2	L	7	2 	4T			RT	A56EU   					 
1999082700347	19990827	00347	SW  	1999	8	27	99ZZZX3079       	1	19990803	G	2612	M250381229	WIRE            			SWRNGN	SA226 	SA226T      	8780122	SW  										FIRE DETECTOR	CHAFED          	C				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			SW	01	142NR					T227				WIRE ON OIL COOLER FIRE DETECTOR CHAFED TO ASPIRATOR ASSEMBLY CAUSING FALSE FIRE INDICATION.						2	L	7	2 	4T			RT	A5SW    					 
1999082700348	19990827	00348	EU  	1999	8	27	99ZZZX3080       	1	19990728	G	3230	101A703013	SLIDE TUBE      		B00A702925A 	BAG   	JETSTM	JETSTM3101  	1500215	EU  										LT MLG	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	838JS		4126 		BADL479	741				J31 LT MLG, PN B00A702925A, SN BADL-479, WAS SENT IN FOR REPAIR.  MAGNETIC PARTICLE NDT INSPECTION OF SLIDE TUBE, PN 101	A703013, SN BD48, REVEALED AN INDICATION (CRACK) EXTENDING FROM THE TOP OF THE TUBE THROUGH THE HOLE FOR SOCKET SET SCRE	W, PN 741M1-4D, AND DOWN THE TUBE FOR AN ADDITIONAL 0.520 INCH.  SUBJECT SLIDE TUBE HAS BEEN REJECTED, AND WILL BE REPLA	CED.			2	L	7	2 	4T			RT	A21EU   					 
1999082700349	19990827	00349	EU  	1999	8	27	99ZZZX3081       	1	19990728	G	3230	100A703029	SLIDE TUBE      		107A703031A 	BAG   	JETSTM	JETSTM3201  	1500217	EU  										RT MLG	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03		15936	7463 		BADL798					J32 RT MLG, PN 107A703031A, SN BADL-798, WAS SENT IN FOR SCHEDULED OVERHAUL.  MAGNETIC PARTICLE NDT INSPECTION OF SLIDE 	TUBE, PN 100A703029, SN AP008, REVEALED AN INDICATION (CRACK) EXTENDING FROM THE TOP OF THE TUBE THROUGH THE HOLE FOR SO	CKET SET SCREW, PN 741M1-4D, AND DOWN THE TUBE FOR AN ADDITIONAL 0.400 INCH.  SUBJECT SLIDE HAS BEEN REJECTED, AND WILL 	BE REPLACED.			2	L	7	2 	4T			RT	A56EU   					 
1999082700350	19990827	00350	NE  	1999	8	27	99ZZZX3082       	2	19990730	G	7230	5008T20P01	ROTOR DISC      		5012T75G24  	SKRSKY	S61   	S61A        	814210C	NE  	GE    	CT58  	CT581401    	30011	NE  					COMPRESSOR	CRACKED         	B	P	A	JYER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	693CC	940  			8991	61215	2803C8A			DURING LIGHT OVERHAUL, THE STAGE 1 COMPRESSOR ROTOR DISC WAS VISUALLY INSPECTED.  TWO CRACKS WERE FOUND ON THE AFT FACE,	 IN THE CORNER, OF THE LT BLADE COVETHAIL SLOTS.  ONE EACH IN TWO SLATS.  POSSIBLE CAUSE, PITTING AND/OR INCLUSION.  REC	URRENCE PREVENTION:  MATERIAL (AM355) INSPECTION UPGRADE AT MANUFACTURER AND/OR CORROSION INHIBITING CLATING.				2	G	7	2 	4U	4	U		H2EA    	1E3				 
1999082700351	19990827	00351	SW  	1999	8	27	99ZZZX3083       	1	19990722	G	6300	406340102101	CARBON SEAL     			BELL  	407   	407         		SW  										FREEWHEEL UNIT	LEAKING         	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	407FC	1300 				53050				CARBON SEAL LEAKING.  REPLACED WITH NEW SEAL FROM BELL HELICOPTER.						1	G	7	1 	3U			O	H2SW    					 
1999082700352	19990827	00352	SW  	1999	8	27	99ZZZX3084       	1	19990722	G	6240	407375008101	INDICATOR       			BELL  	407   	407         		SW  										DUAL TACHOMETER	FAILED          	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	6298Z	20   			0433	53361				INDICATOR FAILED.  REPLACED WITH NEW INDICATOR FROM BELL HELICOPTER.						1	G	7	1 	3U			O	H2SW    					 
1999082700353	19990827	00353	NM  	1999	8	27	99ZZZX3085       	1	19990726	G	6700	600N76055	BELLCRANK       			DOUG  	600N  	600N        	3027377	NM  										FLIGHT CONTROL	DAMAGED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	17	609BP	300  				RN038				DURING AN ANNUAL INSPECTION LOOKING OVER THE FLIGHT CONTROLS, THE LATERAL CONTROL ROD BELLCRANK HAD PLAY.  REMOVING PART	 FROM AIRCRAFT, BEARING FELL OUT.  SUBMITTER STATED FINDING THIS PROBLEM IN OTHER 600N AIRCRAFT.					1	G	7	1 	3U			NC	H3WE    					 
1999082700354	19990827	00354	SW  	1999	8	27	99ZZZX3086       	1	19990714	G	2435	23032022	STARTER         			BELL  	206   	OH58A       	1181579	SW  										START/GENERATOR	FAILED          	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	54AG		186  		22191	7120721				SHAFT SHEARED APPROXIMATELY .1250 INCH IN GENERATOR BODY.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999082700355	19990827	00355	GL  	1999	8	27	99ZZZX3087       	2	19990712	G	7532	23005366	BLEED VALVE     			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE	LOOSE           	B		A	IIFR	O				OTHER                   				J			WARNING INDICATION        			CR	CRUISE         	1			SW	03	517R	809  			FF57519	53231	CAE847254			PILOT REPORTED 40 DEGREE HIGHER TEMPERATURE THAN NORMAL CAUSING LOW POWER TREND READINGS AND CRUISE FLIGHT TEMP EXCEEDIN	G GREEN ARC.  INSPECTION REVEALED HOUSING LOOSE DUE TO MOUNTING BOLTS LOSING TORQUE.					1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999082700356	19990827	00356	SW  	1999	8	27	99ZZZX3088       	1	19990712	G	6720	406312103101	LINK            		407012107   	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	B			IIFR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	517R	807  			A256	53231				MECHANIC FOUND WORN BEARINGS, WHILE C/W DAILY INSPECTION, DUE TO STAKING OF BEARING OR PREMATURE WEAR (ON 2 EACH PC LINK	S).					1	G	7	1 	3U			O	H2SW    					 
1999082700357	19990827	00357	SW  	1999	8	27	99ZZZX3089       	1	19990712	G	6710	406310405101	BEARING         			BELL  	407   	407         		SW  										M/R PITCH LINK	LOOSE           	B			IIFR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407AK	547  			RXFS3730	53269				DURING DAILY INSPECTION, FOUND BEARING LOOSE IN HOUSING.  EXCESSIVE AXIAL PLAY.						1	G	7	1 	3U			O	H2SW    					 
1999082700358	19990827	00358	SW  	1999	8	27	99ZZZX3090       	1	19990722	G	6240	407375008101	INDICATOR       			BELL  	407   	407         		SW  										DUAL TACHOMETER	FAILED          	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	60648	8    			0400	53356				DUAL TACHOMETER INDICATOR FAILED.  REPLACED WITH NEW INDICATOR FROM BELL HELICOPTER.						1	G	7	1 	3U			O	H2SW    					 
1999082700359	19990827	00359	EA  	1999	8	27	99ZZZX3091       	2	19990730	G	8500		POWERPLANT      			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE BAY	MALFUNCTIONED   	B				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			SO	15	426ER	1165 				17280647	L2780951A			PILOT REPORTED HE EXPERIENCED A MOMENTARY POWER LOSS WHILE AT A CRUISE POWER SETTING IN LEVEL FLIGHT. THIS AIRCRAFT HAS 	EXPERIENCED SEVERAL OTHER SIMILAR POWER LOSSES.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999082700360	19990827	00360	EA  	1999	8	27	99ZZZX3092       	2	19990706	G	7414		GEAR            		D6LN3P00    	PIPER 	PA32  	PA32R300    	7103213	SO  	LYC   	O540  	IO540K1A5   	41532	EA  					MAGNETO	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	09	8337C	662  			HO39809GR	32R7680101				UPON INSPECTION OF MAGNETO, NOTICED A GEAR TOOTH MISSING ON LEFT DISTRIBUTOR GEAR.						1	L	7	1 	3O	3	O		A3SO    	1E4				 
1999082700361	19990827	00361	EA  	1999	8	27	99ZZZX3093       	2	19990730	G	8500		POWER PLANT     			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE BAY	MALFUNCTIONED   	B				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			SO	16	446ER	1087 				17280609	L2776351A			DURING LEVEL FLIGHT, THE PILOT REPORTED A MOMENTARY LOSS OF POWER.  THIS AIRCRAFT HAS HAD OTHER POWER INTERRUPTIONS.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999082700362	19990827	00362	SW  	1999	8	27	99ZZZX3094       	1	19990805	G	5711	5271	SPAR            			BBAVIA	7     	7GCBC       	1220601	SW  										WING	CRACKED         	B			CXNR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	05	36233					54873				WHILE C/W AD 98-05-04 INSPECTING WING SPARS FOR CRACKS, FOUND A CRACK ON THE RT FORWARD INBOARD SPAR ATTACH POINT.  THE 	CRACK PROTRUDED OUT FROM UNDERNEATH A PLYWOOD DOUBLER ABOUT 2 INCHES.  INSTALLED NEW WINGS WITH METAL SPARS FROM CHAMPIO	N AIRCRAFT.				1	H	7	1 	3O			NC	A759    					 
1999082700363	19990827	00363	SO  	1999	8	27	99ZZZX3095       	1	19990809	G	2820	11502650234	HOSE            			PIPER 	PA24  	PA24260     	7102406	SO  										FUEL SYSTEM	MISMANUFACTURED 	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	11	9306P	312  				244802				FULE HOSE CHANGED 3-14-97, CURE DATE/LOT NR 290 1 Q96. HOSE MANUFACTURE DATE 3-13-97.  HOSE GOES FROM FUEL PUMP TO FUEL 	CONTROL.  HOSE REMOVED TO SHORTEN LENGTH.  HOSE MANDREL WOULD NOT FIT INSIDE HOSE DUE TO COLLAPSED INNER WALL OF HOSE. T	T ON HOSE, 312 HOURS.				1	L	7	1 	3O				1A15    					 
1999082700364	19990827	00364		1999	8	27	99ZZZX3096       	1	19990805	G	3246	152058	WHEEL           	BENDIX      	1542511     															MLG	CRACKED         	B			INWR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					H355					NDT INSPECTION (EDDY CURRENT) SHOWS CRACK INDICATIONS IN OUTBOARD TUBE WELL AREA.																			 
1999082700365	19990827	00365		1999	8	27	99ZZZX3097       	4	19990718	G	3424	1394T100	TURN COORDINATOR																	COCKPIT	MISINSTALLED    	C				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	21										THIS MAKE/MODEL TURN COORDINATOR CONTAINS A PERMANENT MAGENT DC MOTOR THAT GIVES OFF A VERY POWERFUL MAGNETIC FIELD, WHE	THER THE POWER TO IT IS ON OR OFF, THAT CAN ADVERSELY EFFECT OPERATION OF AN INSTRUMENT OVER 14 INCHES AWAY.  ANY INSTRU	MENT MOUNTED NEARBY WITH FERROUS METAL MOVABLE PARTS, ELECTRO-MAGNETIC CIRCUITS AND SIGNAL/ANTENNA CABLES COULD GIVE DAN	GEROUSLY INCORRECT INSTRUMENT READINGS AND/OR HAVE OTHER DEGRADATIONS IN PERFORMANCE.																 
1999082700366	19990827	00366	EA  	1999	8	27	99ZZZX3098       	2	19990730	G	8500		POWER PLANT     			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE BAY	MALFUNCTIONED   	B				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			SO	16	446ER	1092 				17280609	L2776351A			DURING AN INSTRUCTIONAL FLIGHT, THE PILOT REPORTED A TWO TO THREE SECOND POWER LOSS.  THIS OCCURRED JUST BEGINNING CRUIS	E FLIGHT.  THE AIRCRAFT HAS A HISTORY OF MOMENTARY POWER LOSSES AND IS CURRENTLY GROUNDED PENDING FURTHER INVESTIGATION.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999082700367	19990827	00367	EA  	1999	8	27	99ZZZX3099       	2	19990801	G	8500		POWERPLANT      			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE BAY	MALFUNCTIONED   	B				C				ABORTED TAKEOFF         				R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			SO	16	411ER	1753 				17280262	L2729451A			PILOT REPORTED A BRIEF POWER LOSS SHORTLY AFTER TAKEOFF.  AIRCRAFT IS CURRENTLY GROUNDED PENDING INVESTIGATION.  SUBMITT	ER STATED THIS AIRCRAFT HAS HAD OTHER BRIEF POWER INTERRUPTIONS.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999082700368	19990827	00368	EA  	1999	8	27	99ZZZX3100       	2	19990802	G	8500		POWERPLANT      			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE BAY	MALFUNCTIONED   	B				C				ABORTED TAKEOFF         				R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			SO	16	448ER	1077 				17280610	L27773851A			PILOT REPORTED A BRIEF POWER LOSS SHORTLY AFTER TAKEOFF.  AIRCRAFT IS CURRENTLY GROUNDED PENDING INVESTIGATION.						1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999082700369	19990827	00369	EA  	1999	8	27	99ZZZX3101       	2	19990804	G	8500		POWERPALNT      			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE BAY	MALFUNCTIONED   	B				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			SO	16	500ER	714  				17280653	L2782851A			DURING INSTRUCTIONAL FLIGHT, THE INSTRUCTOR REPORTED A HESITATION WHEN POWER WAS APPLIED.  SUBMITTER STATED THIS AIRCRAF	T HAS HAD OTHER SIMILAR POWER INTERRUPTIONS AND IS CURRENTLY GROUNDED PENDING FURTHER INVESTIGATION.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999082700370	19990827	00370	EA  	1999	8	27	99ZZZX3102       	2	19990806	G	8500		POWERPLANT      			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE BAY	MALFUNCTIONED   	B				O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		DE	DESCENT        	1			SO	16	475ER	1055 				17280670	L2786551A			DURING AN INSTRUCTIONAL FLIGHT, THE PILOT REPORTED A TWO TO THREE SECOND ROUGH ENGINE.  THIS WAS ON FINAL AND OCCURRED B	ETWEEN 400 FEET AND 100 FEET.  SUBMITTER STATED THE AIRCRAFT HAS A HISTORY OF MOMENTARY POWER LOSSES AND IS CURRENTLY GR	OUNDED PENDING FURTHER INVESTIGATION.				1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999082700371	19990827	00371	CE  	1999	8	27	99ZZZX3103       	1	19990817	G	2822	5100001	PUMP            	DUKES       		CESSNA	172   	172R        	2072401	CE  										FUEL SYSTEM	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	432ER	933  			0957	17280652				SMALL PARTICLES OF BRASS-LIKE METAL WERE FOUND IN THE FUEL STRAINER.  THE FUEL SYSTEM WAS FLUSHED OUT, AND THE FUEL SERV	O AND FLOW DIVIDER WERE CHANGED.					1	H	7	1 	3O			NT	3A12    					 
1999082700372	19990827	00372	CE  	1999	8	27	99ZZZX3104       	1	19990817	G	5540	053100649	HINGE           			CESSNA	172   	172R        	2072401	CE  										RUDDER	MISDRILLED      	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	99	480ER	739  				17280624				THE LOWER RUDDER HINGE ON THE REAR VERTICAL SPAR IS A LAMINATE OF THE BRACKET AND TWO PLATES ABOUT .1250 INCH THICK EACH	.  THE HOLES THROUGH ALL THREE PIECES SHOULD BE FOR NR 4 RIVETS.  THE HOLES IN THE BRACKET, HOWEVER, APPEAR TO BE NR 5 H	OLES.				1	H	7	1 	3O			NT	3A12    					 
1999082700373	19990827	00373	SO  	1999	8	27	99ZZZX3105       	2	19990813	G	8520	SA630826	BEARING         	SUPAIRPART  		BEECH 	55    	D55         	1152730	CE  	CONT  	O520  	IO520C      	17032	SO  					ENGINE	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	8451N	14   				TE571	287333R			NR 2 AND NR 3 CYLINDERS AND CONNECTING RODS REMOVED FROM BOTH ENGINES FOR C/W TCM CSB99-3.  UPON REMOVAL OF THE CONNECTI	NG RODS, THE ROD BEARINGS (SUPERIOR PN SA630826) WERE FOUND TO HAVE LOST SIGNIFICANT AMOUNT OF BABBITT MATERIAL.  THE RE	MAINING CYLS AND CONNECTING RODS WERE REMOVED FROM BOTH ENGS.  THE ROD BEARINGS WERE FOUND TO BE IN VARIOUS STAGES OF DI	STRESS RANGING FROM SUPERFICIAL PITTING TO COMPLETE LOSS OF BABBITT AND COPPER LAYERS.  BOTH ENGINES WERE TCM FACTORY RE	-MFG.  BOTH DISASSEMBLED FOR PROPELLER STRIKE INSPECTIONS IN 11-98.  AT THAT TIME, BOTH CRANKSHAFTS AND RELATED BEARINGS	 WERE REPLACED.  AT THE TIME BEARING PROBLEM FOUND, TT ON ENGINES 231.0 HRS, TT CONNECTING ROD BEARINGS 14.0 HRS.	1	L	7	2 	3O	3	O		3A16    	E5CE				 
1999082700867	19990827	00867	CE  	1999	8	27	99ZZZX3111       	1	19990727	G	8120	4066104005	TURBOCHARGER    			CESSNA	207   	T207A       	2073614	CE  										ENGINE	FAILED          	D				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			WP	07	9482M	1203 			AG001938	20700698				PILOT REPORTED GOOD M.A.P. AT TAKEOFF.  TWO MINUTES INTO FLIGHT, M.A.P. DROPPED TO 23 INCHES.  THIRTY SECONDS LATER, M.A	.P. DROPPED TO 20 INCHES.  SUSPECT THIS IS WHEN TURBO FROZE UP AND RESTRICTED EXHAUST FLOW LIMITING ENGINE POWER.  SUBMI	TTER STATED NO PASSENGERS ONBOARD OR THIS WOULD HAVE BEEN AN EMERGENCY LANDING.				1	H	7	1 	3O				A16CE   					 
1999082700868	19990827	00868		1999	8	27	99ZZZX3112       	4	19990801	G	3452		TRANSPONDER     	GENAVE      	B5000       	PIPER 	PA28  	PA28140     	7102802	SO  										COCKPIT	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	9305				7580	2821829				REPLACED TRANSPONDER WITH OVERHAULED KING KT76A.  TESTED AND CERTIFIED BY AVIONICS SYSTEMS, CRSFK6R538N.						1	L	7	1 	3O				2A13    					 
1999082700869	19990827	00869		1999	8	27	99ZZZX3113       	1	19990730	G	3242	7010FS9545708	SEAL            		50105201    															BRAKE	FAILED          	B			XC4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19		756  			OCT981513					BRAKE ASSEMBLY, PN 5010520-1, FAILED PREMATURELY.  ONE EACH PISTON LEAKING FROM INSULATOR AREA.  PISTON INTERNALLY FILLE	D WITH FLUID.  EVIDENCE OF T-SEAL FAILURE.  SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY.  FACTORY NEW BRAKE ASSEMBL	Y.																	 
1999082700870	19990827	00870	CE  	1999	8	27	99ZZZX3114       	1	19990806	G	5312	24130013	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9741B	3121 				172RG1004				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700871	19990827	00871	CE  	1999	8	27	99ZZZX3115       	1	19990806	G	5312	24130014	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9741B	3121 				172RG1004				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700872	19990827	00872	CE  	1999	8	27	99ZZZX3116       	1	19990806	G	5312	24130015	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9741B	3121 				172RG1004				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700873	19990827	00873	CE  	1999	8	27	99ZZZX3117       	1	19990806	G	5312	24130016	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9741B	3121 				172RG1004				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700874	19990827	00874	CE  	1999	8	27	99ZZZX3118       	1	19990606	G	5313	24130013	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9654B	11120				172RG0947				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700875	19990827	00875	CE  	1999	8	27	99ZZZX3119       	1	19990606	G	5313	24130014	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9654B	11120				172RG0947				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700876	19990827	00876	CE  	1999	8	27	99ZZZX3120       	1	19990606	G	5313	24130015	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9654B	11120				172RG0947				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700877	19990827	00877	CE  	1999	8	27	99ZZZX3121       	1	19990606	G	5313	24130016	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9654B	11120				172RG0947				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700878	19990827	00878	CE  	1999	8	27	99ZZZX3122       	1	19990606	G	5312	24130013	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	5199U	5695 				172RG0279				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700879	19990827	00879	CE  	1999	8	27	99ZZZX3123       	1	19990606	G	5312	24130014	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	5199U	5695 				172RG0279				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700880	19990827	00880	CE  	1999	8	27	99ZZZX3124       	1	19990606	G	5312	24130015	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	5199U	5695 				172RG0279				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700881	19990827	00881	CE  	1999	8	27	99ZZZX3125       	1	19990606	G	5312	24130016	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	5199U	5695 				172RG0279				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700882	19990827	00882	CE  	1999	8	27	99ZZZX3126       	1	19990606	G	5312	24130013	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9646B	9572 				172RG0942				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700883	19990827	00883	CE  	1999	8	27	99ZZZX3127       	1	19990606	G	5312	24130014	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9646B	9572 				172RG0942				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700884	19990827	00884	CE  	1999	8	27	99ZZZX3128       	1	19990606	G	5312	24130015	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9646B	9572 				172RG0942				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700885	19990827	00885	CE  	1999	8	27	99ZZZX3129       	1	19990606	G	5312	24130016	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9646B	9572 				172RG0942				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700886	19990827	00886	CE  	1999	8	27	99ZZZX3130       	1	19990606	G	5312	24130013	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	93100	9783 				172RG1118				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700887	19990827	00887	CE  	1999	8	27	99ZZZX3131       	1	19990606	G	5312	24130014	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	93100	9783 				172RG1118				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700888	19990827	00888	CE  	1999	8	27	99ZZZX3132       	1	19990606	G	5312	24130015	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	93100	9783 				172RG1118				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700889	19990827	00889	CE  	1999	8	27	99ZZZX3133       	1	19990606	G	5312	24130016	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	93100	9783 				172RG1118				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700890	19990827	00890	CE  	1999	8	27	99ZZZX3134       	1	19990606	G	5312	24130013	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9925B	9383 				172RG1107				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700891	19990827	00891	CE  	1999	8	27	99ZZZX3135       	1	19990606	G	5312	24130014	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9925B	9383 				172RG1107				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700892	19990827	00892	CE  	1999	8	27	99ZZZX3136       	1	19990606	G	5312	24130015	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9925B	9383 				172RG1107				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700893	19990827	00893	CE  	1999	8	27	99ZZZX3137       	1	19990606	G	5312	24130016	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CRACKED         	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	13	9925B	9383 				172RG1107				PILOT REPORTED RUDDER AND TRIM STIFFNESS.  EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 	2413001-4, 2413001-5, 2413001-6, CRACKED.  THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. 	 SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.				1	H	7	1 	3O				3A17    					 
1999082700894	19990827	00894	EA  	1999	8	27	99ZZZX3138       	2	19990612	G	8500		ENGINE          		05K21237A   	PIPER 	PA28  	PA28140     	7102802	SO  	LYC   	O320  	O320E2A     	41508	EA  					FORWARD	MISOVERHAULED   	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	16	8153H					2825347	L2357827A			DURING ANNUAL INSPECTION, NR 3 CYLINDER INDICATED ZERO.  LEAKING PAST VALVE.  REMOVED EXHAUST NOTED SPLIT EXHAUST GUIDE.	  REMOVED CYLINDER, SHIPPED FOR REPAIR AND SUBMITER NOTIFIED THAT CYINDER WAS NEW.  ALL FOUR CYLINDERS WERE BOUGHT NEW F	ROM LCY THROUGH A VENDOR AND SHIPPED TO THE SHOP WHICH INSTALLED THE CYLINDERS AS A SET.				1	L	7	1 	3O	3	O		2A13    	E274				 
1999082700895	19990827	00895	SO  	1999	8	27	99ZZZX3139       	2	19990715	G	8500		ENGINE          			CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  					ENGINE BAY	FAILED          	D				A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CL	CLIMB          	1			NE	05	995RA	3447 	898  			U20604252				PILOT REPORTED ENGINE VIBRATING BADLY AND LOSING POWER ON CLIMB-OUT.  AIRCRAFT MADE A SAFE LANDING AT DEPARTURE AIRPORT.	  OIL WAS ALL ALONG THE RIGHT SIDE OF THE AIRCRAFT.  ON REMOVING THE COWL, A HOLE APPROXIMATELY 2 INCHES BY 3 INCHES WAS	 IN THE CASE AND A CONNECTION ROD CAP WHICH APPEARED TO BE NR 3 WAS STICKING OUT OF THE HOLE WHICH WAS AT THE DATA PLATE	 ATTACH POINT.  THE ENGINE WAS SEIZED.			1	H	7	1 	3O	3	O		A4CE    	E5CE				 
1999082700896	19990827	00896	EA  	1999	8	27	99ZZZX3140       	2	19990729	G	7414	4371	MAGNETO         			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE	FAILED          	B				O				OTHER                   				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			EA	13	9522Q	270  				17280426	L2753051A			WHILE RETURNING HOME FROM A LONG CROSS-COUNTRY, THE ENGINE STARTED TO RUN ROUGH AND THEN IT SMOOTHED OUT.  THE MAGNETOS 	WERE CHECKED IN-FLIGHT, AND FOUND THE LEFT MAGNETO WAS DEAD.  UPON LANDING MAINTENANCE WAS CALLED.  AFTER REMOVING THE C	OWLING, THE LT MAGNETO WAS FOUND BROKEN AT THE LOWER MOUNTING FLANGE AND WAS TILTED UPWARD.  THE MAGNETO WAS REMOVED AND	 FOUND INTERNALLY JAMMED AND THE DRIVE GEAR WAS DAMAGED DUE TO A PARTIAL ENGAGEMENT OF THE ACCESSORY DRIVE GEARS.  THE M	AGNETO AND DRIVE GEAR WERE REPLACED WITH NEW, TIMED TO ENGINE, AND A RUN-UP CHECK WAS COMPLETED.		1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999082700897	19990827	00897		1999	8	27	99ZZZX3141       	4	19990701	G	3416		ENCODER         			PIPER 	PA28  	PA28161     	7102803	SO  										COCKPIT	MALFUNCTIONED   	B			D3BR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	44996					287816054				FOUND THE APOLLO ALT ENCODER PLUS 700 FEET ON INITIAL EVALUATION.  ADJUSTED AND RAN IT UP TO 20,000 FEET AND ERRORS WERE	 WITHIN ACCEPTABLE TOLERANCE.  REPAIRED A STATIC LEAK (OPEN) AT THE PITOT STATIC MAST ASSY AND CHECKED STATIC AND TRANSP	ONDER GOOD.  COULD NOT ISOLATE CAUSE OF 'INVALID' TO SPECIFIC COMPONENT.				1	L	7	1 	3O				2A13    					 
1999082700898	19990827	00898	CE  	1999	8	27	99ZZZX3142       	1	19990629	G	3244	301393353	TIRE            	GOODYEARAERO		BEECH 	B300  	B300        	1159232	CE  										NLG	FAILED          	B			HUNR	O				OTHER                   				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			NM	01	10UN	27   				FL158				TIRE MOUNTED IN NOSE POSITION.  PILOT SAYS SEVERE SHIMMY OCCURRED AT LAST TWO TAKEOFFS, GROUNDED THE AIRCRAFT.  FOUND FA	CTORY INTERNAL BALANCE PATCH HAD COME LOOSE, SHIFTED INSIDE TIRE, CAUSING SEVERE OUT-OF-BALANCE CONDITION.  NO PREVIOUS 	DAMAGE HISTORY.  REPLACED TIRE.				2	L	7	2 	4T			RT	A24CE   					 
1999082700900	19990827	00900	NE  	1999	8	27	99ZZZX3144       	3	19990527	G	6111	D5133	SHIELD          		E10950PK    											HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01					210CMA			HJ30A		NR 3 BLADE EROSION SHIELD DEBOND REQUIRED BLADE OVERHAUL TO REPLACE EROSION SHIELD.																5	C	P10NE	 
1999082700901	19990827	00901	CE  	1999	8	27	99ZZZX3145       	1	19990729	G	7920		PICK-UP         			CESSNA	337   	P337H       	2075731	CE  										ENGINE OIL	OBSTRUCTED      	B			PB2R	O				OTHER                   				W			INADEQUATE Q C            			NR	NOT REPORTED   	1			GL	23	5KV	920  				P3370338				ENGINE OIL PRESSURE LOW (25 PSI MAX).  COULD NOT FIND OBVIOUS CAUSE, SO REMOVED ENGINE FROM AIRCRAFT.  DISASSEMBLED SUMP	 AND ACCESSORY CASE.  FOUND MAG DRIVE CUSHION LODGED IN PICK-UP TUBE RESTRICTING OIL FLOW.  REMOVED AND RE-ASSEMBLED ENG	INE.				1	H	7	2 	3O				A6CE    					 
1999082700902	19990827	00902	CE  	1999	8	27	99ZZZX3146       	1	19990730	G	3230	08411132	ADJUSTING SCREW 			CESSNA	310   	310R        	2074245	CE  										RT MLG	BROKEN          	B			BSYR	O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			GL	07	3597G					310R0875				CMH - RIGHT GEAR COLLAPSED TAXIING OFF RUNWAY.  FOUND EAR BROKEN ON TOP OF GEAR TRUNNION AND ADJUSTING SCREW BROKEN ON D	RAG BRAKE.  REPAIR IN PROGRESS AT THIS TIME.					1	L	7	2 	3O				3A10    					 
1999082700903	19990827	00903	NE  	1999	8	27	99ZZZX3147       	2	19990817	G	7230	56A511	BLADE           			BOEING	767   	7673Y0      		NM  	PWA   	4060  	PW4060      	52119	NE  					COMPRESSOR	FOD DAMAGE      	B			WA2D	K				NONE                    				C			F.O.D.                    			IN	INSP/MAINT     	1			NE	03	632TW					24953	P724603			ENGINE REMOVED, POSITION 2, FOLLOWING INGESTION SEVERAL BIRDS DURING TAKEOFF FROM TLV.  DIS-ASSEMBLED, INSPECTION FOUND 	1 BLADE FRACTURED, OTHER BLADE DAMAGED.  BLADES FORWARDED TO P&W ENGINEERING FOR ANALYSIS.					2	L	7	2 	4F	4	F	RT	A1NM    	E24NE				 
1999082700904	19990827	00904	NE  	1999	8	27	99ZZZX3148       	2	19990814	G	7230	50B798	BEARING         								PWA   	4060  	PW4060      	52119	NE  					COMPRESSOR	FAILED          	B			WA2D	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		2079 			CCWKAM4971		P727854			ETHIOPIAN AIRLINES OPERATED ENGINE REMOVED FOR METAL IN MAIN OIL STRAINER CHIP COLLECTOR.  DISASSEMBLY INSPECTION REVEAL	ED HEAVY SPALLNG ON ONE BALL OF THE NR 1 MAIN BEARING.  THE BEARING WILL BE SENT TO PRATT & WHITNEY ENGINEERING FOR INVE	STIGATION.  CYCLES:  569.									4	F			E24NE				 
1999082700905	19990827	00905	SO  	1999	8	27	99ZZZX3149       	1	19990805	G	5280	47529032	HINGE           			PIPER 	PA31T 	PA31T1      	7103126	SO  										GEAR DOOR	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	2415W					31T8004010				DURING A NORMAL 100-HOUR EVENT INSPECTION, THE RIGHT FORWARD INBOARD GEAR DOOR HINGE WAS FOUND CRACKED.  THE HINGE WAS R	EMOVED AND REPLACED AND RE-RIGGED THE GEAR DOOR.					1	L	7	2 	3T				A8EA    					 
1999090300197	19990903	00197	CE  	1999	9	3	99ZZZX3155       	1	19990819	G	2822	5100001	BOOST PUMP      			CESSNA	172   	172R        	2072401	CE  										FUEL SYSTEM	MAKING METAL    	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	432ER	933  				17280652				RECENTLY, THE AIRCRAFT AND ENGINE MANUFACTURERS HAVE ISSUED A PROCEDURE CHANGE REQUIRING THE BOOST PUMP REMAIN FOR TAKEO	FF AND LANDING.  SINCE THE INCORPORATION OF THIS PROCEDURE, THIS FLEET OF 172R'S HAS BEGUN TO HAVE VERY SMALL BRASS-LIKE	 PARTICLES ACCUMULATE IN THE FUEL STRAINER.  INITIAL REPORTS ON THE PARTICULAR SIZE INDICATE THAT SOME OF THE PARTICLES 	ARE SMALLER THAN THE GASCOLATOR FILTER AND THE INLET SCREEN TO THE FUEL SERVO, POSSIBLY AS SMALL AS 15 MICRON.  WHEN THE	SE PUMPS FAIL, THE SERVO AND THE FUEL MANIFOLD ARE REPLACED AND THE SYSTEM IS FLUSHED.		1	H	7	1 	3O			NT	3A12    					 
1999090300198	19990903	00198	EA  	1999	9	3	99ZZZX3156       	2	19990730	G	8500		POWER PLANT     			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE BAY	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	16	417ER	1580 				17280305	L2727851A			DURING AN INSTRUCTIONAL FLIGHT, THE INSTRUCTOR WAS DEMONSTRATING A SIMULATED EMERGENCY LANDING.  WHEN THE POWER WAS APPL	IED, THERE WAS NO RESPONSE FOR SEVERAL SECONDS.  PRECAUTIONARY LANDING WAS MADE.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999090300199	19990903	00199	EA  	1999	9	3	99ZZZX3157       	2	19990725	G	8530		KEEPER          			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					INTAKE VALVE	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	11	711WX					317552131	L814361A			LEFT ENGINE NR 2 INTAKE VALVE KEEPER BROKE CAUSING VALVE TO HIT PISTON.  PERFORMED TOP OVERHAUL.  CLEANED OUT ALL OIL HO	SES, CHECKED CRANKSHAFT FOR SCORING, CLEANED INTAKE SYSTEM.  FIVE HOURS LATER (TOP) INTAKE VALVE AND PISTON WERE BEAT UP	 BY A PIECE OF METAL.  ENGINE.  REMAINED OUT OF SERVICE FOR TEAR DOWN.				1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999090300201	19990903	00201	SW  	1999	9	3	99ZZZX3159       	1	19990701	G	5711		SPAR            			BBAVIA	7     	7GCAA       	21101N8	SW  										LT WING	CRACKED         	D	L			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	02	5057P					38579				INSPECTED SPARS ON LEFT WING AFTER GROUND LOOP.  FOUND A COMPRESSION FAILURE ON THE REAR SPAR.  COULD NOT TELL CONCLUSIV	ELY IF FRONT SPAR WAS CRACKED OR NOT.  AFTER DISASSEMBLY OF WING, 5 COMPRESSION FAILURES WERE FOUND IN THE AFT SPAR.					1	H	7	1 	3O				A759    					 
1999090300202	19990903	00202	CE  	1999	9	3	99ZZZX3160       	1	19990720	G	7931	26060153	INDICATOR       			CESSNA	208   	208         	2073702	CE  										ENGINE OIL	MALFUNCTIONED   	B			NZBR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	05	248A					20800225				NOTED UPON INSTALLATION AND ENGINE LEAK/FUNCTIONAL TESTS, THAT OIL PRESSURE/TEMPERATURE INDICATOR WAS INDICATING 'LOW' P	RESSURE (SYSTEM WAS BLED PRIOR TO TESTS).  INSTALLED "CALIBRATED' DIRECT READING PRESSURE GAUGE FOR CONFIRMATION.  ENGIN	E RUN-UP AND TEST CONFIRMED ERRONEOUS INDICATION OF 'NEW' INDICATOR.  INSTALLED ANOTHER LIKE SERVICEABLE INDICATOR.				1	H	7	1 	3T			NT	A37CE   					 
1999090300203	19990903	00203	SO  	1999	9	3	99ZZZX3161       	2	19990818	G	8520	25117	PLUG            			PIPER 	J3    	J3          	7100502	SO  	CONT  	A65   	A65*        	17003	SO  					PISTON	WORN            	B	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	88336	85   				15984	31143			FOLLOWING MAJOR OVERHAUL, ALUMINUM PARTICLES WERE FOUND IN THE OIL SCREEN AT ABOUT 30, 55, AND 75 HOURS.  THE DECISION W	AS MADE TO REMOVE THE CYLINDERS AND THE PISTON PIN PLUGS WERE FOUND TO BE THE SOURCE OF THE ALUMINUM.  ALL PLUGS WERE WO	RN BEYOND SERVICE LIMITS IN THE FORM OF A TAPER.  ONE PLUG IN NR 1 CYLINDER WAS WORN .095 INCH AND THE REST WERE .005 IN	CH TO .010 INCH.			1	H	7	1 	3O	3	O		ATC660  	E205				 
1999090300204	19990903	00204	EA  	1999	9	3	99ZZZX3162       	2	19990809	G	8530		STUD            			PIPER 	PA28  	PA28R200    	7102811	SO  	LYC   	O360  	IO360C1C    	41514	EA  					NR 3 CYLINDER	FAILED          	D				O				OTHER                   				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	NR	NOT REPORTED   	1			EA	01	9455N					28R35170	L6230151A			PEN YAN O.H. 8-93 WO NR 11057 TOTAL TIME 1,671 HRS.  PILOT EXPERIENCED ROUGH RUNNING ENGINE.  NR 3 CYLINDER HOLD-DOWN ST	UDS TOP AND BOTTOM RIGHT SNAPPED OFF A CYLINDER FLANGE.  TOP 2 CENTER STUDS SNAPPED AT FLANGE.  BOTTOM RIGHT CENTER STUD	 SNAPPED AT CASE. SMOH:  143 HRS.  TOTAL TIME:  1,814 HRS.				1	L	7	1 	3O	3	O		2A13    	1E10				 
1999090300205	19990903	00205	EA  	1999	9	3	99ZZZX3163       	2	19990728	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE BAY	MALFUNCTIONED   	B				O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		CL	CLIMB          	1			SO	16	425ER	916  				17280646	L2782351A			JUST AFTER ROTATION ON INITIAL CLIMB, THERE WAS A MOMENTARY POWER LOSS.  AFTER A THOROUGH INSPECTION, ALL EIGHT SPARK PL	UGS WERE REPLACED.  AIRCRAFT IS GROUNDED AWAITING FURTHER DIAGNOSES.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999090300206	19990903	00206	CE  	1999	9	3	99ZZZX3164       	1	19990729	G	7910	S19515	OIL DRAIN       			CESSNA	172   	172P        	2072436	CE  										ENGINE	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	01	98574					17276313				DURING 11-HOUR INSPECTION, OIL DRAIN VALVE CAME APART WHILE CLOSING IT AFTER OIL DRAINING.						1	H	7	1 	3O			NT	3A12    					 
1999090300207	19990903	00207	CE  	1999	9	3	99ZZZX3165       	1	19990811	G	5730	052309512	SKIN            			CESSNA	172   	172R        	2072401	CE  										RT WING	CRACKED         	B			WIWR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	852CP	665  				17280485				DURING ROUTINE INSPECTION FOUND THE RIGHT WING INBOARD UPPER FLAP WELL SKIN CRACKED ALONG THE TRAILING EDGE INBOARD NEAR	 THE WING ROOT AREA.  THE CRACKS EXTENDED THROUGH THE RIVET LINE.					1	H	7	1 	3O			NT	3A12    					 
1999090300208	19990903	00208	SO  	1999	9	3	99ZZZX3166       	2	19990726	G	7314	6467681A1	PUMP            			CESSNA	210   	T210N       	2073456	CE  	CONT  	O520  	TSIO520L    	17040	SO  					FUEL SYSTEM	FAILED          	H				O				OTHER                   				Y	J		ENGINE STOPPAGE           	WARNING INDICATION        		NR	NOT REPORTED   	1			SO	15	6622N	383  			F159809BR	21063125	294003R			REPEATEDLY HAD TO ADJUST LOW PRESSURE. ADJUSTED TO 6 POUNDS.   AFTER FLIGHT, ENGINE QUIT AT IDLE ON GROUND.  PRESSURE WE	NT TO 2 POUNDS.  SUBMITTER STATED HAD TO BE ADJUSTED 4 TIMES.					1	H	7	1 	3O	3	O		3A21    	E8CE				 
1999090300209	19990903	00209	SO  	1999	9	3	99ZZZX3167       	1	19990811	G	5521	40075014	SPAR            		5423220     	PIPER 	PA31  	PA31310     	7103103	SO  										ELEVATOR	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	8RU	5737 				317612109				C/W PIPER SB 998A.  FOUND LEFT ELEVATOR SPAR CRACKED.  BOTTOM, OUTBOARD LOCATION IN BEND ABOUT 1.25 INCHES LONG.  SUBMIT	TER STATED THEY HAVE FOUND CRACKS EVERY TIME THEY C/W SB 998A, AND HAVE FOUND MORE CRACKS IN RIBS AND STIFFENERS AT REPL	ACEMENT OF SPAR.				1	L	7	1 	3O			RT	A20SO   					 
1999090300210	19990903	00210	SO  	1999	9	3	99ZZZX3168       	2	19990810	G	8530	654651A5	CYLINDER        			CESSNA	210   	210R        	2073458	CE  	CONT  	O520  	IO520L      	17032	SO  					NR 2	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	23	962CC	1011 				21064986	294785R			DURING A ROUTINE 100-HOUR COMPRESSION TEST, EXCESSIVE LEAKAGE WAS NOTED GOING PAST THE EXHAUST VALVE.  THE EXHAUST VALVE	, EXHAUST VALVE GUIDE FOUND TO BE WORN OUT. THERE WAS NO CHOKE LEFT IN THE CYLINDER BORE.  THIS IS A FACTORY RE-MANUFACT	URED ENGINE.				1	H	7	1 	3O	3	O	RT	3A21    	E5CE				 
1999090300211	19990903	00211	SO  	1999	9	3	99ZZZX3169       	1	19990813	G	8120	565454	SUPPORT         			PIPER 	PA46  	PA46350P    		SO  										TURBOCHARGER	DELAMINATED     	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	05	881DB	1472 				4622067				DURING ROUTINE ENGINE INSPECTION, THE DUCT WAS REMOVED FOR INSPECTION OF THE COMPRESSOR.  THE INTERNAL SUPPORTING WIRE H	AD DELAMINATED AND WAS FOUND RESTING APPROXIMATELY .50 INCH FROM COMPRESSOR WHEEL.  THIS WIRE IS SUPPOSED TO BE HELD IN 	PLACE BY THE ATTACHMENT CLAMP ON THE OUTSIDE OF THE INLET.				1	L	7	1 	3O			RT	A25SO   					 
1999090300212	19990903	00212	EA  	1999	9	3	99ZZZX3170       	2	19990723	G	7414		GEAR            	BENDIX      	SGRN1208    	PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					LT MAGNETO	FRACTURED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	4109D	843  				31853012				PILOT COMPLAINED OF DEAD LT MAGNETO, RT ENGINE.  UPON INSPECTION, FOUND THE MAIN ROTOR GEAR HAD FRACTURED INTO SEVERAL P	IECES.  ALL BREAKS APPEARED FRESH AND CLEAN.					1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999090300213	19990903	00213	EA  	1999	9	3	99ZZZX3171       	2	19990701	G	7414	M3333	IMPULSE COUPLING	SLICK       	6351        	PIPER 	PA32  	PA32301     	7103207	SO  	LYC   	O540  	IO540K1G5   	41532	EA  					MAGNETO	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	8216T	202  				328206037				UPON ROUTINE INSPECTION OF IMPULSE COUPLING, FOUND THAT ONE OF THE PAWL ANCHOR PINS WAS LOOSE IN THE BODY OF THE IMPULSE	.  PART WAS IN SERVICE 202 HOURS.					1	L	7	1 	3O	3	O		A3SO    	1E4				 
1999090300214	19990903	00214	EA  	1999	9	3	99ZZZX3172       	2	19990818	G	8530		VALVE           			CESSNA	172   	172M        	2072418	CE  	LYC   	O320  	O320E2D     	41508	EA  					NR 2 CYLINDER	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	12129	5174 	30   			17261827	L3440727A			DURING A ROUTINE COMPRESSION CHECK, CYLINDER AIR PRESSURE ABOVE 6 PSI COULD NOT BE MAINTAINED IN NR 2 CYLINDER.  AIR WAS	 FELT ESCAPING FROM THE INDUCTION AIRBOX.  MECHANIC TAPPED ON INTAKE VALVE WITH A DRIFT.  SUBSEQUENT COMPRESSION CHECKS 	FAILED AS WELL.  CYLINDER REMOVED.  FOUND EXHAUST VALVE CORRODED AND PITTED BEYOND LIMITS.  INTAKE AND EXHAUST VALVES WE	RE RE-SEATED AND CYLINDER BENCH CHECKED.			1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999090300215	19990903	00215	EA  	1999	9	3	99ZZZX3173       	2	19990818	G	7310		LINE            			CESSNA	172   	172M        	2072418	CE  	LYC   	O320  	O320E2D     	41508	EA  					NR 2 CYLINDER	CHAFED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	12129	5174 				17261827	L3440727A			DURING REMOVAL OF THE NR 2 CYLINDER, MECHANIC NOTED B-NUT ON THE NR 2 CYLINDER FUEL LINE LOCATED AT THE T-FITTING WAS WO	RN.  THE B-NUT HAD BEEN CHAFING AGAINST THE STARTER MOTOR CABLE AND HAD WORN THE FUEL LINE NUT TO AN UNSERVICEABLE CONDI	TION.  REPLACED B-NUT AND REPOSITIONED LINE.				1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999090300216	19990903	00216	GL  	1999	9	3	99ZZZX3174       	3	19990806	G	6114	D7015C87	HUB             			CESSNA	310   	310Q        	2074242	CE  						MCAULY	3AF32C	3AF32C87    	GL  	PROPELLER	MISREPAIRED     	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	07			232  					803852		THE HUB WAS DEEMED UNAIRWORTHY DUE TO IMPROPER PROCEDURES WHEN MODIFYING THE RETENTION NUTS DURING C/W AD NOTE 95-24-05R	1.					1	L	7	2 	3O				3A10    		5	C	P22EA	 
1999090300217	19990903	00217		1999	9	3	99ZZZX3175       	1	19990806	G	3246	313752	WHEEL           	BFGOODRICH  																MLG	CRACKED         	B			INWR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					2403					CRACK ACROSS DRIVE KEY THROUGH TO TUBE WELL AREA, VISUALLY DETETED PRIOR TO NDT INSPECTIONS.																			 
1999090300218	19990903	00218	SO  	1999	9	3	99ZZZX3176       	1	19990701	G	5102		VALVE LINE      			BALWKS	FIREFY	FIREFLY9    	1050124	SO  										ENVELOPE	FAILED          	H	L			O				OTHER                   				O			OTHER                     			LD	LANDING        	1			SW	99	2570E					F9060				IN A HOT AIR BALLOON ENVELOPE EQUIPPED WITH A PARACHUTE, TOP DEFLATION SYSTEM INCLUDING A 3:1 PULLEY ASSIST, THE UPPER S	ECTION OF THE VALVE LINE (BRAIDED KEVLAR CORE COVERED WITH BRAIDED POLYESTER OUTER COVERING) SEPARATED IN A CLEAN CUT BR	EAK FIVE FEET BELOW THE ATTTACH POINT TO THE PARACHUTE LINES, AND FELL OUT OF THE ENVELOPE.  APPROXIMATE TIME ON ENVELOP	E IS 400 HOURS, AGE IS UNDER 5 YEARS. MAXIMUM TEMPERATURE, 275 DEGREES.			1	B	0	0 					A14SO   					 
1999090300219	19990903	00219		1999	9	3	99ZZZX3177       	1	19990803	G	6220	206011111001	BEARING         																	M/R HUB	OVERHEATED      	B			LS1R	K				NONE                    				M	W		OVER TEMP                 	INADEQUATE Q C            		IN	INSP/MAINT     	1			EA	13										DURING HEATING, RACES TURNED TO A GOLDEN BRONZE COLOR TEMPERATURE 200 DEGREES - 250 DEGREES, HEATED LESS THAN 10 MINUTES	.  CONTACTED BELL PRODUCT SUPPORT, SENT FOR EVALUATION.																		 
1999090300220	19990903	00220	CE  	1999	9	3	99ZZZX3178       	1	19990622	G	7800	1650040502	CONTROLLER      			CESSNA	207   	T207A       	2073614	CE  										EXHAUST	MALFUNCTIONED   	H				C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			WP	07	6491H	1200 				20700543				DURING TAKEOFF ROLL, A LOSS OF MANIFOLD PRESSURE OCCURRED OF APPROXIMTAELY 10 IN HG.  TAKEOFF ABORTED WITHOUT INCIDENT. 	 DURING GROUND RUN AND TROUBLESHOOTING, THE PROBLEM WAS DUPLICATED AND DETERMINED TO BE A STICKING WASTEGATE CONTROLLER 	VALVE.  THE CONTROLLER ASSY WAS REPLACED.				1	H	7	1 	3O				A16CE   					 
1999090300221	19990903	00221	CE  	1999	9	3	99ZZZX3179       	1	19990701	G	3242	09113600	CYLINDER        	CLEVELAND   	30143       	CESSNA	441   	441         	2076020	CE  										BRAKE	MISMANFUACTURED 	B		A	WTXR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	2721D					4410161				WHEN THE LEFT AND RIGHT MAIN LANDING GEAR ARE RETRACTED, THE CLEVELAND BRAKE ASSY (PN 30-143) MAKES HOLES IN THE UPPER W	ING SKIN HONEYCOMB (PN 5722311-1).  AT THE SAME TIME, THE BRAKE PISTONS ARE PUSHED INTO THE HOUSING ALLOWING ENOUGH SPAC	E FOR THE BRAKE PADS (PN 066-07300) TO FALL OUT IN-FLIGHT.  THESE BRAKES ARE INSTALLED ON THE CESSNA 441 UNDER STC NR SA	644GL.			1	L	7	2 	3T			RT	A28CE   					 
1999090300222	19990903	00222		1999	9	3	99ZZZX3180       	1	19990803	G	7120	2050601051	MOUNT           																	ENGINE	CRACKED         	B	S		XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01					SC24					FATIGUE CRACKS IN WELDS DETECTED DURING MAGNETIC PARTICLE INSPECTION.  RE:  SKY CONTROLS, INC. P.O NR 3721.																			 
1999090300224	19990903	00224	SO  	1999	9	3	99ZZZX3182       	1	19990813	G	3213	2078900	STRUT           			PIPER 	PA24  	PA24250     	7102404	SO  										MLG	BENT            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	5850P	3607 				24932				DURING AN ANNUAL INSPECTION, THE RT MAIN GEAR STRUT WAS FOUND LEAKING.  THE ASSY WAS DISASSEMBLED.  WHILE TRYING TO RE-I	NSTALL THE LOWER PISTON TUBE BEARING, IT WAS FOUND TO GET STUCK ON THE STRUT TUBE ABOUT HALF-WAY DOWN.  FURTHER INVESTIG	ATION REVEALED THE CHROME WAS WORN ALMOST THROUGH IN THAT LOCATION AND THE TUBE WAS BENT MAKING IT ALMOST IMPOSSIBLE FOR	 THE BEARING WITH NEW O-RING TO GO BEYOND MID-TUBE.			1	L	7	1 	3O				1A15    					 
1999090300225	19990903	00225	SO  	1999	9	3	99ZZZX3183       	1	19990813	G	2740	2039B02	STABILATOR HORN 			PIPER 	PA24  	PA24250     	7102404	SO  										TAIL	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	5850P	3607 				24932				DURING AN ANNUAL INSPECTION, THE STABILATOR HORN TUBE WAS FOUND CORRODED WHERE IT ENTERED THE TORQUE TUBE FITTING.						1	L	7	1 	3O				1A15    					 
1999090300226	19990903	00226	SO  	1999	9	3	99ZZZX3184       	1	19990701	G	5510	AN46A	BOLT            			PIPER 	PA32  	PA32R301    	7103218	SO  										HORIZONTAL STAB	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	16	233PG					32R8013075				NUT BOTTOMED OUT ON SHANK OF BOLT ALLOWING MOVEMENT IN THE VERTICAL FIN DURING FLIGHT.  THE MOUNTING HOLES FOR THE VERTI	CAL FIN ATTACH BRACKET AND REAL BULKHEAD WERE FOUND WORN AND ELONGATED.  FOR THE PROPER GRIP ON THE BOLT, AND EXTRA AN96	0-10 WASHER SHOULD BE ADDED UNDER THE HEAD OF THE BOLT AND A TALLER NUT SUCH AS AN MS 21043-4.  THIS CONDITION WAS FOUND	 AFTER INSPECTION OF CRACKS IN THE FORWARD DORSAL FAIRING.			1	L	7	1 	3O				A3SO    					 
1999090300227	19990903	00227	CE  	1999	9	3	99ZZZX3185       	1	19990813	G	2740	2265500	TORQUE TUBE     			PIPER 	PA24  	PA24180     	7102402	CE  										STABILATOR	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	6747P	3763 				241875				REMOVED BOTH STABILATORS TO REPLACE BEARINGS.  FOUND TORQUE TUBE CORRODED. THIS SECTION CANNOT BE SEEN WITHOUT REMOVING 	STABILATORS.  IT IS AN UNPAINTED STEEL TUBE.  REMOVED CORROSION, ALODINED, PRIMED AND PAINTED.					1	L	7	1 	3O			NT	1A15    					 
1999090300228	19990903	00228	SW  	1999	9	3	99ZZZX3186       	1	19990819	G	7921	8432E	OIL COOLER      	STWARNER    		MOONEY	M20   	M20E        	5870212	SW  										ENGINE OIL	LEAKING         	B			RF3R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	23					4936					PART FAILED DURING NORMAL SERVICE DUE TO EPOXY REPAIR FAILURE.  EPOXY FAILURE IS COMMON IN OIL COOLERS THAT HAVE BEEN RE	PAIRED USING EPOXY.					1	L	7	1 	3O				2A3     					 
1999090300231	19990903	00231	CE  	1999	9	3	99ZZZX3189       	1	19990823	G	2822	5100001	BOOST PUMP      	DUKES       		CESSNA	172   	172R        	2072401	CE  										FUEL SYSTEM	MAKING METAL    	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	477ER	959  			1941	17280622				RECENTLY, THE AIRCRAFT AND ENGINE MANUFACTURER ISSUED A PROCEDURE CHANGE REQUIRING THE BOOST PUMP REMAIN ON FOR TAKEOFF 	AND LANDING.  SINCE THE INCORPORATION OF THIS PROCEDURE, THIS FLEET OF 172R'S HAS BEGUN TO HAVE VERY SMALL BRASS-LIKE PA	RTICLES ACCUMULATE IN THE FUEL STRAINER. INITIAL REPORTS ON THE SIZE INDICATE THAT SOME OF THE PARTICLES ARE SMALLER THA	N THE GASCOLATOR FILTER AND THE INLET SCREEN TO THE FUEL SERVO, POSSIBLY AS SMALL AS 15 MICRON.  WHEN THESE PUMPS FAIL T	HE SERVO AND THE FUEL MANIFOLD ARE REPLACED AND THE SYSTEM IS FLUSHED.		1	H	7	1 	3O			NT	3A12    					 
1999090300232	19990903	00232	CE  	1999	9	3	99ZZZX3190       	1	19990824	G	7312		FLOW DIVIDER    			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE FUEL	MALFUNCTIONED   	H				C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			SW	99	417ER	1613 				17280305	L2727851A			THE STUDENT PILOT REPORTED A ROUGH ENGINE WHEN TAKEOFF WAS ATTEMPTED.  THE FLOW DIVIDER AND FUEL SERVO WERE BOTH CHANGED	.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999090300233	19990903	00233	EA  	1999	9	3	99ZZZX3191       	2	19990824	G	7322		FUEL SERVO      			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE	MALFUNCTIONED   	H				C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			SW	99	417ER	1613 				17280305	L2727851A			THE STUDENT PILOT REPORTED A ROUGH ENGINE WHEN TAKEOFF WAS ATTEMPTED.  THE FLOW DIVIDER AND FUEL SERVO WERE BOTH CHANGED	.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999090300234	19990903	00234	CE  	1999	9	3	99ZZZX3192       	1	19990810	G	5720	0713610910	FITTING         			CESSNA	182   	182G        	2072716	CE  										WING STRUT	CRACKED         	G	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	3111S					18255611				FOUND CRACK IN LOWEST (AS INSTALLED) RIVET HOLE.  INSPECTING SIMILAR (1963-1974) 182'S, SUBMITTER HAS FOUND 3 CRACKS IN 	A MONTH.					1	H	7	1 	3O			NT	3A13    					 
1999090300235	19990903	00235	CE  	1999	9	3	99ZZZX3193       	1	19990727	G	7603	565549021	CONTROL CABLE   			CESSNA	172   	172S        	2072439	CE  										CARBURETOR	DISCONNECTED    	B			PHKR	O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			CE	01	947SP	49   				172S8142				THROTTLE CONTROL DISCONNECTED FROM CARBURETOR ROD END IN-FLIGHT. FOUND TWO JAM NUTS INSTALLED.  CHECKED SERVICE MANUAL, 	ONLY SUPPOSED TO BE ONE.  REMOVED ONE JAM NUT AND RE-ATTACHED THROTTLE CONTROL TO ROD END, RIGGED AND TIGHTENED JAM NUT.	  CHECKED OPERATION.				1	H	7	1 	3O			NT	3A12    					 
1999090300236	19990903	00236	GL  	1999	9	3	99ZZZX3194       	3	19990212	G	6111	V84334R	BLADE           			BEECH 	35    	S35         	1151532	CE  						HARTZL	HCA3V	PHCA3VF4    	GL  	PROPELLER	CRACKED         	B			PHKR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01	5831S	3274 			41605	D7731		BL450		FOUND CRACK RUNNING AROUND THE CIRCUMFERENCE OF THE BLADE SHANK BETWEEN THE TWO SHOULDERS.  THE PROPELLER WAS UNDERGOING	 THE INSPECTION FOR AD 97-18-02.					1	L	7	1 	3O				3A15    		5	C	P6EA	 
1999090300751	19990903	00751		1999	9	3	99ZZZX3200       	4	19990507	G	2312	064105430	TRANSCEIVER     		KY196A      	SNIAS 	350   	AS350B2     	8680813	EU  										VHF COMM	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	350AZ	44   			24720	3127				TRANSCEIVER WILL NOT STORE AND HOLD CHANNELS.  REF:  MCN 70.  REMOVED AND REPLACED.						1	G	7	1 	3U				H9EU    					 
1999090300752	19990903	00752	EU  	1999	9	3	99ZZZX3201       	1	19990404	G	2432	45043003	BATTERY         			UROCOP	EC135 	EC135P1     	8680990	EU  										E/E BAY	DISCHARGED      	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4066P	57   			1037	0070				AIRCRAFT WILL NOT START ON BATTERY.  BOX WILL NOT TEST.  REF:  RMA NR R019573 MCN NR 8.  REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999090300753	19990903	00753	EU  	1999	9	3	99ZZZX3202       	1	19990331	G	2450	45033500	MASTER BOX      			UROCOP	EC135 	EC135P1     	8680990	EU  										ELECTRICAL	SHORTED         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	4066P	43   			1074	0070				GENERATOR DISCONNECT LIGHT 'ON'.  FAILED SELF-TEST.  FAIL CODE LIGHTS RF2.  REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999090300754	19990903	00754	EU  	1999	9	3	99ZZZX3203       	1	19990609	G	6330	L633M2001105	MOUNT           		ZRIS        	UROCOP	EC135 	EC135P1     	8680990	EU  										TRANSMISSION	OUT OF TOLERANCE	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	4066P	113  			303	0070				STOP GAP OUT OF TOLERANCE (.045 INCH).  LEAKING FLUID.  REF:  RMA NR R020111 MCN 92.  REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999090300755	19990903	00755	EU  	1999	9	3	99ZZZX3204       	1	19990519	G	3242	L635M1021001	CALIPER         			UROCOP	EC135 	EC135P1     	8680990	EU  										BRAKE	LEAKING         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	4066P	113  				0070				CALIPER LEAKING.  REF:  RMA NR R020114 MCN 90.  REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999090300756	19990903	00756	EU  	1999	9	3	99ZZZX3205       	1	19990519	G	6330	L633M2001105	MOUNT           			UROCOP	EC135 	EC135P1     	8680990	EU  										TRANSMISSION	LEAKING         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	4066P	113  				0070				TRANSMISSION MOUNT LEAKING FLUID.  REF:  RMA NR R020111MCN 91.  REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999090300757	19990903	00757	EU  	1999	9	3	99ZZZX3206       	1	19990529	G	7714	L771M40C1005	INDICATOR       			UROCOP	EC135 	EC135P1     	8680990	EU  										TRIPLE TACH	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4066P	136  			034	0070				NO N2 INDICATION.  REF:  RMA NR R020324 MCN 94.  REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999090300758	19990903	00758	EU  	1999	9	3	99ZZZX3207       	1	19990423	G	7714	6147640311	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	INACCURATE      	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	5206W	5    			607	3140				INDICATOR READS 100 WHEN INSTALLED.  REF:  RMA R019830.  REF:  MCN 36.  REMOVED AND REPLACED.						1	G	7	1 	3U				H9EU    					 
1999090300759	19990903	00759	EU  	1999	9	3	99ZZZX3208       	1	19990423	G	7110	350A5801160001	COWLING         			SNIAS 	350   	AS350B2     	8680813	EU  										ENGINE	DELAMINATED     	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	5206W	5    				3140				COWLING DELAMINATED.  REF:  RMA NR R019830.  REF:  MCN 35.  REMOVED AND REPLACED.						1	G	7	1 	3U				H9EU    					 
1999090300760	19990903	00760	EU  	1999	9	3	99ZZZX3209       	1	19990414	G	6230	1051310114	SILVER SHIM     			BOLKMS	117   	BK117A4     	5626017	EU  										MAIN ROTOR	LEAKING         	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	711FC	152  				7070				SILVER SHIM ON MAIN ROTOR LEAKING.  REF:  MCN 33.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999090300761	19990903	00761	EU  	1999	9	3	99ZZZX3210       	1	19990407	G	3340	G62504	SEARCH LIGHT    			BOLKMS	117   	BK117A4     	5626017	EU  										FUSELAGE	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	711FC	49   				7070				SEARCH LIGHT WILL NOT EXTEND OR SHUT OFF.  REF:  MCN 23.						1	G	7	2 	3U				H13EU   					 
1999090300762	19990903	00762	EU  	1999	9	3	99ZZZX3211       	1	19990414	G	6210	1171310315	BUSHING         			BOLKMS	117   	BK117A4     	5626017	EU  										MAIN ROTOR	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	711FC	5836 				7070				BUSHINGS WORN ON MAIN ROTOR.  REF:  MCN 34.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999090300763	19990903	00763	EU  	1999	9	3	99ZZZX3212       	1	19990619	G	2840	DK042MOD0	TRANSMITTER     		DK042       	BOLKMS	105   	BO105LSA3   	5626020	EU  										FUEL	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	911SY	48   			12436	2033				TERMINAL BROKEN.  REF:  MCN 108.  REMOVED AND REPLACED.						1	G	7	2 	3U				H3AU    					 
1999090300766	19990903	00766	SW  	1999	9	3	99ZZZX3214       	1	19990413	G	7810	206064300005	STACK           			BELL  	206   	206L3       	1182108	SW  										EXHAUST	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7159H	883  			980210	51397				EXHAUST STACK CRACKED.						1	G	7	1 	3U				H2SW    					 
1999090300767	19990903	00767	SW  	1999	9	3	99ZZZX3215       	1	19990828	G	6310	222044006109	SHAFT           			BELL  	430   	430         	1182150	SW  										TRANSMISSION	CORRODED        	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	30   			A390	49037				MAIN DRIVE SHAFT 12-MONTH INSPECTION AND REPACK.  DISASSEMBLED, FOUND RUSTED AND PITTED ON COUPLINGS AND GEARS.						1	G	7	2 	3U			RT	H9SW    					 
1999090300768	19990903	00768	SW  	1999	9	3	99ZZZX3216       	1	19990828	G	6310	222044006109	SHAFT           			BELL  	430   	430         	1182150	SW  										TRANSMISSION	CORRODED        	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	30   			A399	49037				MAIN DRIVE SHAFT DUE 12-MONTH INSPECTION AND REPACK.  DISASSEMBLED, INSPECTED.  FOUND CORRODED ON COUPLINGS AND GEARS.						1	G	7	2 	3U			RT	H9SW    					 
1999090300769	19990903	00769	SW  	1999	9	3	99ZZZX3217       	1	19990109	G	6730	065001620200	SERVO ACTUATOR  			BELL  	430   	430         	1182150	SW  										MAIN ROTOR	FAILED          	B			AC2R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	430CH	381  			2167	49037				INTERMITTENT FAILURE - AFCS YAW CAUTION LIGHT ILLUMINATED AFTER AFCS TEST AND WHEN AP IS SELECTED ON THE FLIGHT DIRECTOR	, LIGHT EXTINGUISHES WHEN F.D. IS PLACED IN SCAS.  (FAILURE CODE 1605).  REPLACED PER BRIAN JENKINS BHT PRODUCT SUPPORT.					1	G	7	2 	3U			RT	H9SW    					 
1999090300772	19990903	00772	SW  	1999	9	3	99ZZZX3220       	1	19990120	G	3340	01077028521C	LIGHT           		02141       	BELL  	430   	430         	1182150	SW  										STROBE	INOPERATIVE     	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	414  				49037				STROBE LIGHT INOPERATIVE.						1	G	7	2 	3U			RT	H9SW    					 
1999090300773	19990903	00773	SW  	1999	9	3	99ZZZX3221       	1	19990324	G	6410		BEARING         		222012701125	BELL  	430   	430         	1182150	SW  										T/R BLADE	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  			A405	49037				TAIL ROTOR FEATHERING BEARINGS CRACKED ON BOTH TAIL ROTOR BLADES AND TAIL ROTOR TRUNNION BEARINGS ROUGH.  RE:  CHEVRON S	/O NR 526657PNAV.					1	G	7	2 	3U			RT	H9SW    					 
1999090300774	19990903	00774	SW  	1999	9	3	99ZZZX3222       	1	19990324	G	6420		BEARING         		222012701125	BELL  	430   	430         	1182150	SW  										TRUNNION	ROUGH           	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  			A405	49037				TAIL ROTOR FEATHERING BEARINGS CRACKED ON BOTH TAIL ROTOR BLADES AND TAIL ROTOR TRUNNION BEARINGS ROUGH.  RE:  CHEVRON S	/O NR 526657PNAV.					1	G	7	2 	3U			RT	H9SW    					 
1999090300775	19990903	00775	SW  	1999	9	3	99ZZZX3223       	1	19990322	G	5210	NAS5623R7A	CAM FOLLOWER    			BELL  	430   	430         	1182150	SW  										DOOR	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  				49037				CAM FOLLOWER CRACKED AND MISSING.  DOOR WILL NOT LOCK OPEN.						1	G	7	2 	3U			RT	H9SW    					 
1999090300776	19990903	00776	SW  	1999	9	3	99ZZZX3224       	1	19990322	G	7810	230063301102	STACK           			BELL  	430   	430         	1182150	SW  										EXHAUST	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  				49037				NR 2 ENGINE EXHAUST DUCT ASSY CRACKED.  REPLACED EXHAUST DUCT.						1	G	7	2 	3U			RT	H9SW    					 
1999090300777	19990903	00777	SW  	1999	9	3	99ZZZX3225       	1	19990323	G	6230	430310450101	BEARING         			BELL  	430   	430         	1182150	SW  										SWASHPLATE	FAILED          	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  			ZV7050	49037				FAILED ASB-430-99-0, GREASE HAS METAL IN IT.  REPLACED SWASHPLATE DUPLEX BEARING.						1	G	7	2 	3U			RT	H9SW    					 
1999090300797	19990903	00797	SW  	1999	9	3	99ZZZX3245       	1	19990324	G	6310	222044607003	COUPLING        			BELL  	430   	430         	1182150	SW  										M/R DRIVE	CORRODED        	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	1158 			A1648	49037				CORROSION UNDER PRIMER.  TRANSMISSION END OF SHAFT HAD CORROSION.  ENGINE END WITH NO PRIMER DID NOT HAVE CORROSION.						1	G	7	2 	3U			RT	H9SW    					 
1999090300798	19990903	00798	SW  	1999	9	3	99ZZZX3246       	1	19990324	G	6310	222044672101	COUPLING        			BELL  	430   	430         	1182150	SW  										M/R DRIVE	CORRODED        	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  			A1280	49037				CORROSION UNDER PRIMER AND ON SPLINES.						1	G	7	2 	3U			RT	H9SW    					 
1999090300799	19990903	00799	SW  	1999	9	3	99ZZZX3247       	1	19990324	G	6310	222044672101	COUPLING        			BELL  	430   	430         	1182150	SW  										M/R DRIVE	CORRODED        	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	1158 			A1296	49037				CORROSION UNDER PRIMER ON TRANSMISSION END.						1	G	7	2 	3U			RT	H9SW    					 
1999090300800	19990903	00800	SW  	1999	9	3	99ZZZX3248       	1	19990703	G	6230	430340036101	BEARING         			BELL  	430   	430         	1182150	SW  										MAST	FAILED          	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	930  			AV7079	49037				BEARING CAUSING CHIP LIGHT.						1	G	7	2 	3U			RT	H9SW    					 
1999090300801	19990903	00801	SW  	1999	9	3	99ZZZX3249       	1	19990320	G	3340		BULB            		01077050100 	BELL  	430   	430         	1182150	SW  										STROBE	FAILED          	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	541  				49037				BULB BURNED OUT AND LENS CRACKED.						1	G	7	2 	3U			RT	H9SW    					 
1999090300802	19990903	00802	SW  	1999	9	3	99ZZZX3250       	1	19990320	G	3340		LENS            		01077050100 	BELL  	430   	430         	1182150	SW  										STROBE	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	541  				49037				BULB BURNED OUT AND LENS CRACKED.						1	G	7	2 	3U			RT	H9SW    					 
1999090300803	19990903	00803	SW  	1999	9	3	99ZZZX3251       	1	19990327	G	6220		LOCK RING       			BELL  	430   	430         	1182150	SW  										DRIVE HUB	MISSING         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	590  				49037				LOCK RING MISSING FROM BOLT.  REPLACED BOLT.						1	G	7	2 	3U			RT	H9SW    					 
1999090300804	19990903	00804	SW  	1999	9	3	99ZZZX3252       	1	19990326	G	2431	39563001	BATTERY         			BELL  	430   	430         	1182150	SW  										E/E BAY	DISCHARGED      	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  			9700853	49037				BATTERY FAILED FUNCTIONAL CHECK.  REPLACED BATTERY.						1	G	7	2 	3U			RT	H9SW    					 
1999090300805	19990903	00805	SW  	1999	9	3	99ZZZX3253       	1	19990328	G	6320	222020576103	COVER           			BELL  	430   	430         	1182150	SW  										ROTOR BRAKE	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  				49037				ROTOR BRAKE COVER CRACKED.  REPLACED COVER.						1	G	7	2 	3U			RT	H9SW    					 
1999090300806	19990903	00806	SW  	1999	9	3	99ZZZX3254       	1	19990323	G	6220		LONG RING       			BELL  	430   	430         	1182150	SW  										PITCH LINK	BROKEN          	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  				49037				M/R UNIVERSAL TO P.C. LINK BOLT HAS BROKEN LOCK RING.						1	G	7	2 	3U			RT	H9SW    					 
1999090300808	19990903	00808	SW  	1999	9	3	99ZZZX3256       	1	19990329	G	6210	430015001123	BLADE           			BELL  	430   	430         	1182150	SW  										MAIN ROTOR	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  			A569	49037				OUTBOARD TRIM TAB CRACKED.						1	G	7	2 	3U			RT	H9SW    					 
1999090300809	19990903	00809	SW  	1999	9	3	99ZZZX3257       	1	19990329	G	6210	430015001123	BLADE           			BELL  	430   	430         	1182150	SW  										MAIN ROTOR	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  			A565	49037				OUTBOARD TRIM TAB CRACKED.						1	G	7	2 	3U			RT	H9SW    					 
1999090300810	19990903	00810	SW  	1999	9	3	99ZZZX3258       	1	19990329	G	6210	430015001123	BLADE           			BELL  	430   	430         	1182150	SW  										MAIN ROTOR	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  			A570	49037				OUTBOARD TRIM TAB CRACKED.						1	G	7	2 	3U			RT	H9SW    					 
1999090300811	19990903	00811	SW  	1999	9	3	99ZZZX3259       	1	19990329	G	6210	430015001123	BLADE           			BELL  	430   	430         	1182150	SW  										MAIN ROTOR	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  			A568	49037				OUTBOARD TRIM TAB CRACKED.						1	G	7	2 	3U			RT	H9SW    					 
1999091000001	19990910	00001	CE  	1999	9	10	99ZZZX3273       	1	19990810	G	3230	05412024	BUSHING         			CESSNA	172   	172R        	2072401	CE  										RT MLG	FAILED          	B			WIWR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	852CP	665  				17280485				THE RIGHT MAIN LANDING GEAR BUSHING WAS FOUND SEVERELY DEFORMED DURING A ROUTINE INSPECTION.  THE BUSHING MATERIAL WAS P	RESSED ALMOST COMPLETELY OUT OF THE BUSHING CASE PROTRUDING AROUND THE GEAR LEG.					1	H	7	1 	3O			NT	3A12    					 
1999091000003	19990910	00003	CE  	1999	9	10	99ZZZX3275       	1	19990805	G	2701	9652402915	COLUMN          		965240113   	BEECH 	56    	56TC        	1152736	CE  										CONTROL WHEEL	BROKEN          	G				A				UNSCHED LANDING         				D	F		INFLIGHT SEPARATION       	FLT CONT AFFECTED         		NR	NOT REPORTED   	1			NM	02	6252V	1981 				TG49				AIRCRAFT ENCOUNTERED TURBULENCE IN-FLIGHT, CONTROL BROKE, PILOT CONTROLLED AIRCRAFT IN ROLL AXIS WITH AUTOPILOT TO SAFE 	LANDING.  WELD BROKE WHERE SHAFT WELDED TO FLANGE OF CONTROL WHEEL ADAPTER ASSEMBLY.  AD 71-24-10 WAS C/W 2-17-72.  SUBM	ITTER RECOMMENDED AD BE ISSUED TO EITHER REMOVE AND INSPECT ADAPTER ASSEMBLY OR REPLACE USING LATER IMPROVED PART NUMBER	 ADAPTER ASSEMBLY.			1	L	7	2 	3O				3A16    					 
1999091000004	19990910	00004	EA  	1999	9	10	99ZZZX3276       	2	19990719	G	7414	LW3852411585F	POINTS          		D4RN2021    	CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					MAGNETO	WORN            	H				A				UNSCHED LANDING         				X	J		ENGINE FLAMEOUT           	WARNING INDICATION        		NR	NOT REPORTED   	1			SW	99	739ZY				9663K	17270948	L599476T			AIRCRAFT ENGINE QUIT IN-FLIGHT.  MAGNETO CONTACT POINTS CLOSED, CONTACT POINTS WORE DOWN.  SUBMITTER SUGGESTED CHECKING 	CONTACT POINTS EVERY 100 HOURS AND CHECK CAM FOR PITS.					1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999091000005	19990910	00005	SO  	1999	9	10	99ZZZX3277       	1	19990802	G	3213	67926804	TRUNNION        			PIPER 	PA44  	PA44180     	7104402	SO  										MLG	FRACTURED       	C				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	05	2126X					447995273				LEFT MAIN LANDING GEAR TRUNNION FRACTURED UPON LANDING.  LEFT WING AND PROPELLER CONTACTED RUNWAY.  NO INJURIES.  AIRCRA	FT REPAIRABLE.  FRACTURE IS AT AFT WEB.					1	L	7	2 	3O				A19S0   					 
1999091000006	19990910	00006	EA  	1999	9	10	99ZZZX3278       	2	19990813	G	8530	SL10545	PISTON          			PIPER 	PA32  	PA32RT300T  	7103216	SO  	LYC   	O540  	TIO540S1AD  	41532	EA  					CYLINDER	DAMAGED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	2144C					32R7987046	L591161A			DURING TOP OVERHAUL, NOTICED LOWER EDGE OF PISTON SKIRT ON SUPERIOR SL10545 PISTONS HAD BEEN CONTACTING OPPOSING CONNECT	ING ROD CAPS AT BOTTOM OF STROKE.  THE NEW PISTON REPLACMENTS SL10545 HAVE DIFFERENT DIMENSIONS MEASURED FROM LOWER EDGE	 OF PISTON PIN HOLE TO LOWER EDGE OF SKIRT BY APPROXIMATELY .015 INCH ALLOWING CLEARANCE WITH OPENING CONNECTION ROD CAP	S.			1	L	7	1 	3O	3	O		A3SO    	E14EA				 
1999091000007	19990910	00007		1999	9	10	99ZZZX3279       	1	19990816	G	3246	152059	WHEEL           	BENDIX      																MLG	CRACKED         	B			INWR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					B4977					NDT INSPECTION SHOWED CRACK INDICATIONS AROUND BOLT HOLE AREA.																			 
1999091000008	19990910	00008	GL  	1999	9	10	99ZZZX3280       	2	19990810	G	7230	68760050	BEARING         		6858348     	HILLER	FH1100	FH1100      	3376502	NM  	ALLSN 	250C  	250C18      	03011	GL  					COMPRESSOR	GALLED          	E				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	370FH	866  			CAC21331B	98	CAE80001B			BEARING FOUND GALLED IN ENGINE COMPRESSOR SECTION.						1	G	7	1 	3U	3	U		H2WE    	E4CE				 
1999091000009	19990910	00009	EU  	1999	9	10	99ZZZX3281       	1	19990810	G	2560	DOAP101JK	PUMP            			BOLKMS	117   	BK117A3     	5626015	EU  										CABIN	FAILED          	B		A	TI1R	A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			SW	05	527MB				9704	7103				MED VAC PUMP MOTOR SEIZING-UP CAUSING SMOKE AND FUMES IN COCKPIT WHICH CREATED AN EMERGENCY LANDING.  REPLACED WITH SERV	ICEABLE VAC PUMP ASSY.  FUNCTIONAL CHECK OK.  NO FURTHER PROBLEMS.					1	G	7	2 	3U				H13EU   					 
1999091000010	19990910	00010	EU  	1999	9	10	99ZZZX3282       	1	19990803	G	6230	1171260901	BEARING         		1171200501  	BOLKMS	117   	BK117A1     	5626010	EU  										M/R MAST	CRACKED         	B		A	TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	117M	5731 	2783 		R22	S7023				DURING A MAST NUT TORQUE CHECK, A MECHANIC NOTICED EXCESSIVE AXIAL PLAY IN MAIN ROTOR MAST.  UPON MEASURING PLAY, IT WAS	 FOUND TO BE OUT OF LIMITS AND TRANSMISSION WAS SENT TO OVERHAUL SHOP FOR EVALUATION.  TRANSMISSION WAS INSPECTED AND TH	IS BALLBEARING WAS FOUND CRACKED THROUGH ON THE OTHER RACE.  EUROCOPTER WAS CONTACTED AND BEARING WAS REPLACED.  MAST AX	IAL PLAY WAS FOUND WITHIN LIMITS IAW BK117 REM 108 RU 7 AFTER BEARING REPLACEMENT.			1	G	7	2 	3U				H13EU   					 
1999091000011	19990910	00011	SW  	1999	9	10	99ZZZX3283       	1	19990731	G	6220	204031920003	BEARING         			BELL  	212   	212         	1181420	SW  										DAMPER	LOOSE           	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530B					30702				UPPER BEARING LOOSE IN DAMPER.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999091000012	19990910	00012	SW  	1999	9	10	99ZZZX3284       	1	19990731	G	3213	2120304371	CAP             			BELL  	212   	212         	1181420	SW  										CROSSTUBE	DEBONDING       	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8520B					30702				RUBBER DEBONDING. REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999091000013	19990910	00013	GL  	1999	9	10	99ZZZX3285       	2	19990816	G	7230	6877410	CASE HALVES     			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	DAMAGED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	5211K	1177 			SET26111	1161D	CAE834135			DRESSED OUT MINOR FOD DAMAGE.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999091000014	19990910	00014		1999	9	10	99ZZZX3286       	4	19990731	G	3120	16100	CLOCK           			HUGHES	369   	369D        	4470706	WP  										COCKPIT	DAMAGED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	1097J				B9601	900801D				KNOB BROKEN FROM SHAFT.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999091000015	19990910	00015	WP  	1999	9	10	99ZZZX3287       	1	19990804	G	2810	369H81013	FUEL CELL       			HUGHES	369   	369D        	4470706	WP  										FUSELAGE	CRACKED         	B			LS1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13	5211R	4394 			83	1161D				FUEL CELL HAS SLIGHT HAIRLINE CRACK IN TOP OF BLADDER AROUND PLATE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999091000016	19990910	00016	SW  	1999	9	10	99ZZZX3288       	1	19990731	G	6240	206070265001	DUAL TACHOMETER 			BELL  	206   	206B        	1181511	SW  										COCKPIT	INOPERATIVE     	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	90322				1461D	1736				TURBINE PORTION OF DUAL TACHOMETER DOES NOT OPERATE.  NEEDLE DOES NOT MOVE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999091000017	19990910	00017	WP  	1999	9	10	99ZZZX3289       	1	19990731	G	7712	369H45267	INDICATOR       			HUGHES	369   	369E        	4470707	WP  										COCKPIT	FLUCTUATES      	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8330P		1508 		1217	0330E				TORQUE GAUGE FLUCTUATES 4-8 PSI.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999091000018	19990910	00018		1999	9	10	99ZZZX3290       	4	19990731	G	3120	7916190	CLOCK           			BELL  	206   	206B3       	1181506	SW  										COCKPIT	INOPERATIVE     	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	20BY					2871				CLOCK INOPERATIVE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999091000019	19990910	00019		1999	9	10	99ZZZX3291       	4	19990730	G	3453	KFS598	VHF CONTROL     			BELL  	206   	206L3       	1182108	SW  										COCKIT	CONTAMINATED    	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	17238				3816	51492				MOISTURE GETS TRAPPED UNDER THE HEADER AND CAUSES A SHORT ON THE 180V DC LINE.  BURNS THE BOARD AND HEADER.						1	G	7	1 	3U				H2SW    					 
1999091000020	19990910	00020	NM  	1999	9	10	99ZZZX3292       	1	19990726	G	6710	600N76051	BEARING         			DOUG  	600N  	600N        	3027377	NM  										BELLCRANK	LOOSE           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	17	609BP	200  				RN038				DURING AN ANNUAL INSPECTION LOOKING OVER THE FLIGHT CONTROLS, THE LONG CONTROL ROD BELLCRANK WAS LOOSE.  REMOVED PART FR	OM AIRCRAFT.  BEARING WAS INSIDE HOUSING.					1	G	7	1 	3U			NC	H3WE    					 
1999091000021	19990910	00021	SW  	1999	9	10	99ZZZX3293       	1	19990726	G	6210	407015001117	BLADE           			BELL  	407   	407         		SW  										MAIN ROTOR	PEELING         	B			ULXR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01	1116H	300  			A580	53046				DURING ROUTINE INSPECTION, DISCOVERED LEADING EDGE ABRASION STRIP PEELING OFF.  POSSIBLE BONDING METHOD AT TIME OF MANUF	ACTURE.					1	G	7	1 	3U			O	H2SW    					 
1999091000022	19990910	00022	SW  	1999	9	10	99ZZZX3294       	1	19990611	G	6510	406040340101	DISK PACK       			BELL  	407   	407         		SW  										T/R DRIVE	BROKEN          	B			ULXR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01	1116H	328  			RNFS8909	53046				INSPECTING HELICOPTER PER AD 97-22-15.  FOUND MOST FORWARD POSITION DISK PACK WITH ONE BROKEN DISK.  REPLACED DAMAGED PA	RTS.					1	G	7	1 	3U			O	H2SW    					 
1999091000023	19990910	00023	NE  	1999	9	10	99ZZZX3295       	2	19990805	G	7323	PTG3	GOVERNOR        	CHNDLREVANS 		BELL  	204   	204B        	1181404	SW  	LYC   	T53   	T53*        	41549	NE  					ENGINE	MISOVERHAULED   	B		A	SF3R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NE	03			2991 		692AM13163					DURING ROUTINE OVERAHAUL DISASSEMBLY PROCEDURE, FOUND ONE OF THE TWO 'S' WIRES INSTALLED AT EACH END OF THE FLYWEIGHT PI	VOT PIN WAS MISSING AND PRESUMED NOT INSTALLED DURING LAST OVERHAUL OR MAJOR MAINTENANCE.  THE EVIDENCE OF OPERATION IN 	THIS CONDITION OVER AN EXTENDED PERIOD OF TIME WAS THE PRESENCE OF A CIRCUMFERENTIAL GROOVE THAT WAS FORMED BY CONTACT B	ETWEEN THE PIVOT PIN AND GOVERNOR HOUSING ASSEMBLY.			1	G	7	1 	4U	4	U		H1SW    	E1EA				 
1999091000026	19990910	00026	NE  	1999	9	10	99ZZZX3298       	2	19990131	G	7230	1015551561	COMPRESSOR      			BEECH 	200   	B200        	1152922	CE  	PWA   	PT6   	PT6A42      	52043	NE  					ENGINE	SEIZED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	75LV	13   				BB1075				COMPRESSOR LOCKED UP.  REF:  MCN NR 4.						1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999091000027	19990910	00027		1999	9	10	99ZZZX3299       	1	19990413	G	6320	1171211501	GEAR            																	M/R GEARBOX	CORRODED        	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05					KA0443					CORROSION PITTING ON BEARING RACE.  REJECTED.  REF:  RMA NR R019740.  MCN NR 7.  REMOVED AND REPLACED.																			 
1999091000029	19990910	00029		1999	9	10	99ZZZX3301       	1	19990114	G	6320	B4678	CHIP DETECTOR   																	M/R GEARBOX	FAILED          	B			AC2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										PART FAILED NEW 'OUT OF BOX'.																			 
1999091000030	19990910	00030		1999	9	10	99ZZZX3302       	1	19990902	G	6310	222044006109	SHAFT ASSY      																	TRANSMISSION	CORRODED        	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03					A429					NEW PART DISASSEMBLED.  FOUND CORRODED ON GEAR AND SHAFT MISSING CORK AT ONE END.																			 
1999092100007	19990921	00007	NE  	1999	9	21	99ZZZX3303       	2	19990618	G	8530	126742	CYLINDER        			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R9855       	52008	NE  					ENGINE	CRACKED         	E				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	144Q		1263 		7310	1465	JP203564			NR 2 CYLINDER CRACK APPROXIMATELY 300 DEGREE CIRCUMFERENCE ON 3RD FIN AREA BELOW SPARK PLUG HOLE.  AIRCRAFT HAD A SLIGHT	 CYLINDER HEAD INCREASE WHICH ALERTED THE PILOT TO SEEK MAINTENANCE.					1	H	7	1 	3R	3	R		A806    	5E1				 
1999091000031	19990910	00031	EA  	1999	9	10	99ZZZX3304       	1	19990809	G	3260	60157778827	DOWNLOCK        			CNDAIR	CL600 	CL6002B16   	1900305	EA  										NLG	FAILED          	D				O				OTHER                   				N			FALSE WARNING             			AP	APPROACH       	1			EA	25	399CF	1849 			259	5084				ON APPROACH TO KEWR, LANDING GEAR WAS LOWERED.  INDICATION SHOWED 2 MAIN GEAR GREEN.  NO NOSE GEAR INDICATION AND RED NO	SE DOOR OPEN LIGHT ILLUMINATED AS WELL AS FLASHING RED GEAR HANDLE.  RECYCLED LANDING GEAR AND RECEIVED 3 GREEN INDICATI	ONS AND NO RED NOSE DOOR OPEN LIGHT.  BOOT ON NR 2 NOSE LANDING GEAR DOWNLOCK SENSOR (PROXIMITY SWITCH) FOUND LOOSE.  RE	PLACED SENSOR.  ALSO ADJUSTED RIGHT NOSE LANDING GEAR DOOR SENSOR (PROXIMITY SWITCH).			2	L	7	2 	4F			RT	A21EA   					 
1999091000032	19990910	00032	EA  	1999	9	10	99ZZZX3305       	1	19990809	G	3260		SENSOR          			CNDAIR	CL600 	CL6002B16   	1900305	EA  										NLG	OUT OF ADJUST   	D				O				OTHER                   				N			FALSE WARNING             			AP	APPROACH       	1			EA	25	399CF	1849 				5084				ON APPROACH TO KEWR, LANDING GEAR WAS LOWERED.  INDICATION SHOWED 2 MAIN GEAR GREEN.  NO NOSE GEAR INDICATION AND RED NO	SE DOOR OPEN LIGHT ILLUMINATED AS WELL AS FLASHING RED GEAR HANDLE.  RECYCLED LANDING GEAR AND RECEIVED 3 GREEN INDICATI	ONS AND NO RED NOSE DOOR OPEN LIGHT.  BOOT ON NR 2 NOSE LANDING GEAR DOWNLOCK SENSOR (PROXIMITY SWITCH) FOUND LOOSE.  RE	PLACED SENSOR.  ALSO ADJUSTED RIGHT NOSE LANDING GEAR DOOR SENSOR (PROXIMITY SWITCH).			2	L	7	2 	4F			RT	A21EA   					 
1999091000033	19990910	00033	EU  	1999	9	10	99ZZZX3306       	1	19990714	G	3250	618212	PISTON          			BAG   	JETSTM	JETSTM3201  	1500217	EU  										NLG STEERING	LEAKING         	B				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	05	940AE		2006 			940				STEERING JACK, PN 6182/3, SN SJA-414, WAS RECEIVED WITH COMMENT 'MASSIVE HYDRAULIC LEAK AROUND PISTON - PISTON SHEARED'.	  PISTON ROD, PN 618212, HAD FAILED AT THE TRANSITION RADIUS AT THE TERMINATION OF THE INSIDE DIAMETER THREADS ON THE EN	D WHERE END FITTING, PN 618213 IS ATTACHED.  TIME SINCE OVERHAUL WAS REPORTED TO 2,006.0 HOURS.  FAILED PISTON ROD HAS B	EEN RETURNED TO APPH FOR INVESTIGATION.			2	L	7	2 	4T			RT	A56EU   					 
1999091000034	19990910	00034	EU  	1999	9	10	99ZZZX3307       	1	19990728	G	3230	101A703013	SLIDE TUBE      		B00A702925A 	BAG   	JETSTM	JETSTM3101  	1500215	EU  										MLG	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	838JS	23332	4126 		BD48	741				J31 LEFT MLG, PN B00A702925A, SN BADL-479, WAS SENT IN FOR REPAIR.  MAGNETIC PARTICLE NDT INSPECTION OF SLIDE TUBE, PN 1	01A703013, SN BD48, REVEALED AN INDICATION (CRACK) EXTENDING FROM THE TOP OF THE TUBE, THROUGH THE HOLE FOR SOCKET SET S	CREW, PN 741M1-4D, AND DOWN THE TUBE FOR AN ADDITIONAL 0.520 INCH.  SUBJECT SLIDE TUBE HAS BEEN REJECTED, AND WILL BE RE	PLACED.			2	L	7	2 	4T			RT	A21EU   					 
1999091000035	19990910	00035	EU  	1999	9	10	99ZZZX3308       	1	19990728	G	3230	100A703029	SLIDE TUE       		107A703031A 	BAG   	JETSTM	JETSTM3201  	1500217	EU  										MLG	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05		15936	7463 		AP008					J32 RIGHT MLG, PN 107A703031A, SN BADL-798, WAS SENT IN FOR SCHEUDLED OVERHAUL.  MAGNETIC PARTICLE NDT INSPECTION OF SLI	DE TUBE, PN 100A703029, SN AP008, REVEALED AN INDICATION (CRACK) EXTENDING FROM THE TOP OF THE TUBE THROUGH THE HOLE FOR	 SOCKET SET SCREW, PN 741M1-4D, AND DOWN THE TUBE FOR AN ADDITIONAL 0.400 INCH.  SUBJECT SLIDE HAS BEEN REJECTED, AND WI	LL BE REPLACED.			2	L	7	2 	4T			RT	A56EU   					 
1999091000036	19990910	00036	EA  	1999	9	10	99ZZZX3309       	2	19990802	G	7414	AB382585	CAM FOLLOWER    		S6LN1209    	PIPER 	PA60  	PA60601P    	7106012	NM  	LYC   	O540  	IO540S1A5   	41532	EA  					MAGNETO	LOOSE           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	564RA	228  			88672	61P0365115	RL1904648A			PILOT REPORTED DEAD MAGNETO ON SECOND LEG OF TRIP.  MAGNETO REMOVED AND BREAKER COMPARTMENT INSPECTED REVEALING THE CAM 	FOLLOWER ON THE CONTACT POINTS WAS NO LONGER SECURED TO THE SPRING BY THE TWO SMALL STAINLESS STEEL RIVETS.  REPLACED CO	NTACT BREAKER POINTS.				1	M	7	2 	3O	3	O	RT	A17WE   	1E4				 
1999091000037	19990910	00037	GL  	1999	9	10	99ZZZX3310       	3	19990811	G	6111	57D0495	FORK            			BEECH 	200   	200BEECH    	1152920	CE  						HARTZL	HCD4N3	HCD4N3A     	GL  	PITCH CHANGE	CRACKED         	B			EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03					912NR			FY561		FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD SURFACE OF PITCH PIN ENGAGEMENT SLOTS.  TWO CRACKS.						1	L	7	2 	4T				A24CE   		5	C	STC	 
1999091000038	19990910	00038	NM  	1999	9	10	99ZZZX3311       	1	19990726	G	2710	65448455	MANIFOLD        		654476112   	BOEING	737   	737*        		NM  										AILERON	CRACKED         	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		23277			2215					MANIFOLD IS CRACKED DOWN INSIDE BORE WHERE INNER BEARING FOR INPUT SHAFT RIDES.						2	L	7	2 	4F			RT	A16WE   					 
1999091000039	19990910	00039	NM  	1999	9	10	99ZZZX3312       	1	19990726	G	2710	65448455	MANIFOLD        		654476112   	BOEING	737   	737*        		NM  										AILERON	CRACKED         	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		57267	6005 		A549					MANIFOLD IS CRACKED DOWN INSIDE BORE WHERE INNER BEAERING FOR INPUT SHAFT RIDES.						2	L	7	2 	4F			RT	A16WE   					 
1999091000040	19990910	00040	NM  	1999	9	10	99ZZZX3313       	1	19990803	G	2742	69778551	SPRING          		65C3475111A 	BOEING	737   	737*        		NM  										HORIZONTAL STAB	FAILED          	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		14088			KE00695					SPRINGS, PN 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPR	INGS.  SPRINGS, PN 69-77855-1, SHOULD BE REPLACED WITH PN 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB-94-0195RR.					2	L	7	2 	4F			RT	A16WE   					 
1999091000041	19990910	00041	NM  	1999	9	10	99ZZZX3314       	1	19990720	G	2742	69778551	SPRING          		65C347514   	BOEING	737   	737*        		NM  										HORIZONTAL STAB	FAILED          	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		18738			KE00068					SPRINGS, PN 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPR	INGS.  SUBMITTER SUGGESTED SPRINGS, N 69-77855-1, SHOULD BE REPALCED IWTH PN 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB	-94-0195RR.				2	L	7	2 	4F			RT	A16WE   					 
1999091000042	19990910	00042	NM  	1999	9	10	99ZZZX3315       	1	19990803	G	3240	51161	PLUG            			BOEING	737   	737*        		NM  										MLG	BROKEN          	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		3097 	1570 		2446					PLUG IS BROKEN/SHEARED.  FATIGUED OR OVERTORQUED.  SUBMITTER RECOMMENDED REPLACING WITH PLUG MADE FROM FERROUS MATERIAL.						2	L	7	2 	4F			RT	A16WE   					 
1999092100008	19990921	00008	NM  	1999	9	21	99ZZZX3316       	1	19990803	G	2720	MKP4A	BEARING         		65C370529   	BOEING	737   	737*        		NM  										RUDDER	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					869					BEARING ITEM 19,  FIG 1106, WAS FOUND CRACKED.  REF:  737-SL-27-112B						2	L	7	2 	4F			RT	A16WE   					 
1999091000043	19990910	00043	NM  	1999	9	10	99ZZZX3317       	1	19990720	G	2742	69778551	SPRING          			BOEING	737   	737*        		NM  										HORIZONTAL STAB	FAILED          	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		18738								SPRINGS, PN 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING OR INCORRECT ALLOYS IN THE SPR	INGS.  SUBMITTER STATED SPRINGS PN 69-77855-1 SHOULD BE REPLACED WITH PN 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB-94-	0195RR.				2	L	7	2 	4F			RT	A16WE   					 
1999091000044	19990910	00044		1999	9	10	99ZZZX3318       	1	19990812	G	7120	LK83060	BEARING         								RROYCE	RB211 	RB211*      	54555	NE  					ENGINE MOUNT	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07					22363		31109			CRACK INDICATIONS FOUND ON MAGNETIC PARTICLE INSPECTION.											4	F			A12EU				 
1999091000045	19990910	00045	NE  	1999	9	10	99ZZZX3319       	3	19990812	G	6111	7826584	NICKEL SHEATH   		SFA13M1ROAD 	DHAV  	DHC8  	DHC8*       		NM  						HAMSTD	14SF	14SF*       	NE  	PROPELLER	MISSING         	B			BN4R	O				OTHER                   				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			WP	05		4149 			859160					REF:  330133 SO.  BLADE VIBRATION DUE TO NICKEL SHEATH SEPARATION FROM BLADE IN-FLIGHT.						2	H	7	2 	4T			RT	A13NM   		6	C	P7NE	 
1999091000046	19990910	00046	NM  	1999	9	10	99ZZZX3320       	1	19990801	G	3213		DYNAMIC SEAL    			BOEING	747   	74745E      	1384947	NM  										RT MLG	FAILED          	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	03	408EV					28092				RIGHT BODY GEAR OLEO STRUT HAD SEVERE HYDRAULIC LEAKING.  REPLACED DYNAMIC SEAL AND BACK-UP SEALS.  AIRCRAFT RETURNED TO	 SERVICE.					2	L	7	4 	4F			RT	A20WE   					 
1999091000047	19990910	00047	CE  	1999	9	10	99ZZZX3321       	1	19990726	G	3520	17400630	OXYGEN MASK     			CESSNA	500   	S550        	2076607	CE  										CABIN	TORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05	288QS					S5500088				DURING ROUTINE INSPECTION OF THE PASSENGER OXYGEN MASKS, A TEAR WAS FOUND AROUND THE COLLAR OF THE BAG WHERE THE OXYGEN 	FEED TUE ENTERS IT.					1	L	7	2 	4F			RT	A22CE   					 
1999091000048	19990910	00048	EU  	1999	9	10	99ZZZX3322       	1	19990715	G	2435		BEARING         	GE          	2CM504D2D   	AMD   	FALC10	FALCON10    	2730101	EU  										STARTER/GEN	FAILED          	B			JGVR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	09	282T				MME0034	042				OVERVOLTAGE CONDITION RESULTING IN OVERHEATING AND PARTIAL INTERNAL FAILURE OF STARTER/GENERATOR.  SUBMITTER RECOMMENDED	 BEARING INSPECTION INTERVAL TO BE INCLUDED IN FALCON MOUNT MANUAL TIME LIMIT (CHAPTER 5-20-00).  SUSPECT BEARING FAILUR	E CAUSED OVERVOLTAGE CONDITION CAUSING INTERNAL FAILURE OF COMPONENT.				2	L	7	2 	4F				A33EU   					 
1999091000049	19990910	00049	WP  	1999	9	10	99ZZZX3323       	2	19990806	G	7230	30723963	DISK            			RAYTHN	DH125 	HAWKER800XP 		CE  	GARRTT	TFE731	TFE7315BR   		WP  					COMPRESSOR	FAILED          	B				A				UNSCHED LANDING         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CR	CRUISE         	1			SW	09	754TA	109  	78   			258406	P107351			WHILE IN CRUISE AT FL 390, ENGINE BEGAN VIOLENT VIBRATION WITH INCREASE ITT.  IF&D AND SAFE LANDING EXECUTED.						2	L	7	2 	4F	4	F	RT	A3EU    	E6WE				 
1999091000050	19990910	00050	EU  	1999	9	10	99ZZZX3324       	1	19990805	G	5330		SKIN            			AMD   	FALC50	FALCON900   	2700160	EU  										BS 10	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	990MC					65				DURING NORMAL MAINTENANCE INSPECTION, A PAINT BUBBLE WAS NOTED AT FRAME 10 BETWEEN STR 19L AND STR 20L.  CORROSION WAS N	OTED AND THE FAIRING REMOVED.  MORE CORROSION AND LOOSE FILLER WAS NOTED.  SUFFICIENT CORROSION ON FR 10 (EXTERNAL SKIN)	 BETWEEN STR 21L AND STR 21R TO REQUIRE FALCON JET ENGINEERING REPAIR SCHEME.  AREA IN QUESTION IS ADDRESSED BY SD 900-1	07 WHICH WAS ACCOMPLISHED AT ACTT:  3055, BUT NOT DONE CORRECTLY.  THE SB MUST BE FOLLOWED AS WRITTEN TO PREVENT THE COR	ROSION FROM STARTING.  ACTT:  4,714.0 HOURS.		2	L	7	3 	4F			RT	A46EU   					 
1999091000052	19990910	00052	EU  	1999	9	10	99ZZZX3326       	1	19990802	G	2425	D2W8328001003	VOLTMETER       			ISRAEL	1125  	ASTRASPX    	4500205	EU  										COCKPIT	FAILED          	B			QRRR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	275RA	690  			066	098				RIGHT VOLTMETER/AMMETER  AMPS DROP TO ZERO.  CAN BE RESET TO NORMAL BY PUSHING VOLTS BUTTON.  WILL THEN DROP BACK TO ZER	O.  REPLACED METER WITH NEW.  OPS TESTED NORMAL.					2	L	7	2 	4F			RT	A16NM   					 
1999092100009	19990921	00009	WP  	1999	9	21	99ZZZX3327       	2	19990722	G	7250	30723424	STATOR          								GARRTT	TFE731	TFE7313     	01518	WP  					TURBINE SECTION	DEFLECTED       	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19		7636 	4424 				P76241			LPT3 STATOR DEFLECTED AFT ALLOWING THE HONEYCOMB SEAL RING TO RUB (CONTACT) THE LPT3 ROTOR FOUND DURING SCHEDULED MAINTE	NANCE.  CAUSE FOR DEFLECTION UNKNOWN.  REPLACED LPT3 STATOR AND LPT3 ROTOR ASSEMBLY.										4	F			E6WE				 
1999091000053	19990910	00053	WP  	1999	9	10	99ZZZX3328       	2	19990709	G	7250	30740962	WHEEL           								GARRTT	TFE731	TFE7313     	01518	WP  					TURBINE SECTION	CHAFED          	B			AN3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23		1093 					P83158			UPON DISASSEMBLY OF ENGINE FOR MAJOR PERIODIC INSPECTION, NOTED 'RUBBING' OF 3RD STAGE TURBINE WHEEL.  THIRD STAGE WHEEL	-STATOR AND HONEYCOMB SEAL SENT TO ALLIED SIGNAL FOR EVALUATION.  ENGINE RE-ASSEMBLED PER NORMAL MAINTENANCE MANUAL INST	RUCTIONS AND TEST CELL RUN COMPLETED.  S/N OF TURBINE WHEEL, 4-12172-0154.  CYCLES:  915.  (X)									4	F			E6WE				 
1999091000054	19990910	00054	NM  	1999	9	10	99ZZZX3329       	1	19990726	G	5720	65B228451	PANEL           			BOEING	747   	747245F     	1384897	NM  										WING	DISBONDED       	G				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CL	CLIMB          	1			WP	07	638FE	61047				21841				FERRY FLIGHT FROM MARANA, AZ, TO HONG KONG, PILOT REPORTED.  CLIMB THROUGH 34,000 FEET AT .84 MACH, A SUDDEN ONSET AIRFR	AME SHUDDER OCCURRED.  ALL DOORS CLOSED, BUT HAD LEFT INBORD FLAP VIBRATING VISIBLY GETTING WORSE AS IT WENT INBOARD.  S	LOW TO .60 MACH AND VISIBLE VIBRATION MOVEMENT STOPPED.  THE FLIGHT DIVERTED TO EVERETT, WA, WHERE GROUND INSPECTION REV	EALED THE LT INBD AFT T/E PANEL, P/N 65B22845-1, MEASURING 8 FEET BY 3 FEET WAS MISSING AND THE REMAINING PART IS DISBON	DED OVER ITS ENTIRE AREA.  UPPER SURFACE OF 65B39011-9 FOREFLAP DELAMINATED AND UPPER PLY MISSING.  HONEYCOMB CORE EXPOS	ED OVER 30 PERCENT OF ITS SURFACE FROM INBD END, LT OTBD.	2	L	7	4 	4F				A20WE   					 
1999091000055	19990910	00055	CE  	1999	9	10	99ZZZX3330       	1	19990701	G	2913	99121033	RESERVOIR ASSY  			CESSNA	500   	500CESSNA   	2076602	CE  										HYDRAULIC SYS	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	307EW	218  			1303	5000323				CORROSION FOUND INSIDE RESERVOIR DURING HYDROSTAT TESTING AND INSPECTION.						1	L	7	2 	4F				A22CE   					 
1999091000057	19990910	00057	EA  	1999	9	10	99ZZZX3332       	1	19990701	G	3221	C3UT853	FORK ASSY       			DHAV  	DHC3  	DHC3        	2800202	EA  										NLG	CRACKED         	B	P	A	VM9R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	11	21PG					310				THREE EACH CRACKS DISCOVERED ON LEFT AND RIGHT SIDES OF FORK ASSEMBLY APPROXIMATELY 3 HOURS AFTER NEW INSTALLATION WAS C	OMPLETED.  CRACKING WAS VERIFIED BY DIE PENETRANT INSPECTION.					1	H	7	1 	3R				A815    					 
1999091000131	19990910	00131	SW  	1999	9	10	99ZZZX3333       	1	19990727	G	6321	DD1661	BOLT            		DD1631      	BELL  	407   	407         		SW  										ROTOR BRAKE	WORN            	B			IIFR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407JR	991  				53245				BOLTS HAVE STEPS (GROOVES) WORN IN THEM.  THIS CAUSES THE PAD ASSY TO STICK.  BOLTS ARE USED AS GUIDE PINS.						1	G	7	1 	3U			O	H2SW    					 
1999091000132	19990910	00132	SW  	1999	9	10	99ZZZX3334       	1	19990727	G	6321	DD1631	BRAKE PAD       			BELL  	407   	407         		SW  										ROTOR BRAKE	WORN            	B			IIFR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407JR	991  				53245				HOLES FOR BOLTS THAT GUIDE PAD AND HOLD IN PLACE ARE ELONGATED.  ONCE BEFORE THE SAME P/N PAD CAME LOOSE DUE TO HOLE OPE	NING UP.  SUBMITTER SUGGESTED BASE OR METAL BE MADE OF THICKER MATERIAL AROUND GUIDE PIN HOLES.					1	G	7	1 	3U			O	H2SW    					 
1999091000133	19990910	00133	SW  	1999	9	10	99ZZZX3335       	1	19990806	G	6230	206010443001	BEARING         			BELL  	206   	206L1       	1182107	SW  										SWASHPLATE	ROUGH           	B			ZV1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40LP	638  			19155	45233				SWASHPLATE ASSY WAS REMOVED DUE TO BEARING ROUGHNESS.  FOUND BEARING INNER RACE BREAKING DOWN.  SUBMITTER STATED THIS IS	 SECOND BEARING ON ASSY, S/N JIJA-90059, IN 9 MONTHS.					1	G	7	1 	3U				H2SW    					 
1999091000134	19990910	00134	SW  	1999	9	10	99ZZZX3336       	1	19990712	G	3040	204070907101	MOTOR           			BELL  	212   	212         	1181420	SW  										WINDSHIELD WIPER	INOPERATIVE     	B			GJQR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	98W	171  			01984	35100				WINDSHIELD WIPER WILL NOT WORK.  REPLACED WITH NEW MOTOR.						1	G	7	1 	4U				H4SW    					 
1999091000135	19990910	00135	SW  	1999	9	10	99ZZZX3337       	1	19990714	G	6500	407340339103	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	ROUGH           	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427AL					53107				FOUND 2 EACH 407-340-339-103, BEARINGS ROUGH.  FOUND 206-061-432-116 HOUSING CRACKED.  FOUND 406-040-320-101 SHAFT SPLIN	ES WORN.					1	G	7	1 	3U			O	H2SW    					 
1999091000136	19990910	00136	SW  	1999	9	10	99ZZZX3338       	1	19990714	G	6500	206062532116	HOUSING         			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427AL					53107				FOUND 2 EACH 407-340-339-103, BEARINGS ROUGH.  FOUND 206-061-432-116 HOUSING CRACKED.  FOUND 406-040-320-101 SHAFT SPLIN	ES WORN.					1	G	7	1 	3U			O	H2SW    					 
1999091000137	19990910	00137	SW  	1999	9	10	99ZZZX3339       	1	19990714	G	6510	406040320101	SHAFT           			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427AL					53107				FOUND 2 EACH 407-340-339-103, BEARINGS ROUGH.  FOUND 206-061-432-116 HOUSING CRACKED.  FOUND 406-040-320-101 SHAFT SPLIN	ES WORN.					1	G	7	1 	3U			O	H2SW    					 
1999091000138	19990910	00138	SW  	1999	9	10	99ZZZX3340       	1	19990701	G	6500	206061432116	HOUSING         			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407AL	147  				53044				FOUND HOUSING, 206-061-432-116, CRACKED AND WORKING RIVETS.  FOUND 2 EACH BEARINGS, 407-340-339-103, ROUGH.  TT 146.8 HO	URS.  FOUND SHAFT 407-040-320-101 SPLINES WORN.  TT 1,234.4 HOURS.					1	G	7	1 	3U			O	H2SW    					 
1999091000139	19990910	00139	SW  	1999	9	10	99ZZZX3341       	1	19990701	G	6500	407340339103	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	ROUGH           	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407AL	147  				53044				FOUND HOUSING, 206-061-432-116, CRACKED AND WORKING RIVETS.  FOUND 2 EACH BEARINGS, 407-340-339-103, ROUGH.  TT 146.8 HO	URS.  FOUND SHAFT 407-040-320-101 SPLINES WORN.  TT 1,234.4 HOURS.					1	G	7	1 	3U			O	H2SW    					 
1999091000140	19990910	00140	SW  	1999	9	10	99ZZZX3342       	1	19990718	G	6500	206061432116	HOUSING         			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	477AL	881  				53203				FOUND HOUSING 206-061-432-116 CRACKED AND WORKING RIVETS.  FOUND 2 EACH BEARINGS 407-340-339-103 ROUGH.						1	G	7	1 	3U			O	H2SW    					 
1999091000141	19990910	00141	SW  	1999	9	10	99ZZZX3343       	1	19990718	G	6500	407340339103	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	ROUGH           	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	477AL	881  				53203				FOUND HOUSING 206-061-432-116 CRACKED AND WORKING RIVETS.  FOUND 2 EACH BEARINGS 407-340-339-103 ROUGH.						1	G	7	1 	3U			O	H2SW    					 
1999091000142	19990910	00142	SW  	1999	9	10	99ZZZX3344       	1	19990718	G	6500	407340339109	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467AL	950  				53190				FOUND HOUSING 206-061-432-116 CRACKED.  FOUND 2 EACH BEARINGS 407-340-339-109 ROUGH.  FOUND SHAFT 406-040-320-101 SPLINE	S WORN.					1	G	7	1 	3U			O	H2SW    					 
1999091000143	19990910	00143	SW  	1999	9	10	99ZZZX3345       	1	19990718	G	6510	406040320101	SHAFT           			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467AL	950  				53190				FOUND HOUSING 206-061-432-116 CRACKED.  FOUND 2 EACH BEARINGS 407-340-339-109 ROUGH.  FOUND SHAFT 406-040-320-101 SPLINE	S WORN.					1	G	7	1 	3U			O	H2SW    					 
1999091000144	19990910	00144	SW  	1999	9	10	99ZZZX3346       	1	19990317	G	6510	406040320101	SHAFT           		407040303101	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437AL	2253 			A94	53141				FOUND SPLINES WORN BEYOND LIMITS (406-040-320-101).  FOUND HOUSING CRACKED (206-061-432-116).  FOUND 2 EACH BEARINGS ROU	GH (407-340-339-103).  TT 4.77.4 HOURS.					1	G	7	1 	3U			O	H2SW    					 
1999091000145	19990910	00145	SW  	1999	9	10	99ZZZX3347       	1	19990801	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	DAMAGED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	487AL				RNFS8161	53204				DURING 25-HOUR, DISC PACK AD 97-24-17 PARA 'A', FOUND DISC PACK DAMAGED.						1	G	7	1 	3U			O	H2SW    					 
1999091000146	19990910	00146	SW  	1999	9	10	99ZZZX3348       	1	19990724	G	6210	206015001107	BLADE           			BELL  	206   	206L4       	1182110	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	176AL	6015 			A2170	52146				TRAILING EDGE EXTRUSION CORRODED BEYOND REPAIRABLE LIMITS.  (INTERGRANULAR CORROSION).						1	G	7	1 	3U			NC	H2SW    					 
1999091000147	19990910	00147	SW  	1999	9	10	99ZZZX3349       	1	19990624	G	5302	407023800118	SUPPORT         		407030800101	BELL  	407   	407         		SW  										TAILBOOM	MISINSTALLED    	B			ALGR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	627AL	779  				53284				SUPPORT MISINSTALLED.						1	G	7	1 	3U			O	H2SW    					 
1999091000148	19990910	00148	SW  	1999	9	10	99ZZZX3350       	1	19990210	G	5302	407023800117	SUPPORT         		407030800101	BELL  	407   	407         		SW  										TAILBOOM	MISINSTALLED    	B			ALGR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	497AL	1583 				53172				SUPPORT MISINSTALLED.						1	G	7	1 	3U			O	H2SW    					 
1999091000149	19990910	00149	SW  	1999	9	10	99ZZZX3351       	1	19990622	G	3213	407050202115	CROSSTUBE       			BELL  	407   	407         		SW  										MLG	CORRODED        	B			ALGR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	587AL	1425 			154	53248				CORROSION FOUND UNDER SUPPORT AND CLAMPS DUE POSSIBLY TO IMPROPER TREATMENT DURING MANUFACTURING AND/OR MATERIAL DEFECT.						1	G	7	1 	3U			O	H2SW    					 
1999091000150	19990910	00150	SW  	1999	9	10	99ZZZX3352       	1	19990725	G	5302	407023800118	SUPPORT         		407030800101	BELL  	407   	407         		SW  										TAILBOOM	CRACKED         	B			ALGR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	577AL	1443 				53247				CRACK IN RADIUS, POOR QUALITY CONTROL WHEN FABRICATING AND PART PUT IN LOAD ON INSTALLATION.						1	G	7	1 	3U			O	H2SW    					 
1999091000151	19990910	00151	SW  	1999	9	10	99ZZZX3353       	1	19990721	G	3411	206075634001	LINE            			BELL  	206   	206L        	1181522	SW  										ALTIMETER	CORRODED        	B			ALGR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										THE PART IS NOT NEW, IT HAS A SERVICEABLE TAG ON IT FROM INTERNATIONAL HELICOPTER TRANSPORT, DATED 9-24-86, REPAIR STATI	ON CERT NR 3695-IC, BOTH FERRULES ON THE TUBE ARE FROZEN.  THE TUBE HAS CORROSION ON IT ALONG WITH A CUT.  THE TUBE IS U	NSERVICEABLE.				1	G	7	1 	3U				H2SW    					 
1999091000152	19990910	00152	SW  	1999	9	10	99ZZZX3354       	1	19990722	G	6500	406040339111	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	WRONG PART      	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03					L970828					RECEIVED NEW ASSEMBLY FROM BELL HELICOPTER NEW TYPE BEARINGS NOT INSTALLED.  ASB 407-98-23 NOT C/W.						1	G	7	1 	3U			O	H2SW    					 
1999091000153	19990910	00153	SW  	1999	9	10	99ZZZX3355       	1	19990722	G	6500	406040339111	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	WRONG PART      	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03					L970856					RECEIVED NEW ASSEMBLY FROM BELL HELICOPTER NEW TYPE BEARINGS NOT INSTALLED.  ASB 407-98-23 NOT C/W.						1	G	7	1 	3U			O	H2SW    					 
1999091000156	19990910	00156	EU  	1999	9	10	99ZZZX3358       	1	19990630	G	6210	L621M1010054	BLADE           			UROCOP	EC135 	EC135P1     	8680990	EU  										MAIN ROTOR	DAMAGED         	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	911SV	183  			505	0070				REMOVED IWTH OTHER BLADES AS PRECAUTION PER AEC.  MCN 137.  REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999091000157	19990910	00157		1999	9	10	99ZZZX3359       	4	19990216	G	2300	CI122	ANTENNA         			BOLKMS	117   	BK117A3     	5626015	EU  										FUSELAGE	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	1140H	948  			8634	7078				ANTENNA REFLECTS POWER.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999091000158	19990910	00158	EU  	1999	9	10	99ZZZX3360       	1	19990316	G	6420	10513241	BEARING         			BOLKMS	BK117 	BK117C1     	5626025	EU  										T/R FORK	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC	2912 			3426	7505				BEARINGS WORN.  REF:  RMA NR R019259 MCN NR 12.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999091000163	19990910	00163	SW  	1999	9	10	99ZZZX3365       	1	19990608	G	7810	206064300005	STACK           			BELL  	206   	206L3       	1182108	SW  										EXHAUST	CRACKED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	17592	314  			980526	51535				EXHAUST STACK CRACKED.						1	G	7	1 	3U				H2SW    					 
1999091000164	19990910	00164		1999	9	10	99ZZZX3366       	4	19990204	G	3425	430375001105	DISPLAY         			BELL  	430   	430         	1182150	SW  										COCKPIT	MALFUNCTIONED   	B			AC2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	430CH				95100004	49037				DISPLAY, SN 95100004, WAS INSTALLED AND REMOVED DUE TO DISCREPANCY.  INITIALLY PERFORMED CORRECTLY WHEN INSTALLED, BUT M	ALFUNCTIONED SHORTLY AFTERWARDS.  THE FOLLOWING SHOWED NO INCIDATION.  EOP AND TEMP, TRANSMISSION, FUEL QUANTITY, AND TE	MP AND OAT.  REINSTALLED ORIGINAL IIDS DISPLAY.				1	G	7	2 	3U			RT	H9SW    					 
1999091000165	19990910	00165		1999	9	10	99ZZZX3367       	4	19990412	G	3425	430375001105	DISPLAY         			BELL  	430   	430         	1182150	SW  										COCKPIT	MALFUNCTIONED   	B			AC2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	430CH	118  			96090027	49037				NO NR 2 HYDRAULIC SYSTEM PRESSURE SHOWING.  NO CARROT INDICATION.						1	G	7	2 	3U			RT	H9SW    					 
1999091000167	19990910	00167		1999	9	10	99ZZZX3369       	4	19990210	G	3425	430375001105	DISPLAY         			BELL  	430   	430         	1182150	SW  										COCKPIT	MALFUNCTIONED   	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	469  			96090034	49037				ROTOR BRAKE CAUTION LIGHT STAYS ON.						1	G	7	2 	3U			RT	H9SW    					 
1999091000169	19990910	00169	SW  	1999	9	10	99ZZZX3371       	1	19990323	G	6500	430010124103	BUSHING         			BELL  	430   	430         	1182150	SW  										T/R DRIVE	WORN            	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	589  				49037				BUSHING WORN BEYOND LIMITS.						1	G	7	2 	3U			RT	H9SW    					 
1999091000171	19990910	00171	SW  	1999	9	10	99ZZZX3373       	1	19990619	G	3201	430036140105	CROSSTUBE       			BELL  	430   	430         	1182150	SW  										AIR FRAME	CORRODED        	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	866  				49037				CORROSION NEAR RIGHT SADDLE INBOARD BOTTOM SIDE.						1	G	7	2 	3U			RT	H9SW    					 
1999091000464	19990910	00464	WP  	1999	9	10	99ZZZX3374       	2	19990727	G	7230	30740962	ROTOR ASSY      								GARRTT	TFE731	TFE7313R1H  	29001	WP  					POWER TURBINE	WORN            	B			MJ1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	11							P84225			DURING DISASSEMBLY OF ENGINE TURBINE SECTION FOR AN OVERTEMP INSPECTION/MPI, THIRD LPT ROTOR DISK, PN 3074096-2, SN 9653	32200320, WAS FOUND TO HAVE BEEN RUB DAMAGED AT THE FORWARD SIDE OF THE DISK IN FIR TREE AREAS.  CONDITION APPEARS TO HA	VE BEEN CAUSED BY DISK CONTACT WITH THIRD LPT STATOR ASSY, PN 3072342-4.  THIRD LPT DISK, PN 3074096-2, WAS SCRAPED BY D	AMAGE CAUSED PER APPLICABLE ENGINE MM NR 72-02-15 REV 12/98.  ALLIED SIGNAL ENGINEERING RECOMMENDED THIRD LPT STATOR, PN	 3072342-4, BE REPLACED DUE TO SUSPECT VANE SHIFT OR FLEX.							4	F			E6WE				 
1999091000465	19990910	00465	CE  	1999	9	10	99ZZZX3375       	1	19990802	G	3213	5081032017	TORQUE KNEE     		114810000   	BEECH 	1900  	1900D       	1154162	CE  										MLG	CRACKED         	B		A	VNNR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	05		19000								SOCKET WAS CRACKED BELOW ATTACH POINT OF LOWER TORQUE KNEE.  SUBMITTER STATED THEY HAVE FOUND THE SAME CRACK IN THE LAST	 EIGHT LANDING GEAR OVERHAULED.					2	L	7	2 	4T			RT	A24CE   					 
1999091000466	19990910	00466	NM  	1999	9	10	99ZZZX3376       	1	19990206	G	2740	32ENA44	POWER CAM       			BOEING	737   	7377K9      	138447E	NM  										STABILIZER TRIM	CRACKED         	B			ZUFY	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	35	101UN	4397 				28089				DEFECTIVE INSTALLATION OF THE STABILIZER TRIM SWITCH ATTACHMENT BRACKET.  DUE TO THIS FAILURE, THE STABILIZER TRIM SWITC	HES S145 AND THE S546 CAME IN CONTACT AND DESTROYED THE ROLLER CAM OF S145, IF THE STABILIZER MOVES IN NOSE-UP DIRECTION	.				2	L	7	2 	4F			RT	A16WE   					 
1999091000467	19990910	00467	WP  	1999	9	10	99ZZZX3377       	1	19990707	G	2460	M142AA8A	HARNESS         			DOUG  	DC10  	DC1030      	3023501	WP  										NR 2 HYD PUMP	FAILED          	B			ZUFY	K				NONE                    				B	P		SMOKE/FUMES/ODORS/SPARKS  	NO WARNING INDICATION     		IN	INSP/MAINT     	1			EA	35	12080					47981				AIRCRAFT ON MAINTENANCE.  PRE-INPUT WASH COMPLETED FUNCTIONS ON FLYING CONTROLS WITH 1-3 AND 2-3 REVERSABLE MOTOR PUMPS 	RUNNING.  GROUND CREW REPORTED SMOKE SPARKS AND FLAMES IN THE RT MLG BAY.  ACFT SYSTEMS WERE IMMEDIATELY SHUT DOWN.  ON 	INSP, THE WIRING TO THE NR 2 AUX PUMP HAD BURNED THROUGH AT THE HYD PUMP PLUG.  THE CIRCUIT BREAKERS TO THE HYD PUMP WER	E PULLED.  THEY HAD NOT TRIPPED WITH THE CABLE DAMAGE.  CONTINENTAL A/L, HOUSTON ARE CARRYING OUT AN INVESTIGATION ON TH	E CABLE LOOM.		2	L	7	3 	4F				A22WE   					 
1999092100011	19990921	00011	SO  	1999	9	21	99ZZZX3378       	1	19990809	G	4920		HOUSING         			GULSTM	G1159 	G1159A      	3970109	SO  										APU EXHAUST	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	11	545JT	5309 	901  			347				DURING A SCHEDULED 450-HOUR INSPECTION, FOUND A 3.50 INCH CRACK AFT OF TURBINE WHEEL IN EXHAUST HOUSING.  APU SENT TO AL	LIED-SIGNAL FOR REPAIR.					2	L	7	2 	4F				A12EA   					 
1999091000468	19990910	00468	CE  	1999	9	10	99ZZZX3379       	1	19990720	G	3230		DRAG BRACE      			BEECH 	95    	95B55       	1152729	CE  										NLG	BROKEN          	G		A		O				OTHER                   				O			OTHER                     			LD	LANDING        	1			SO	03	56AW	3500 				TC110				DURING LANDING AT BNA, PILOT HEARD A 'POP' AS THE NOSE WHEEL TOUCHED DOWN.  THE NOSE GEAR THEN COLLAPSED.  THE NOSE GEAR	 AFT DRAG BRACE BROKE WHERE THE NOSE GEAR RETRACT ROD ATTACHES.  BOTH OF THE TANGS THAT THE RETRACT ROD END FITS BETWEEN	 BROKE ALLOWING THE NOSE GEAR TO FOLD.				1	L	7	2 	3O			RT	3A16    					 
1999091000471	19990910	00471	EU  	1999	9	10	99ZZZX3382       	1	19990730	G	7730	21180026	DEEC            			BRAERO	DH125 	BAE125800A  	1500285	EU  	GARRTT	TFE731	TFE7315R    	01518	WP  					NR 1 ENGINE	MALFUNCTIONED   	H				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			SO	13	75MT	3811 			1291572	258231	P91576			AIRCRAFT LEVEL FLIGHT - FL 350.  ON ITS OWN, ENGINE WENT TO AN OVERSPEED CONDITION OF 105 PERCENT (103 PERCENT MAX ALLOW	ABLE).  THROTTLE MOVEMENT HAD NO AFFECT. NORMAL THROTTLE CONTROL REGAINED ON DESCENT OUT OF FL 300. LANDING UNEVENTFUL. 	 MANDATORY ENGINE OVERHAUL REQUIRED BY MFG.  SUSPECTED ENGINE COMPUTER (DEEC).   NO EVALUATION OR CAUSE IDENTIFIED.  LOA	NER ENGINE WITH REPLACEMENT DEEC HAS WORKED NORMALLY.			2	L	7	2 	4F	4	F	RT	A3EU    	E6WE				 
1999091000473	19990910	00473	SO  	1999	9	10	99ZZZX3384       	1	19990804	G	2100	5048900	LINE            			PIPER 	PA31T 	PA31T1      	7103126	SO  										RT WING	CORRODED        	B			SO5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	935CA	5189 				31T8004033				DURING AN EVENT 2 INSPECTION, THE AIR CONDITIONING SYSTEM WAS BEING SERVICED WITH FREON R-12 DUE TO LOW OUTPUT.  AFTER S	ERVICING, A LEAK WAS FOUND ON THE LOW PRESSURE SIDE IN THE RIGHT WING LEADING EDGE. UNABLE TO STOP LEAK BY TIGHTENING B-	NUT.  EVACUATED SYSTEM AND REMOVED LINE FOR INSPECTION.  THE FLARE WAS FOUND HEAVILY CORRODED WITH A HOLE THROUGH IT. RE	PLACED LINE, LEAK CHECK SATISFACTORY.  LINE IS LOWEST POINT IN SYSTEM.			1	L	7	2 	3T				A8EA    					 
1999091000474	19990910	00474	EU  	1999	9	10	99ZZZX3385       	1	19990817	G	3240	MY20745144	LINE            			AMD   	FALCON	FALCON20    	2730103	EU  										NLG WW	CRACKED         	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CE	09	148MC	7854 				428				NOTED HYDRAULIC LEAK IN THE NOSE AREA.  FOUND CRACKS LOCATED ON THE INSIDE RADIUS OF A 90 DEGREE BEND ON A HYDRAULIC HAR	D LINE.  THIS HYDRAULIC LINE IS THE LEFT BRAKE PRESSURE LINE.					2	L	7	2 	4F			RT	A7EU    					 
1999091000475	19990910	00475	WP  	1999	9	10	99ZZZX3386       	2	19990817	G	7250	8650821	NUT             			SWRNGN	SA227 	SA227TT     		SW  	GARRTT	TPE331	TPE33110    	01514	WP  					LT ENGINE	CRACKED         	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	17	227TT	3026 	597  			TT444				REAR TURBINE NUT PN 865082-1 WAS REMOVED AND FOUND TO HAVE GALLED THREADS AND CRACKS IN THE THREADS.  THIS ENGINE HAS 59	6.0 HOURS SINCE OVERHAUL.  TURBINE NUT APPEARS TO HAVE BEEN RE-USED.  SUBMITTER STATED THESE NUTS SHOULD BE A ONE-TIME U	SE ONLY.				2	L	7	2 	4T	4	T	RT	A5SW    	E4WE				 
1999091000477	19990910	00477	EA  	1999	9	10	99ZZZX3388       	1	19990806	G	2931	600591341	SWITCH          			CNDAIR	CL600 	CL6002B16   	1900305	EA  										HYD PRESSURE	FAILED          	B			QRRR	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			EA	13	270RA	390  			2573	5337				'GROUND SPOILER' CAUTION (AMBER) MESSAGE ON EICAS WITH FLAPS DOWN.  NEW SWITCH CLEARED MESSAGE.						2	L	7	2 	4F			RT	A21EA   					 
1999091000478	19990910	00478		1999	9	10	99ZZZX3389       	4	19990816	G	3414	6229210004	TRANSPONDER     			ISRAEL	1125  	ASTRASPX    	4500205	EU  										E/E BAY	FAILED          	B			QRRR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	273RA	529  			5720	097				TRANSPONDER WAS HARD FAILED.  REPLACED WITH SERVICEABLE UNIT.						2	L	7	2 	4F			RT	A16NM   					 
1999091000479	19990910	00479		1999	9	10	99ZZZX3390       	4	19990816	G	3442	6228440003	RADAR           			ISRAEL	1125  	ASTRASPX    	4500205	EU  										RADOME	INOPERATIVE     	B			QRRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	273RA		43   		1525	097				RADAR IS INOPERATIVE IN ANY MODE.  REPLACED.						2	L	7	2 	4F			RT	A16NM   					 
1999091000480	19990910	00480	EU  	1999	9	10	99ZZZX3391       	1	19990816	G	2425	D25W8328001003	AMMETER         			ISRAEL	1125  	ASTRASPX    	4500205	EU  										COCKPIT	FAILED          	B			QRRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	275RA	690  			066	098				AMPS-METER WILL DROP TO ZERO.  WILL RESET BY PUSHING VOLT BUTTON, BUT FALLS BACK TO ZERO IN A FEW SECONDS.  REPLACED GAU	GE WITH SERVICEABLE UNIT.					2	L	7	2 	4F			RT	A16NM   					 
1999091000481	19990910	00481	EU  	1999	9	10	99ZZZX3392       	1	19990816	G	7930	12412111	TRIPLE INDICATOR			ISRAEL	1125  	ASTRASPX    	4500205	EU  										COCKPIT	INOPERATIVE     	B			QRRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	275RA	705  			98020022	098				AT AN POWER-UP, NEEDLE STAYED AT ZERO IN FUEL TEMPERATURE, CABIN TEMP AND OAT.  REPLACED WITH SERVICEABLE UNIT.						2	L	7	2 	4F			RT	A16NM   					 
1999091000482	19990910	00482	CE  	1999	9	10	99ZZZX3393       	1	19990723	G	2760	20544470	FILTER          			CESSNA	650   	650         	2076802	CE  										SPOILER	FAILED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	39WP	1027 				6500039				DURING SMIP INSPECTION, OPERATION 10, ITEM 27-20, INSPECTION REVEALED FILTER SEPARATED FROM MOUNTING FLANGE IN THE END O	F ELBOW FITTING PERMITTING FILTER TO SLIDE BACK AND FORTH WITHIN THE FITTING.  REPLACED WITH NEW UNIT.  FILTER NOW HAS 3	,600 HOUR LIFE-LIMIT, BUT THIS ONE FAILED AT OR BEFORE 1,027 HOURS.  ONE OTHER ONE RECENTLY REPLACED FOR 3,600 HOUR LIFE	-LIMIT WAS STILL OK.			2	L	7	2 	4F				A9NM    					 
1999091000483	19990910	00483	CE  	1999	9	10	99ZZZX3394       	1	19990726	G	5320	50430043619	CHANNEL         			BEECH 	200   	200BEECH    	1152920	CE  										FUSELAGE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	5ST	7601 				BB289				DURING A PHASE INSPECTION, A CRACK WAS FOUND ON THE AFT END OF THE ENTRY DOOR BOTTOM CHANNEL WHERE THE DOOR HINGE HALF A	TTACHES.  THE CRACK WAS ABOUT 4 INCHES LONG AND WAS THROUGH THE AFT SET OF RIVETS.  THE CHANNEL IS TO BE REPLACED WITH A	 NEW UNIT.				1	L	7	2 	4T				A24CE   					 
1999091000484	19990910	00484	CE  	1999	9	10	99ZZZX3395       	1	19990728	G	3242	23151673130	ADJUSTMENT SCREW	BENDIX      	3321200     	LEAR  	55    	55LEAR      	5170702	CE  										RT BRAKE	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	520SC				8220384	087				ADJUSTMENT SCREW BEGINNING TO FAIL.  NOTED UPON VISUAL INSPECTION AFTER FAILURE OF SAME PART ON LEFT BRAKE.						2	L	7	2 	4F				A10CE   					 
1999091000485	19990910	00485	CE  	1999	9	10	99ZZZX3396       	1	19990728	G	3242	23151673130	ADJUSTMENT SCREW	BENDIX      	3321200     	LEAR  	55    	55LEAR      	5170702	CE  										LT BRAKE	BROKEN          	B				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			EA	25	520SC				8220341	087				ADJUSTMENT SCREW SHEARED IN 2 PIECES, NOTED UPON VISUAL INSPECTION.  AIRCRAFT ARRIVED AT TEB WEDNESDAY EVENING 7-28-99. 	 UPON LANDING, LEFT BRAKES DID NOT WORK AND AIRCRAFT WENT OFF RUNWAY INTO GRASS.					2	L	7	2 	4F				A10CE   					 
1999091000486	19990910	00486		1999	9	10	99ZZZX3397       	4	19990716	G	2210	5TEC	AUTOPILOT       			BEECH 	55    	95C55       	1152708	CE  										COCKPIT	MALFUNCTIONED   	H		A		E				ENGINE SHUTDOWN         				J			WARNING INDICATION        			NR	NOT REPORTED   	1			WP	11	407T					TE231				WHILE IN HEADING MODE, AUTOPILOT WENT INTO A 30 DEGREE RIGHT TURN, UN-COMMANDED.  ALSO, THE DISCONNECT BUTTON HAD NO EFF	ECT (IT WOULD NOT DISCONNECT).  IT WAS NECESSARY TO SHUT OFF POWER TO APPROACH TO DISCONNECT CONTROL LOAD.					1	L	7	2 	3O				3A16    					 
1999091000487	19990910	00487	EA  	1999	9	10	99ZZZX3398       	2	19990819	G	8530	AEL13622	VALVE           		LW12988     						LYC   	O360  	HIO360E1AD  	41514	EA  					EXHAUST STEM	FAILED          	B			QX2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	11		45   					L2138851A			INSTALLED NEW VALVES AT TIME OF OVH.  VALVE STEM END BROKE OFF DUE TO ABNORMAL WEAR.											3	O			1E10				 
1999091000488	19990910	00488	SW  	1999	9	10	99ZZZX3399       	1	19990705	G	7810	9910758101	STACK           		625000501   	GULSTM	114   	114B        	O145001	SW  										EXHAUST	CHAFED          	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	01	6024N	298  				14605				DURING ANNUAL INSPECTION, NOTICED THE ENGINE EXHAUST STACK PN 9910758-101 WAS CHAFING ON ENGINE MOUNT PN 625-000-501 AT 	THE TUBE THAT CONNECTS THE RIGHT LOWER ENGINE MOUNT BRACKET AT THE FIREWALL WITH THE RIGHT NOSE GEAR TRUNNION MOUNT.  TU	BE WAS WORN APPROXIMATELY .035 INCH FROM .750 INCH NOMINAL OUTSIDE DIAMETER.  CLAMP PN Q5200M645 USED TO SUPPORT STACK W	AS MISSING, BUT SPRING AND BRACKET USED IN CONJUNCTION WITH CLAMP WERE INTACT.  SUSPECT CLAMP LOOSENED.			1	L	7	1 	3O			RT	A12SO   					 
1999091000489	19990910	00489	CE  	1999	9	10	99ZZZX3400       	1	19990805	G	2910		SOLENOID        		99101883    	CESSNA	402   	402C        	207590R	CE  										HYD MANIFOLD	STUCK           	D				O				OTHER                   				B	J		SMOKE/FUMES/ODORS/SPARKS  	WARNING INDICATION        		NR	NOT REPORTED   	1			SW	01	2649Z				2011	402C0333				DURING FIGHT, PILOT REPORTED SMOKE IN THE COCKPIT AND RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING.  THE MAINTENANCE DE	PARTMENT WAS DISPATCHED.  POSSIBLE CAUSE WAS HYDRAULIC MANIFOLD SOLENOID STUCK AND CAUSED SYSTEM TO OVERHEAT CAUSING A P	IN HOLE IN THE HYDRAULIC SIGHT GAUGE.  THIS CAUSED THE HYDRAULIC FLUID TO ESCAPE AS A MIST.				1	L	7	2 	3O				A7CE    					 
1999091000490	19990910	00490		1999	9	10	99ZZZX3401       	1	19990801	G	3246	2601475	WHEEL           	BENDIX      	26014112    															MLG	CRACKED         	B			INWR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					B1912					NDT INSPECTION REVEALED CRACK INDICATION IN TUBE WELL AREA.																			 
1999091000491	19990910	00491	SO  	1999	9	10	99ZZZX3402       	1	19990816	G	5513	69624	COUNTERWEIGHT   			PIPER 	PA28  	PA28161     	7102803	SO  										STABILATOR	CRACKED         	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	09	47836	5407 				287816140				AT PRE-PURCHASE INSPECTION, FOUND MOVEMENT IN BALANCE TUBE AT FORWARD STABILATOR FITTING.  REMOVED PAINT, INSPECTED.  FO	UND WHAT LOOKED LIKE CRACK.  REMOVED FROM AIRCRAFT, MAGNAFLUXED, FOUND 1 INCH CRACK AROUND TUBE AND SECOND CRACK OPPOSIT	E SIDE OF TUBE.  TUBE WAS HEAVY WALL COMPLYING WITH AD.  CLOSE INSPECTION NEEDED AT THIS AREA OF TUBE EVEN IF AD THAS BE	EN COMPLIED WITH.			1	L	7	1 	3O				2A13    					 
1999091000492	19990910	00492	CE  	1999	9	10	99ZZZX3403       	1	19990813	G	8120	4706889007	CONTROLLER      			CESSNA	207   	T207A       	2073614	CE  	CONT  	O520  	TSIO520F    	17040	SO  					ENGINE	FAILED          	C				O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			WP	07	9482M		1269 		AG011972	20700689				ON ROLL-OUT, AIRCRAFT WOULD NOT DEVELOP POWER.  ONLY REACHED 24 MAP.  APC WAS FOUND WITH CARBON AND METAL CONTAMINATION.	  AIRCRAFT HAD TURBOCHARGER CATASTROPHIC FAILURE 2 WEEKS PRIOR.  POSSIBLE CAUSE WAS METAL PARTICLES FROM TURBO FAILURE C	ONTAMINATED SEAT VALVE IN CONTROLLER AND CAUSED APC TO FAIL.				1	H	7	1 	3O	3	O		A16CE   	E8CE				 
1999091000493	19990910	00493	SW  	1999	9	10	99ZZZX3404       	1	19990820	G	3230	AN3937	CLEVIS PIN      			TMPSON	NAVION	NAVION*     	6150130	SW  										MLG	FAILED          	D		A		D				RETURN TO BLOCK         				O			OTHER                     			NR	NOT REPORTED   	1			GL	17	100DD					NAV41518				CLEVIS PIN ATTACHING LANDING GEAR LOCK RELEASE CABLE TO HYDRAULIC POWER PACK BROKE AROUND COTTER KEY HOLE WHICH DISCONNE	CTED THE GEAR LOCK RELEASE CABLE FROM THE LANDING GEAR HANDLE.  WHEN GEAR WAS SELECTED DOWN, THE LOCKS DID NOT RELEASE.					1	L	7	1 	3O				A782    					 
1999091000494	19990910	00494	GL  	1999	9	10	99ZZZX3405       	3	19990820	G	6111	HE018	BLADE           			PIPER 	PA18  	PA18150     	7101828	SO  	LYC   	O320  	O320A2A     	41508	EA  	MCAULY	1A175	1A175GM     	GL  	PROPELLER	FRACTURED       	B			CL4R	A				UNSCHED LANDING         				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	91240	1616 	883  			188209006	L4966927A	HE018		APPROXIMATELY 5 INCHES OF ONE PROPELLER BLADE TIP DEPARTED AIRCRAFT IN-FLIGHT.  A SUCCESSFUL EMERGENCY LANDING WAS MADE.	  PROPELLER HAD BEEN RECONDITIONED AFTER PROP STRIKE 883.3 HOURS PREVIOUSLY.  THERE IS NO EVIDENCE OF DAMAGE ON THE REMA	INING PORTION OF THE BLADE.				1	H	7	1 	3O	3	O		1A2     	E274	5	N	P857	 
1999091000495	19990910	00495	GL  	1999	9	10	99ZZZX3406       	3	19990806	G	6111	A13011	CLAMP           			CESSNA	441   	441         	2076020	CE  						HARTZL	HCB3T	HCB3TN5     	GL  	PROPELLER	WRONG PART      	B			M71R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	15								BVA6093		PROPELLER JUST OVERHAULED.  HAS WRONG CLAMPS, PN A1301-1.  HARTZELL OVERHAUL MANUAL CALLS FOR A1301-9S, SHOT PEENED.						1	L	7	2 	3T			RT	A28CE   		6	C	P15EA	 
1999091000496	19990910	00496	SO  	1999	9	10	99ZZZX3407       	2	19990422	G	8530		ROCKER COVER    			CESSNA	340   	340A        	2076405	CE  	CONT  	O520  	TSIO520NB   	17040	SO  					CYLINDER	MISINSTALLED    	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	01	2741R	14   				340A0922	519294			NEW ECI PMA CYLINDER ASSEMBLIES WERE INSTALLED AND IN 14 HOURS TIS, 4 OF THE 6 INTAKE ROCKER ARMS WORE HOLES THROUGH ROC	KER COVERS.  TCM STOCK ROCKER COVERS AND ROCKER COVER GASKETS WERE USED.					1	L	7	2 	3O	3	O		3A25    	E8CE				 
1999091000497	19990910	00497	SO  	1999	9	10	99ZZZX3408       	1	19990507	G	2740	15658029	TUBE            		1563830     	PIPER 	PA23  	PA23250     	7102308	SO  										LT STABILIZER	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	23	27CY				270368	277654118				DURING INSPECTION PER AD 78-02-03, FOUND LEFT TUBE AND WT ASSY CRACKED THROUGH APPROXIMATELY 1.50 INCHES FORWARD OF TUBE	 ATTACHMENT PLATE.  SUBMITTER STATED THIS IS THE FOURTH ONE IN PAST YEAR, ALL WERE MODIFIED PER SB 540A.					1	L	7	2 	3O				1A10    					 
1999091000498	19990910	00498	CE  	1999	9	10	99ZZZX3409       	1	19990801	G	2560	TJ4194	ELT             	LEIGH       		CESSNA	177   	177RG       	2073709	CE  										CABIN	FAILED          	D				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	99	33230				303099	177RG0930				DURING INSPECTION IAW FAR 91.207, THE UNIT COULD NOT BE ACTIVATED BY MEANS OF THE 'G' SHOCK SWITCH.						1	H	7	1 	3O				A20CE   					 
1999091000499	19990910	00499	CE  	1999	9	10	99ZZZX3410       	1	19990820	G	3610		VANES           	AIRBORNE    	216CW       	BEECH 	36    	A36         	1151604	CE  										PUMP	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03	17669	71   			8AP2053	E1002				PUMP HAD DRIVE COUPLING CHANGED AT THE FACTORY TO C/W AD 98-23-01.  ALL PRECAUTIONS WERE TAKEN AT INSTALLATION, BUT VANE	S FAILED FOR UNKNOWN REASON.					1	L	7	1 	3O				3A15    					 
1999091000500	19990910	00500	CE  	1999	9	10	99ZZZX3411       	1	19990813	G	5311		FRAME           			CESSNA	172   	172P        	2072436	CE  										FUSELAGE	CRACKED         	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	99467	3115 				17276451				DURING ANNUAL INSPECTION, FOUND BOTH REAR DOOR FRAME STRUCTURES CRACKED.						1	H	7	1 	3O			NT	3A12    					 
1999091000501	19990910	00501	NM  	1999	9	10	99ZZZX3412       	1	19990726	G	2782		ACTUATOR        		65C2561610  	BOEING	707   	707338C     	138367N	NM  										NR 6 SPOILER	MISINSTALLED    	B		A	TR1R	O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		AP	APPROACH       	1			SW	05	770JS				TC67	19626				AIRCRAFT WAS FLYING TOUCH-AND-GO PATTERN WORK WHEN THE CREW NOTICED BUFFETING AND LOST THEIR AUX HYD SYSTEM.  AFTER LAND	ING, DISCOVERED NR 6 SPOILER ACTUATOR UPPER MOUNT BOLT HAD SHEARED AND THE ACTUATOR DROPPED DOWN ONTO THE FOREFLAP.  AFT	ER FLAPS WERE LOWERED AND RE-RAISED, THE ACTUATOR PUNCTURED THE FOREFLAP AND BOTH ACTUATOAR HYD B-NUTS WERE SNAPPED OFF 	CAUSING AUX HYD SYS FAILURE.  DISCOVERED THE UPPER ACTUATOR ATTACH BOLT FITTING BUSHINGS WERE NOT INSTALLED AT SPOILER O	VERHAUL CAUSING EXCESSIVE PLAY ON THE BOLT LEADING TO ITS FAILURE.		2	L	7	4 	4F				4A26    					 
1999091000502	19990910	00502	EU  	1999	9	10	99ZZZX3413       	1	19990728	G	3233	184811	CYLINDER        		1862K       	BAG   	JETSTM	JETSTM3201  	1500217	EU  										RADIUS ROD	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	484UE	14954	2640 		LK8706352	899				RADIUS ROD, PN 1862/K, SN LK-8706352, WAS RECEIVED WITH COMMENT 'CRACKED'.  INSPECTION REVEALED APPROXIMATELY A 10 INCH 	CRACK ORIENTED ALONG THE FORGING FLASH LINE ON THE ONE-WAY RESTRICTOR MOUNTING LUG SIDE, RUNNING FROM THE 'OPEN' END OF 	THE CYLINDER, PN 184811, SN PIP304.  COMPLETE RADIUS ROD HAS BEEN RETURNED TO APPH FOR INVESTIGATION.				2	L	7	2 	4T			RT	A56EU   					 
1999091000503	19990910	00503	EU  	1999	9	10	99ZZZX3414       	1	19990728	G	3411		STATIC DRAINS   			BRAERO	DH125 	BAE125800A  	1500285	EU  										FUSELAGE	MISINSTALLED    	B	P		JGVR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CE	09	4402	4244 				258199				WHILE INSTALLING PITOT/STATIC DRAIN VALVE MODIFICATIONS, FOUND S2 STATIC DRAIN SYSTEM DISABLED.  S2 DRAIN VALVE RESERVOI	R HAD BLANKING CAP INSTALLED.  THE T-FITTING CONNECTING THE LEFT AND RIGHT S2 STATIC SYSTEM WAS CAPPED.  THIS LEFT THE S	2 SYSTEM WITHOUT A DRAIN.  THIS DRAIN IS LOCATED UNDER THE COPILOT SEAT IN AN UNACCESSIBLE AREA DUE TO AVIONICS THAT ARE	 INSTALLED IN THIS AREA.  SUBMITTER STATED THE LOG BOOKS DO NOT REFLECT THIS CHANGE.			2	L	7	2 	4F			RT	A3EU    					 
1999091000504	19990910	00504	EU  	1999	9	10	99ZZZX3415       	1	19990801	G	5751	258WS20052A	BRACKET         			BRAERO	DH125 	BAE125800A  	1500285	EU  										AILERON	CRACKED         	B	P	A	JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	4402	4244 				258199				FLIGHT CONTROLS WERE REMOVED FOR NDT INSPECTION.  RIGHT AILERON CENTER UPPER HINGE BEARING MOUNT CRACKED ON AFT SIDE.  N	EW HINGE BRACKET INSTALLED.					2	L	7	2 	4F			RT	A3EU    					 
1999091000505	19990910	00505	EU  	1999	9	10	99ZZZX3416       	1	19990727	G	3411	25SF1155	RESERVOIR       			BRAERO	DH125 	HS125700A   	4230170	EU  										FUSELAGE	CONTAMINATED    	B	P		JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	137WR					257035				DURING INSTALLATION OF THE PITOT/STATIC DRAIN VALVE MOD, S2 DRAIN RESERVOIR WAS FULL OF WATER WHEN IT WAS DISASSEMBLED. 	 UPON INSPECTION OF THE RESERVOIR BODY, THE WATER HAD FROZEN AND BULGED THE RESERVOIR SIDES.  ALL PITOT AND STATIC DRAIN	 VALVES WERE SEALED FROM THE OUTSIDE WITH A SEALANT.				2	L	7	2 	4F				A3EU    					 
1999091000506	19990910	00506	CE  	1999	9	10	99ZZZX3417       	1	19990304	G	5542	101630000613	SKIN            			BEECH 	200   	200BEECH    	1152920	CE  										RUDDER	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	5ST	8010 				BB289				DURING INSPECTION OF THE AIRCRAFT, DAMAGE TO THE LEFT SIDE OF THE RUDDER AT THE TRIM ACTUATOR CUT-OUT ON THE LEADING EDG	E OF THE RUDDER WAS NOTICED.  DAMAGE WAS THE RESULT OF WIND BLAST.  INSPECTION OF THE DAMAGE REVEALED A .75 INCH CRACK N	EAR THE TOP SIDE OF THE CUT-OUT.				1	L	7	2 	4T				A24CE   					 
1999091000507	19990910	00507	GL  	1999	9	10	99ZZZX3418       	3	19990723	G	6114	C4716C98	HUB             													MCAULY	2A34C	D2A34C98    	GL  	PROPELLER	CRACKED         	B			PI4R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	07								747984		HUB LEAKING RED DYE.  CRACK VISIBLE WITH NAKED EYE (DUE TO DYE LEAKING THROUGH).  CAUSE UNKNOWN.																5	C	P3EA	 
1999091000508	19990910	00508		1999	9	10	99ZZZX3419       	4	19990726	G	3416	066306200	ALTIMETER       			BEECH 	1900  	1900D       	1154162	CE  										COCKPIT	MALFUNCTIONED   	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01	255GL				3258	UE255				ALERT LIGHT IN ALTIMETER COMES ON WHEN POWER IS APPLIED. THIS UNIT WAS REMOVED FROM STOCK AND HAD BEEN OVERHAULED AND WA	S BACK FOR SUBSEQUENT REPAIRS UNDER WARRANTY ON TWO OCCASIONS SINCE MARCH 2, 1999.  INITIAL TESTS BY INSTALLER FOUND THA	T PINS B AND E WERE SHORTED.				2	L	7	2 	4T			RT	A24CE   					 
1999091000509	19990910	00509	WP  	1999	9	10	99ZZZX3420       	2	19990809	G	7210	30700934	GEARBOX         			LEAR  	35    	35LEAR      	5170600	CE  	GARRTT	TFE731	TFE73122B   	01518	WP  					LT ENGINE	FAILED          	B			MJIR	O				OTHER                   				X	J		ENGINE FLAMEOUT           	WARNING INDICATION        		NR	NOT REPORTED   	1			EA	11	600DT				P312	35017	P74152			LEFT ENGINE, SN P74152, EXPERIENCED AN IN-FLIGHT SHUT DOWN.  ATTEMPTS TO RESTART WERE UNSUCCESSFUL.  ENGINE P74152 WAS R	EMOVED FROM THE AIRCRAFT.  UPON TEARDOWN, NOTED ENGINE TRANSFER GEARBOX PN 3070093-4, SN P312, PART TSN:  10,452.4 HOURS	, CSN:  10,039, HAD FAILED (BEVEL GEAR AREA).  THIS GEARBOX FAILURE HAD CAUSED A LOSS OF ENGINE DRIVEN FUEL PUMP PRESSUR	E; THIS LACK OF FUEL CAUSED THE ENGINE TO SHUT DOWN.  ALIED SIGNAL ENG HAS BEEN ADVISED OF THIS CONDITION.  ENG SN P7415	2 - TSN:  10,452.4 HOURS - CSN:  10,039 HOURS.		2	L	7	2 	4F	4	F		A10CE   	E6WE				 
1999091000510	19990910	00510	NE  	1999	9	10	99ZZZX3421       	2	19990811	G	7230		LP TURBINE      								PWA   	JT8   	JT8D9A      	52048	NE  					COMPRESSOR	FAILED          	H				E				ENGINE SHUTDOWN         				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SW	99							P666390			ENGINE TT:  40,541 HRS.  ENGINE TC:  26,975.  PRECAUTION IFSD DUE TO HIGH EGT AND VIBRATION.  INCOMING INSPECTION REVEAL	ED AIRFOIL FRACTURED T3 AND T4 BLADE SETS.  LPT COULD NOT BE REMOVED BY THE REGULAR PROCEDURE, HPC SPLIT FROM THE FRONT 	LPT.  ENGINE CURRRENTLY UNDER INVESTIGATION.  FIRST SHOP VISIT AT GE CELMA.									4	F			E2EA				 
1999091000511	19990910	00511	NM  	1999	9	10	99ZZZX3422       	1	19990801	G	3244		TIRE            			BOEING	747   	747283B     	1384867	NM  										LT MLG	FAILED          	B			GK4Y	O				OTHER                   				O			OTHER                     			LD	LANDING        	1			WP	03	921FT					21575				ON LANDING, NR 6 MAIN WHEEL ASSY BLEW CAUSING MINOR DAMAGE TO LEFT BODY GEAR INNER DOOR.  BOTH NR 5 AND NR 6 MAIN WHEELS	 CHANGED, AS WELL AS NR 7 WHEEL WHICH HAD FLAT SPOT.  MINOR REPAIR WAS CARRIED OUT ON LEFT BODY GEAR INNER DOOR PER SRM.	  LEFT BODY GEAR STRUT FOUND LOW.  LEFT BODY GEAR SERVICED PER MM.				2	L	7	4 	4F				A20WE   					 
1999091000512	19990910	00512	NM  	1999	9	10	99ZZZX3423       	1	19990801	G	5280		DOOR            			BOEING	747   	747283B     	1384867	NM  										LT MLG	DAMAGED         	B			GK4Y	O				OTHER                   				O			OTHER                     			LD	LANDING        	1			WP	03	921FT					21575				ON LANDING, NR 6 MAIN WHEEL ASSY BLEW CAUSING MINOR DAMAGE TO LEFT BODY GEAR INNER DOOR.  BOTH NR 5 AND NR 6 MAIN WHEELS	 CHANGED, AS WELL AS NR 7 WHEEL WHICH HAD FLAT SPOT.  MINOR REPAIR WAS CARRIED OUT ON LEFT BODY GEAR INNER DOOR PER SRM.	  LEFT BODY GEAR STRUT FOUND LOW.  LEFT BODY GEAR SERVICED PER MM.				2	L	7	4 	4F				A20WE   					 
1999091000513	19990910	00513	NM  	1999	9	10	99ZZZX3424       	1	19990806	G	5753		SKIN            			BOEING	727   	727225      	1384077	NM  										TE FLAP	GOUGED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND RT OUTBOARD FOREFLAP GOUGED IN LEADING EDGE.  BURNISHED GOUGE,	 ALODINED AND PRIMED, FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-4.					2	L	7	3 	4F				A3WE    					 
1999091000514	19990910	00514	NM  	1999	9	10	99ZZZX3425       	1	19990810	G	5315		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 440	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTE C-CHECK WORK CARD, FOUND CORROSION ON FLOORBEAM AT FS 440 LBL 62 TO RBL 62.  REMOVED DAMA	GED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8.					2	L	7	3 	4F				A3WE    					 
1999091000515	19990910	00515	NM  	1999	9	10	99ZZZX3426       	1	19990809	G	5320		EXTRUSION       			BOEING	727   	727225      	1384077	NM  										BS 303	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND 2 EACH CRACKS AT FS 303.9, LEFT SIDE OF COCKPIT DOOR LOWER ATT	ACH POINT.  STOP DRILLED CRACKS PER SRM 51-10-1.  FABRICATED AND INSTALLED PER SRM 51-40-3.					2	L	7	3 	4F				A3WE    					 
1999091000516	19990910	00516	NM  	1999	9	10	99ZZZX3427       	1	19990809	G	5320		WEB             			BOEING	727   	727225      	1384077	NM  										BS 1343 RT	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE 'C'  CHECK WORK CARD, FOUND A CRACK IN LOWER RIGHT TORQUE BOX, THIRD LOWER LIGHTENING H	OLE FROM FRONT, FS 1343.  STOP DRILLED CRACK PER SRM 51-10-1.  FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2.					2	L	7	3 	4F				A3WE    					 
1999091000517	19990910	00517	NM  	1999	9	10	99ZZZX3428       	1	19990809	G	5320		WEB             			BOEING	727   	727225      	1384077	NM  										BS 1333	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND A CRACK AT LIGHTENING HOLE IN LOWER RT TORQUE BOX, SECOND LO	WER HOLE FROM FRONT, FS 1333 RT.  STOP DRILLED HOLE PER SRM 51-10-1.  FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51	-40-2.				2	L	7	3 	4F				A3WE    					 
1999091000518	19990910	00518	NM  	1999	9	10	99ZZZX3429       	1	19990809	G	5320		WEB             			BOEING	727   	727225      	1384077	NM  										BS 1363	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND A CRACK IN LOWER RT TORQUE BOX AREA, FIFTH UPPER LIGHTENING HO	LE FROM FRONT, BS 1363.  REMOVED EXISTING DOUBLER.  STOP DRILLED CRACK.  FABRICATED AND INSTALLED NEW DOUBLER PER SRM 5-	40-2.				2	L	7	3 	4F				A3WE    					 
1999091000519	19990910	00519	NM  	1999	9	10	99ZZZX3430       	1	19990806	G	5330		SKIN            			BOEING	727   	727225      	1384077	NM  										BS 620	CORRODED        	B				K				NONE                    				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION AT AFT LOWER CORNER OF LOW CARGO DOOR CUT-OUT, BS 	620.  REMOVED CORROSION AND FOUND OUT OF LIMITS PER SRM 53-10-2.  FABRICATED AND INSTALLED NEW SUPPORT WEB PER SRM'S 51-	10-1 AND 51-30-2.				2	L	7	3 	4F				A3WE    					 
1999091000520	19990910	00520	NM  	1999	9	10	99ZZZX3431       	1	19990806	G	5210		BRACKET         			BOEING	727   	727225      	1384077	NM  										PASSENGER DOOR	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND MAIN ENTRY DOOR BRACKET CRACKED AT FORWARD LOWER CORNER.  RE	MOVED DAMAGED BRACKET.  FABRICATED AND INSTALLED NEW BRACKET PER SRM'S 51-10-1 AND 51-30-2.					2	L	7	3 	4F				A3WE    					 
1999091000521	19990910	00521	NM  	1999	9	10	99ZZZX3432       	1	19990806	G	5320		EXTRUSION       			BOEING	727   	727225      	1384077	NM  										BS 1030	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION AT UPPER LOBE BS 1030 BL ZERO.  REMOVED CORROSION 	AND FOUND OUT OF LIMITS PER SRM 51-10-1.  FABRICATED AND INSTALLED REPAIR PER SRM 51-40-4.					2	L	7	3 	4F				A3WE    					 
1999091000522	19990910	00522	NM  	1999	9	10	99ZZZX3433       	1	19990806	G	5320		SUPPORT         			BOEING	727   	727225      	1384077	NM  										BS 420-460	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION ON FLOOR SUPPORT AT BS 420 TO BS 460 RBL 62.  FABR	ICATED AND INSTALLED NEW SUPPORT PER SRM 53-10-8 FIG 6.					2	L	7	3 	4F				A3WE    					 
1999091000523	19990910	00523	NM  	1999	9	10	99ZZZX3434       	1	19990806	G	5315		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 360	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND CORROSION ON FLOORBEAM AT BS 360 LBL 62 TO RBL 62.  REMOVED 	FLOORBEAM UPPER CHORD PER SRM 51-30-2.  FABRICATED AND INSTALLED NEW UPPER CHORD PER 53-10-8.					2	L	7	3 	4F				A3WE    					 
1999091000524	19990910	00524	NM  	1999	9	10	99ZZZX3435       	1	19990806	G	5315		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 460	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND FLOORBEAM CORRODED AT BS 460 LBL 62 TO RBL 62.  REMOVED CORR	OSION AND FOUND OUT OF LIMITS PER SRM 53-10-1.  REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR TO UPPER CHORD PER	 SRM 53-10-8.				2	L	7	3 	4F				A3WE    					 
1999091000525	19990910	00525	NM  	1999	9	10	99ZZZX3436       	1	19990806	G	5320		STRAP           			BOEING	727   	727225      	1384077	NM  										CARGO BAY	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND FLOOR SUPPORT CROSSMEMBER CORRODED AT BS 1030 LBL 45.50 AND 	LBL 24.75.  REMOVED CORROSION PER SRM 51-10-6 AND FOUND OUT OF LIMITS.  REMOVED CROSSMEMBER AND FABRICATED AND INSTALLED	 REPAIR PER SRM 53-10-8 FIG 6.  REINSTALLED CROSSMEMBER PER SRM 51-30-2.				2	L	7	3 	4F				A3WE    					 
1999091000526	19990910	00526	NM  	1999	9	10	99ZZZX3437       	1	19990806	G	5753		SKIN            			BOEING	727   	727225      	1384077	NM  										TE FLAP	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, RIGHT INBOARD AFT FLAP SKIN CRACKED AT OUTBOARD ATTACH POINT.  STO	P DRILLED CRACK PER SRM 51-10-1.  FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-50-4.					2	L	7	3 	4F				A3WE    					 
1999091000527	19990910	00527	NM  	1999	9	10	99ZZZX3438       	1	19990806	G	5751		SKIN            			BOEING	727   	727225      	1384077	NM  										AILERON	DELAMINATED     	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND LT OUTBOARD AILERON DELAMINATING ON UPPER OUTBOARD CORNER. R	EBONDED DELAMINATION PER SRM 51-40-5.					2	L	7	3 	4F				A3WE    					 
1999091000528	19990910	00528	NM  	1999	9	10	99ZZZX3439       	1	19990806	G	5753		SKIN            			BOEING	727   	727225      	1384077	NM  										TE FLAP	GOUGED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND RT INBOARD FOREFLAP GOUGED, INBOARD OF INBOARD TRACK.  BURNI	SHED GOUGED, ALODINED AND PRIMED.  FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-4.					2	L	7	3 	4F				A3WE    					 
1999091000529	19990910	00529	NM  	1999	9	10	99ZZZX3440       	1	19990820	G	5315		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 312	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	354PA					20624				DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORK CARD, FOUND FLOORBEAM CORRODED AT BS 312R RBL 62.5.  REMOVED DAMAGED ARE	A, FABRICATED AND INSTALLED REPAIR PER SRM 51-10-1.					2	L	7	3 	4F				A3WE    					 
1999091000530	19990910	00530	CE  	1999	9	10	99ZZZX3441       	1	19990812	G	5610	66004048	WINDSHIELD      			LEAR  	55    	55LEAR      	5170702	CE  										COCKPIT	CRACKED         	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	11	355DB	4545 			5WU9498790	006				ACFT TT:  8,511.9 HOURS.  LANDINGS:  6,959.  WHILE PERFORMING MFG 300-HOUR/12-MONTH INSPECTION A VOID/CRACK, MATERIAL WA	S MISSING ON THE RT WINDSHIELD OUTER SURFACE IN THE LOWER FWD AREA UNDER THE DEFROST DUCT.  THE DAMAGED AREA MEASURED AP	PROX .3125 INCH DEEP, .8750 INCH WIDE, AND 5 INCHES LONG WITH ADDITIONAL 1 INCH CRACKS EXTENDING FROM EACH END OF THE DA	MAGED AREA.  THE WINDSHIELD WAS INSTALLED 92-93, ACTT:  3,966.8  HRS, TT ON WINDSHIELD WAS 4,545.1 HRS.  CAUSE OF DAMAGE	 UNKNOWN, AND THERE IS NO VISUAL EVIDENCE AS TO WHAT CAUSED THIS DAMAGE.  SENT INFORMATION AND PHOTOS OF DAMAGE TO LEAR 	FOR EVALUATION.  NOTE:  THE DAMAGE CANNOT BE SEEN WITHOUT REMOVAL OF THE DEFROST DUCT.	2	L	7	2 	4F				A10CE   					 
1999091000531	19990910	00531	SO  	1999	9	10	99ZZZX3442       	1	19990813	G	2740	2020302	TORQUE TUBE     			PIPER 	PA24  	PA24250     	7102404	SO  										STABILATOR	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	5850P	3607 				24932				DURING ANNUAL INSPECTION, FOUND IT WAS NECESSARY TO REMOVE THE STABILATOR TORQUE TUBE ASSY TO CORRECT ANOTHER DISCREPANC	Y.  THE RT AND LT STABILATORS WERE FOUND DIFFICULT TO REMOVE FROM THE TORQUE TUBE.  THE INBD FITTING (PN 21420-02) WAS U	NBOLTED FROM THE STABILATORS AND LEFT ON THE TUBE WHILE THE STABILATORS WERE REMOVED.  DISCOVERED THE TORQUE TUBE HAD A 	LOT OF CORROSION BUILT UP ON IT.			1	L	7	1 	3O				1A15    					 
1999091000532	19990910	00532	SO  	1999	9	10	99ZZZX3443       	1	19990813	G	5711	2366200	RIVETS          			PIPER 	PA24  	PA24250     	7102404	SO  										RT/LT WING	SHEARED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	5850P	3607 				24932				DURING AN ANNUAL INSPECTION, THE RT AFT ATTACH FITTING, UNDER THE AFT BAGGAGE FLOOR, WAS FOUND TO HAVE SEVERAL MISSING R	IVETS AND THE PLATE WAS MISALIGNED WITH THE FITTING ASSY.  THE RIVETS THAT WERE STILL IN THE HOLES WERE ALL SHEARED.  TH	E LT ATTACH WAS INSPECTED AND APPEARED TO BE ALIGNED AND ALL OF RIVETS IN PLACE.  HOWEVER, UPON PULLING ON SOME OF THE R	IVET TAILS BY HAND, MANY WERE FOUND SHEARED AND EASILY PULLED OUT.  SUBMITTER SUGGESTED THIS MAY HAVE BEEN CAUSED BY HAR	D LANDINGS.		1	L	7	1 	3O				1A15    					 
1999091000533	19990910	00533	NM  	1999	9	10	99ZZZX3444       	1	19990806	G	5315		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 312	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	361KP					20627				DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND CORROSION ON FLOORBEAM AT BS 312, BL ZERO.  REMOVED DAMAGED AR	EA, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8.					2	L	7	3 	4F				A3WE    					 
1999091700537	19990917	00537	WP  	1999	9	17	99ZZZX3445       	1	19990617	G	6230		BUNGEE SOCKET   			HUGHES	369   	369D        	4470706	WP  										COLLECTIVE	LOOSE           	B			EOOR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	5074R					1151D				PILOT COMPLAINED OF A STIFF COLLECTIVE.  FOUND COLLECTIVE BUNGEE BRACKET DEFLECTING EXCESSIVELY DURING CONTROL MOVEMENT.	   FOUND THE BUNGEE PLUNGER 369A 7372-5 DRAGGING WITHIN BUNGEE SOCKET 369A 7371-7.  CLEANED OUT DRIED OUT MOLYBOENUM DIS	ULPHIDE GREASE AND RE-LUBED.				1	G	7	1 	3U				H3WE    					 
1999091700555	19990917	00555	NE  	1999	9	17	99ZZZX3454       	2	19990605	G	7261	23063144	FILTER          			BELL  	430   	430         	1182150	SW  	ALLSN 	250C  	250C40B     	03032	NE  					ENGINE	CLOGGED         	B			AC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	816  				49037				FILTERS CHANGED FOR BYPASS BUTTON ACTIVATION IN 100 HOURS.						1	G	7	2 	3U	3	U	RT	H9SW    	E1GL				 
1999091700572	19990917	00572	SW  	1999	9	17	99ZZZX3455       	1	19990727	G	5302	407023800117	SUPPORT         		407030800101	BELL  	407   	407         		SW  										TAILBOOM	CRACKED         	B			ALGR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	527AL	1700 			53212	53211				CRACK IN RADIUS, POOR QUALITY CONTROL MEASURES WHEN FABRICATING AND POSSIBLE PRE-LOADED CONDITION.  BETTER QUALITY WHEN 	FABRICATING SUPPORT AND POSSIBLE SHIM TO PREVENT PRE-LOAD.  (X)					1	G	7	1 	3U			O	H2SW    					 
1999091700573	19990917	00573	SW  	1999	9	17	99ZZZX3456       	1	19990312	G	5302	407023800118	SUPPORT         		407030800101	BELL  	407   	407         		SW  										TAILBOOM	MISINSTALLED    	B			ALGR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	557AL	517  				53243				DURING DAILY INSPECTION FOUND SUPPORT MISINSTALLED.  SUBMITTER STATED PART INSTALLED UNDER STRESS AND POOR QUALITY CONTR	OL.					1	G	7	1 	3U			O	H2SW    					 
1999091700585	19990917	00585	EU  	1999	9	17	99ZZZX3462       	1	19990111	G	6220	10513143	ROD END         			BOLKMS	BK117 	BK117C1     	5626025	EU  										MAIN ROTOR	WORN            	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4042H	394  				7509				BEARING WORN.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999091700587	19990917	00587	EU  	1999	9	17	99ZZZX3464       	1	19990804	G	6220	10513143	ROD END         			BOLKMS	117   	BK117A4     	5626017	EU  										MAIN ROTOR	MAIN ROTOR      	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	8765J	163  				7054				BEARINGS WORN.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999092400026	19990924	00026	SO  	1999	9	24	99ZZZX3467       	2	19990812	G	8530		CYLINDER        			BEECH 	95    	95B55       	1152729	CE  	CONT  	O470  	IO470L      	17026	SO  					RT ENGINE	CRACKED         	H	P			E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			E	K	J	VIBRATION/BUFFET          	FLUID LOSS                	WARNING INDICATION        	NR	NOT REPORTED   	1			SW	03	7630N					TC1164	272949R			ENGINE HAD 266.2 HOURS SINCE A FACTORY ZERO TIMED OVERHAUL 11-24-99.  RIGHT ENGINE SHUT DOWN IN-FLIGHT DUE TO VIBRATION 	AND VISIBLE OIL LEAKAGE.  UPON NORMAL SINGLE ENGINE LANDING, TOP COWL WAS REMOVED TO FACILITATE INVESTIGATION.   FOUND N	R 5 CYL CRACKED AT 75 PERCENT AROUND THE BARREL AT MID-POINT.  THE CYL AND PISTON ASSY WERE REMOVED TO REPLACE WITH NEW 	CYL ASSY.  CRACK IN CYL BARREL WENT 100 PERCENT AROUND BARREL, AND APPROX 80-90 PERCENT OF THE CRACK WAS SEPARATED COMPL	ETELY THROUGH.  UPON REMOVAL OF CYL, FOUND THE WHOLE PISTON SKIRT AND SOME OF THE PISTON RINGS MISSING.  ENGINE WAS GROU	ND RUN AND CHECKED FOR LEAKS AND FLIGHT TESTED FOR 20 MINS, THEN FLOWN 1.5 HRS TO HOME FIELD WITH NO OTHER INCIDENTS.	1	L	7	2 	3O	3	O	RT	3A16    	3E1				 
1999092400028	19990924	00028	CE  	1999	9	24	99ZZZX3469       	1	19990806	G	7930	384500	THERMOSTAT      			RKWELL	NA265 	NA26560     	7630106	CE  										LT ENGINE	FAILED          	B			WK4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	400JH				7015	306133				THERMOSTAT INSTALLED ON A FRESHLY OVERHAULED ENGINE.  ENGINE WAS OVERHAULED BY FAA CRS OTUR438L.  PART DID NOT FAIL UNTI	L ONE HOUR INTO FIRST FLIGHT.					2	L	7	2 	4J			RT	A2WE    					 
1999092400029	19990924	00029	EU  	1999	9	24	99ZZZX3470       	1	19990824	G	3246	95437411	WHEEL           	GOODYEARAERO	95504632    	FOKKER	F28   	F28MK1000   	4990808	EU  										MLG	CRACKED         	B			QH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	43AE	4000 			JAN80878	11016				THIS PART, LOCATED IN THE O-RING SEALING AREA,  WAS TESTED FOR MILLION AIR, SALT LAKE CITY, UT, IAW AIRCRAFT BRAKING SYS	TEMS 32-42-05.					2	L	7	2 	4F			RT	A20EU   					 
1999092400030	19990924	00030	CE  	1999	9	24	99ZZZX3471       	1	19990205	G	7540	66002125	LIMITER         			LEAR  	25    	25D         	5170514	CE  										TAILCONE	BROKEN          	E				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			NM	03	444MK	11854				252				AIRCRAFT LOST PRESSURIZATION DURING CLIMB THROUGH FL 200.  AIRCRAFT RETURNED TO  MAINTENANCE BASE FOR REPAIR.  DUCT TEMP	 LIMITER FOR CABIN PRESSURIZATION FOUND BROKEN AT MOUNT BASE AND WAS REPLACED WITH AN UPDATED, IMPROVED PART IAW A FACTO	RY SUPPLIED AIRCRAFT MODIFICATION KIT (AMK).				2	L	7	2 	4J				A10CE   					 
1999092400031	19990924	00031	EU  	1999	9	24	99ZZZX3472       	1	19990819	G	3010	58J83123403	DUCT            			AMD   	FALC50	FALCON50MYST	2730106	EU  										ANTI-ICE VALVE	BROKEN          	B			J2BR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	50AE	1016 			0009	254				DUCT BROKEN AT WELD SIX INCHES FROM ANTI-ICE VALVE.  BOTH SUPPORTING CLAMPS BROKEN.  HOT AIR FROM BROKEN PIPE DAMAGE ANT	I-ICE VALVE AND DIGITAL ELECTRONIC ENGINE CONTROL.  SUSPECT TOO MUCH PRELOAD ON DUCT BROKE CLAMPS AND DUCT FAILURE OCCUR	RED.				2	L	7	3 	4F				A46EU   					 
1999092400032	19990924	00032	SO  	1999	9	24	99ZZZX3473       	2	19990817	G	8520		CRANKSHAFT      			MOONEY	M20   	M20R        	5870225	SW  	CONT  	O550  	IO550N      	17042	SO  					ENGINE	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	1172L	10   				290183	683356			ENGINE SHOOK VIOLENTLY.  MIXTURE CONTROL WAS PULLED BACK TO CUT-OFF IMMEDIATELY.  THE ENGINE SEIZED UP.  A SAFE LANDING 	WAS MADE.  TEAR-DOWN INSPECTION REVEALED THE CRANKSHAFT HAD FAILED.					1	L	7	1 	3O	3	O	RT	2A3     	E3SO				 
1999092400033	19990924	00033	SO  	1999	9	24	99ZZZX3474       	2	19990817	G	7313	627335D1212E	INJECTOR        			MOONEY	M20   	M20R        	5870225	SW  	CONT  	O550  	IO550G      	17042	SO  					ENGINE	FAILED          	H				C				ABORTED TAKEOFF         				W	J		INADEQUATE Q C            	WARNING INDICATION        		TO	TAKEOFF        	1			SW	99	21625	10   				290170				NEW AIRCRAFT AND NEW ENGINE.  ENGINE RAN ROUGH ON TAKEOFF, TOP COWL REMOVED AND COLD CYLINDER ESTABLISHED.  UPON REMOVAL	 OF FUEL MANIFOLD, WRENCH WAS APPLIED TO INJECTOR AND ASSY TWISTED IN HALF.  INJECTOR WAS BROKEN LONG BEFORE ATTEMPTED R	EMOVAL.  A SECOND INJECTOR APPEARS TO BE CRACKED IN THE SAME LOCATION ON ANOTHER CYLINDER.				1	L	7	1 	3O	3	O	RT	2A3     	E3SO				 
1999092400035	19990924	00035	CE  	1999	9	24	99ZZZX3476       	1	19990801	G	2710	0510105216	CONTROL CABLE   			CESSNA	172   	172H        	2072424	CE  										AILERON	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	35	3788F					M255283				YOKE WAS ABOUT 10 DEGREES TO THE LEFT DURING LEVEL FLIGHT.  PILOT REQUESTED AN ADJUSTMENT.  AN ATTEMPT WAS MADE TO ADJUS	T CABLES, WHEN PLASTIC COVER WAS REMOVED BEHIND INSTRUMENT PANEL, THE ROD END THAT SCREWED INTO TURNBUCKLE WAS BROKEN AN	D THE AILERONS WERE OPERATING WITH A SINGLE STRAND OF SAFETY WIRE, 041 INCH.				1	H	7	1 	3O			NT	3A12    					 
1999092400036	19990924	00036	SO  	1999	9	24	99ZZZX3477       	1	19990822	G	5540	9538600	ARM             			PIPER 	PA34  	PA34200     	7103405	SO  										RUDDER	CRACKED         	D		A		O				OTHER                   				F			FLT CONT AFFECTED         			NR	NOT REPORTED   	1			WP	23	56795	5200 				347450032				PART FAILED WHERE THE ARM IS WELDED TO THE CROSS BAR ASSEMBLY CAUSING COMPLETE LEFT RUDDER DEFLECTION FAILURE.  SUBMITTE	R SUGGESTED IMMEDIATE INSPECTION OF THIS PART FOR CRACKS.  THIS AIRCRAFT IS USED FOR FLIGHT TRAINING AND IS CONSISTENTLY	 USED FOR SINGLE ENGINE OPERATIONS THAT CAUSE EXTRA STRESS ON THIS PART.  PART FAILED DURING GROUND OPERATIONS.				1	L	7	2 	3O				A7SO    					 
1999092400037	19990924	00037	CE  	1999	9	24	99ZZZX3478       	1	19990404	G	3230	12802091	PIN             		12880243F   	CESSNA	182   	182Q        	2072732	CE  										NLG	BROKEN          	B	L		IFRR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	01	2AJ	4384 			MMA2014	R18201789				NOSE GEAR WOULD NOT LOCK DOWN.  AFTER MASTER WAS SHUT OFF, NOSE GEAR COLLAPSED CAUSING DAMAGE TO PROPELLER, NOSE GEAR DO	ORS, AND COWL FLAP DOORS.  THE TWO LOCKING PINS ATTACHED TO ACTUATOR CYLINDER WERE LOOSE/BROKEN AND FLOATED OUT TO TOUCH	 THE ACTUATING CYLINDER SHAFT.  NEAR THE END OF THE TRAVEL THERE IS A BUSHING WHICH IS LARGER IN SIZE THAN THE SHAFT.  T	HE PINS MADE CONTACT WITH THE BUSHING SO THE NOSE GEAR COULD NOT GET INTO LOCKED POSITION.			1	H	7	1 	3O			NT	3A13    					 
1999092400041	19990924	00041	SO  	1999	9	24	99ZZZX3482       	1	19990825	G	5330	6206102	SKIN            			PIPER 	PA28  	PA28*       		SO  										FUSELAGE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	09										DOUBLER UNDER RIGHT UPPER WING ROOT SKIN CRACKING (BOTH FORWARD AND AFT SECTIONS).  DUE TO NORMAL STRESS FROM GETTING IN	 AND OUT OF AIRCRAFT, THE UPPER SKIN FLEXES ENOUGH TO CONCENTRATE STRESSES AROUND THE STIFFENERS BEND RADIUS TO CAUSE CR	ACKING.  THIS LEADS TO UPPER WING SKIN FLEXING AND CRACKING AND POPPED RIVET HEADS.				1	L	7	1 	3O				2A13    					 
1999092400042	19990924	00042	SO  	1999	9	24	99ZZZX3483       	1	19990828	G	2820	9804472	LINE            			PIPER 	PA28  	PA28181     	7102807	SO  										COCKPIT	CORRODED        	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	09	17762					288390023				CLAMP HOLDS MOISTURE IN AND AROUND FUEL LINE CAUSING CORROSION AND LEAKAGE INSIDE COCKPIT.						1	L	7	1 	3O				2A13    					 
1999092400043	19990924	00043	SO  	1999	9	24	99ZZZX3484       	1	19990624	G	2740	6270140	CONTROL CABLE   			PIPER 	PA32  	PA32R300    	7103213	SO  										STABILATOR	BROKEN          	D		A		A				UNSCHED LANDING         				F			FLT CONT AFFECTED         			CL	CLIMB          	1			GL	05	47JE	1468 				32R7780532				AFTER DEPARTURE, PILOT NOTICED LOSS OF STABILATOR CONTROL.  BY USING TRIM TAB AND LIMITED DOWN STABILATOR, HE WAS ABLE T	O BRING AIRCRAFT BACK INTO A NORMAL PATTERN AND MAKE AN UNEVENTFUL LANDING.  UPON INITIAL INSPECTION, UP FORWARD STABILA	TOR CABLE WAS FOUND TO BE SEPARATED.  SAFETY WIRE WAS STILL PARTIALLY INTACT WITH ENDS OF CABLE PULLED ABOUT 6 INCHES AP	ART.  UPON INSPECTION OF AFT CABLE, MINOR PITTING WAS OBSERVED.  AIRCRAFT HAS SIGNS OF PITTING, WITH WATER TRAPPED IN BE	LLY POSSIBLY WITH STABILATOR REMOVED, AND CABLE LYING IN BELLY.		1	L	7	1 	3O			 	A3SO    					 
1999092400045	19990924	00045	SO  	1999	9	24	99ZZZX3486       	2	19990818	G	7414	662	MAGNETO         	SLICK       		CESSNA	182   	182P        	2075816	CE  	CONT  	O470  	O470S       	17026	SO  					ENGINE	DAMAGED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	05	84731	815  			L7010504	18261896	464556			WHILE DOING AN ANNUAL INSPECTION, BOTH MAGS WERE FOUND TO HAVE LOOSE DISTRIBUTOR BLOCKS.  THE SCREWS IN THE LEFT MAGNETO	 WERE COMPLETELY OUT AND THE BLOCK FELL OUT WHEN THE COVER WAS REMOVED.  THE INSIDES OF BOTH BLOCKS WERE VERY DIRTY AND 	DID NOT LOOK LIKE THEY HAD BEEN EVER OPENED FOR INSPECTION OR LUBRICATION.				1	H	7	1 	3O	3	O	NT	TA13    	E273				 
1999092400046	19990924	00046	SO  	1999	9	24	99ZZZX3487       	1	19990610	G	5530	6697504	BOLT            			PIPER 	PA32  	PA32R301T   	7103220	SO  										VERTICAL STAB	DAMAGED         	H	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	27	94D					32R8229050				DURING ANNUAL INSPECTION, VERTICAL FIN WAS HAND FLEXED AT TOP.  MOVEMENT WAS APPARANT.  NOISE FROM LOWER ATTACHMENT WAS 	NOTED.  REMOVED FOUR REAR SPAR ATTACHING BOLTS AN4-61 FOUND MARKING FROM MOVEMENT.  REPLACED WITH NEW AN4-6A BOLTS AND H	ARDWARE.  TORQUE TO 100 INCHES/POUNDS.  AIRCRAFT TT:  2,278.0 HOURS.				1	L	7	1 	3O				A3SO    					 
1999092400047	19990924	00047	EA  	1999	9	24	99ZZZX3488       	2	19990817	G	7313	LW18265	NOZZLE          			CESSNA	172   	172S        	2072439	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE	LOOSE           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	948SP	247  				172S8144	L2812651A			DURING PHASE INSPECTION, FOUND ALL FOUR FUEL INJECTION NOZZLES, PN LW18265, HAD SCREENS AND SHIELDS LOOSE AROUND NOZZLE 	BODY.  REFERENCE LYCOMING OHM 'SHIELD MUST HAVE A TIGHT FIT ON BODY WHEN INSTALLED'.  THIS IS THE SECOND NEW ENGINE WITH	 SAME PROBLEM.				1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999092400048	19990924	00048	EA  	1999	9	24	99ZZZX3489       	2	19990813	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B				A				UNSCHED LANDING         				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		CR	CRUISE         	1			SO	16	470ER	1177 				17280614	L12239051A			THIS WAS A DUAL INSTRUCTIONAL FLIGHT.  DURING CRUISE, THE ENGINE WAS DESCRIBED AS RUNNING ROUGH FOR ABOUT 5 MINUTES.  TH	E PILOT ELECTED TO MAKE A PRECAUTIONARY LANDING.  THE AIRCRAFT IS GROUNDED PENDING FURTHER INVESTIGATION.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999092400049	19990924	00049		1999	9	24	99ZZZX3490       	1	19990414	G	7810		PIPE            	ROTAX       		AMTR  		AVIDCATALINA												EXHAUST	SEPARATED       	C	S			O				OTHER                   				D			INFLIGHT SEPARATION       			NR	NOT REPORTED   	1			SO	15	9224T	100  				155AB				A 2 INCH LONG PIECE OF THE EXHAUST PIPE MADE OF STAINLESS STEEL, PROVIDED BY ROTAX (THAT PART THAT FITS INTO THE CYLINDE	R HEAD), BROKE DUE TO FATIGUE.  OPERATING A PUSHER CONFIGURATION, THAT WHOLE EXHAUST PIPE WENT THROUGH THE PROPELLER AND	 TOOK 2 BLADES OFF.							0 										 
1999092400050	19990924	00050	GL  	1999	9	24	99ZZZX3491       	3	19990802	G	6114		HUB             			CESSNA	206   	U206G       	2073356	CE  						MCAULY	3A32C	D3A32C90    	GL  	PROPELLER	CRACKED         	B			LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	756BB	2600 	1100 			U20603950		775389		ET INDICATIONS IN BLADE SOCKETS 2 AND 3 IN EXCESS OF 350 MICRORAMPS.						1	H	7	1 	3O				A4CE    		5	C	P21EA	 
1999092400051	19990924	00051	NM  	1999	9	24	99ZZZX3492       	1	19990801	G	5511		SPAR            			GRTLKS	2T1   	2T1A2       	3910101	NM  										HORIZ STABILIZER	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	3808F					0776				WHEN REMOVING STABILIZER BRACE WIRES AND FINE BRACE WIRES, THE HORIZONTAL STABILIZER SPARS WERE FOUND CRACKED AT THE INT	ERCONNECT FITTINGS.  THERE IS NO REQUIREMENT TO DISSASEMBLE THE STABILIZER TO INSPECT THE SPARS AND THE PRE-FLIGHT WILL 	NOT DETECT ANY MOVEMENT BECAUSE OF THE TENSION OF THE SUPPORT WIRES.  POSSIBLE CAUSE OF THESE FAILURES IS WHEN EXCESSIVE	 LOADS ARE PLACED ON THE EMPENNAGE ASSEMBLY.			1	Q	7	1 	3O				A18EA   					 
1999092400052	19990924	00052	EA  	1999	9	24	99ZZZX3493       	2	19990816	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	FAILED          	D				A				UNSCHED LANDING         				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SO	16	427ER					17280606	L2776751A			THE PILOT WAS A SOLO STUDENT PRACTICING GROUND REFERENCE MANEUVERS.  THERE WAS A MOMENTARY POWER LOSS ABOUT 1-2 SECONDS.	  THE PILOT ELECTED TO MAKE A PRECAUTONARY LANDING AT WHICH TIME THE ENGINE HAD ANOTHER MOMENTARY POWER INTERRUPTION.  T	HE AIRCRAFT IS GROUNDED PENDING FURTHER INVESTIGATION.				1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999092400053	19990924	00053	CE  	1999	9	24	99ZZZX3494       	1	19990820	G	7130	56560061	FIRE SCREEN     			CESSNA	340   	340A        	2076405	CE  										BS 120	FAILED          	B		A	QC0R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	171AR	1051 				340A1270				FIRE RESISTANT SPACES AFT OF FIREWALL BETWEEN FIREWALL AND RUBBER FUEL BLADDER BURNED THROUGH.  FIREWALL SHOWS NO SIGN O	F OVERTEMP.  FOUND DURING INSPECTION OF FUEL BLADDER AT ANNUAL INSPECTION.  REPLACED SPACER ASSEMBLY.  RECOMMEND INSPECT	ION MINIMUM 500 HOURS.  LEFT ENGINE NACELLE.  REF:  AD 75-23-08R5.				1	L	7	2 	3O				3A25    					 
1999092400054	19990924	00054	SO  	1999	9	24	99ZZZX3495       	2	19990512	G	8520	530182RRM010	CRANKSHAFT      			CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  					ENGINE	CRACKED         	B	L		YECR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	212AF		1468 			15076277	285283R			CRANKSHAFT REMOVED FROM REBUILT ENGINE DURING OVERHAUL WAS FOUND TO HAVE NUMEROUS HEAT CRACKS IN ALL FORWARD FILLETS OF 	CRANKPINS.  FILLET RADII OF ALL CRANKPINS AND MAIN JOURNALS WERE FOUND BELOW TOLERANCES OF OVERHAUL MANUAL.  CRANK WAS .	010 INCH UNDERSIZE, AND CRACKS WERE APPARENTLY CAUSED AND UNDETECTED BY IMPROPER GRINDING TECHNIQUES.				1	H	7	1 	3O	3	O		3A19    	E252				 
1999092400056	19990924	00056	CE  	1999	9	24	99ZZZX3497       	1	19990729	G	5280	54221531	FITING          			LEAR  	55    	55C         	5170706	CE  										MLG DOOR	FAILED          	B				A				UNSCHED LANDING         				O			OTHER                     			IN	INSP/MAINT     	1			GL	05	10CR	2380 				145				AFTER TAKEOFF DURING GEAR REATRACTION, LOUD NOISE WAS HEARD IN CABIN.  ALL SYSTEMS APPEARED NORMAL.  UPON LANDING CREW F	OUND RIGHT OUTBOARD GEAR DOOR ATTACH FITTING BROKEN AT TURNBUCKLE ATTACH POINT, AND BOLT, NUT, AND BUSHING STILL IN TURN	BUCKLE. SUBMITTER RECOMMENED THICKER MATERIAL ON FITTING ATACH FLANGES.				2	L	7	2 	4F			RT	A10CE   					 
1999092400057	19990924	00057		1999	9	24	99ZZZX3498       	4	19990722	G	3416	0660306200	ALTIMETER       		KEA346      	BEECH 	1900  	1900D       	1154162	CE  										COCKPIT	BINDING         	B			GLBR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CE	01	184UX				4348	UE184				KOLLSMAN KNOB FOUND BINDING WHEN REMOVED FROM STOCK. RETURNED.						2	L	7	2 	4T			RT	A24CE   					 
1999092400058	19990924	00058	EU  	1999	9	24	99ZZZX3499       	1	19990902	G	7711	218901002	INDICATOR       			AMD   	FALC50	FALCON50MYST	2730106	EU  										COCKPIT	INACCURATE      	B			FX1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	11	97BZ				124	89				INSTALLED N2 INDIATOR, IMPROPER INDICATION ON START.  N2 DID NOT RISE ABOVE 5 PERCENT.						2	L	7	3 	4F				A46EU   					 
1999092400059	19990924	00059	EU  	1999	9	24	99ZZZX3500       	1	19990907	G	2820		LINE            			BRAERO	DH125 	HS125700A   	4230170	EU  										FUEL SYSTEM	CHAFED          	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	555CB					NA0228				AFTER RETURNING FROM A FLIGHT, GROUND PERSONNEL NOTED FLUID SPILLING FROM THE REAR FUSELAGE AREA OF ACFT.  MAINT INSP RE	AR EQUIP BAY OF ACFT AND IDENTIFIED THE LEAK AS 5606 HYD FLUID.  UPON STARTING ENGINES TO PRESS THE HYD SYS, FLUID WAS N	OTED SPEWING IN A FINE SPRAY FROM THE LT ENG PYLON.  AFTER REMOVING SEVERAL COMPONENTS TO GAIN ACCESS, FOUND TWO SS HYD 	LINES CHAFING TOGETHER WHICH CAUSED A PINHOLE IN A 3,000 PSI PRESS LINE ALLOWING FLUID TO SPRAY INTO REAR EQUIP BAY.  TH	IS AREA HOUSES THE APU, ELEC PANELS, RELAYS, AND CONTACTORS.  AFTER LINES WERE REMOVED, NOTED A FUEL LINE WAS CHAFED APP	ROX HALF-WAY THRU.  TT:  3,097 HRS.  TT LANDINGS:  2,479.	2	L	7	2 	4F				A3EU    					 
1999092400060	19990924	00060	CE  	1999	9	24	99ZZZX3501       	1	19990908	G	5350		FAIRING         			LEAR  	35    	35LEAR      	5170600	CE  										FUSELAGE	WRINKLED        	H		A		O				OTHER                   				O			OTHER                     			LD	LANDING        	1			SW	99	90WR					35022				DURING LANDING, LEFT WING TIP TANK CONTACTED THE RUNWAY.  BOTTOM OF TIP TANK DENTED AND SCRAPED.  LEFT WING TO FUSELAGE 	UPPER FAIRING WRINKLED.  LEFT SIDE OF FUSELAGE ABOVE AFT END OF INBOARD FAIRING SLIGHTLY WRINKLED.  EXACT CAUSE YET TO B	E DETERMINED, BUT APPEARS TO BE PILOT TECHNIQUE.  CURRENTLY, CONSULTING WITH LEARJET ENGINEERING FOR REPAIR ACTIONS.				2	L	7	2 	4F				A10CE   					 
1999092400061	19990924	00061	CE  	1999	9	24	99ZZZX3502       	1	19990908	G	5730		SKIN            			LEAR  	35    	35LEAR      	5170600	CE  										LT TIP TANK	DENTED          	H				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			SW	99	90WR					35022				DURING LANDING, LEFT WING TIP TANK CONTACTED THE RUNWAY.  BOTTOM OF TIP TANK DENTED AND SCRAPED.  LEFT WING TO FUSELAGE 	UPPER FAIRING WRINKLED.  LEFT SIDE OF FUSELAGE ABOVE AFT END OF INBOARD FAIRING SLIGHTLY WRINKLED.  EXACT CAUSE YET TO B	E DETERMINED, BUT APPEARS TO BE PILOT TECHNIQUE.  CURRENTLY, CONSULTING WITH LEARJET ENGINEERING FOR REPAIR ACTIONS.				2	L	7	2 	4F				A10CE   					 
1999092400062	19990924	00062	NE  	1999	9	24	99ZZZX3503       	3	19990901	G	6111	57D0495	FORK            			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	PITCH CHANGE	CRACKED         	B		A	EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03			4651 		2370NR			HJ150A		FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS.  TWO CRACKS.						2	L	7	2 	4T			RT	A24CE   		5	C	P10NE	 
1999092400063	19990924	00063	NE  	1999	9	24	99ZZZX3504       	3	19990901	G	6111	57D0495	FORK            			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	PITCH CHANGE	CRACKED         	B		A	EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03		9123 	4648 		3132NR			HJ480		FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS.  FOUR CRACKS.  SUBMITTER STATE	D RECURRING PROBLEM.					2	L	7	2 	4T			RT	A24CE   		5	C	P10NE	 
1999092400065	19990924	00065	NE  	1999	9	24	99ZZZX3506       	2	19990722	G	7250	S66170	TURBINE DISK    								PWA   	JT8   	JT8D17      	52049	NE  					ENGINE	CRACKED         	B			EM4Y	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	23		13113	6    				649126			PART PRESENTED CRACK ON RETAINING LUG AREA.  OEM INVESTIGATION REQUESTED.											4	F			E2EA				 
1999092400066	19990924	00066	NE  	1999	9	24	99ZZZX3507       	2	19990722	G	7230	701509	COMPRESSOR DISK 		NENCAH2314  						PWA   	JT8   	JT8D9A      	52048	NE  					ENGINE	DAMAGED         	B			EM4Y	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	23		3939 					666964			PART PRESENTED A BORE DISTORTION CAUSED BY FIRE.  IT WAS SENT TO OEM FOR INVESTIGATION.											4	F			E2EA				 
1999092400067	19990924	00067	NE  	1999	9	24	99ZZZX3508       	2	19990722	G	7230	772510	COMPRESSOR DISK 								PWA   	JT8   	JT8D9       	52048	NE  					ENGINE	DAMAGED         	B			EM4Y	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	23		7131 	3939 		BENCAK8522		666964			PART PRESENTED A BORE DISTORTION CAUSED BY FIRE.											4	F			E2EA				 
1999092400068	19990924	00068	CE  	1999	9	24	99ZZZX3509       	1	19990801	G	5730		SKIN            			BEECH 	90    	C90         	1152913	CE  										LT AND RT WING	CRACKED         	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	800PW	6612 				LJ548				ON THE LOWER SURFACE OF THE WING AT FORWARD WING BOLT ATTACH POINT, A CRACK IN THE WING SKIN BOTH FORWARD AND AFT OF THE	 ATTACH FITTING WAS FOUND DURING A ROUTINE INSPECTION.  THE CRACK ON THE FORWARD SIDE STARTED AT THE FUEL CELL DRAIN NIP	PLE CUT-OUT AND EXTENDED TO THE NR 10 SCREW LOCATION JUST AFT OF THE CUT-OUT.  THE AFT CRACK STARTED AT THE INBOARD MOST	 NR 10 SCREW HOLE OF THE WING ATTACH FITTING AND EXTENDED TO THE FORWARD EDGE OF THE SKIN.  THIS CONDITION WAS FOUND IN 	THE SAME LOCATION ON BOTH LEFT AND RIGHT HAD WINGS.  SUBMITTER STATED HE HAS SEEN SEVERAL AIRCRAFT WITH CRACKS IN THE SA	ME LOCATIONS.  THE DEFECT APPEARS TO HAVE BEEN CAUSED BY STRESS LOAD ON THE SKIN.	1	L	7	2 	3T				3A20    					 
1999092400069	19990924	00069	SO  	1999	9	24	99ZZZX3510       	1	19990831	G	5511	46538024	SPAR            			PIPER 	PA31T 	PA31T       	7103124	SO  										HORIZONTAL STAB	CRACKED         	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	20TN	4595 				31T7920019				FOUND CRACK ON LEFT AFT HORIZONTAL SPAR WEB.  DURING PROCESS OF REPAIR, MUCH OF THE RIVETS WERE FOUND LOOSE AND WORKING.						1	L	7	2 	3T				A8EA    					 
1999092400072	19990924	00072		1999	9	24	99ZZZX3513       	4	19990826	G	2310	8220074102	RTV             			ISRAEL	1125  	ASTRASPX    	4500205	EU  										COCKPIT	INOPERATIVE     	B			QRRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	273RA	588  				099				COPILOT TRV INOPERABLE.  REPLACED WITH OVERHAULED UNIT.						2	L	7	2 	4F			RT	A16NM   					 
1999092400073	19990924	00073	EU  	1999	9	24	99ZZZX3514       	1	19990826	G	2820	FS103	FLOAT SWITCH    			ISRAEL	1125  	ASTRASPX    	4500205	EU  										FUEL TANK	INOPERATIVE     	B			QRRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	273RA	588  			21388	097				TRANSFER VALVE WOULD NOT WORK IN THE 'AUTO' POSITION.  REPLACED SWITCH WITH NEW.						2	L	7	2 	4F			RT	A16NM   					 
1999092400074	19990924	00074		1999	9	24	99ZZZX3515       	1	19990816	G	3246	2601483	TIE BOLT        	BENDIX      	26088911    															MLG	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07					B5051					BROKEN TIE-BOLT ON ALASKA AIRLINES MAIN WHEEL ASSY.																			 
1999092400075	19990924	00075	EU  	1999	9	24	99ZZZX3516       	1	19990827	G	3250	618212	ROD             		61823       	BAG   	JETSTM	JETSTM3201  	1500217	EU  										NLG	CRACKED         	B				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	25	862JX				SJA451	862				NOSE LANDING GEAR STEERING JACK, PN 6182/3, SJA-451, WAS RETURNED WITH A REPORT OF 'LEAKING FROM SHAFT END'.  TESTING RE	VEALED VERY SLIGHT FLUID LEAKAGE FROM INSIDE THE PISTION ROD.  UNIT WAS DISASSEMBLED, AND MAGNETIC PARTICLE INSPECTION O	F PISTON ROD, PN 18212, REVEALED AN INDICATION APPROXIMATELY 50 PERCENT AROUND THE OUTSIDE DIAMETER OF THE ROD IN THE TR	ANSITION RADIUS TO THE CENTER PISTON SECTION.  PISTON ROD HAS BEEN RETURNED TO APPH FOR INVESTIGATION.  PART TSO:  4.			2	L	7	2 	4T			RT	A56EU   					 
1999092400214	19990924	00214	GL  	1999	9	24	99ZZZX3519       	2	19990818	G	7323	23057869	GOVERNOR        		ALAA1       	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					LT ENGINE	FAILED          	D		A		E				ENGINE SHUTDOWN         				J			WARNING INDICATION        			NR	NOT REPORTED   	1			NM	03	204PC		946  		26867	S895	836679			AFTER LEFT ENGINE START (NORMAL) AND WARM-UP, THROTTLE LEVER WAS MOVED TO FLIGHT IDLE.  ENGINE WENT TO 90 PERCENT TORQUE	 WITH A ROTOR RPM OF 110 PERCENT.  N1 AND N2 SPEEDS WERE ERRATIC.  ENGINE SHUT DOWN.  PR LINE ISOLATED FROM GOVERNOR TO 	FUEL CONTROL.  FUEL CONTROL RESPONDED NORMALLY TO THROTTLE LEVER MOVEMENT.  GOVERNOR REMOVED.  IT WAS NOTICED GOVERNOR D	RIVE SHAFT COUPLING WAS SLIPPING/OVERRUNNING.			1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999092400215	19990924	00215	SW  	1999	9	24	99ZZZX3520       	1	19990824	G	7933	2060751873	INDICATOR       			BELL  	206   	206B        	1181511	SW  										COCKPIT	DAMAGED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	49718				1411	1917				OIL TEMP INDICATOR LENS CRACKED.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999092400218	19990924	00218	SW  	1999	9	24	99ZZZX3523       	1	19990805	G	6510	407340339103	BEARING         		407044303105	BELL  	407   	407         		SW  										T/R DRIVE	ROUGH           	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427AL	87   			C992211	53107				UNIT WAS REMOVED FOR VIBRATIONS.  FOUND 2 EACH 407-340-339-103 BEARINGS ROUGH.  FOUND 1 EACH 206-061-432-116 HOUSING CRA	CKED.					1	G	7	1 	3U			O	H2SW    					 
1999092400220	19990924	00220	SW  	1999	9	24	99ZZZX3525       	1	19990817	G	6510	407340340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457AL	271  	45   		RNFS0781	53151				DURING DAILY/50-HOUR INSPECTION, FOUND NR 3 DISC PACK AFT DISC CRACKED AT 4 LOCATIONS.						1	G	7	1 	3U			O	H2SW    					 
1999092400221	19990924	00221	SW  	1999	9	24	99ZZZX3526       	1	19990820	G	7120	2060641031	BEARING         			BELL  	206   	206L1       	1182107	SW  										ENGINE MOUNT	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5740L					45459				DURING INSTALLATION ON ENGINE MOUNT TO REPLACE WORN BEARING, LOOSE IN RACE.  (NEW - MFG DATE 3-6-98).						1	G	7	1 	3U				H2SW    					 
1999092400222	19990924	00222	SW  	1999	9	24	99ZZZX3527       	1	19990819	G	5510	206023119109	SUPPORT         		407023002117	BELL  	407   	407         		SW  										HORIZONTAL STAB	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	607AL					53264				SUPPORT CRACKED, THIRD FROM OUTBOARD EDGE.						1	G	7	1 	3U			O	H2SW    					 
1999092400223	19990924	00223	SW  	1999	9	24	99ZZZX3528       	1	19990812	G	6510	407340340101	DISC PACK       		407040325101	BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	627AL	244  	25   		RNFS2289	53284				DURING 25-HOUR AD INSPECTION, FOUND NR 3 DISC PACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999092400224	19990924	00224	SW  	1999	9	24	99ZZZX3529       	1	19990812	G	6510	407340340101	DISC PACK       		407040325101	BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	627AL	40   	25   		RNFS3345	53284				DURING 25-HOUR AD INSPECTION, NR 7 DISC PACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999012200589	19990122	00589	WP  	1999	1	22	99ZZZX353        	1	19990106	G	3246	152058	WHEEL           	BENDIX      	1542511     	DOUG  	DC8   	DC8*        		WP  										MLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					B6437					CRACK DETECTED BY EDDY CURRENT PER SPEC MIL-I-68070, IN THE OUTBOARD WHEEL HALF INBOARD FACE SPOKE AREA.  NO CRACKS PERM	ITTED THIS AREA.  OHM 32-40-05 REV 15 DATE 10-15-96.  CHECK SECT C PARA 2B.  S/N INBOARD, BH4738.					2	L	7	4 	4J			F	4A25    					 
1999092400225	19990924	00225	SW  	1999	9	24	99ZZZX3530       	1	19990806	G	6510	407340340101	DISC PACK       		407040325101	BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	627AL	204  	25   			53284				DURING 25-HOUR AD INSPECTION.  NR 7 DISC PACK HAS 2 CRACKS.						1	G	7	1 	3U			O	H2SW    					 
1999092400226	19990924	00226	SW  	1999	9	24	99ZZZX3531       	1	19990812	G	6510	407340340101	DISC PACK       		407040325101	BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	627AL	244  			RNFS2481	53284				DURING 25-HOUR AD INSPECTION, FOUND NR 3 DISC PACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999092400227	19990924	00227	SW  	1999	9	24	99ZZZX3532       	1	19990812	G	6510	407340340101	DISC PACK       		407040325101	BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	627AL	40   			RNFS2419	53284				DURING 25-HOUR AD INSPECTION, FOUND NR 7 DISC PACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999092400228	19990924	00228	SW  	1999	9	24	99ZZZX3533       	1	19990806	G	6510	407340340101	DISC PACK       		407040325101	BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	627AL	204  			RNFS3345	53284				DURING 25-HOUR AD INSPECTION, FOUND NR 7 DISC PACK HAS 2 CRACKS.						1	G	7	1 	3U			O	H2SW    					 
1999092400229	19990924	00229	GL  	1999	9	24	99ZZZX3534       	2	19990831	G	7532	23053176	BLEED VALVE     			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	MALFUNCTIONEWD  	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	369AW		441  		FF35627	470117D	CAE833998			ENGINE HAD LOW POWER DETERMINED THAT THE BLEED VALVE WAS NOT FULLY CLOSING.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999092400230	19990924	00230	SW  	1999	9	24	99ZZZX3535       	1	19990831	G	6240	8DJB1LAV1	INDICATOR       		FD125       	BELL  	212   	212         	1181420	SW  										TRIPLE TACH	INPERATIVE      	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	8530B		558  			30702				THE NUMBER TWO NEEDLE DOES NOT OPERATE WHEN ENGINE IS RUNNING.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999092400231	19990924	00231	SW  	1999	9	24	99ZZZX3536       	1	19990831	G	2822	2C273	PUMP            			BELL  	212   	212         	1181420	SW  										FUEL BOOST	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530B				1AB198	30702				WITH SUFFICIENT FUEL AND CURRENT TO PUMP, NO FUEL PRESSURE WAS CREATED.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999092400438	19990924	00438	EU  	1999	9	24	99ZZZX3541       	1	19990729	G	6320	355A32060880	GEARBOX         			AEROSP	AS355 	AS355E      	8680805	EU  										TAIL ROTOR	MAKING METAL    	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	17	102UM		2359 			5075				MAIN ROTOR TRANSMISSION CHIP LIGHT CAME ON IN-FLIGHT WHILE LANDING AT ITS BASE OF OPERATION.  MAINTENANCE REMOVED CHIP P	LUG.  SEVERAL CHIPS WERE FOUND ON PLUG.  EXAMINED OIL FILTER METAL AND ALUMINUM WAS PRESENT IN FILTER.  REMOVED BEVEL RE	DUCTION GEARBOX ON COMBINING GEARBOX FOR REPAIR.  TSO:  2,359.4 HOURS.  OVERHAUL IS 3,000 HOURS.				1	G	7	2 	3U				H11EU   					 
1999092400439	19990924	00439	WP  	1999	9	24	99ZZZX3542       	1	19990831	G	7722	35918152C304	INDICATOR       			HUGHES	369   	369D        	4470706	WP  										COCKPIT	READS HIGH      	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	1097J				0136	900801D				HIGH TOT READING IN A HOVER.  OUT OF PARAMETERS WITH TEST UNIT.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999092400440	19990924	00440	GL  	1999	9	24	99ZZZX3543       	2	19990831	G	7532	23053176	BLEED VALVE     			BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	MALFUNCTIONED   	B			LS1R	O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			EA	13	206BY		1094 		FF35464	2871	CAE800002F			ENGINE HAD LOW POWER.  DETERMINED THE BLEED VALVE WAS NOT CLOSING.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999092400441	19990924	00441	SW  	1999	9	24	99ZZZX3544       	1	19990831	G	2435	23032022	GENERATOR       			BELL  	206   	206B3       	1181506	SW  										STARTER/GEN	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY		546  		15923	2871				GENERATOR COMES OFF-LINE WHEN UNDER LOAD.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999092400442	19990924	00442	WP  	1999	9	24	99ZZZX3545       	1	19990901	G	6230	369A7607501	LINK ASSY       			HUGHES	369   	369D        	4470706	WP  										MAIN ROTOR	WORN            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	500DC					290456D				DURING 100-HOUR INSPECTION, FOUND BEARING WORN BEYOND LIMITS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999092400443	19990924	00443	WP  	1999	9	24	99ZZZX3546       	1	19990901	G	3610	369118402	LINE            			HUGHES	369   	369D        	4470706	WP  										PNEUMATIC SYSTEM	CRACKED         	B			LS1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13	500DC					290456D				AIR LINE UNDER BRADING ON FLEX PORTION CRACKED.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999092400444	19990924	00444		1999	9	24	99ZZZX3547       	4	19990824	G	2340	C1611	ICS BOX         			BELL  	204   	UH1H        	1181407	SW  										INTERCOM	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	52AG				29208	7015746				KCS BOX HAS NO SIDE TONE.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999092400445	19990924	00445	SW  	1999	9	24	99ZZZX3548       	1	19990831	G	7330	DSF419	INDICATOR       			BELL  	204   	UH1H        	1181407	SW  										COCKPIT	ERRATIC         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	52AG				8110901	7015746				INDICATOR IS ERRATIC AND UNRELIABLE.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999092400446	19990924	00446	SW  	1999	9	24	99ZZZX3549       	1	19990901	G	6330	2060325095	PIN ASSY        		206040003005	BELL  	206   	OH58A       	1181579	SW  										TRANSMISSION	WORN            	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	54AG				BLW3619	7120721				NOTICED EXCESSIVE TRANSMISSION ROCKING.  NOTICED BEARING ON LOWER MOUNT WORN BEYOND LIMITS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999092400447	19990924	00447	SW  	1999	9	24	99ZZZX3550       	1	19990901	G	3340	A413A	POWER SUPPLY    			BELL  	206   	OH58A       	1181579	SW  										STROBE	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	58AG				04693	7221131				SUPPLY CURRENT WITHIN LIMITS WITH NO OUTPUT VOLTAGE.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999092400448	19990924	00448	WP  	1999	9	24	99ZZZX3551       	1	19990831	G	7714	65011040	TACHOMETER      			HUGHES	369   	369E        	4470707	WP  										COCKPIT	ERRATIC         	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	8330P				1326	0330E				ERRATIC BELOW 30 PERCENT.  NEEDLE BOUNCES.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999092400449	19990924	00449	WP  	1999	9	24	99ZZZX3552       	1	19990831	G	7712	43081046	INDICATOR       			HUGHES	369   	369E        	4470707	WP  										TORQUE	FLUCTUATES      	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	8330P				682	0330E				INSTALLED NEWLY OVERHAULED UNIT, FLUCTUATED 4-8 PSI.  NOT WITHIN LIMITS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999092400450	19990924	00450	SW  	1999	9	24	99ZZZX3553       	1	19990831	G	2750	8002039	ANNUNCIATOR     			BELL  	212   	212         	1181420	SW  										INSTRUMENT PANEL	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530F	15108			604	30920				MASTER CAUTION WILL NOT RESET.  INVERTERS NR 2 AND NR 3 WILL NOT LIGHT UP.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999092400451	19990924	00451	GL  	1999	9	24	99ZZZX3554       	2	19990708	G	7323	23001986	TUBE            			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C30P     	03013	GL  					ENGINE	CRACKED         	B			KBTR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	920EH					45769	890491P			GOVERNOR TUBE CRACKED.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999092400452	19990924	00452	NE  	1999	9	24	99ZZZX3555       	2	19990729	G	7210	3024780	GEARBOX         			BELL  	212   	212         	1181420	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					M/R DRIVE	CONTAMINATED    	H				A				UNSCHED LANDING         				J			WARNING INDICATION        			NR	NOT REPORTED   	1			WP	17	911HW		2895 		CP68189B	31101	CPPS62032			ENGINE C-BOX CHIP LIGHT CAME ON IN-FLIGHT.  AIRCRAFT WAS ON FINAL TO WORK SITE WHEN C-BOX OIL PRESSURE DROPPED TO ZERO. 	 MAINTENANCE INSPECTED CHIP PLUG AND OIL FILTER.  C-BOX WAS REMOVED FROM SERVICE AND SENT FOR REPAIR.  POSSIBLE OIL PUMP	 SHAFT DRIVE FAILURE OR GEAR FAILURE.  OIL SAMPLES SHOWED SLIGHT INCREASE IN IRON OVER PAST 100 HOURS.  OIL SAMPLES WERE	 TAKEN EVERY 25 HOURS.  (OVERHAUL IS 4,000 HRS).			1	G	7	1 	4U	4	U		H4SW    	E22EA				 
1999092400453	19990924	00453	SW  	1999	9	24	99ZZZX3556       	1	19990831	G	2435	23032027	STARTER/GEN     			BELL  	206   	206B        	1181511	SW  										ENGINE	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	9907K		655  		5495	2040				ARMATURE GROUND BEYOND LIMITS.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999092400454	19990924	00454	NE  	1999	9	24	99ZZZX3557       	2	19990821	G	7261	9609000166	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  	TMECA 	ARRIEL	ARRIEL1D    		NE  					ENGINE	FAILED          	D				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			WP	13	982BH				961023	2876	9339			DURING SIGHTSEEING FLIGHT, PILOT EXPERIENCED AN ENGINE CHIP WARNING ILLUMINATION AND MADE PRECAUTIONARY LANDING.  UPON F	URTHER EXAMINATION, MECHANIC DETERMINED THERE WAS SUFFICIENT METAL CONTENT ON MAGNETIC PLUG TO CEASE FURTHER FLIGHT UNTI	L CORRECTIVE ACTION TAKEN.  ENGINE ASSY REMOVED AND REPLACED WITH SERVICEABLE UNIT.				1	G	7	1 	3U	3	U		H9EU    	E19EU				 
1999092400455	19990924	00455	GL  	1999	9	24	99ZZZX3558       	2	19990817	G	7210	6871534	CHIP PLUG       		23035179    						ALLSN 	250C  	250C30S     	03013	GL  					GEARBOX	LEAKING         	B			ALGR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03					CAG90415					UPON INSPECTION, BEFORE INSTALLING PART, FOUND TIP OF CHIP DETECTOR TO HAVE A HOLE IN IT.											3	U			E1GL				 
1999092400456	19990924	00456	GL  	1999	9	24	99ZZZX3559       	2	19990819	G	7321	104900A4	FCU             			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	90322		3855 		1AAC262	1736	CAE830571			FCU WOULD NOT ADJUST.  REMOVED AND REPLACED.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999092400457	19990924	00457	SW  	1999	9	24	99ZZZX3560       	1	19990819	G	7712	2120701607	INDICATOR       			BELL  	212   	212         	1181420	SW  										COCKPIT	FLUCTUATES      	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	8530F				SD859	30920				TORQUE INDICATOR FLUCTUATES.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999092400458	19990924	00458	SW  	1999	9	24	99ZZZX3561       	1	19990824	G	2420	CR2795E100A1	VOLT REGULATOR  			BELL  	206   	206B3       	1181506	SW  										E/E BAY	INTERMITTENT    	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY		1536 		6488137	2871				VOLTAGE REGULATOR INTERMITTENT.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999092400459	19990924	00459	SW  	1999	9	24	99ZZZX3562       	1	19990816	G	2822		COUPLING        	DELCO       	C386A1      	SKRSKY	S58T  	S58T        	8141800	SW  										BOOST PUMP	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	23	58S				6375	581502				MOTOR TO PUMP COUPLING HAD BROKEN TEETH.  MOST LIKELY DUE TO AGE AND NORMAL WEAR TO LIMITS OF PART.						2	G	7	1 	4U			NC	1H11    					 
1999092400460	19990924	00460	GL  	1999	9	24	99ZZZX3563       	1	19990827	G	7922	53E22144	VALVE           			ENSTRM	F28   	280F        	3300550	GL  										ENGINE OIL TEMP	MALFUNCTIONED   	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01	199TV	11   			87088	1510				NEW FACTORY OVERHAULED ENGINE RUNNING HIGH OIL TEMPS, SOMETIMES TO RED LINE.  REPLACED VERNATHERM VALVE.  OIL TEMPS RETU	RNED TO NORMAL.					1	G	7	1 	3O				H1CE    					 
1999092400461	19990924	00461	SW  	1999	9	24	99ZZZX3564       	1	19990819	G	2435	23046020	STARTER/GEN     			BELL  	212   	212         	1181420	SW  										ENGINE	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530F		905  		2710	30920				STARTER/GENERATOR WILL NOT COME ON-LINE.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999092400462	19990924	00462		1999	9	24	99ZZZX3565       	4	19990824	G	2300	KY196E	LIGHT           			BELL  	204   	UH1H        	1181407	SW  										RADIO	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	52AG				8373	7015746				RADIO TRANSMIT LIGHT WILL NOT ILLUMINATE.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999092400463	19990924	00463	EA  	1999	9	24	99ZZZX3566       	1	19990830	G	7500	2150809501	DUCT            			CNDAIR	CL600 	CL6001A11   	1900302	EA  	LYC   	ALF502	ALF502L2    	41580	NE  					ENGINE	CHAFED          	B	S		G1FR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	601SA	4974 				1079	LF03149S			DURING SCHEDULED INSPECTION, THE BLEED AIR DUCT, PN 215-0809-501, WAS FOUND CHAFING ON NR 2 BEARING OIL TUBE, PN 2-263-0	60-01.  BOTH PARTS WERE CHAFED BEYOND LIMITS AND REQUIRED REPLACEMENT.  OIL TUBE CHAFED 50 PERCENT WALL THICKNESS AND BL	EED AIR DUCT CHAFED THROUGH.				2	L	7	2 	4F	4	F	RT	A21EA   	E6NE				 
1999092400464	19990924	00464		1999	9	24	99ZZZX3567       	2	19990818	G	8530		SNAP RING       			AMTR  	KITFOX	KITFOXI     	05613KF	GL  			EA81        							ROCKER SHAFT	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	130NM					130				AIRCRAFT MADE AN OFF-AIRPORT LANDING DUE TO LOSS OF POWER.  ENGINE WAS DISASSEMBLED.  THE SNAP RING THAT HOLDS NR 1 CYLI	NDER EXHAUST ROCKER ARM WAS BROKEN ALLOWING THE ROCKER ARM TO COME OFF OF THE SHAFT.					1	H	7	1 	3I			NC	EXPA    					 
1999092400469	19990924	00469	EU  	1999	9	24	99ZZZX3572       	1	19990902	G	7714	218901002	N2 GAUGE        			AMD   	FALC50	FALCON50MYST	2730106	EU  										NR 2 ENGINE	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	01	97BZ				1508	89				INSTALLED N2 INDICATOR.  ON NORMAL START,  N2 GOT TO 30 PERCENT AND THEN STOPPED.  REPAIRED BY PARKER HANNIFIN FAA STATI	ON FX1R156K.					2	L	7	3 	4F				A46EU   					 
1999092400471	19990924	00471	NE  	1999	9	24	99ZZZX3574       	2	19990915	G	7230	1B4706	BLADE           			BOEING	757   	7572Q8      	1384972	NM  	PWA   	2037  	PW2037      		NE  					COMPRESSOR	FAILED          	H				O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		LD	LANDING        	1			SW	99	710TW	8436 				28169	P727220			ENGINE SURGED WITH OVERTEMP - METAL IN BLEEDS.  DISASSEMBLED, INSPECTION DISCLOSED FAILURE OF 6TH STAGE COMPRESSOR BLADE	.  BLADES WILL BE FORWARDED TO P&W ENGINEERING FOR ANALYSIS.  CYCLES, 2,867.					2	L	7	2 	4F	4	F	RT	A2NM    	E17NE				 
1999092400473	19990924	00473	CE  	1999	9	24	99ZZZX3576       	1	19990824	G	5553	04311481	FITTING         			CESSNA	150   	152         	2071835	CE  										VERTICAL STAB	CRACKED         	B	S		C54R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	25	67975	9035 				15282122				UPON INSPECTION OF AIRFRAME, DISCOVERED THAT LOWER RIGHT AFT VERTICAL STABILIZER ATTACH FITTING WAS CRACKED, AND LEFT HA	ND SIDE CORRODED.  SUBMITTER STATED CAUSE APPEARS TO BE AGE RELATED.					1	H	7	1 	3O			NT	3A19    					 
1999092400474	19990924	00474	SO  	1999	9	24	99ZZZX3577       	2	19990831	G	8530	654650A4	VALVE           			CESSNA	182   	182P        	2075816	CE  	CONT  	O470  	O470U       	17026	SO  					NR 4 CYLINDER	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	952CC	933  				18263638	470757			DURING A ROUTINE 100-HOUR INSPECTION, EXCESSIVE LEAKAGE WAS FOUND LEAKING PAST THE PISTON RINGS ON THE NR 4 CYLINDER.  T	HE REMOVED CYLINDER WAS FOUND TO HAVE A WORN OUT EXHAUST VALVE, A WORN OUT VALVE GUIDE, AND WORN TO A BELL MOUTH CONDITI	ON AT THE TOP OF THE CYLINDER BORE.				1	H	7	1 	3O	3	O	NT	TA13    	E273				 
1999092400475	19990924	00475	CE  	1999	9	24	99ZZZX3578       	1	19990902	G	7120	TH472	MOUNT           			BEECH 	55    	E55         	1152732	CE  										ENGINE	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13										ENGINE MOUNT WAS RECEIVED FOR COMPLIANCE TO AD 91-15-20.  DURING MAGNETIC PARTICAL INSPECTION, AN INDICATION APPEARED AT	 UPPER RT DYNA FOCAL ATTACH AREA WHERE REINFORCEMENT STRAP IS WELDED TO PLATE.  THE INDICATION WAS APPROXIMATELY 1.50 IN	CHES IN LENGTH, AREA WAS LIKELY NOT COMPLETELY WELDED.  THE WELD WAS GROUND OUT AND RE-WELDED, THEN RE-MAG/PARTICAL INSP	ECTED.  NOTE:  SUBMITTER STATED THIS AREA IS NOT CALLED OUT IN AD 91-15-20.			1	L	7	2 	3O				3A16    					 
1999092400476	19990924	00476	EA  	1999	9	24	99ZZZX3579       	2	19990817	G	7313	LW18265	NOZZLE          			CESSNA	172   	172S        	2072439	CE  	LYC   	IO360 	IO360L2A    		EA  					ENGINE	LOOSE           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	789EP	249  				172S8135	L2812351A			DURING PHASE INSPECTION, FOUND ALL FOUR FUEL INJECTION NOZZLES PN LW 18265 HAD SCREENS AND SHIELDS LOOSE AROUND NOZZLE B	ODY.  REPLACED WITH 4 EACH SERVICEABLE NEW NOZZLES.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999092400477	19990924	00477	CE  	1999	9	24	99ZZZX3580       	1	19990903	G	3242	651710022	RESERVOIR       			CESSNA	500   	560CESSNA   	2076750	CE  										BRAKE SYSTEM	RUPTURED        	D				O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		TX	TAXI/GRND HDL  	1			SO	07	361EC	2366 				5600279				DURING LANDING, ACFT HAD COMPLETE PRIMARY BRAKE SYSTEM FAILURE.  PILOTS STOPPED ACFT USING EMERG BRAKING SYS AND THRUST 	REVERSERS.  RAMP MECH SAW HYD FLUID COMING OUT OF NOSE DRAIN HOLES AROUND NLG.  BRAKE SYS HYD RESERVOIR FOUND RUPTURED A	T FWD INBD WELDED SEAM STARTING FROM THE LOWER FWD CORNER TRAVELING UP THE WELDED SEAM ABOUT 4 INCHES.  THIS CAUSED COMP	LETE LOSS OF HYD FLUID IN THE BRAKE RESERVOIR.  THE SYS VENT LINE CHECKED AND NO OBSTRUCTIONS FOUND.  RUPTURED RESERVOIR	 REMOVED AND NEW ONE INSTALLED IAW MFG'S INSTRUCTIONS.  THE SYS WAS BLED AND EMERG BRAKE SYS SERVICED.  SYS FUNCTION CHE	CKED AND OPERATED NORMALLY, LOW SPEED AND HIGH SPEED TAXI TESTS CONDUCTED, NORMAL SYS OPER, ACFT RETURNED TO SERVICE.	2	L	7	2 	4F			RT	A22CE   					 
1999092400699	19990924	00699		1999	9	24	99ZZZX3581       	4	19990901	G	3160	69140	DDMP            			PIPER 	PA32  	PA32301T    	7103209	SO  										COCKPIT	MALFUNCTIONED   	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	9288X	318  			0086EC	3257027				FAILURE CODE 1.  COULD NOT FIND IN SARATOGA II TC MM, SERIAL NUMBERS 3257001 AND UP.  CODE ONE IS WHEN THE INSTRUMENTS T	AKE TOO LONG TO UPDATE INFORMATION TO THE DDMP (DIGITAL DATA MULTIPURPOSE DISPLAY), AND WHEN IT SHUTS DOWN, A FAILURE MO	DE CODE 1 IS DISPLAYED.				1	L	7	1 	3O				A3SO    					 
1999092400700	19990924	00700	SO  	1999	9	24	99ZZZX3582       	2	19990826	G	7320		MIXTURE PLATE   	PRECISION   	RSA5AD2     	PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	LTSIO360KB  	17025	SO  					FUEL SERVO	GALLED          	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4123C	24   	8    			3449042	321676			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  REMOVED SERVO FROM ENGINE AND INSPECTED IDLE MIXTURE PLATE FOR GALLING.	  PLATE WAS FOUND GALLED.  SERVO SENT TO PRECISION FOR REPAIR.  THIS SERVO HAS 24 HOURS TT SINCE NEW.  8 HOURS SINCE PRE	CISION REPAIRED SERVO AT FACTORY.				1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999092400701	19990924	00701	SO  	1999	9	24	99ZZZX3583       	2	19990818	G	7320		MIXTURE PLATE   	PRECISION   	RSA5AD2     	PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360KB   	17025	SO  					FUEL SERVO	SCORED          	B			B4VS	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4167B	435  			70179003	3449098	321483			ENGINE OPERATING SQUAWKS INCLUDE STIFF THROTTLES, ENGINES DYING, ROUGH RUNNING, AND IMPROPER FUEL MIXTURES.  THE ENGINE 	PARAMETERS WERE RESET, BUT THE PROBLEMS RETURNED.  THE MIXTURE CONTROL ON THE THROTTLE SIDE OF THE SERVO WAS DISASSEMBLE	D.  FOUND THE BRASS MIXTURE PLATE BADLY SCORED.  THIS ALLOWED EXCESS FUEL TO FLOW THROUGH THE SCORES AND DISRUPT THE MIX	TURES.  FOUND THE FUEL SCREEN IN THE MANIFOLD VALVE WAS FULL OF METAL SHAVINGS.  THE SCORES IN THE BRASS MIXTURE PLATE W	ERE REMOVED AND THE CONTAMINATION WAS REMOVED FROM THE MANIFOLD VALVE.  THIS WAS DONE BY LAPPING MIXTURE PLATE WITH VERY	 FINE SANDPAPER AND OIL ON A SURFACE PLATE.  THAT CORRECTED ENG OPER SQUAWKS, BUT WITHIN 200 HRS, PROBLEM RECURRED.	1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999092400702	19990924	00702	SO  	1999	9	24	99ZZZX3584       	2	19990818	G	7320		MIXTURE PLATE   	PRECISION   	R5A5AD2     	PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360KB   	17025	SO  					FUEL SERVO	SCORED          	B			B4VS	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4178R	84   				3449113	321499			ENGINE OPERATING SQUAWKS INCLUDE STIFF THROTTLES, ENGINES DYING, ROUGH RUNNING, AND IMPROPER FUEL MIXTURES.  THE ENGINE 	PARAMETERS WERE RESET, BUT THE PROBLEMS RETURNED.  THE MIXTURE CONTROL ON THE THROTTLE SIDE OF THE SERVO WAS DISASSEMBLE	D.  FOUND THE BRASS MIXTURE PLATE BADLY SCORED.  THIS ALLOWED EXCESS FUEL TO FLOW THROUGH THE SCORES AND DISRUPT THE MIX	TURES.  FOUND THE FUEL SCREEN IN THE MANIFOLD VALVE WAS FULL OF METAL SHAVINGS.  THE SCORES IN THE BRASS MIXTURE PLATE W	ERE REMOVED AND THE CONTAMINATION WAS REMOVED FROM THE MANIFOLD VALVE.  THIS WAS DONE BY LAPPING MIXTURE PLATE WITH VERY	 FINE SANDPAPER AND OIL ON A SURFACE PLATE.  THAT CORRECTED ENG OPER SQUAWKS, BUT WITHIN 200 HRS, PROBLEM RECURRED.	1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999092400703	19990924	00703	SO  	1999	9	24	99ZZZX3585       	2	19990818	G	7320		MIXTURE PLATE   	PRECISION   	R5A5AD2     	PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	LTSIO360KB  	17025	SO  					FUEL SERVO	SCORED          	B			B4VS	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4162K	440  				3449097	321736			ENGINE OPERATING SQUAWKS INCLUDE STIFF THROTTLES, ENGINES DYING, ROUGH RUNNING, AND IMPROPER FUEL MIXTURES.  THE ENGINE 	PARAMETERS WERE RESET, BUT THE PROBLEMS RETURNED.  THE MIXTURE CONTROL ON THE THROTTLE SIDE OF THE SERVO WAS DISASSEMBLE	D.  FOUND THE BRASS MIXTURE PLATE BADLY SCORED.  THIS ALLOWED EXCESS FUEL TO FLOW THROUGH THE SCORES AND DISRUPT THE MIX	TURES.  FOUND THE FUEL SCREEN IN THE MANIFOLD VALVE WAS FULL OF METAL SHAVINGS.  THE SCORES IN THE BRASS MIXTURE PLATE W	ERE REMOVED AND THE CONTAMINATION WAS REMOVED FROM THE MANIFOLD VALVE.  THIS WAS DONE BY LAPPING MIXTURE PLATE WITH VERY	 FINE SANDPAPER AND OIL ON A SURFACE PLATE.  THAT CORRECTED ENG OPER SQUAWKS, BUT WITHIN 200 HRS, PROBLEM RECURRED.	1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999092400704	19990924	00704		1999	9	24	99ZZZX3586       	4	19990820	G	3120	754817	FILTER          			PIPER 	PA31  	PA31350     	7103110	SO  										COCKPIT	MISMARKED       	B	L	A	UJDR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	05	130LS					317752140				SUBMITTER STATED THEIR SUPPLIER IS PROVIDING P/N 754-817 (PIPER) FILTERS THAT ARE THE WRONG SIZE.  THE PART (FILTER) THA	T IS BEING SUPPLIED IS TOO LARGE AND WILL NOT FIT INTO THE FILTER HOUSING.					1	L	7	2 	3O				A20SO   					 
1999092400705	19990924	00705	NE  	1999	9	24	99ZZZX3587       	2	19990817	G	7412	90497703	EXCITER BOX     			GULSTM	560   	560         	0141402	SW  	PWA   	JT15  	JT15D5      	52112	NE  					ENGINE	FAILED          	B	L		AC1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	356WC	358  			98257453	5600432	JC0354			DURING PHASE 3 AND 4 INSPECTION, THE RIGHT INBOARD IGNITER WAS NOT FIRING.  INSPECTION OF THE PLUG REVEALED THERE WAS LI	TTLE WEAR ON THE PLUG AND RECORDS SHOWED IT WAS INSTALLED 150 HOUR PREVIOUS ON A PHASE 1 AND 2 INSP.  VOLTAGE CHECKED TO	 THE BOX AND THERE WAS 28 VOLTS PRESENT.  THE GROUND WAS CHECKED AND WAS GOOD.  A NEW LUG WAS INSTALLED AND IT WOULD NOT	 FIRE.  A NEW LEAD WAS INSTALLED ALONG THE NEW PLUG AND STILL NOT SPARK.  THE OLD PLUG WAS TRIED ON THE OUTBOARD POSITIO	N AND IT WOULD SPARK.  IT WAS OBVIOUS THE EXCITER BOX WAS AT FAULT.  THIS BOX WAS INSTALLED ON 11-18-98 AND HAS 358.2 HR	S AND 281 CYCLES.  INSTALLED NEW EXCITER BOX.  OPER CHECK OKAY.  BOX S/N 98257440.	1	H	7	2 	3O	4	F		6A1     	E25EA				 
1999092400706	19990924	00706	SW  	1999	9	24	99ZZZX3588       	1	19990817	G	5210	S287375	CABLE           			GULSTM	560   	560         	0141402	SW  										DOOR STEP	BROKEN          	B	L		AC1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	356WC	476  				5600432				THE FORWARD STEP CABLE BROKE AS A MAINTENANCE WAS BOARDING AIRCRAFT.  OCCURRED JUST AFTER ACFT CAME IN FROM A FLIGHT.  T	HE CABLE BROKE IN THE THREADS OF THE TURNBUCKLE WHERE IT ATTACHES TO THE BOTTOM OF THE STEP.  THIS IS THE THIRD CABLE TH	AT HAS BROKEN IN THE FWD POSITION.  THE FIRST BROKE AT 151.8 HRS, THE SECOND AT 616.8 HRS AND THIS ONE AT 1,093.2 HRS. A	N AFT CABLE BROKE AT 358.4 HRS.  THE PREVIOUS CABLES BROKE AT THE SWAGE AT THE TURNBUCKLE END.  THIS WAS THE FIRST CABLE	 TO BREAK AT THE THREADS OF THE TURNBUCKLE.  REF:  NR 158969 DATED 10-5-98.  NEW CABLE INSTALLED AND RIGGED.		1	H	7	2 	3O			 	6A1     					 
1999092400707	19990924	00707	NE  	1999	9	24	99ZZZX3589       	2	19990817	G	7230	310281401	FAN ASSY        			GULSTM	560   	560         	0141402	SW  	PWA   	JT15  	JT15D5      	52112	NE  					ENGINE	DAMAGED         	B	L		AC1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	357WC	4132 	684  		20A268	5600069	PCE108134			ON  PRE-FLIGHT, THE COPILOT DISCOVERED DAMAGE TO THE RIGHT FAN ASSY WHICH RESULTED IN THE FLIGHT BEING CANCELLED.  FOUND	 DAMAGE TO 12 BLADES RANGING FROM SMALL NICKS TO A SECTION MISSING FROM THE TIP OF ONE BLADE THAT WAS APPROX .25 SQUARE 	INCH IN SIZE.  THE INFORMATION WAS SENT TO P & W-CANADA TO DETERMINE IF ACFT COULD BE FLOWN TO A MAINT SHOP TO EFFECT A 	REPAIR.  THE FAN WAS DISASSEMBLED AND 10 SERVICEABLE BLADES INSTALLED.  THE ASSY WAS BALANCED AND RE-INSTALLED. THE CORE	 WAS INSPECTED AND NO DAMAGE NOTED.  APPARENTLY, THE PIECES EXITED THROUGH THE BYPASS DUCT.		1	H	7	2 	3O	4	F		6A1     	E25EA				 
1999092400708	19990924	00708	CE  	1999	9	24	99ZZZX3590       	1	19990911	G	5610		WINDSCREEN      			CESSNA	421   	421C        	2076016	CE  										COCKPIT	FAILED          	H				A				UNSCHED LANDING         				F			FLT CONT AFFECTED         			CR	CRUISE         	1			SW	99										AIRCRAFT WAS AT 17,000 FEET, WHEN IT EXPERIENCED A CATASTROPHIC FAILURE OF THE PILOT'S WINDSCREEN CAUSING INSTANT DEPRES	SURIZATION OF CABIN.  CAUSE OF THIS FAILURE AT THIS TIME IS UNKNOWN.  A POSSIBILITY IS THAT THE WINDSCREENS WERE REWORKE	D TO REMOVE SCRATCHES AND THIS WEAKENED THEM.				1	L	7	2 	3O				A7CE    					 
1999092400709	19990924	00709	SO  	1999	9	24	99ZZZX3591       	2	19990831	G	8530	654960A1	CYLINDER        			CESSNA	182   	182P        	2075816	CE  	CONT  	O470  	O470U       	17026	SO  					NR 6	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	23	952CC	833  				18263638	470757			DURING A ROUTINE 100-HOUR INSPECTION, EXCESSIVE LEAKAGE WAS FOUND PAST THE PISTON RINGS ON THE NR 6 CYLINDER.  THE REMOV	ED CYLINDER WAS FOUND WORN TO A BELL MOUTH CONDITION AT THE TOP OF THE CYLINDER BORE.					1	H	7	1 	3O	3	O	NT	TA13    	E273				 
1999092400710	19990924	00710	SO  	1999	9	24	99ZZZX3592       	2	19990831	G	8530	654960A1	CYLINDER        			CESSNA	182   	182P        	2075816	CE  	CONT  	O470  	O470U       	17026	SO  					NR 2	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	23	952CC	833  				18263638	470757			DURING A ROUTINE 100-HOUR INSPECTION, EXCESSIVE LEAKAGE WAS FOUND PAST THE PISTON RINGS ON THE NR 2 CYLINDER.  THE REMOV	ED CYLINDER WAS FOUND WORN TO A BELL MOUTH CONDITION AT THE TOP OF THE CYLINDER BORE.					1	H	7	1 	3O	3	O	NT	TA13    	E273				 
1999092400711	19990924	00711	CE  	1999	9	24	99ZZZX3593       	1	19990830	G	5320	07120591	SUPPORT         			CESSNA	182   	182R        	2072731	CE  										E/E BAY	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	182MT	1381 				18268157				BATTERY BOX SUPPORT ANGLES WERE FOUND CRACKED DURING ANNUAL INSPECTION.  IF UNDETECTED, BATTERY CAN BECOME LOOSE IN TAIL	.  IT IS VERY COMMON IN THIS TYPE OF DESIGN, USING THESE ANGLES.  SUBMITTER STATED SHOULD HAVE A STRONGER RE-DESIGN FOX.					1	L	7	1 	3O			NT	3A13    					 
1999092400712	19990924	00712	CE  	1999	9	24	99ZZZX3594       	1	19990909	G	2820	05001185	LINE            			CESSNA	172   	R172E       	2072413	CE  										FUEL SYSTEM	CRACKED         	G	S			K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	35	667GA					R1720150				CRACKED FUEL LINE FROM FIRE WALL TO INLET SIDE OF GASCOLATOR.  CRACK OCCURRED AT A BEND DIRECTLY BEHIND THE FERREL SLEEV	E/NUT.  CRACK APPEARED TO BE OLD AND NOT A RESULT OF AIRCRAFT ACCIDENT.  SUBMITTER SUSUPECTED CRACKED FUEL LINE MAY HAVE	 CAUSED A FUEL LEAK THAT WAS UNDETECTED.				1	H	7	1 	3O				3A17    					 
1999092400713	19990924	00713	SO  	1999	9	24	99ZZZX3595       	2	19990729	G	7314	6467671A1	PUMP            			BEECH 	58    	58          	1152740	CE  	CONT  	O550  	IO550C      		SO  					FUEL SYSTEM	LEAKING         	H				C				ABORTED TAKEOFF         				K	R	J	FLUID LOSS                	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	TO	TAKEOFF        	1			SW	99	FGKZE	159  			E059904BR	TH1494	815351R			LOSS OF POWER ENGINE 2 DURING TAKEOFF.  INSPECTION REVEALED A LEAK OF FUEL BY DRAIN FUEL PUMP.						1	L	7	2 	3O	3	O		3A16    	E3SO				 
1999092400714	19990924	00714	CE  	1999	9	24	99ZZZX3596       	1	19990726	G	2120	08145521	COVER           			CESSNA	310   	310R        	2074245	CE  										CARGO BAY	MISMANUFACTURED 	B	S		DINR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	5336C	7220 				310R1542				DURING SCHEDULED INSTRUMENT AIR FILTER REPLACEMENT, FOUND THE PLASTIC COVER (SHROUD) P/N 0814552-1 FOR THE FILTER WAS IN	TERFERING WITH AND PREVENTING THE FILTER GASKET FROM SEALING COMPLETELY.  TRIMMED INNER EDGES OF FLANGES TO ALLOW COMPLE	TE GASKET SEALING.				1	L	7	2 	3O				3A10    					 
1999092400715	19990924	00715	CE  	1999	9	24	99ZZZX3597       	1	19990726	G	2120	08145521	COVER           			CESSNA	310   	310R        	2074245	CE  										CARGO BAY	MISMANUFACTURED 	B	S		DINR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	90FC	6729 				310R1838				DURING SCHEDULED INSTRUMENT AIR FILTER REPLACEMENT, FOUND THE PLASTIC COVER (SHROUD) P/N 0814552-1 FOR THE FILTER WAS IN	TERFERING WITH AND PREVENTING THE FILTER GASKET FROM SEALING COMPLETELY.  TRIMMED INNER EDGES OF FLANGES TO ALLOW COMPLE	TE GASKET SEALING.				1	L	7	2 	3O				3A10    					 
1999092400716	19990924	00716	CE  	1999	9	24	99ZZZX3598       	1	19990826	G	2421	DOFF10300BR	BOLT            			CESSNA	172   	172N        	2072434	CE  										ALTERNATOR	BROKE           	B			BCBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	4873G				A898024	17273420				PENN YAN CONVERION WAS COMPLETED 1-22-97 AT TT 2,954 HRS.  ON 4-28-99 AT 2,987 = 33 HRS IN SERVICE, AN ALTERNATOR THROUG	H-BOLT WAS FOUND BROKEN.  UNIT REPAIRED AT PENN YAN RE-INSTALLED.  ON 8-7-99 AT 3,066 = 112:00 HRS IN SERVICE, THROUGH-B	OLTS BROKEN AGAIN.  UNIT REPLACED THIS TIME WITH S/N 202511 PENN YAN OVERHAULED UNIT.				1	H	7	1 	3O			NT	3A12    					 
1999092400717	19990924	00717	CE  	1999	9	24	99ZZZX3599       	1	19990721	G	7810	99102953	EXHAUST RISER   			CESSNA	414   	414         	2075908	CE  										RT ENGINE	CRACKED         	B		A	JZBR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	25	1582T	5000 				4140362				EXHAUST RISER SPLIT OPEN AT PIPE TO RISER CONNECTION.  HOT SPOTS AT CLUSTER IS NORMAL, CAUSING FATIGUE WITH AGING PIPES.	  NEW INCONEL RISER, PN 9912095-12, ASSY INSTALLED.					1	L	7	2 	3O			RT	A7CE    					 
1999092400718	19990924	00718	CE  	1999	9	24	99ZZZX3600       	1	19990721	G	5312	00244002375	BULKHEAD        			BEECH 	58    	58          	1152740	CE  										BS 257	CRACKED         	B			JZRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	45FM					TH739				CRACK WAS FOUND AT BS 257.60 IN UPPER LEFT CORNER OF BULKHEAD.  CRACK WAS APPROXIMATELY 1 INCH LONG.  MOVEMENT FROM HORI	ZONTAL STABILIZER PUTS STRESS ON BULKHEAD.  BEECH SI 0990 REV 11 GIVES INSPECTION AND KIT REFERENCES.  NEW BULKHEAD ASSY	, PN 002-440023-75 WITH REINFORCEMENT PLATES INSTALLED, WAS INSTALLED IN AIRCRAFT.				1	L	7	2 	3O				3A16    					 
1999092400719	19990924	00719	SO  	1999	9	24	99ZZZX3601       	1	19990615	G	2120	3716503	DUCT            			PIPER 	PA34  	PA34220T    	7103420	SO  										CARGO BAY	LOOSE           	B	S		LF1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	4128U	78   				3449100				DUCT 37165-03 DROPPED DOWN ONTO RUDDER, ELEVATOR, ELEVATOR TRIM CONTROL CABLES.  DUCT RE-INSTALLED AND SECURED USING MET	AL TAB POP RIVETED TO NEXT FORWARD DUCT.					1	L	7	2 	3O				A7SO    					 
1999092400720	19990924	00720	GL  	1999	9	24	99ZZZX3602       	1	19990903	G	7160	19165910	AIR DOOR        			BLANCA	17    	1731A       	1220435	GL  										AIRBOX	BROKEN          	B		A	LF1R	A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CL	CLIMB          	1			EA	07	4113B	1307 				7432145				AIRCRAFT LOST POWER ON TAKEOFF AND HAD TO MAKE AN EMERGENCY LANDING.  AIRCRAFT WAS ABLE TO RETURN TO AIRPORT.  TOWER REP	ORTED A LARGE AMOUNT OF BLACK SMOKE COMING FROM AIRCRAFT.  DUPLICATED PROBLEM ON GROUND RUN.  REMOVED AIRBOX AND FOUND A	LTERNATE AIR DOOR LAYING INSIDE.  INSPECTED SERVO FOR FOD, NONE FOUND.  DOOR DID NOT APPEAR TO HAVE ANY PIECES MISSING F	ROM IT.  REPLACED DOOR AND RAN AIRCRAFT.  ALL OPERATIONS SATISFACTORY,   AIRBOX SHOULD BE LOOKED AT MORE OFTEN, POSSIBLY	 EVERY 50 HOURS		1	L	7	1 	3O				A18CE   					 
1999092400721	19990924	00721	CE  	1999	9	24	99ZZZX3603       	1	19990830	G	2510		SEAT            			CESSNA	188   	A188B       	2073005	CE  										COCKPIT	DAMAGED         	G				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	13	731JY	5288 				18802941T				PILOT SEAT SLID BACK ON LANDING CAUSING THE PILOT TO LOSE DIRECTIONAL CONTROL.  THE FRONT LEFT ROLLER HOUSING WAS FOUND 	SPREAD OPEN TO .4687 INCH.  THE SEAT RAIL MEASURED .5000 INCH.  AD 87-20-03 HAD BEEN SIGNED OFF AS ACOMPLISHED APPROX 4 	MONTHS EARLIER.  THE FRONT RIGHT HOUSING WAS ALSO SPREAD OPEN.  BOTH HOUSINGS WERE BELIEVED TO BE SPREAD OPEN PRIOR TO T	HE ACCIDENT.			1	L	7	1 	3O				A9CE    					 
1999092400722	19990924	00722	EA  	1999	9	24	99ZZZX3604       	2	19990829	G	7322	105135	CARBURETOR      			CESSNA	172   	172M        	2072418	CE  	LYC   	O320  	O320E2D     	41508	EA  					ENGINE	LOOSE           	B			UKJR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	23	6996H				CK12420	17265685				OWNER COMPLAINED THAT THE AIRCRAFT WOULD NOT SHUT DOWN USING THE MIXTURE CONTROL. MAINTENANCE PERFORMED ENGINE RUN, NORM	AL.  PERFORMED ONE MORE RUN AND COULD NOT SHUT DOWN USING MIXTURE CONTROL.  TROUBLESHOT SYSTEM, FOUND ALL 4 SCREWS HOLDI	NG THE 2 HALVES OF THE CARBURETOR VERY LOOSE.  THE LOCKING TABS WERE IN PLACE.  AFTER REMOVAL OF THE CARB, ALL THE FUEL 	IN IT COULD BE POURED OUT OF THE PARTING FLANGE.			1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999092400723	19990924	00723	CE  	1999	9	24	99ZZZX3605       	1	19990829	G	8011	PM2401	STARTER         			CESSNA	182   	182S        	2072701	CE  										ENGINE	MALFUNCTIONED   	B			UKJR	C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			EA	23	4193Y	87   			85007411	18280359				ON TAKEOFF ROLL, PILOT NOTICED ALL RADIO LIGHTS FLICKERING AND VOLTMETER AT AROUND 21 VDC.  PILOT ABORTED TAKEOFF AND PE	RFORMED RUN-UP AGAIN, OK.  STARTED TAKEOFF AND HAD SAME PROBLEM.  AIRCRAFT TURNED OVER TO MAINTENANCE.  MAINTENANCE TECH	 WENT OUT TO START AIRCRAFT AND FOUND STARTER INOPERABLE.  TROUBLESHOT AND FOUND POWER UP TO THE STARTER.  REPLACED STAR	TER, OPS CHECK NORMAL.			1	H	7	1 	3O			NT	3A13    					 
1999092400724	19990924	00724	SO  	1999	9	24	99ZZZX3606       	1	19990830	G	2720	1607000	TORQUE TUBE     			PIPER 	PA23  	PA23250     	7102308	SO  										RUDDER	CORRODED        	B			BIER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	32WW	4546 				278054036				FOUND RUSTY TUBE ASSEMBLY (RUDDER TORQUE).  WHEN REMOVED FROM TAIL, TOP OF TUBE ASSY WAS ALSO RUSTY.  HIDDEN CORROSION T	HAT COULD NOT BE SEEN DURING INSPECTION.					1	L	7	2 	3O				1A10    					 
1999092400725	19990924	00725	EA  	1999	9	24	99ZZZX3607       	2	19990825	G	8530		VALVE           			GULSTM	AA5   	AA5B        	3960105	SO  	LYC   	O360  	O360A4K     	41514	EA  					NR 3 CYLINDER	FAILED          	D				O				OTHER                   				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	NR	NOT REPORTED   	1			EA	23	74641					AA5B0311	L2153336A			REMOVED NR 3 CYLINDER DUE TO BROKEN EXHAUST VALVE.  VALVE BROKE IN-FLIGHT AND ENGINE STARTED RUNNING ROUGH.  REPLACED CY	LINDER ASSEMBLY, PISTON AND RINGS.  ENGINE HAS 888.41 HRS SMOH.					1	L	7	1 	3O	3	O		A16EA   	E286				 
1999092400726	19990924	00726	EA  	1999	9	24	99ZZZX3608       	2	19990830	G	8500		ENGINE          			DOUG  	DC3   	R4D8        	3021474	WP  	WRIGHT	R1820 	R182080     	67020	EA  					NACELLE	FAILED          	H				A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			SW	17	3906J	18836	1064 			43344	BL519560			CRUISING VMC AT 9,500 FEET NEAR LFK, ENGINE SHOOK AND OIL PRESSURE BEGAN TO LOWER.  CAPTAIN ELECTED PRECAUTIONARY SHUTDO	WN OF ENGINE AND LANDED AT LFK WITHOUT INCIDENT.  CARGO WAS DISPATCHED ON ANOTHER AIRCRAFT.  SUSPECT PROBLEM AS VALVE FA	ILURE DAMAGING PISTON.  AS YET UNCONFIRMED.				2	L	7	2 	4R	4	R		6A2     	E259				 
1999092400727	19990924	00727	CE  	1999	9	24	99ZZZX3609       	1	19990825	G	2822	5100001	PUMP            	DUKES       		CESSNA	182   	182S        	2072701	CE  										FUEL SYSTEM	LEAKING         	B			EIYR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	07	383ES	239  			0690	18280024				OWNER/OPERATOR REPORTED FUEL LEAK FROM UNDER COWL WHEN AIRCRAFT WAS PARKED. INSPECTION REVEALED THAT ELECTRIC BOOST PUMP	 WAS LEAKING OUT OVERBOARD VENT LINE.  REPLACED FUEL PUMP WITH NEW PART, OPS CHKS GOOD.					1	H	7	1 	3O			NT	3A13    					 
1999012200597	19990122	00597	EU  	1999	1	22	99ZZZX361        	1	19990102	G	2520	3410	SEAT            			AIRBUS	320   	A320232     	3930326	EU  										PASSENGER CABIN	CRACKED         	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	407UA					456				DURING THE FIRST HEAVY MAINTENANCE VISIT (HMV-1) VIRTUALLY 100 PERCENT OF THE COACH SEATS IN THE PASSENGER CABIN WERE FO	UND TO HAVE SEAT PANS THAT WERE CRACKED AT THE FORWARD ATTACHMENT HOLES FOR THE SEAT PANS.  THESE ARE RECARO 720 SERIES 	SEATS INSTALLED IN THE AIRBUS A-320-232 AIRCRAFT.  THE SEAT MANUFACTURER DESIGNATES THE SEAT PAN AS PRIMARY STRUCTURE FO	R THE SEAT.  THIS IS THE 7TH CONSECUTIVE A-320-232 TO SHOW A 100 PERCENT FAILURE RATE OF THESE SEAT PANS.			2	L	7	2 	4F			RT	A28NM   					 
1999092400728	19990924	00728	SO  	1999	9	24	99ZZZX3610       	2	19990801	G	8520	536421	GEAR            			CESSNA	210   	P210N       	2073454	CE  	CONT  	O520  	TSIO520P    	17040	SO  					CRANKSHAFT	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	4759K	1443 				P21000290	513283			TT:  1,443.0 HRS AIR FRAME AND ENGINE.  ORIGINAL ENGINE FROM THE FACTORY, NEVER REMOVED.  GEAR TOOTH FOUND DURING OIL DR	AIN CHANGE, MTAL FOUND IN THE OIL FILTER.  NO MOTOR OR PART FROM IN THE PREVIOUS OIL CHANGE 35 HRS PIOR.  ENGINE WAS RUN	NING NORMAL.				1	H	7	1 	3O	3	O		3A21    	E8CE				 
1999092400729	19990924	00729		1999	9	24	99ZZZX3611       	4	19990801	G	3452		TRANSPONDER     			CESSNA	421   	421C        	2076016	CE  										COCKPIT	INTERMITTENT    	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	510DB				2205	421C0063				REMOVED KXP 755 TRANSPONDER FROM AIRCRAFT.  FOUND RECEIVER INTERMITTENT, FOUND BURST CLOCK TOO LONG, CHANGED COIL AND AS	SOCIATED PARTS, FOUND POWER OUTAGE ONLY 10 WATTS, AND FREQUENCY UNRECOGNIZABLE.  SWAPPED CAVITIES AND FOUND LOWER SUPPLY	 TOO LOW, TREAD PROBLEM TO BAD TRANSFORMER.  REMOVED AND REPLACED. ALIGNED UNIT AND BURN TESTED ON BENCH 8 HRS.  CHECKED	 ALIGNMENT, UNIT TESTED TO MFG'S SPECS.			1	L	7	2 	3O				A7CE    					 
1999092400731	19990924	00731	CE  	1999	9	24	99ZZZX3613       	1	19990830	G	5312	0412112	BULKHEAD        			CESSNA	140   	140         	2071602	CE  										TAIL	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	07	1850V	4006 				14020				DURING ROUTINE INSPECTION, FOUND ELEVATOR CONTROL CABLE TENSION LOW.  ATTEMPT TO ADJUST, COULD NOT ATTAIN PROPER TEST. I	NSPECT CABLE ROUTING, NOT ABLE TO VERIFY PULLEY MOVEMENT.  THERE ARE NO ACCESS PLATES OR PANELS TO VISUALLY INSPECT.  EN	TIRE TAIL GROUP WAS REMOVED TO FURTHER FACILITATE INSPECTION.  FOUND AFT HORIZONTAL BULKHEAD CRACKED SEVERAL LOCATIONS. 	 ELEVATOR CONTROL CABLES WERE DETERMINED TO BE STRETCHED.			1	H	7	1 	3O			NC	A768    					 
1999092400732	19990924	00732	SO  	1999	9	24	99ZZZX3614       	1	19990902	G	3411	63913122	HOSE            			PIPER 	PA28  	PA28181     	7102807	SO  										PITOT SYSTEM	SEPARATED       	B			KL2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	23	151CL	406  				2843090				PILOT NOTICED INACCURATE AIRSPEED INDICATION.  UPON TROUBLESHOOTING, FOUND THE 2 FLEXIBLE HOSES CONNECTED FROM PITOT MAS	T TO HARD LINES IN LEFT WING HAD BEEN TORN AT HARD LINE CONNECTION.  THE REMAINDER OF THE HOSES APPEARED TO BE WITHOUT D	AMAGE.				1	L	7	1 	3O				2A13    					 
1999092400733	19990924	00733	SO  	1999	9	24	99ZZZX3615       	1	19990902	G	3411	63913123	HOSE            			PIPER 	PA28  	PA28181     	7102807	SO  										PITOT SYSTEM	SEPARATED       	B			KL2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	23	151CL	406  				2843090				PILOT NOTICED INACCURATE AIRSPEED INDICATION.  UPON TROUBLESHOOTING, FOUND THE 2 FLEXIBLE HOSES CONNECTED FROM PITOT MAS	T TO HARD LINES IN LEFT WING HAD BEEN TORN AT HARD LINE CONNECTION.  THE REMAINDER OF THE HOSES APPEARED TO BE WITHOUT D	AMAGE.				1	L	7	1 	3O				2A13    					 
1999092400734	19990924	00734	SO  	1999	9	24	99ZZZX3616       	2	19990817	G	8520		CRANKSHAFT      			CESSNA	188   	A188B       	2073005	CE  	CONT  	O520  	IO520D      	17032	SO  					ENGINE	BROKEN          	D				A				UNSCHED LANDING         				Y	J		ENGINE STOPPAGE           	WARNING INDICATION        		NR	NOT REPORTED   	1			SO	07	91409		909  			18802039	175626R			ENGINE LOCKED UP IN-FLIGHT.  FOUND REAR PULLEY NOT MOVING WHEN MOVING PROPELLER.  SUSPECT CRANKSHAFT BROKEN AT NR 1/NR 2	 JOURNAL.  AD 87-23-08 PREVIOUSLY C/W 909 HOURS AGO.					1	L	7	1 	3O	3	O		A9CE    	E5CE				 
1999092400735	19990924	00735	CE  	1999	9	24	99ZZZX3617       	1	19990818	G	2823		SELECTOR        			CESSNA	182   	182K        	2072724	CE  										FUEL VALVE	CORRODED        	H	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	2656R	3808 				18258356				SELECTOR APPEARS TO BE ORIGINAL BY RECORDS RESEARCH.  ELECTOR VALVE WAS NOT DETENTING.  UPON DISASSEMBLY, SPRING LOADED 	DETENT BALL WAS FOUND SEIZED IN ITS CHANNEL AND WAS DIFFICULT TO FREE.  REASON FOR SEIZING WAS DUE TO CORROSION ON BALL.	  RECOMMEND PERIODIC DISASSY, INSPECTION, AND CLEANING, AS THIS OCCURRED BETWEEN ANNUALS AND WAS OPERATING PROPERLY BEFO	RE INCIDENT.			1	H	7	1 	3O			NT	3A13    					 
1999092400736	19990924	00736	NM  	1999	9	24	99ZZZX3618       	1	19990805	G	5740	200012001	FITTING         			PIPER 	PA60  	PA60600     	7106001	NM  										LT WING	CRACKED         	B		A	H5GR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	600VF	6322 				600757806122				INSPECTION OF LEFT MAIN GEAR WELL AREA FOUND WING ATTACH FITTINGS TO HAVE VERTICAL CRACKS APPROXIMATELY .50 INCH IN LENG	TH BETWEEN RIVETS THAT ATTACH FITTING TO SPAR.  THESE CRACKS ARE LOCATED IN THE WEB/RADIUS AREA OF THE FITTING ANGLE.					1	M	7	2 	3O			RT	A17WE   					 
1999092400737	19990924	00737	CE  	1999	9	24	99ZZZX3619       	1	19990817	G	2435	23079004	BEARING         			CESSNA	441   	441         	2076020	CE  										STARTER/GEN	FAILED          	G				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			NM	04	185GA					4410066				GENERATOR BEARING FAILURE CAUSING OVERHEATING OF THE GENERATOR.  ALERTED THE FIRE WARNING SYSTEM TO REACT GIVING A FALSE	 FIRE WARNING INDICATION DURING FLIGHT.					1	L	7	2 	3T			RT	A28CE   					 
1999092400738	19990924	00738	CE  	1999	9	24	99ZZZX3620       	1	19990830	G	5320	07120591	SUPPORT         			CESSNA	182   	182         	2072702	CE  										BATTERY BOX	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	182MT	1381 				18268157				BATTERY BOX SUPPORT ANGLES WERE FOUND CRACKED DURING ANNUAL INSPECTION.						1	H	7	1 	3O			NT	3A13    					 
1999092400739	19990924	00739	CE  	1999	9	24	99ZZZX3621       	1	19990819	G	3246	31372	WHEEL           			CESSNA	441   	441         	2076020	CE  										MLG	CRACKED         	B			F3NR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	04	88QT				0217	4410228				CRACK IN WHEEL HALF (INNER) ALONG FLANGE APPROXIMATELY 3 INCHES LONG, P/N 3-1372, S/N 0217.  RECOMMENDED INSPECT WHEEL H	ALF FLANGES FOR CRACKS PERIODICALLY USING DYE PENETRANT METHOD.  RIGHT MAIN LANDING GEAR.  ACFT TT:  3718.3 HOURS.					1	L	7	2 	3T			RT	A28CE   					 
1999092400740	19990924	00740	CE  	1999	9	24	99ZZZX3622       	1	19990726	G	3246	31372	WHEEL           	BFGOODRICH  		CESSNA	441   	441         	2076020	CE  										MLG	CRACKED         	B			F3NR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	04	88QT				0216	4410228				WHEEL HALF, INNER, AT ROTOR AND TIRE RADIUS FLANGE CRACKED APPROXIMATELY 4 INCHES. RECOMMEND DYE PEN OR ZYGLO PERIODIC I	NSPECTION.  LEFT MLG.  ACFT TT: 3,985.7 HOURS.					1	L	7	2 	3T			RT	A28CE   					 
1999092400741	19990924	00741	EU  	1999	9	24	99ZZZX3623       	1	19990803	G	2842	TB2052041002	TRANSMITTER     			SOCATA	TB20  	TB20TRINIDAD	8680695	EU  										FUEL QUANTITY	ERRATIC         	B			BIGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	2822A				118	1122				PILOT REPORTED ERRATIC FUEL QUANTITY INDICATIONS ON RT FUEL TANK.  TROUBLE WAS TRACED TO A FUEL QUANTITY TRANSMITTER, PN	 TB2052041002.  WHEN CHECKED PER MM, OHM VALUES WERE ERRATIC AND OUT OF TOLERANCE.  TWO NEW UNITS WERE ORDERED AND EACH 	CHECKED OUT OF TOLERANCE AND ERRATIC.				1	L	7	1 	3O			RT	A51EU   					 
1999092400742	19990924	00742	SO  	1999	9	24	99ZZZX3624       	1	19990727	G	7332	8004804	HOSE            			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					FUEL PRESSURE	FAILED          	B				A				UNSCHED LANDING         				K	B		FLUID LOSS                	SMOKE/FUMES/ODORS/SPARKS  		NR	NOT REPORTED   	1			NM	04	27956	9278 				317952064				PILOT SMELLED STRONG ODOR OF FUEL AND NOTED FUEL DRIPPING FROM BEHIND INSTRUMENT PANEL ONTO COPILOT RUDDER PEDALS.  MADE	 UNEVENTFUL LANDING AT DESTINATION.  TRACED LEAK TO FAULTY FUEL PRESSURE HOSE AT FUEL PRESSURE GAUGE. REPLACED HOSE AND 	STOPPED LEAK.  HOSE HAD SMELL, SPLIT, POSSIBLY DUE TO OLD AGE.				1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999092400743	19990924	00743	EA  	1999	9	24	99ZZZX3625       	2	19990830	G	8530		FOLLOWER        		72877       	CESSNA	172   	172P        	2072436	CE  	LYC   	O320  	O320D2J     	41508	EA  					ENGINE	BROKE           	H	S			A				UNSCHED LANDING         				Y			ENGINE STOPPAGE           			NR	NOT REPORTED   	1			NM	01	531PC	2260 				17274698	L1082039A			STUDENT PILOT FLYING, HAD ENGINE QUIT WHILE DOING TOUCH AND GOES.  A TEST RUN OF THE ENGINE AFTER RECOVERY REVEALED THE 	ENG WOULD MAKE 1,850 RPM'S WHEN LEANED OUT.  INVESTIGATIVE DISASSEMBLY REVEALED THE NR 1 INTAKE VALVE STUCK OPEN APPROX 	.3750 INCH.  THE VALVE WAS NOT STUCK IN THE GUIDE.  FURTHER DISSASSY REVEALED THE CAM FOLLOWER (BODY HYD TAPPET) HEAD HA	D BROKEN OFF OF THE NR 1 EXHAUST VALVE.  DEBRIS FROM THE EXHAUST CAM FOLLOWER BECAME TANGLED IN THE NR 1 INTAKE CAM, CAM	 FOLLOWER INTERFACE, THAT JAMMED THE NR 1 INTAKE PLUNGER ASSY OF THAT CAM FOLLOWER AND BROKE THE NR 1 INTAKE CAM FOLLOWE	R OUT OF THE CASE.	1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999100100005	19991001	00005	SO  	1999	10	1	99ZZZX3629       	1	19990908	G	2434	1159AV2046713	GROUND PAD      			GULSTM	G1159 	G1159       	3953505	SO  										GENERATOR	BURNT           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	154C	5157 				253				LEFT DC GENERATOR WOULD OCCASSIONALLY TRIP OFF-LINE DURING A GROUND RUN-UP.  FOUND THE LEFT GENERATOR SHUNT GROUND PAD M	ELTED AND BURNT.  GROUND PAD HAD RECENTLY BEEN REMOVED BY AN OUTSIDE MAINT FACILITY (AT CUSTOMER REQUEST) TO CHECK IT AN	D SHUNT FOR CORROSION.  BOTH SHUNT AND GROUND PAD WERE IN GOOD CONDITION.  IT APPEARS EITHER THE BOLT SECURING THE GROUN	D PAD TO THE SHUNT WAS NOT TORQUED OR THE GROUND PAD WAS NOT MATED FLUSH WITH THE SHUNT BEFORE ALL SECURING HARDWARE FOR	 THE SHUNT AND GROUND PAD WERE TIGHTENED.		2	L	7	2 	4F			RT	A12EA   					 
1999100100006	19991001	00006	SW  	1999	10	1	99ZZZX3630       	1	19990817	G	3230	55656194	ARM             			GULSTM	560   	560         	0141402	SW  										NLG	WORN            	B	S		AC1R	O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			SO	01	356WC	1045 				5600432				PILOTS SQUAWKED A NOISE FROM NOSE WHEELWELL WHILE TAXIING.  INSPECTION REVEALED EXCESSIVE CLEARANCE BETWEEN THE ARM THAT	 ATTACHES THE STEERING BUNGEE TO THE NOSE STEERING UNIVERSAL JOINT.  THIS CLEARANCE ALLOWED THE BUNGEE TO CONTACT THE PU	LLEY BRACKET LOCATED UNDER THE BUNGEE, CREATING THE NOISE.  THE WEAR IN THE ARM WAS IN THE SIDE-TO-SIDE DIRECTION.  A SI	NGLE BOLT IN THE FORE AND AFT DIRECTION ATTACHES THE ARM TO THE UNIVERSAL.  THERE SHOULD BE NO MOVEMENT BETWEEN THE ARM 	AND UNIVERSALS TO CAUSE WEAR.  SUBMITTER STATED THE HOLE IN THE ARM MAY HAVE BEEN ENLARGED TO PERMIT EASIER ASSY.  THIS 	ALLOWED ARM ENOUGH CLEARANCE TO FLEX AND CAUSE MORE WEAR WHICH LEAD TO PRODUCTION OF NOISE.  INSTALLED NEW ARM.	1	H	7	2 	3O				6A1     					 
1999100100007	19991001	00007	NM  	1999	10	1	99ZZZX3631       	1	19990909	G	2740	69778551	SPRING          		654997025   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		26692	19016		KEO0722					SPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  POSSIBLE CAUSE, IMPROPER HEAT TREATING, AUSTENITE, FATI	GUE AND INCREASED SPRING COIL STRESSES.  SPRINGS PN 69-77855-1 ARE TO BE REPLACED WITH PN 69-77855-2 SPRINGS ON ACTUATOR	 ASSYS MANUFACTURED PRIOR TO S/N KE01730 PER BOEING SL 737-SL-27-090-B.				2	L	7	2 	4F			RT	A16WE   					 
1999100100008	19991001	00008	NM  	1999	10	1	99ZZZX3632       	1	19990827	G	2740	69778551	SPRINGS         		654997025   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		18942			KE01675					SPRINGS PN 69-77855-1 ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  POSSIBE CAUSE, IMPROPER HEAT TREATING OR INCORRECT ALLO	YS IN THE SPRINGS.  SPRINGS PN 69-777855-1 SHOULD BE REPLACED WITH PN 69-77855-2 SPRINGS PER BOEING TELEX AEO-AUB-94-019	5RR.				2	L	7	2 	4F			RT	A16WE   					 
1999100100009	19991001	00009	NM  	1999	10	1	99ZZZX3633       	1	19990827	G	3230	6314157	CAP             	SARGENT     	731414      	BOEING	727   	727         	UTILSYS	NM  										MLG	CRACKED         	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					615					CAP IS CRACKED BEHIND THE C-PORT DUE TO FATIGUE.						2	L	7	3 	4J			RT	A3WE    					 
1999100100010	19991001	00010	NM  	1999	10	1	99ZZZX3634       	1	19990812	G	3243	65445214	VALVE           		65445231    	BOEING	737   	737*        		NM  										BRAKE	CRACKED         	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					M87					BODY IS CRACKED ABOVE PORT 5 RADIATING OUTWARD FROM ORIFICE PLUG POSSIBLY DUE TO FATIGUE, DEFECT IN THE CASTING, OR OVER	STRESSED AT ASSEMBLY.					2	L	7	2 	4F			RT	A16WE   					 
1999100100018	19991001	00018	SO  	1999	10	1	99ZZZX3642       	1	19990826	G	3610		LINE            			GULSTM	G1159 	GIV         	3980115	SO  										PNEUMATIC SYSTEM	CHAFED          	B	P		RO3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03	4PC					1174				THE STANDBY POWER RECTIFIER/HEAT SINK ASSY PN 1159F40669-11, LOCATED UNDER FLOORBOARD NR 19, WAS CHAFING AGAINST TOTAL T	EMP PROBE LINE PN 1159AC40071-025P6. THIS WORE A HOLE IN THE LINE.  THERE IS EVIDENCE OF AN AIR BLAST ON THE BLACK PAINT	 OF THE HEAT SINK.				2	L	7	2 	4F			RT	A12EA   					 
1999100100023	19991001	00023	EU  	1999	10	1	99ZZZX3647       	1	19990801	G	7933	648574181	INDICATOR       			AMD   	FALC20	FALCON20F5  	2730105	EU  										COCKPIT	READS LOW       	B			BJYR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	23	1881Q					414				GAUGE INSTALLED.  ENGINE GROUND RUN AND FUNCTIONED NORMALLY.  ON NEXT FLIGHT, CREW NOTICED TEMPERATURE WAS READING LOW. 	 REPLACED GAUGE.					2	L	7	2 	4F			RT	A7EU    					 
1999100100024	19991001	00024	NE  	1999	10	1	99ZZZX3648       	2	19990909	G	7200	2A2833	BEARING         								IAE   	V2500 	V2500A1     		NE  					ENGINE	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	01					3304					PART RECEIVED FROM WESTFIELD GAGE CO FOR FLUORESCENT PENETRANT INSPECTION PER SECTION 70-23-01, INSPECTION CHECK-01, TAS	K 70-23-01-230-501 OF THE INTERNATIONAL AERO ENGINE V2500 PROPULSION SYSTEM ENGINE MANUAL (REVISION 38).  PART REJECTED 	AT FPI DUE TO CRACK 0.100 INCH LONG ON TOP SURFACE, AS MARKED.									4	F			E311NE				 
1999100100025	19991001	00025	SW  	1999	10	1	99ZZZX3649       	1	19990817	G	7500		LINE            			GULSTM	690TP 	690A        	0141722	SW  	GARRTT	TPE331	TPE3315251K 		NM  					BLEED AIR	LEAKING         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	38WA					11169	P06119			A BLEED AIR LEAK AT STA 234 DAMAGED A NEARBY WIRING BUNDLE CAUSING VARIOUS ANNUNCIATOR INDICATIONS RESULTING IN THE REQU	EST FOR AN EMERGENCY LANDING.  BLEED AIR LEAK WAS CAUSED BY FLARE DEFORMING ALLOWING TUBING TO PULL OUT OF THE FITTING. 	 ESCAPING BLEED AIR GASES DAMAGED NEARBY WIRING HARNESS AT STA 223.  POSSIBLE CAUSE, IMPROPERLY MADE FLARE.  SUBMITTER R	ECOMMENDED FREQUENT INSPECTION OF BLEED AIR LINES ESPECIALLY NEAR WIRIING BUNDLES.			1	H	7	2 	3T	4	T		2A4     	E2WE				 
1999012200734	19990122	00734	SO  	1999	1	22	99ZZZX365        	2	19990104	G	8530	643724	CRANKCASE       			CESSNA	421   	421C        	2076016	CE  	CONT  	O520  	GTSIO520N   	17032	SO  					LT ENGINE	CRACKED         	B			DPOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	883FL		1056 			421C1407	241295R			DURING A PHASE 3 INSPECTION, A 1.50 INCH CRACK WAS NOTED ABOVE THE LEFT ENGINE, NR 2 CYLINDER.  PER M90-17, THIS WAS IN 	A NON-CRITICAL AREA, SO THE CRACK WAS SCRIBE MARKED AND RETURNED TO SERVICE.  DURING THE PHASE 4 INSPECTION, THE CRACK W	AS NOTED TO HAVE PROGRESSED BY .50 INCH (BEYOND LIMITS PER M90-17).  SUBMITTER SUGGESTED POSSIBLE CAUSE AS MANUFACTURING	 DEFECTS.  ENGINE TO BE REMOVED FOR OVERHAUL.			1	L	7	2 	3O	3	O		A7CE    	E7CE				 
1999100100026	19991001	00026	CE  	1999	10	1	99ZZZX3650       	1	19990908	G	3710		HOSE            			CESSNA	172   	172P        	2072436	CE  										INST VACUUM SYS	CRACKING        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	98637	2680 			04A	17276326				AIRCRAFT BEGAN TO LOSE VACUUM ON THE INSTRUMENT AIR SYS.  FOUND A POSSIBLE LINE CRACKED ON THE OUTSIDE FROM AGE.  AFTER 	REMOVING THAT LINE AND OTHER LINES ALSO CONNECTED TO THE INSTRUMENTS, DISCOVERED NOT ONLY THE OUTSIDE OF THE LINE WAS CR	ACKED, BUT THE INSIDE LINER (RED) WAS CRUMBLING FROM AGE AND PARTICLES FOUND IN SOME OF THE INSTRUMENT SCREENS.  THESE L	INES WERE ORIG EQUIP LINES INSTALLED WHEN ACFT WAS BUILT.  ALL OF THE LINES INSTALLED WITH IMPERIAL EASTMAN HYTRON REDI-	SEAL 04A HOSE HAD BE BE REPLACED AND INSTRUMENTS HAD TO BE REMOVED AND CHECKED FOR CONTAMINATES BEFORE RETURNING TO SERV	ICE.  3 OF 12 ACFT OPERATED BY SUBMITTER HAD THE IDENTICAL SAME PROBLEM. ONE C-182R, AND 2 C-172P'S MFG IN 1985 OR 1986.	1	H	7	1 	3O			NT	3A12    					 
1999100100027	19991001	00027	SO  	1999	10	1	99ZZZX3651       	2	19990910	G	8530		GEAR            			BEECH 	58    	58          	1152740	CE  	CONT  	O550  	IO550C      		SO  					CRANKSHAFT	FAILED          	H				O				OTHER                   				Y	J		ENGINE STOPPAGE           	WARNING INDICATION        		NR	NOT REPORTED   	1			CE	03	5574T	262  				TH1570				LEFT ENGINE QUIT IN-FLIGHT.  UPON INVESTIGATION ON GROUND, FOUND NO OIL PRESSURE DURING ENGINE TEST RUNS.  UPON FURTHER 	INVESTIGATION, FOUND DRIVE GEAR ON CAMSHAFT BROKEN OFF.  REMOVED ENGINE SENT TO TCM FOR ANALYTIC TEAR-DOWN.					1	L	7	2 	3O	3	O		3A16    	E3SO				 
1999100100028	19991001	00028	CE  	1999	10	1	99ZZZX3652       	1	19990908	G	5312	07126167	BULKHEAD        			CESSNA	182   	182P        	2075816	CE  										FUSELAGE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	888SR					18261455				SMALL CRACK ON LEFT TOP AND RIGHT TOP LIGHTNING HOLES IN BULKHEAD.  CRACK ORIGINATED FROM TIGHT RADIUS IN LIGHTNING HOLE	S.  THIS M OR D REPORT SUBMITTED PER AD 72-07-09 AND PART WAS REPLACED WITH NEW.					1	H	7	1 	3O			NT	TA13    					 
1999100100029	19991001	00029	SO  	1999	10	1	99ZZZX3653       	1	19990828	G	7600	6391602	CLAMP           			PIPER 	PA28  	PA28160     	7102806	SO  										THROTTLE CABLE	DETERIORATED    	G				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			GL	03	5199W	3574 				28234				THE RUBBER IN THE ADEL CLAMP DETERIORATED UNTIL THE CLAMP WAS NO LONGER SECURE AROUND THE THROTTLE CONTROL CABLE.  WITH 	NO RESISTANCE ON THE HOUSING AND THROTTLE MOVEMENT, THE CARBURETOR BUTTERFLY ENDED AT THE 1,500 RPM LOCATION.  WITH ONLY	 PARTIAL POWER, THE AIRCRAFT LANDED IN LAKE MICHIGAN.  NO INJURIES.				1	L	7	1 	3O				2A13    					 
1999100100030	19991001	00030	CE  	1999	10	1	99ZZZX3654       	1	19990909	G	8010	635050A8	ADAPTER         			CESSNA	421   	421B        	2076014	CE  										RT ENGINE	FAILED          	B			DPOR	A				UNSCHED LANDING         				K			FLUID LOSS                			CL	CLIMB          	1			NM	07	678DB		585  			421B0876				JUST AFTER TAKEOFF, PILOT NOTICED OIL COMING OUT OF THE RIGHT ENGINE COWL AND RETURNED TO THE AIRPORT.  OIL WAS FOUND CO	MING FROM THE STARTER DRIVE ADAPTER DAMPER.  ENGINE WAS REMOVED AND SENT TO OVERHAUL FACILITY.  ON TEAR-DOWN THE ADAPTER	 BEARING WAS FOUND TO HAVE FAILED.   THIS IS AN INTERNAL ENGINE COMPONENT.				1	L	7	2 	3O				A7CE    					 
1999100100031	19991001	00031	CE  	1999	10	1	99ZZZX3655       	1	19990908	G	3710		HOSE            			CESSNA	182   	182R        	2072731	CE  										INST VACUUM SYS	CRACKING        	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	9476X	2550 				18268536				AIRCRAFT BEGAN TO LOSE VACUUM ON INSTRUMENT AIR SYSTEM.  FOUND A POSSIBLE LINE CRACK ON THE OUTSIDE FROM AGE.  AFTER REM	OVING THAT LINE AND OTHER LINES ALSO CONNECTED TO THE INSTRUMENTS, FOUND THAT NOT ONLY THE OUTSIDE OF THE LINE WAS CRACK	ED, BUT THE INSIDE LINER (RED) WAS CRUMBLING FROM AGE AND PARTICLES WERE FOUND IN SOME OF THE INSTRUMENT SCREENS.  THESE	 LINES WERE ORIG EQUIP LINES INSTALLED WHEN ACFT WAS BUILT.  ALL OF THE LINES INSTALLED WITH IMPERIAL EASTMAN HYTRON RED	I-SEAL 04A HOSE HAD TO BE REPLACED AND THE INSTRUMENTS HAD TO BE REMOVED AND CHECKED FOR CONTAMINATES BEFORE RETURNING T	O SERVICE.  3 OF 12 ACFT SUBMITTER OPERATES HAD IDENTICAL PROBLEM, 1 C-182 AND 2 C-172'S MFG 1985/1986.	1	L	7	1 	3O			NT	3A13    					 
1999100100032	19991001	00032	CE  	1999	10	1	99ZZZX3656       	1	19990910	G	2810	0029200131	FUEL CELL       			BEECH 	58    	58          	1152740	CE  										LT WING	LEAKING         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CE	03	14XM				762926	TH758				CUSTOMER COMPLAINED OF FUEL TANK LEAKAGE.  UPON INVESTIGATION, FOUND FUEL CELL NIPPLES BROKEN OFF.  REMEMBERING AD 78-05	-06 CONCERNING GOODYEAR FUEL CELLS OF THIS VINTAGE, FOUND NOT TO BE APPLICABLE BUT NOTICED FAILURE OF SAME TYPE OCCURING	.  THIS IS A GOODYEAR FUEL CELL OF THE BTC-67 CONSTRUCTION NUMBER.				1	L	7	2 	3O				3A16    					 
1999100100033	19991001	00033	CE  	1999	10	1	99ZZZX3657       	1	19990909	G	3230	0341110	SPRING          			CESSNA	190   	190         	2072902	CE  										MLG	FAILED          	B			A5OR	O				OTHER                   				O			OTHER                     			LD	LANDING        	1			SO	09	9872A	2786 				7574				DURING LANDING, THE LEFT MAIN LANDING GEAR SPRING FAILED CAUSING SUBSTANTIAL DAMAGE TO THE AIRCRAFT FUSELAGE AND WING. P	ART REMOVED AND TURNED OVER TO FAA FOR INVESTIGATION.  POSSIBLE CAUSE - IMPROPER HEAT TREATMENT OF SPRING.					1	H	7	1 	3R			NC	A790    					 
1999100100034	19991001	00034	GL  	1999	10	1	99ZZZX3658       	2	19990710	G	7320	6893073	B-NUT           			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C30P     	03013	GL  					CNTRL TO PC TEE	FAILED          	B			KBTR	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			NM	07	5746N					45461	890669			FAILURE - B-NUT FLAIRED						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999100100035	19991001	00035	NE  	1999	10	1	99ZZZX3659       	2	19990805	G	7210	3024780	GEARBOX         			BELL  	212   	212         	1181420	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					NR 1 ENGINE	MAKING METAL    	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	17	212RA		3654 			31269	CPPS62013			ON START, NR 1 ENGINE CHIP LIGHT ILLUMINATED.  SHUT AIRCRAFT DOWN.  MAINTENANCE INSPECTED NR 1 ENGINE C-BOX CHIP PLUG AN	D METAL WAS FOUND ON CHIP PLUG AND IN OIL FILTER.  AMOUNT OF METAL WAS FOUND TO BE UNACCEPTABLE AND C-BOX WAS REMOVED. S	ERVICEABLE C-BOX INSTALLED.				1	G	7	1 	4U	4	U		H4SW    	E22EA				 
1999100100036	19991001	00036	SW  	1999	10	1	99ZZZX3660       	1	19990907	G	2844	407375007103	INDICATOR       			BELL  	407   	407         		SW  										FUEL PRESSURE	INTERMITTENT    	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	62LH	486  			0064	53045				FUEL PRESSURE INDICATOR HAS INTERMITTENT OPERATION.  REPLACED WITH NEW INDICATOR FROM BELL HELICOPTER.						1	G	7	1 	3U			O	H2SW    					 
1999100100037	19991001	00037	NE  	1999	10	1	99ZZZX3661       	2	19990813	G	7261		PLUG            			BOLKMS	117   	BK117B1     	5626012	EU  	LYC   	LTS101	LTS101750B1 	41560	NE  					ENGINE	MISINSTALLED    	B		A	TI1R	K				NONE                    				W	K		INADEQUATE Q C            	FLUID LOSS                		IN	INSP/MAINT     	1			SW	05	460H					7142	7142			APPARENTLY, DID NOT GET CHIP PLUG TURNED AND LOCKED PROPERLY DURING 25-HOUR CHIP CHECK.  UPON INSPECTION, FOUND CHIP PLU	G OUT OF THE SOCKET.  APPARENTLY,THE VALVE IN THE PLUG HOUSING DID NOT SEAT AND ALLOWED FOR A LARGE OIL LEAK.  SUBMITTER	 RECOMMENDED AFTER TURNING THE CHIP PLUG TO LOCK, A FIRM PULL DOWN ON PLUG TO ASSURE IT IS DEFINITELY LOCKED.				1	G	7	2 	3U	3	U		H13EU   	E5NE10				 
1999100100039	19991001	00039	NE  	1999	10	1	99ZZZX3663       	2	19990908	G	7230	2A0003	BEARING         								IAE   	V2500 	V2500A1     		NE  					COMPRESSOR	SPALLED         	B			RA1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05		384  			PGGUAK6529		V0202			ENGINE WAS REMOVED DUE TO M50 MATERIAL ON THE MAG CHIP DETECTORS.  DISASSEMBLY OF THE ENGINE REVEALED THE NR 4 BEARING E	XHIBITED SPALLING DAMAGE TO THE OUTER RACE.  THE BEARING WAS SUBMITTED TO THE LAB FOR ANALYSIS.  THE INVESTIGATION IS ST	ILL IN PROGRESS AT THIS AGENCY.									4	F			E311NE				 
1999100100041	19991001	00041		1999	10	1	99ZZZX3665       	1	19990802	G	3230		FORK            			AMTR  		VELOCITY    												NLG	SEPARATED       	G				O				OTHER                   				D			INFLIGHT SEPARATION       			LD	LANDING        	1			GL	03	107JD	90   				DM062				UPON LANDING, NOSE WHEEL DEPARTED THE AIRCRAFT SINKING IN LAKE MICHIGAN.  KIT MFG HAS RELATED THERE MAY BE A PROBLEM WIT	H THE NOSE GEAR FORK ASSY BROUGHT ON BY VIBRATION OR HARD LANDING.								0 										 
1999100100042	19991001	00042	CE  	1999	10	1	99ZZZX3666       	1	19990801	G	3230	ADNE5323	ROD END         			BEECH 	58    	58          	1152740	CE  										MLG	FAILED          	B	P		CGHR	A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			GL	03	1817S	6000 				TH1271				AFTER TAKEOFF, GEAR 'IN TRANSIT' LIGHT STAYED ON AFTER GEAR RETRACTION AND A 'POP' WAS HEARD.  GEAR CYCLED DOWN WITH 3 S	AFE ANNUNCIATORS.  AIRCRAFT LANDED SAFELY.  INSPECTION FOUND FAILED ROD END ON NOSE GEAR DRAG BRACE RETRACT ROD.  INSPEC	TION OF ROD ENDS AT SCHEDULED INSPECTIONS ESPECIALLY AROUND GREASE ZERK HOLE.				1	L	7	2 	3O				3A16    					 
1999100100201	19991001	00201	EA  	1999	10	1	99ZZZX3667       	2	19990831	G	8520	1065	DOWEL PIN       		61155135190 	PIPER 	PA28  	PA28140     	7102802	SO  	LYC   	O320  	O320E3D     	41508	EA  					CRANKSHAFT GEAR	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	09	5518U					2826231	L3928727A			REMOVED ENGINE ACCESSORY HOUSING FOR INSPECTION DUE TO ENGINE FAILURE.  CRANKSHAFT GEAR (PN 61155/13519646).  DOWEL PIN 	(P/N STD 1065) SHEARED.  CRANKSHAFT GEAR RETAINER BOLT LOOSE DUE TO ENGINE TORQUE RESULTING IN COMPLETE SHUT DOWN OF CAM	SHAFT AND ASSOCIATED EQUIPMENT.  TOTAL TIME OF ENGINE UNKNOWN DUE TO INCOMPLETE LOGS.  ENGINE MAJORED 10-29-89, NR 13346	41.  INSTALLED 12-11-89 ON ACFT  N2657T.  REMOVED FROM N2657T 10-5-92 WITH 851 HRS SMOH.  4-15-93 ENGINE RECEIVED TOP OV	ERHAUL NR 1334641.  9-22-95 ENGINE INSTALLED IN ACFT  N5518U WITH 85 HRS SMOH AND ZERO HRS STOH.		1	L	7	1 	3O	3	O		2A13    	E274				 
1999100100202	19991001	00202	CE  	1999	10	1	99ZZZX3668       	1	19990715	G	5312	05530311	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										FUSELAGE	CRACKED         	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	372ES					17280053				AIRCRAFT IN SHOP FOR S/B WORK.  FOUND FIREWALL HAD BEEN REPAIRED AT COWL MOUNTS.  FIRST MOUNT ON RIGHT AND LEFT SIDE, ON	 LOWER HALF OF FIREWALL.  SUBMITTER STATED 3 OUT OF 4 OF 172R'S HAVE BEEN CRACKED.					1	H	7	1 	3O			NT	3A12    					 
1999100100203	19991001	00203	CE  	1999	10	1	99ZZZX3669       	1	19990715	G	5312	05530311	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										FUSELAGE	CRACKED         	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	9968F	512  				17280208				AIRCRAFT IN SHOP FOR 100-HOUR INSPECTION.  REMOVED ENGINE COWL, FOUND FIREWALL CRACKED AT COWL MOUNT, FIRST MOUNT ON LEF	T AND SECOND MOUNT ON RIGHT SIDE ON LOWER HALF OF FIREWALL.  SB 98-53-024.					1	H	7	1 	3O			NT	3A12    					 
1999100100204	19991001	00204	SO  	1999	10	1	99ZZZX3670       	1	19990722	G	2840	486439	TRANSDUCER      			PIPER 	PA38  	PA38112     	7103812	SO  										FUEL PRESSURE	FAILED          	D	L			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	9974T	65   			28065	3878A0269				THIS IS THE THIRD FUEL PRESSURE TRANSDUCER FAILURE IN 5 MONTHS.  HAVING MAINTAINED PA-38 TOMAHAWKS FOR SEVERAL YEARS, FA	ILURE OF MANY FUEL PRESSURE TRANSDUCERS AND OIL PRESSURE TRANSDUCERS HAVE BEEN SEEN.  SUBMITTER STATED THE VIBRATION AND	 HEAT THAT THESE TRANSDUCERS ARE SUBJECTED TO IN THEIR ORIGINAL MOUNTING LOCATIONS ARE THE CAUSE.				1	L	7	1 	3O				A18SO   					 
1999100100205	19991001	00205	CE  	1999	10	1	99ZZZX3671       	1	19990715	G	5312	05530311	FIREWALL        			CESSNA	172   	172R        	2072401	CE  										FUSELAGE	CRACKED         	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	747KT	389  				17280020				AIRCRAFT IN SHOP FOR 100-HOUR INSPECTION.  REMOVED ENGINE COWL, FOUND FIREWALL CRACKED AT COWL MOUNT, FIRST MOUNT ON LEF	T SIDE ON LOWER HALF OF FIREWALL.  SB 98-53-02 R1 WAS C/W AT TACHOMETER , 195.0 HOURS.  NO CRACKS FOUND AT THAT TIME.  R	EPAIRED FIREWALL PER SB 98-53-02 R1.				1	H	7	1 	3O			NT	3A12    					 
1999100100206	19991001	00206	SO  	1999	10	1	99ZZZX3672       	1	19990607	G	3230	455180	CONTROL CABLE   			PIPER 	PA30  	PA30        	7103002	SO  										RT MLG	FRAYED          	B			JZRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	7746Y	3421 				3030837				UPON INSPECTION OF THE LANDING GEAR SYSTEM, THE RIGHT LANDING GEAR CABLE HAD A FRAYED INTERCABLE.  THIS FRAYED CABLE CAU	SED THE GEAR TO STOP IN TRANSIT TO THE ALMOST FULL DOWN POSITION, BUT NOT LOCKED. THIS WOULD HAVE CAUSED THE CIRCUIT BRE	AKER TO BLOW.  THE PILOT MAY HAVE THOUGHT THE GEAR WAS IN THE DOWN POSITION.  THE WEIGHT OF THE AIRCRAFT WOULD HAVE FORC	ED THE GEAR TO RETRACT.  THE AIR PRESSURE ON THE LANDING GEAR WOULD CAUSE THE PROBLEM.  SUBMITTER STATED THIS PROBLEM WI	LL LOCK EMERGENCY GEAR SYSTEM AND WILL NOT LET IT WORK.		1	L	7	2 	3O			 	A1EA    					 
1999100100207	19991001	00207	SO  	1999	10	1	99ZZZX3673       	1	19990528	G	3230	455180	CONTROL CABLE   			PIPER 	PA30  	PA30        	7103002	SO  										LT MLG	FRAYED          	B			JZRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	9NY	4102 				30739				UPON INSPECTION OF THIS LANDING GEAR SYSTEM, THE LEFT LANDING GEAR CABLE HAD A FRAYED INTERCABLE.  THIS FRAYED CABLE CAU	SED THE GEAR TO STOP INTRANSIT TO THE ALMOST FULL DOWN POSITION, BUT NOT LOCKED.  THIS WOULD HAVE CAUSED THE CIRCUIT BRE	AKER TO BLOW.  THE PILOT MAY HAVE THOUGHT THAT THE GEAR WAS IN THE DOWN POSITION.  THE WEIGHT OF THE AIRCRAFT WOULD HAVE	 FORCED THE GEAR TO RETRACT.  THE AIR PRESSURE ON THE GEAR WOULD CAUSE THE PROBLEM.  SUBMITTER STATED THIS PROBLEM WILL 	LOCK EMERGENCY GEAR SYSTEM AND WILL NOT LET IT WORK.		1	L	7	2 	3O			 	A1EA    					 
1999100100209	19991001	00209	CE  	1999	10	1	99ZZZX3675       	1	19990914	G	3230	1068100111	UPLOCK CABLE    			BEECH 	58    	58          	1152740	CE  										LT MLG	FRAYED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	48TX	2764 				TH1493				DURING MAINTENANCE, FOUND LT MAIN LANDING GEAR UPLOCK CABLE FRAYED LEAVING ONLY 1 CABLE STRAND CONNECTED.  THE FRAYING O	CCURRED AT THE INBOARD CABLE END ABOUT .125 INCHES FROM WHERE CABLE END IS ATTACHED TO CABLE.  NO OTHER RELATED FAILURE 	WAS NOTED.  CAUSE IS YET TO BE DETERMINED.				1	L	7	2 	3O			 	3A16    					 
1999100100210	19991001	00210	EA  	1999	10	1	99ZZZX3676       	2	19990907	G	8520	LW12440	CAMSHAFT        			PIPER 	PA31  	PA31P       	7103120	SO  	LYC   	O541  	TIGO541E1A  	41539	EA  					ENGINE	SPALLED         	B			EKIR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	110SK	100  				31P7630006	L13962			FOUND FERROUS METAL IN FILTER AND SCREEN DURING OIL CHANGE.  PULLED SUMP, FOUND CAMSHAFT LOBES AND LIFTERS WORN AND SPAL	LED.					1	L	7	2 	3O	3	O		A8EA    	E19EA				 
1999100100211	19991001	00211	EA  	1999	10	1	99ZZZX3677       	2	19990909	G	8520	75456	CRANSHAFT       			PIPER 	PA31  	PA31P       	7103120	SO  	LYC   	O541  	TIGO541E1A  	41539	EA  					ENGINE	CRACKED         	B			EKIR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	7652L	723  				31P7300129	L51162			REMOVED ENGINE DUE TO FERROUS METAL IN FILTER.  FOUND CAMSHAFT WORN AND LIFTER SPALLED.  UPON FURTHER INSPECTION, FOUND 	NR 4 COUNTERWEIGHT ATTACHMENT ON CRANKSHAFT CRACKED AT COUNTERWEIGHT BUSHING.  BUSHING HAS FOUR CRACKS.  NO LOG ENTRY OF	 PROPELLER STRIKE.				1	L	7	2 	3O	3	O		A8EA    	E19EA				 
1999100100212	19991001	00212	GL  	1999	10	1	99ZZZX3678       	1	19990820	G	3230		GEAR            			AMTR  	COZY  	COZY        	05613R8	GL  										NLG	WORN            	G				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			WP	23	795DB	297  				165				NOSE GEAR COLLAPSED DURING TAXI OPERATIONS AFTER LANDING AIRCRAFT.  SUBSEQUENT INVESTIGATION REVEALED DAMAGE AND EXCESS 	WEAR TO THE NOSE GEAR CRANK AND WORM GEAR ASSY.  POSSIBLE CAUSE OF PART DAMAGE LIKELY OCCURRED DURING A LANDING ATTEMPT 	WITH NOSE GEAR NOT FULLY EXTENDED INTO AN OVERCENTER AND LOCKED POSITION.  SUBMITTER RECOMMENDED PILOTS ENSURE THAT NOSE	 GEAR IS FULLY EXTENDED AND LOCKED PRIOR TO LANDING AIRCRAFT.			1	M	7	1 	3O			NT	EXPA1M71					 
1999100100213	19991001	00213	CE  	1999	10	1	99ZZZX3679       	1	19990909	G	2560	E0105	SWITCH          	ACK         		BOEING	75    	E75         	1380120	CE  										ELT	MISINSTALLED    	D				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	13	9077H				033198	758284				THE ACK TSOC91A ELT UNIT WAS ACTIVATED USING REMOTE SWITCH, BUT FAILED TO SHUT OFF WHEN USING THE RESET BUTTON.  FURTHER	 INSPECTION REVEALED THE RESET SWITCH WAS NOT SOLDERED TO THE CIRCUIT BOARD ON ONE OF THE TWO PINS.					1	Q	7	1 	3R				A743    					 
1999100100215	19991001	00215	EU  	1999	10	1	99ZZZX3681       	1	19990913	G	7920	31028501	LINE            			BAG   	JETSTM	JETSTM3101  	1500215	EU  	GARRTT	TPE331	TPE33110U   	01514	WP  					ENGINE	CRACKED         	B			CWQR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05	411MX					660				LINE CRACKED DUE TO RESONANT VIBRATION SET UP BY STARTER/GENERATOR.						2	L	7	2 	4T	4	T	RT	A21EU   	E4WE				 
1999100100216	19991001	00216	WP  	1999	10	1	99ZZZX3682       	2	19990902	G	7250	30740962	TURBINE ROTOR   			HWKSLY	DH125 	DH125400A   	4230140	EU  	GARRTT	TFE731	TFE7313     	01518	WP  					ENGINE	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	745TS	5930 				NA745	P84291			AT DISASSEMBLY FOR MAJOR PERIODIC INSPECTION. NOTED RUB ON FORWARD FACE OF LPT ROTOR IN ONE AREA OF THE ROOT SURFACE.  F	OUND 3RD STAGE LPT SEAL CAUSE OF RUB.  ALLIED SIGNAL HAS SUBMITTED SB 72-3654 FOR REWORK OF 3RD STAGE LPT SEAL TO CORREC	T PROBLEM.  LAST HOT SECTION ENTRY:  TT 5,220.3 HOURS.  CYCLES, 2,877.				2	L	7	2 	4J	4	F		A3EU    	E6WE				 
1999100100217	19991001	00217	SO  	1999	10	1	99ZZZX3683       	1	19990827	G	5511	46538024	SPAR            			PIPER 	PA31T 	PA31T       	7103124	SO  										HORIZ STABILIZER	CRACKED         	B	P	A	AU3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	15	20TN	4595 				31T7920019				DURING SCHEDULED INSPECTION, FOUND CRACK ON LEFT HORIZONTAL REAR SPAR WEB.  CRACK LOCATED AT BL 103.5 ETWEEN UPPER RIVET	 AND BONDING STRAP HOLE.  SPAR WEB REPAIRED IAW APPROVED DATA.					1	L	7	2 	3T				A8EA    					 
1999100100337	19991001	00337	SW  	1999	10	1	99ZZZX3707       	1	19990827	G	5312	26009121	BULKHEAD        			GULSTM	690TP 	690C        	7630517	SW  										MLG WW	CRACKED         	B	L	A	BOER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	67FE					11729				THIS AIRCRAFT IS JUST ONE OF FOUR THIS YEAR (OF THE SAME MAKE AND MODEL) THAT HAVE HAD STC SA 8214SW FROM THE COMMANDER 	SERVICE CENTER (REMOVAL OF THE CLAMSHELL DOORS) THAT WERE FOUND WITH LARGE CRACKS INSIDE THE WHEELWELL ON THE AFT BULKHE	AD.				1	H	7	2 	3T				2A4     					 
1999100100338	19991001	00338	SW  	1999	10	1	99ZZZX3708       	1	19990901	G	6320	204040783003	SPIDER          		212040001141	BELL  	212   	212         	1181420	SW  										TRANSMISSION	CRACKED         	B			GJQR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	82W	5822 	2313 		A1208826	31177				TRANSMISSION REMOVED FOR FERROUS METAL GENERATION.  INITIAL TEAR-DOWN INSPECTION REVEALED LOWER SPIDER GEAR CRACKED NEAR	 SPIDER LEG.  THIS CONDITION WAS PREVIOUSLY EMPHASIZED ASB 212-99-G1A REQUIRING A SPECIAL NDT MAGNAFLUX INSPECTION, ASB 	212-99-66 REV A WAS PREVIOUSLY C/W 2313.1 HOURS EARLIER WITH NDT MAGNAFLUX INSPECTION C/W AND NO EVIDENCE OF DEFECTS WER	E NOTED.			1	G	7	1 	4U				H4SW    					 
1999100100612	19991001	00612	NE  	1999	10	1	99ZZZX3709       	2	19990831	G	7230	30770492	DIFFUSER        								GARRTT	TFE731	TFE73131G   	01518	NE  					COMPRESSOR	CRACKED         	B			UO2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19					7P31078		P77473			FOUND SUBJECT PART CRACKED ON BACK FACE, 2 EACH CRACKS.  APPROXIMATELY AT THE 4 O'CLOCK POSITION.  CRACK LENGTH 1.0 INCH	 AND 0.75 INCH.  ALLIED SIGNAL HAS BEEN NOTIFIED.										4	F			E6WE				 
1999100100613	19991001	00613	GL  	1999	10	1	99ZZZX3710       	2	19990903	G	7250	23062750	NOZZLE SHIELD   								ALLSN 	250C  	250C20F     	03013	GL  					TURBINE	SEPARATED       	B			XZNR	O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			WP	07		899  			CAT40400		CAE840399			OPERATOR REPORTED ENGINE LOW POWER.  ON INVESTIGATION FOR LOW POWER, THE NR 1 NOZZLE SHIELD WAS FOUND WITH THE DOME COMP	LETLY SEPARATED FROM SHIELD INNER RING/BAND.  THIS FAILURE RESULTED IN DAMAGE TO NR 1 TURBINE NOZZLE WHICH MAY HAVE TO B	E SCRAPPED.  THIS FAILURE WAS PRIMARY CAUSE OF REPORTED LOW POWER.									3	U			E4CE				 
1999100100614	19991001	00614	CE  	1999	10	1	99ZZZX3711       	1	19990716	G	5531	1016400123	SPAR            			BEECH 	200   	200BEECH    	1152920	CE  										VERT STABILIZER	CRACKED         	B	P	A	UO2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	505AM	7972 				BB919				AFTER REMOVAL OF THE VERTICAL STABILIZER LEADING EDGE, THE LEFT HORIZONTAL STABILIZER ATTACH FITTING ATTACHED TO THE VER	TICAL STABILIZER FRONT SPAR WAS FOUND CRACKED.  IT ORIGINATED FROM THE BOTTOM HUCK BOLT HOLE, UPWARD AND ALONG SIDE THE 	NEXT HUCK BOLT AND SPREADING OUT IN 4 DIRECTIONS.				1	L	7	2 	4T				A24CE   					 
1999100100615	19991001	00615	NE  	1999	10	1	99ZZZX3712       	2	19990917	G	7250	2A0847	SEAL            								IAE   	V2500 	V2500A1     		NE  					NR 4 BEARING	CRACKED         	B			KB1R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NE	03					135A					PART RECEIVED PER SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501 FOR THE INTERNATIONAL AERO ENGINES V2500 	PROPULSION SYSTEM ENGINE MANUAL, REV 38.  PART REJECTED AT F.P.I. DUE TO 4 CRACKS ADJACENT TO MACHINED FLANGE; 0.020 INC	H, 0.025 INCH, 0.050 INCH, AND 0.060 INCH LONG.									4	F			E311NE				 
1999100100616	19991001	00616	SO  	1999	10	1	99ZZZX3713       	1	19990715	G	2430	DH31DA	RELAY           	HARTMAN     		GULSTM	G1159 	GIV         	3980115	SO  										TRU	SEPARATED       	G	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	99GA				CK30135	1198				RELAY 339A1K6 (AUX AC POWER) HAD A LOOSE C1 TERMINAL POST THAT RESULTED IN THE LOSS OF THE C-PHASE DURING EXTERNAL AC PO	WER OPERATION.  SYMPTOMS WERE LOW TRU OUTPUT VOLTAGE AND POOR BATTERY CHARGING.  WHEN REMOVING THE RELAY, TEMRINAL POST 	B1 SEPARATED FROM THE RELAY.  FAILED RELAY, HARTMAN P/N DH-31DA HAD BEEN PREVIOUSLY REPLACED FOR LOOSE TERMINALS THAT CA	USED APU POWER PROBLEMS.  A DIRECT REPLACEMENT OF THE HARTMAN RELAY IS LEACH P/N ZC-B3N-018.  THE -018 LEACH RELAY HAS I	MPROVED CONTACT RETENTION TO PREVENT SEPARATION.  THE LEACH RELAY WAS THE -018 P/N AND IS ALSO APPROVED FOR INSTALLATION	 IN THE POWER DIST BOX AS K1 (LAC2) AND K2 (RAC2) MAKING IT THE PREFERRED PART FOR SPARE STOCK.	2	L	7	2 	4F			RT	A12EA   					 
1999100100617	19991001	00617	SO  	1999	10	1	99ZZZX3714       	1	19990901	G	2120	476362	SENSOR          			GULSTM	G1159 	GIV         	3980115	SO  										AIR DISTRIBUTION	FAILED          	G	L			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	99GA					1198				INTERMITTENT IN-FLIGHT 'RUDDER KICK' AND BLEED AIR MANIFOLD TEMP SPLITS REPORTED.  TROUBLESHOOTING DID NOT REVEAL ANY PR	OBLEMS, A PHYSICAL INSPECTION OF FAN AIR SYS TEMP PROBES REVEALED A DEFECTIVE RT SIDE ANTICIPATOR 'LAGGED' ELEMENT HOUSI	NG.				2	L	7	2 	4F			RT	A12EA   					 
1999100100618	19991001	00618		1999	10	1	99ZZZX3715       	4	19990729	G	3416	066306200	ALTIMETER       			BEECH 	1900  	1900D       	1154162	CE  										COCKPIT	READS HIGH      	B			GLBR	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			CE	01	255GL		441  		3843	UE255				ALTIMETER FOUND TO BE INDICATING 50 FEET HIGH FROM 1,000 FEET TO 2,500 FEET.  ALL OTHER TEST POINTS WERE WITHIN LIMITS.						2	L	7	2 	4T			RT	A24CE   					 
1999100100619	19991001	00619	EU  	1999	10	1	99ZZZX3716       	1	19990909	G	3210	184811	CYLINDER        		1847E       	BAG   	JETSTM	JETSTM3201  	1500217	EU  										MLG	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	940AE				677	940				RADIUS ROD, PN 1847/E, SN LK-90001622 WAS SENT IN FOR SCHEDULED OVERHAUL.  FLUORESCENT PENETRANT INSPECTION OF CYLINDER,	 PN 184811, SN 677, REVEALED A CRACK INDICATION.   INDICATION APPEARS TO START AT THE EDGE OF THE UNDERCUT FOR THE DOWNL	OCK THREADS, AND PROGRESSES ON DOWN INSIDE THE BORE APPROXIMATELY 0.900 INCH, RUNNING ALONG THE FORGING FLASH LINE TOWAR	D THE MICROSWITCH MOUNTING BOSS.  SUBJECT CYLINDER HAS BEEN RETURNED TO APPH FOR INVESTIGATION.			2	L	7	2 	4T			RT	A56EU   					 
1999100100620	19991001	00620	EU  	1999	10	1	99ZZZX3717       	1	19990909	G	3213	101A703014	STRUT           		B00A702926A 	BAG   	JETSTM	JETSTM3101  	1500215	EU  										RT MLG	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05			8724 		BADL300					RIGHT MLG, PN B00A702926A, SN BADL-300, WAS SENT IN FOR SCHEDULED OVERHAUL.  MAGNETIC PARTICLE NDT INSPECTION OF SLIDE T	UBE, PN 101A703014, SN BA193 REVEALED AN INDICATION (CRACK) EXTENDING FROM THE TOP OF THE TUBE THROUGH THE HOLE FOR SOCK	ET SET SCREW, PN 741M1-4D, AND DOWN THE TUBE FOR AN ADDITIONAL 0.400 INCH.  SUBJECT SLIDE HAS BEEN REJECTED, AND WILL BE	 REPLACED.			2	L	7	2 	4T			RT	A21EU   					 
1999100100622	19991001	00622	EU  	1999	10	1	99ZZZX3719       	1	19990909	G	3250	618212	PISTON ROD      		61823       	BAG   	JETSTM	JETSTM3201  	1500217	EU  										NLG STEERING	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05					DHL365					NOSE LANDING GEAR STEERING JAC, PN 61823, SN SJA-400, WAS RETURNED FOR OVERHAUL.  INSPECTION REVEALED THE PISTON ROD, PN	 618212, SN DHL365, HAD BROKEN OFF AND A PORTION OF THE PISTON ROD WAS STILL THREADED ON THE END WHERE THE END FITTING I	S ATTACHED.  THIS PISTON ROD HAD FAILED AT THE TRANSITION RADIUS AT THE TERMINATION OF THE INSIDE DIAMETER THREADS ON TH	E END WHERE THE END FITTING IS ATTACHED.  TOTAL HOURS SINCE NEW AND SINCE OVERHAUL WERE NOT REPORTED.  FAILED PISTON ROD	 HAS BEEN RETURNED TO APPH FOR INVESTIGATION.		2	L	7	2 	4T			RT	A56EU   					 
1999100100623	19991001	00623	SO  	1999	10	1	99ZZZX3720       	1	19990917	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE	FAILED          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		1145 			0919A					BRAKE ASSY, PN 2-1585, FAILED PREMATURELY.  NR 2 STATOR BROKEN AND DAMAGED, TORQUE TUBE KEY SLOTS BEYOND SERVICEABLE LIM	ITS.  SUBMITTER STATED THIS IS A CONTINUAL DISCREPANCY AS BRAKE ASSY SHOULD LAST 2,500 CYCLES.  NOTE:  OEM PARTS INSTALL	ED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
1999100100624	19991001	00624	CE  	1999	10	1	99ZZZX3721       	1	19990915	G	2435		BEARING         	LUCAS       	23080005    	RAYTHN	DH125 	HAWKER800XP 		CE  										STARTER/GEN	FAILED          	B			UO2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	19	139M	513  			97015	258330				STARTER/GENERATOR FAILED IN-FLIGHT.  WHEN REMOVED, FOUND EXCESSIVE PLAY IN THE STARTER/GENERATOR SHAFT.  BEARING FAILURE	.  STARTER ORIGINALLY INSTALLED ON APU AND INSTALLED ON NR 1 ENGINE AT 375 HRS TSN, AFTER BRUSH CHANGE.  CURRENT OVERHAU	L REQUIREMENTS IS AT 1,000 HRS.				2	L	7	2 	4F			RT	A3EU    					 
1999100100625	19991001	00625		1999	10	1	99ZZZX3722       	4	19990722	G	2216		SERVO           		KS270C      	BEECH 	36    	A36         	1151604	CE  										PITCH TRIM	MALFUNCTIONED   	B	L		PAIR	O				OTHER                   				F			FLT CONT AFFECTED         			NR	NOT REPORTED   	1			SO	05	316P	20   			1949	E3237				DURING FLIGHT, AIRCRAFT HAD ABRUPT PITCH DOWN AND TRIM RAN AWAY CAUSING RAPID DESCENT.  PILOT DISENGAGED AUTOPILOT AND A	IRCRAFT HAD ABRUPT PITCH CHANGE.  TROUBLESHOOTING REVEALED BAD PITCH SERVO COMMANDING TRIM TO RUN.  AIRCRAFT PASSED GROU	ND SELF-TEST, YET UPON ENGAGEMENT, TRIM RUNS AWAY.  REPLACED PITCH SERVO AND FUNCTIONAL TESTED GOOD.				1	L	7	1 	3O				3A15    					 
1999100100626	19991001	00626	EA  	1999	10	1	99ZZZX3723       	2	19990824	G	7250		BLADE           			STBROS	SD3   	SD330       	8100602	EU  	PWA   	PT6   	PT6A45R     	52043	EA  					TURBINE	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	58DD	14919	3846 			SH3008	PCE84159			THIS IS A FOLLOW-UP REPORT FROM THE PT BLADE FAILURE ON THE LEFT SIDE OF 58DD.  THE ENGINE MODULE HAS BEEN CHANGED AND T	HE AIRCRAFT HAS BEEN RETURNED TO SERVICE.					2	H	7	2 	4T	4	T		A41EU   	E4EA				 
1999100100627	19991001	00627	NE  	1999	10	1	99ZZZX3724       	2	19990801	G	7310	20227	DISTRIBUTOR     			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					FUEL PRIMER	LEAKING         	E				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	99	9290Z		1068 			1387	17759			ENGINE PRIMER DISTRIBUTOR LEAKED FUEL WHEN ENGINE PRIMER WAS OPERATED.  AN 823-4D ELBOW FOUND EXTREMELY LOOSE IN DISTRIB	UTOR.  FITTING HAD SOMEHOW ELONGATED PIPE THREADED HOLE IN DISTRIBUTOR CAUSING FUEL LEAK DUE TO LOOSE FIT.					1	H	7	1 	3R	3	R		A806    	5E1				 
1999100100628	19991001	00628	NM  	1999	10	1	99ZZZX3725       	1	19990826	G	5230	69475141	FITTING         			BOEING	727   	727227      	1384078	NM  										CARGO DOOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON THE C-1 DOOR SUPPORT STRUT FITTING.						2	L	7	3 	4F				A3WE    					 
1999100100629	19991001	00629	NM  	1999	10	1	99ZZZX3726       	1	19990913	G	5313		STRINGER        			BOEING	737   	737247      	138448D	NM  										BS 907	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	902WC					19613				DURING A C-CHECK, CORROSION WAS NOTED BS 907 STR 29R.						2	L	7	2 	4F				A16WE   					 
1999100100630	19991001	00630	NM  	1999	10	1	99ZZZX3727       	1	19990913	G	5347		ANGLE           			BOEING	737   	737247      	138448D	NM  										APU DOOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	902WC					19613				DURING A C-CHECK, CORROSION WAS NOTED AT APU ACCESS DOOR, LT FORWARD CORNER, ZEE ANGLE.						2	L	7	2 	4F				A16WE   					 
1999100100631	19991001	00631	NM  	1999	10	1	99ZZZX3728       	1	19990913	G	5320		SUPPORT         			BOEING	737   	737247      	138448D	NM  										BS 293	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	902WC					19613				DURING A C-CHECK, CORROSION WAS NOTED ON FLOOR SUPPORT STA 293, LBL 15 FOR FORWARD LAVATORY, AFT WALL.						2	L	7	2 	4F				A16WE   					 
1999100100632	19991001	00632	NM  	1999	10	1	99ZZZX3729       	1	19990913	G	5320		ANGLE           			BOEING	737   	737247      	138448D	NM  										NLG WW	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	902WC					19613				DURING A C-CHECK, CORROSION WAS NOTED ON LEFT AFT CORNER N/WH/W.						2	L	7	2 	4F				A16WE   					 
1999100100633	19991001	00633	NM  	1999	10	1	99ZZZX3730       	1	19990913	G	5320		SUPPORT         			BOEING	737   	737247      	138448D	NM  										BS 946-966	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	902WC					19613				DURING A C-CHECK, CORROSION WAS NOTED AT BS 946 - BS 966, RBL 15 FLOOR SUPPORT.						2	L	7	2 	4F				A16WE   					 
1999100100634	19991001	00634		1999	10	1	99ZZZX3731       	4	19990916	G	2312	D110028000	TRANSCEIVER     			PIPER 	PA60  	PA60600     	7106001	NM  										VHF COMM	FAILED          	B			ERY3	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	09	35NB				96302865	600839816124				OUT OF THE BOX FAILURE OF VHF COMM SIDE OF UNIT.  GOOD TRANSMIT, BUT NO RECUR AUDIO PRESENT IN SPEAKER OR HEADSET.						1	M	7	2 	3O			RT	A17WE   					 
1999100100635	19991001	00635	CE  	1999	10	1	99ZZZX3732       	1	19990910	G	3230	582212715	ANGLE           			CESSNA	441   	441         	2076020	CE  										RT MLG	CRACKED         	B	P		WTXR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	441TF	10709				4410072				DURING A PHASE INSPECTION, A CRACK WAS FOUND IN THE OUTBOARD END OF THE RIGHT AND LEFT MAIN GEAR UPLOCK HOOK SUPPORT ANG	LE THAT IS ATTACHED TO THE FORWARD WING SPAR WEB.  THE CRACKS ORIGINATE AT THE OUTBOARD HILOCK HOLE AND EXTENDS FOR A TO	TAL LENGTH OF 1.5 INCHES.  NEW ANGLES WERE INSTALLED.				1	L	7	2 	3T			RT	A28CE   					 
1999100100636	19991001	00636	CE  	1999	10	1	99ZZZX3733       	1	19990910	G	3230	582212716	ANGLE           			CESSNA	441   	441         	2076020	CE  										LT MLG	CRACKED         	B			WTXR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	441TF	10709				4410072				DURING A PHASE INSPECTION, A CRACK WAS FOUND IN THE OUTBOARD END OF THE RIGHT AND LEFT MAIN GEAR UPLOCK HOOK SUPPORT ANG	LE THAT IS ATTACHED TO THE FORWARD WING SPAR WEB.  THE CRACKS ORIGINATE AT THE OUTBOARD HILOCK HOLE AND EXTENDS FOR A TO	TAL LENGTH OF 1.5 INCHES.  NEW ANGLES WERE INSTALLED.				1	L	7	2 	3T			RT	A28CE   					 
1999100100637	19991001	00637	SO  	1999	10	1	99ZZZX3734       	1	19990901	G	2130	13048221	SELECTOR        			GULSTM	G1159 	GIV         	3980115	SO  										CABIN PRESSURE	MALFUNCTIONED   	G	L			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	99GA					1198				CABIN PRESSURIZATION SELECTOR.  LANDING ALTITUDE TAPE FAILED.  TAPE/RHEOSTAT SLIPPED INTERNALLY.  TAPE DISPLAYED A DIFFE	RENT ALTITUDE THAN WAS BEING CONTROLLED; THERE WAS APPROX 1,000 FOOT ERROR.  THIS ERROR CAUSED CABIN ALTITUDE AT LANDING	 TO BE APPROX 1,400 FEET BELOW FIELD ELEVATION.  THE CONCERN IS THE ACFT IS PRESSURIZED GREATER THAN NORMAL AND PLUG TYP	E EMERGENCY EXIT WINDOWS AND DOORS CANNOT BE OPENED UNTIL THE PRESSURIZATION IS EQUALIZED.			2	L	7	2 	4F			RT	A12EA   					 
1999100100638	19991001	00638		1999	10	1	99ZZZX3735       	4	19990821	G	2312	3722519040	CONNECTOR       			GULSTM	G1159 	GIV         	3980115	SO  										VHF COMM	FAILED          	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	99GA					1198				INTERMITTENT VHF COMMUNCATION RECEPTION DURING TAXI, TAKEOFF, AND LANDING.  TROUBLESHOOTING REVEALED A 'COLD SOLDER JOIN	T' BETWEEN CENTER CONNECTION AND ANTENNA COAX CABLE CENTER CONDUCTOR.					2	L	7	2 	4F			RT	A12EA   					 
1999100100641	19991001	00641	CE  	1999	10	1	99ZZZX3738       	1	19990924	G	2510	08127761	SEAT            			CESSNA	310   	310R        	2074245	CE  										COCKPIT	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	1203W	7550 				310R2106				DURING ANNUAL INSPECTION, FOUND PILOT AND COPILOT SEAT BACK PIVOT SUPPORTS CRACKED.  CAUSED BY PUSHING ON TOP OF SEAT BA	CK WHILE ENTERING/EXITING AIRCRAFT.					1	L	7	2 	3O				3A10    					 
1999100100642	19991001	00642	CE  	1999	10	1	99ZZZX3739       	1	19990924	G	3221	081308947	MOUNT           			CESSNA	310   	310R        	2074245	CE  										NLG	CRACKED         	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	1203W	7550 			7P31078	310R2106				DURING ANNUAL INSPECTION, FOUND LEFT NOSE CAM TRUNNION MOUNT DOUBLER CRACKED AT FORWARD TOP RIVET HOLE EXTENDING AFT ABO	UT 1 INCH.  SUBMITTER HAS FOUND THIS SAME BRACKET CRACKED IN SAME LOCATION ON SEVERAL 310R MODEL AIRCRAFT.  ALSO, THE RI	GHT DOUBLER, PN 0813089-47, HAS BEEN FOUND CRACKED AT SAME RIVET HOLE.				1	L	7	2 	3O				3A10    					 
1999100800025	19991008	00025	CE  	1999	10	8	99ZZZX3741       	1	19990906	G	7820	085183841	BRACKET         			CESSNA	402   	402C        	207590R	CE  										RT ENGINE	BROKEN          	C		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	1376G					402C0271				ON RT ENGINE START, PILOT NOTICED SMOKE FROM RT COWL, SHUT DOWN ENGINE PER NORMAL PROCEDURE AND EVACUATED PASSENGERS.  M	AINTENANCE FOUND ALTERNATOR POWER CABLE CHAFED BY BROKEN ENGINE BAFFLE BRACKET.  REPAIRED BRACKET, REPAIRED MINOR COWL D	AMAGE, AND ALTERNATOR POWER CABLE.  RELEASED AIRCRAFT BACK TO SERVICE.				1	L	7	2 	3O				A7CE    					 
1999100800026	19991008	00026	SO  	1999	10	8	99ZZZX3742       	1	19990907	G	7120	3512220	MOUNT           		AN626A      	PIPER 	PA28  	PA28161     	7102803	SO  										ENGINE	LOOSE           	B				O				OTHER                   				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			GL	21	252ND	837  				2842043				PILOT REPORTED VIBRATION AT START-UP AND SHUT DOWN.  INSPECTION FOUND RT LOWER ENGINE MOUNT TO FIREWALL BOLT LOOSE.  FUR	THER INSPECTION FOUND BOLT GRIP LENGTH TOO LONG AND NUT BOTTOMED ON THREADS.  ADDED WASHER UNDER NUT TO TAKE UP SPACE. R	ESEARCH OF RECORDS FOUND BOLT HAD NEVER BEEN REMOVED OR REPLACED.				1	L	7	1 	3O				2A13    					 
1999100800027	19991008	00027	SW  	1999	10	8	99ZZZX3743       	1	19990917	G	2621	130835	CARTRIDGE       			GULSTM	560   	560         	0141402	SW  										FIRE EXTINGUISH	FAILED          	B				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	25	3760S					5600276				DURING SCHEUDLED REMOVAL PROCESS OF THIS PART, IT WAS FOUND TO BE INOPERATIVE.  AIRCRAFT WAS SCHEDULED FOR FIRE EXTINGUI	SHER CARTRIDGE TIME REPLACEMENT.  THIS FACILITY DISCHARES ALL FIRE EXTINGUISHER CHARGES PRIOR TO DISPOSAL.					1	H	7	2 	3O				6A1     					 
1999100800028	19991008	00028	EA  	1999	10	8	99ZZZX3744       	2	19990827	G	8530		ROCKER BOSS     			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  					NR 3 CYLINDER	FAILED          	D				A				UNSCHED LANDING         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CR	CRUISE         	1			EA	25	68322		100  			15282256				CRUISE, LEVEL FLIGHT, ENGINE STARTED RUNNING VERY ROUGH; INSTRUCTOR LANDED SAFE IN GRASS FIELD.  INSPECTION REVEALED NR 	3 CYLINDER ROCKER SHAFT BOSS BROKEN OFF.  ENGINE HAD 100 HRS TIS FROM MAJOR OVERHAUL.					1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999100800030	19991008	00030	EA  	1999	10	8	99ZZZX3746       	2	19990706	G	7314	LW15472	PUMP            			BNORM 	BN2   	BN2B26      	1520350	EU  	LYC   	O540  	O540E4C5    	41532	EA  					LT ENGINE	FAILED          	H				O				OTHER                   				J			WARNING INDICATION        			CL	CLIMB          	1			SO	21	861VL	1291 			3296	2155	L1546840C			AFTER TAKEOFF, LEFT ENGINE SURGED.  PILOT NOTICED FUEL PRESSURE DROP.  PERFORMED PROCEDURES, ELECTRICAL FUEL PUMP ACTIVA	TED, ENGINE CONTINUOUS WORKING NORMAL WHEN FUEL PRESSURE INCREASED.					1	H	7	2 	3O	3	O	RT	A17EU   	E295				 
1999100800031	19991008	00031	CE  	1999	10	8	99ZZZX3747       	1	19990802	G	3230	25430121	BELLCRANK       			CESSNA	303   	T303        	2073820	CE  										NLG	CRACKED         	D	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	05	9730T					T30300040				CRACKS FOUND IN BELLCRANK RADIUS.						1	L	7	2 	3O				A34CE   					 
1999100800033	19991008	00033	EA  	1999	10	8	99ZZZX3749       	2	19990820	G	7414	4370	MAGNETO         	SLICK       		CESSNA	172   	172N        	2072434	CE  	LYC   	O360  	O360A4M     	41514	EA  					ENGINE	FAILED          	B			A5OR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	09	6606D	678  			96030135	17272893	L3499736A			PILOT REPORTED THE AIRCRAFT WAS HARD TO START AFTER ENGINE WARMED UP.  TROUBLESHOT SYSTEM AND FOUND RT MAGNETO RUNNING R	OUGH.  MAGNETO ONLY HAD 678 HOURS SINCE NEW.					1	H	7	1 	3O	3	O	NT	3A12    	E286				 
1999100800034	19991008	00034	SO  	1999	10	8	99ZZZX3750       	2	19990819	G	8530	SA643873	VALVE           			CESSNA	210   	T210F       	2073422	CE  	CONT  	O520  	TSIO520C    	17040	SO  					ENGINE	FAILED          	B	L		A5OR	A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			AP	APPROACH       	1			SO	09	6170R	769  				T2100070	178241R			DURING DESCENT FROM ALTITUDE AFTER A 2 HOUR CROSS COUNTRY FLIGHT AND 10 MILES FROM HOME BASE, THE ENGINE BEGAN TO RUN RO	UGH. DESCENT WAS STOPPED AT 2.500 FEET TILL A SAFE LANDING WAS ASSURED.  THE ENGINE, ALTHOUGH RUNNING ROUGH, RAN WITH GO	OD OIL PRESSURE AND NORMAL OIL TEMPERATURE.  EMERGENCY CHECKS DISCOUNTED IGNITION AND FUEL PROBLEMS.  SUSPECTED A STUCK 	OR BROKEN VALVE.  A SAFE LANDING WAS MADE WITHOUT INCIDENT.  UPON INSPECTION, THE NR 2 CYLINDER SPARK PLUG SHOWED SIGNS 	OF MECHANICAL DAMAGE.  THE CYLINDER WAS REMOVED AND CONFIRMED THAT APPROXIMATELY ONE-THIRD OF THE EXHAUST VALVE HEAD HAD	 BROKEN OFF.  THE BROKEN LOOSE PART DID CONSIDERABLE DAMAGE TO THE TOP OF THE CYLINDER HEAD, PISTON, AND SPARK PLUGS.	1	H	7	1 	3O	3	O		3A21    	E8CE				 
1999100800035	19991008	00035	EA  	1999	10	8	99ZZZX3751       	2	19990922	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					NOSE	MALFUNCTIONED   	H				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			DE	DESCENT        	1			SW	99	406ER					18080297	L2731951A			THE AIRCRAFT WAS ON A TRAINING FLIGHT IN A HOLDING PATTERN.  THE ENGINE LOST ABOUT 400 RPM'S FOR ABOUT THREE SECONDS.  T	HE INSTRUCTOR TOOK OVER CONTROL AND APPLIED POWER.  IT WAS THEN THAT THE POWER RETURNED.  SUBMITTER STATED THERE HAVE BE	EN NUMEROUS UNEXPLAINED POWER LOSSES IN THIS FLEET OF 53 172R MODEL AIRCRAFT.				1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999100800036	19991008	00036	EA  	1999	10	8	99ZZZX3752       	2	19990919	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					NOSE	MALFUNCTIONED   	H				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			AP	APPROACH       	1			SW	99	409ER					17280253	L2724051A			ON FINAL (2 MILES) AT 650 FEET FOR RUNWAY 29 AT EVB, EXPERIENCED ABOUT 300-400 RPM LOSS IN ENGINE POWER ('MIXTURE LEANED	 BP ON").  APPLIED FULL RICH MIXTURE AND TRIED TO INCREASE POWER BUT ENGINE RPM STAYED AT 17-1800 RPM WITH FULL THROTTLE	 FOR ABOUT 5 SECONDS.   WHILE THE ENGINE WAS RUNNING VERY ROUGH, PULLED THROTTLE SLOWLY BACK AND INCREASED IT SLOWLY.  E	NIGNE RPM SLOWLY INCREASED BACK TO 2,200 RPM WHILE THE ENGINE WAS STILL SLIGHTLY ROUGH.  CLIMBED TO 2,000 FEET AND RETUR	NED TO DAB.		1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999100800037	19991008	00037	SW  	1999	10	8	99ZZZX3753       	1	19990907	G	6340	407375001105	INDICATOR       			BELL  	407   	407         		SW  										COCKPIT	MALFUNCTIONED   	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	62LH	486  			0063	53045				REPLACED WITH NEW INDICATOR FROM BELL HELICOPTER.						1	G	7	1 	3U			O	H2SW    					 
1999100800039	19991008	00039		1999	10	8	99ZZZX3755       	4	19990914	G	6113	D6199	BULKHEAD        			MOONEY	M20   	M20M        	5870222	SW  										SPINNER	CRACKED         	B	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	09	2168J	33   				270265				UNABLE TO DETERMINE EXACTLY WHAT THE CAUSE FOR CRACKS WAS; AREA POINTED OUT ON PHOTO NR 1 IS WHERE A BOWED AREA BETWEEN 	MOUNTING SCREWS WAS FOUND.  FOUND THIS AT 3 PLACES.  ALSO, FOUND PLASTIC FORWARD SPINNER BULKHEAD NEEDED TO BE SHIMMED F	ORWARD WHEN INSTALLING NEW ASSEMBLY.				1	L	7	1 	3O			RT	2A3     					 
1999100800040	19991008	00040	GL  	1999	10	8	99ZZZX3756       	3	19990903	G	6114		HUB             			CESSNA	337   	337C        	2075712	CE  						MCAULY	2AF34C	D2AF34C61   	GL  	PROPELLER	CRACKED         	B			LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	2577S	3241 				3370877		684820		DURING INITIAL VISUAL INSPECTION, FOUND CRACK IN HUB.						1	H	7	2 	3O				A6CE    		5	C	P5EA	 
1999100800041	19991008	00041	GL  	1999	10	8	99ZZZX3757       	3	19990903	G	6110	C4903	LOCKNUT         			CESSNA	337   	337C        	2075712	CE  						MCAULY	2AF34C	D2AF34C61   	GL  	PROPELLER	CRACKED         	B			LU4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	2577S	3241 				3370877		684820		PART FAILED EDDY CURRENT INSPECTION.						1	H	7	2 	3O				A6CE    		5	C	P5EA	 
1999100800042	19991008	00042	SO  	1999	10	8	99ZZZX3758       	1	19990919	G	3246		WHEEL           			PIPER 	PA32  	PA32R300    	7103213	SO  										RT MLG	FRACTURED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	38171	6713 				32R7780392				DURING ANNUAL INSPECTION, INBOARD HALF OF RIGHT MAIN LANDING GEAR WHEEL WAS FOUND TO HAVE AN APPROXIMATE 2 SQUARE INCH P	IECE MISSING.  NO EVIDENCE OF ABUSE DURING TIRE CHANGE, ETC., WAS EVIDENT.					1	L	7	1 	3O				A3SO    					 
1999100800043	19991008	00043	CE  	1999	10	8	99ZZZX3759       	1	19990912	G	3246	11580014	WHEEL ASSY      			BEECH 	100   	B100        	1152919	CE  										LT MLG	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	23	136MB				A0194	BE50				UPON ROUTINE CLEANING OF THE AIRCRAFT, A CRACK WAS DISCOVERED ALONG THE OUTBOARD END RADIUS OF THE INBOARD WHEEL HALF RU	NNING HORIZONTALLY APPROXIMATELY 3.75 INCHES.  THE WHEEL WAS MOUNTED ON THE INBOARD LEFT MAIN POSITION.  THE WHEEL HALF 	WAS MANUFACTURED IN FEBRUARY, 1989, AND INSTALLED NEW ON THE AIRCRAFT IN JUNE, 1990, ACCUMULATING APPROXIMATELY 2,563 LA	NDINGS.			1	L	7	2 	4T				A14CE   					 
1999100800044	19991008	00044	SO  	1999	10	8	99ZZZX3760       	1	19990921	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										NR 1 & NR 2	DEFECTIVE       	B		A	XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		671  			0208					BRAKE ASSY,PN 2-1585, FAILED PREMATURELY.  NR 1 STATOR OVERHEATED.  NR 2 STATOR BROKEN IN 4 PIECES AND DAMAGED TORQUE TU	BE KEY SLOTS.  THIS IS A CONTINUAL DISCREPANCY.  SUBMITTER STATED BRAKE ASSY SHOULD LAST 2,500 CYCLES.					2	L	7	2 	4T			RT	A31SO   					 
1999100800045	19991008	00045	SO  	1999	10	8	99ZZZX3761       	1	19990922	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										NR 1	DEFECTIVE       	B		A	XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		1869 			1430A					BRAKE ASSY, PN 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE KEY SLOTS.  THIS IS A CONTI	NUAL DISCREPANCY.  SUBMITTER STATED BRAKE ASSY SHOULD LAST 2,500 CYCLES,  NOTE:  OEM PARTS INSTALLED IN BRAKE ASSY AND T	HE MOST RECENT BRAKE CONFIGURATION, P/N 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
1999100800046	19991008	00046	SO  	1999	10	8	99ZZZX3762       	1	19990922	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										NR 1	DEFECTIVE       	B		A	XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		1979 			0288A					BRAKE ASSY, PN 2-1585, FAILED PREMATURELY.  NR 1 STATOR CRACKED AND BINDING IN TORQUE TUBE KEY SLOTS, HEAT STACK WARPED.	 THIS IS A CONTINUAL DISCREPANCY.  SUBMITTER STATED BRAKE ASSEMBLY SHOULD LAST 2,500 CYCLES.  NOTE:  OEM PARTS INSTALLED	 IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATION, PN 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
1999100800047	19991008	00047	SO  	1999	10	8	99ZZZX3763       	1	19990921	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										NR 1	DEFECTIVE       	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		2882 			0353A					BRAKE ASSY, PN 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE TUBE KEY SLOTS.  SUBMITTER 	STATED THIS IS A CONTINUAL DISCREPANCY.  NOTE:  OEM PARTS INSTALLED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATIO	N, PN 2-1585.  NOTE: OEM PARTS INSTALLED IN BRAKE ASSY AND THE  MOST RECENT BRAKE CONFIGURATION, PN 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
1999100800048	19991008	00048	EU  	1999	10	8	99ZZZX3764       	1	19990903	G	2120	188628	ACM             	AIRESRCH    		ISRAEL	1124  	1124        	4500102	EU  										AIR DIST	CRACKED         	B	P		JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	274K					274				CRACK IN THE WELD BETWEEN THE HOT AND COLD AIR PLENUMS ON THE ACM.  SUBMITTER STATED THIS DEFECT AREA NEEDS TO BE ADDED 	TO THE INSPECTION GUIDES OF THE WESTWIND. THIS SAME PROBLEM HAS BEEN FOUND ON AT LEAST 6 OTHER WESTWINDS.  ACFT TT:  796	0.6 HOURS.				2	M	7	2 	4F				A2SW    					 
1999100800049	19991008	00049	CE  	1999	10	8	99ZZZX3765       	1	19990903	G	3230	62171027	UPLOCK          			CESSNA	650   	650         	2076802	CE  										LT MLG	LOOSE           	B	P		JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	654EJ	1949 				6507070				DURING INSPECTION, FOUND LT MLG UPLOCK ASSY LOOSE IN AIRCRAFT STRUCTURE.  ALL 4 BOLTS (AN4-7A) WERE LOOSE.  NO SAFETY DE	VICE OTHER THAN SELF-LOCKING NUTPLATE (MS21069L4).  TORQUED BOLTS AND APPLIED LOCTITE 271 THREAD LOCKER.  FOUND RT UPLOC	K ASSY SECURE, BUT BOLTS ALSO UNDER TORQUED.				2	L	7	2 	4F				A9NM    					 
1999100800050	19991008	00050	CE  	1999	10	8	99ZZZX3766       	1	19990903	G	3230	62171026	UPLOCK          			CESSNA	650   	650         	2076802	CE  										RT MLG	LOOSE           	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	654EJ	1949 				6507070				DURING INSPECTION, FOUND LT MLG UPLOCK ASSY LOOSE IN AIRCRAFT STRUCTURE.  ALL 4 BOLTS (AN4-7A) WERE LOOSE.  NO SAFETY DE	VICE OTHER THAN THAN SELF-LOCKING NUTPLATE (MS21069L4).  TORQUED BOLTS AND APPLIED LOCTITE 271 THREAD LOCKER.  FOUND RT 	UPLOCK ASSY SECURE, BUT BOLTS ALSO UNDER TORQUED.				2	L	7	2 	4F				A9NM    					 
1999012200747	19990122	00747		1999	1	22	99ZZZX378        	4	19990104	G	2562	300011	ELT             	POINTER     		CESSNA	172   	172R        	2072401	CE  										CABIN	MALFUNCTIONED   	B			EIPR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	9713F				324721	17280018				REMOTE ELT SWITCH DID NOT ACTIVATE ELT.  SUBMITTER TALKED WITH FACTORY.  FOUND CESSNA USED CIRCUIT TESTER AND BLEW INTER	NAL FUSES IN ELT.  TESTED ELT AND SWITCH WIRING PER FACTORY.  SENT IN ELT'S TO FACTORY TO HAVE HIGHER AMP FUSES INSTALLE	D.				1	H	7	1 	3O			NT	3A12    					 
1999100800408	19991008	00408	EU  	1999	10	8	99ZZZX3808       	1	19990903	G	3246	TIMKEN	BEARING         	DUNLOP      	AH43221     	BRAERO	DH125 	HS125700A   	4230170	EU  										NR 2 MLG	DESTROYED       	B			LJCR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	23EJ	4352 				NA0340				DAMAGED NR 2 MAIN WHEEL NOTED AFTER LANDING.  EXAMINATION REVEALED LOCKED OUTBOARD BEARING RESULTING IN DAMAGE BEYOND AL	LOWABLE LIMITS TO NR 2 WHEEL, LEFT AXLE ASSY AND NR 2 MAXERET ASSY.  THERE WAS NO INDICATION OF THE WHEEL BEARINGS HAVIN	G BEEN LUCRICATED AT LAST INSTALL.  DAMAGED BEARING DID NOT BEAR CLASS RATING PREFIX OR THE MANUFACTURER'S '-629' AIRCRA	FT ENDORSEMENT; ONLY THE PREVIOUSLY RECOGNIZED BASE, P/N L610549.			2	L	7	2 	4F				A3EU    					 
1999100800409	19991008	00409	WP  	1999	10	8	99ZZZX3809       	1	19990917	G	5753		FITTING         		57511752    	DOUG  	DC8   	DC871F      	302199D	WP  										TE FLAP	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	8079U				CCI242	45947				FITTING CRACKED MORE THAN 90 PERCENT OF FITTING AT FLAP ATTACH POINT,  DEFECT NOTED DURING FLAP OVERHAUL.  FLAP RECEIVED	 FOR OVERHAUL DUE TO AIRCRAFT IN D-CHECK.					2	L	7	4 	4F			RT	4A25    					 
1999012200750	19990122	00750	EA  	1999	1	22	99ZZZX381        	2	19990106	G	8530		VALVE           								LYC   	O360  	O360A4A     	41514	EA  					NR 3 CYLINDER	BROKE           	H	L			A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			SO	11							L2011536A			PILOT REPORTED SUDDEN PARTIAL LOSS OF POWER, ENG RUNNING ROUGH.  SWITCHED MAGS AND APPLICATION OF CARB HEAT, NO HELP.  C	ONTINUED FLT TO HOME AIRPORT, MADE SUCCESSFUL LANDING.  POWER REDUCED AFTER LANDING, ENG QUIT, COULD NOT BE RE-STARTED. 	 INSP NR 3 CYL, NO COMPRESSION, EXHAUST VALVE MISSING.  VALVE HAD BROKEN AT THE STEM AND DAMAGED CYL HEAD, WALL, AND PIS	TON.  CYL REPLACED.  NR 1 CYL REMOVED AND EXHAUST VALVE CHECKED.  VALVE FOUND TO HAVE UNSERVICEABLE PITTING.  NR 2 AND N	R 4 CYLS REMOVED, NO ABNORMALITIES FOUND ON VALVES.  NR 4 CYL FOUND CRACKED, REPLACED.  OIL ANALYSIS MADE,  NO CONTAMINA	TION.  ENG INSTALLED NEW IN 1975, TT 1,683.53 HRS.  NO RECORD OF CYL MAINT, INDICATION OF LONG PERIODS OF INACTIVITY.						3	O			E286				 
1999100800410	19991008	00410	NM  	1999	10	8	99ZZZX3810       	1	19990912	G	3244		TIRE            			DOUG  	MD11  	MD11F       	3023600	NM  										NLG	FAILED          	B			GK4Y	O				OTHER                   				O			OTHER                     			CL	CLIMB          	1			WP	03	612FE					48605				HNL - FLIGHT CREW HEARD LOUD BANG ON GEAR RETRACTION AFTER TAKEOFF.  ON ARRIVAL NAN, RT NOSE WHEEL TREAD WAS FOUND SEPAR	ATED AND CAUSED DAMAGE TO RT GLIDE PATH ANTENNA, ILS REFLECTOR AND NOSE WHEELWELL CEILING INSULATION BLANKET.  RIGHT NOS	E WHEEL REPLACED, PORTION OF BLANKET REMOVED AND NR 2 ILS SYSTEM ON MEL.  AIRCRAFT RETURNED TO SERVICE.				2	L	7	3 	4F			RT	A22WE   					 
1999100800411	19991008	00411	SW  	1999	10	8	99ZZZX3811       	1	19990901	G	2810		FUEL CELL       			MOONEY	M20   	M20R        	5870225	SW  										RT WING	LEAKING         	B			W45R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	07	2155K					290164				FUEL LEAK AT RIGHT WING INBOARD WING ATTACH POINT.  ALSO, LEAKING AT FORWARD WING WALK AT INBOARD SCREWS.						1	L	7	1 	3O			RT	2A3     					 
1999100800412	19991008	00412	SO  	1999	10	8	99ZZZX3812       	1	19990901	G	5753	6232401	FLAP ATTACH     			PIPER 	PA28  	PA28140     	7102802	SO  										TE FLAP	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	14	32687					287525098				RIGHT FLAP MIDDLE AND OUTBOARD ATTACH POINTS CORRODED AND SEPARATED FROM FLAP.  INBOARD ATTACHMENT STAYED ON FLAP.						1	L	7	1 	3O				2A13    					 
1999100800413	19991008	00413	SO  	1999	10	8	99ZZZX3813       	1	19990901	G	5753	6589900	FLAP ATTACH     			PIPER 	PA28  	PA28140     	7102802	SO  										TE FLAP	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	14	32687					287525098				RIGHT FLAP MIDDLE AND OUTBOARD ATTACH POINTS CORRODED AND SEPARATED FROM FLAP.  INBOARD ATTACHMENT STAYED ON FLAP.						1	L	7	1 	3O				2A13    					 
1999100800414	19991008	00414	NE  	1999	10	8	99ZZZX3814       	1	19990920	G	7160	7630207028061	SCREEN          			SKRSKY	S76   	S76C        	8143008	NE  										ENG COWL INLET	BROKEN          	D	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	1WB	142  				760500				DURING POST-FLIGHT CHECK OF NR 1 ENGINE, THE INLET COMPRESSOR WAS FOUND WITH FOD DAMAGE.  THE FOD DAMAGE WAS BEYOND ENGI	NE MANUFACTURER LIMITS.  MAINTENANCE AND FLIGHT CREWS INSPECTED THE AIRCRAFT'S NR 1 ENGINE INLET PLENUM TO DETERMINE WHE	RE THE SOURCE OF FOD CAME FROM.  CREWS FOUND THE ENGINE ARIFRAME COWL PLENUM SCREEN HAD MISSING WIRE SEGMENTS.  THIS WAS	 THE SOURCE OF ENGINE FOD INGESTION.  ENGINE COWL SCREENS SHOULD BE INSPECTED DAILY UNTIL THE AIRFRAME MANUFACTURER PROD	UCES A MORE RELIABLE REPLACEMENT.		1	G	7	2 	3U			NC	H1NE    					 
1999100800415	19991008	00415	NE  	1999	10	8	99ZZZX3815       	1	19990920	G	7160	7630207028062	SCREEN          			SKRSKY	S76   	S76C        	8143008	NE  										ENG COWL INLET	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	1WB	142  				760500				DURING POST-FLIGHT CHECK OF NR 1 ENGINE, THE INLET COMPRESSOR WAS FOUND WITH FOD DAMAGE.  THE FOD DAMAGE WAS BEYOND ENGI	NE MANUFACTURER LIMITS.  MAINTENANCE AND FLIGHT CREWS INSPECTED THE AIRCRAFT'S NR 1 ENGINE INLET PLENUM TO DETERMINE WHE	RE THE SOURCE OF FOD CAME FROM.  CREWS FOUND THE ENGINE ARIFRAME COWL PLENUM SCREEN HAD MISSING WIRE SEGMENTS.  THIS WAS	 THE SOURCE OF ENGINE FOD INGESTION.  ENGINE COWL SCREENS SHOULD BE INSPECTED DAILY UNTIL THE AIRFRAME MANUFACTURER PROD	UCES A MORE RELIABLE REPLACEMENT.		1	G	7	2 	3U			NC	H1NE    					 
1999100800416	19991008	00416	CE  	1999	10	8	99ZZZX3816       	1	19990922	G	3411	072110512	TUBE            			CESSNA	172   	172R        	2072401	CE  										PITOT	MELTED          	B			N3XR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	411ER	1890 				17280262				PILOTS WRITTEN DISCREPANCY (AIR SPEED INDICATOR NOT WORKING).  FOUND AIR SPEED NOT WORKING AFTER CHECKING AIR SPEED AT P	ITOT.  INSPECTED TUBING FROM AIR SPEED OUT TO THE PITOT MAST.  FOUND WIRING FROM HEATED PITOT MAST HAD BURNED THROUGH TU	BE.  CUT DAMAGE PART OFF AND RE-CONNECTED LINE.  SEPARATED WIRE FROM TUBING AND INSTALLED SPYRO IN PITOT TUBING.				1	H	7	1 	3O			NT	3A12    					 
1999100800417	19991008	00417	EA  	1999	10	8	99ZZZX3817       	2	19990913	G	8550		SLEEVE          			CESSNA	172   	172K        	2072430	CE  	LYC   	O320  	O320D2G     	41508	EA  					OIL RELIEF VALVE	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	78676	2059 	132  			17257715	L889639A			REMOVED SUCTION SCREEN DURING OIL CHANGE AND FOUND TWO CHUNKS OF ALUMINUM TRAPPED BY SCREEN.  INVESTIGATION FOUND THE PI	ECES HAD BROKEN OFF THE OIL RELIEF VALVE SLEEVE.  REASON FOR FAILURE NOT DETERMINED.  THERE IS NOT MUCH STRESS ON THIS P	ART.				1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999100800418	19991008	00418	EA  	1999	10	8	99ZZZX3818       	2	19990923	G	8500		ENGINE          			LKHEED	SP2   	SP2H        	5269601	SW  	WRIGHT	R3350 	R3350*      	67040	EA  					FORWARD	CONTAMINATED    	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	05	4235T									FLIGHT CREW WAS INFORMED BY LOCAL FUEL DISTRIBUTORS THAT ALL AIRCRAFT (100 CL) NEEDED TO BE TESTED IN AIRCRAFT FOR POSSI	BLE FUEL CONTAMINATION WITH JET FUEL.  AIRCRAFT WAS SUMPED AND JET FUEL WAS FOUND IN THE FUEL SYSTEM.  REPLACED BOTH REC	IPS AND INSPECTED TURBINES.				4	M	7	4 	4R	4	R	RT	A15SW   	E272				 
1999100800419	19991008	00419	NM  	1999	10	8	99ZZZX3819       	1	19990923	G	3242	2445902	CARRIER         	BFGOODRICH  	21565       	DHAV  	DHC8  	DHC8*       		NM  										NR 2	FAILED          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					0018					BRAKE ASSY, PN 2-1565, FAILED PREMATURELY.  NR 2 CARRIER AND LINING ASSY BROKEN INTO 3 PIECES.  THIS IS A CONTINUED DISC	REPANCY.  NOTE:  OEM PARTS INSTALLED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATION, PN 2-1565.					2	H	7	2 	4T			RT	A13NM   					 
1999100800420	19991008	00420	NM  	1999	10	8	99ZZZX3820       	1	19990923	G	3242	2445902	CARRIER         	BFGOODRICH  	21565       	DHAV  	DHC8  	DHC8*       		NM  										NR 1 & NR 2	FAILED          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					0712					BRAKE ASSEMBLY, PN 2-1565, FAILED PREMATURELY.  NR 1 CARRIER LINING ASSEMBLY BROKEN INTO TWO PIECES.  NR 2 CARRIER AND L	INING ASSEMBLY BROKEN INTO 3 PIECES.  THIS IS A CONTINUED DISCREPANCY.  NOTE: OEM PARTS INSTALLED IN BRAKE ASSY AND THE 	MOST RECENT BRAKE CONFIGURATION, PN 2-1565.				2	H	7	2 	4T			RT	A13NM   					 
1999100800422	19991008	00422	CE  	1999	10	8	99ZZZX3822       	1	19990922	G	7810	5A627429	GASKET          			CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  					EXHAUST	MISMANUFACTURING	B			HO1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	3356V					15076471	59260AR			DURING MAJOR OVERHAUL WHILE INSTALLING MUFFLERS WITH NEW SUPERIOR 'BLO PROOF' EXHAUST GASKETS, FOUND GASKET TO TOUCH INT	AKE ON ADJACENT CYLINDERS 1 AND 3 AND WOULD NOT FIT FLUSH AT CYLINDERS 2 AND 4.  THIS COULD LEAD TO EXHAUST BEING DIRECT	LY PORTED ON INTAKE GASKETS AND BURING THEM OUT  CAUSING A LEAN CYLINDER CONDITION.  PROFILE GASKET EDGE.				1	H	7	1 	3O	3	O		3A19    	E252				 
1999100800423	19991008	00423	SW  	1999	10	8	99ZZZX3823       	1	19990901	G	2810		FUEL CELL       			MOONEY	M20   	M20M        	5870222	SW  										WING	LEAKING         	B			W45R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	89FM	10   				270268				FUEL LEAK UNDER FORWARD WING WALK, TWO INBOARD SCREWS.						1	L	7	1 	3O			RT	2A3     					 
1999100800424	19991008	00424	SW  	1999	10	8	99ZZZX3824       	1	19990901	G	2810		FUEL CELL       			MOONEY	M20   	M20J        	5870219	SW  										WING	LEAKING         	B			W45R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	07	9152N					243408				FUEL LEAK UNDER FORWARD WING WALK TWO INBOARD SCREWS.						1	L	7	1 	3O				2A3     					 
1999100800425	19991008	00425	SW  	1999	10	8	99ZZZX3825       	1	19990901	G	2810		FUEL CELL       			MOONEY	M20   	M20R        	5870225	SW  										WING	LEAKING         	B			W45R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	81FM	12   				290180				FUEL LEAK UNDER FORWARD WING WALK TWO INBOARD SCREWS.						1	L	7	1 	3O			RT	2A3     					 
1999100800426	19991008	00426	SW  	1999	10	8	99ZZZX3826       	1	19990901	G	2810		FUEL CELL       			MOONEY	M20   	M20R        	5870225	SW  										WING	LEAKING         	B			W45R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	07	578TA					290153				FUEL LEAK UNDER FOWARD AND AFT WING WALK.  TWO INBOARD SCREWS.						1	L	7	1 	3O			RT	2A3     					 
1999100800427	19991008	00427	SW  	1999	10	8	99ZZZX3827       	1	19990901	G	2810		FUEL CELL       			MOONEY	M20   	M20K        	5870220	SW  										WING	LEAKING         	B			W45R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	07	37FM	128  				252018				FUEL LEAK UNDER FORWARD WING WALK UNDER TWO INBOARD SCREWS.						1	L	7	1 	3O				2A3     					 
1999100800428	19991008	00428	SW  	1999	10	8	99ZZZX3828       	1	19990901	G	2810		FUEL CELL       			MOONEY	M20   	M20M        	5870222	SW  										LT & RT WING	LEAKING         	B			W45R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	07	234BL					270234				FUEL LEAK UNDER WING INBOARD LEFT AND RIGHT.						1	L	7	1 	3O			RT	2A3     					 
1999100800429	19991008	00429	NE  	1999	10	8	99ZZZX3829       	3	19990909	G	6111	D5133	SHIELD          													HARTZL	HCE4A	HCE4A3I     	NE  	PROP BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			3333 					HJ526		EROSION SHIELD DEBONDED NR  3 BLADE.  REPLACED EROSION SHIELD, OVERHAULED BLADE, SN 1213.  ASSEMBLED PROP SET BLADE ANGL	E, REV 14.5 DEGREES, FEATHER AT 79.6 DEGREES, LP AT 18.6 DEGREES, STATIC BALANCED PROP IAW MFG CMM.															5	C	P10NE	 
1999100800430	19991008	00430	NE  	1999	10	8	99ZZZX3830       	3	19990820	G	6111	D5133	SHIELD          													HARTZL	HCE4A	HCE4A3I     	NE  	PROP BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			2153 					HJ986		NR 4 BLADE HAS 2 CRACKS IN EROSION SHIELD ABOUT 1.5 INCHES FROM DE-ICE BOOT.  DISASSEMBLED, CLEANED, AND INSPECTED.  REM	OVED AND REPLACED EROSION SHIELD ON NR 4 BLADE (SN 2484) OVERHAULED BLADE, RE-ASSEMBLED PROP, STATIC BALANCED, AND LUBRI	CATED IAW MFG CMM.														5	C	P10NE	 
1999100800431	19991008	00431	NE  	1999	10	8	99ZZZX3831       	3	19990826	G	6111	D5133	SHIELD          													HARTZL	HCE4A	HCE4A3I     	NE  	PROP BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			2397 					HJ275		NR 2 BLADE EROSION SHIELD DEBONDED.  DEBONDED BEYOND REPAIRABLE LIMITS.  DISASSEMBLED, CLEANED, AND INSPECTED.  REMOVED 	AND REPLACED EROSION SHIELD ON NR 2 BLADE (SN 1100) OVERHAULED BLADE AND RE-ASSEMBLED PROP IAW MFG CMM.															5	C	P10NE	 
1999100800432	19991008	00432	WP  	1999	10	8	99ZZZX3832       	2	19990928	G	7250	30754372	BLADE           								GARRTT	TFE731	TFE7314R    	01518	WP  					LP TURBINE	DENTED          	B			XB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09		1578 	1274 				P102163			DURING POST-FLIGHT INSPECTION, DISCOVERED THIRD STAGE LPT HAD ONE EACH BLADE SHROUD BROKEN AND SEVERAL BLADES DENTED.  F	IRST AND SECOND STAGE LPT'S HAVE DAMAGED BLADES ALSO.  ENG TSN:  1,578 HOURS.  CSN:  1,274.										4	F			E6WE				 
1999100800434	19991008	00434	NE  	1999	10	8	99ZZZX3833       	2	19990830	G	7260	775761	GEAR            	HAMSTD      	6044T35P10  	SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					RT IDLER AFT	NICKED          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		13584			9288		GEE785592			UPON DISASSEMBLY OF GEARBOX, THE FOLLOWING WAS OBSERVED:  ON AFT SIDE OF BULKHEAD AT THE RT IDLER GEAR OPENING, THERE IS	 A 360 DEGREE GROOVE, .078 INCH DEEP BY .200 INCH WIDE, (PN 775775-31, SET NR 242).  RT IDLER FORWARD TAB WASHER (PN 789	578-1) BROKEN.  BEARINGS REJECTED FOR NICKS/PITS TO ROLLER AND RACE SURFACES.  HSS SO NR 325699 SO.  CUST:  KENDELL.  RE	F:  OPER CNTRL NR 99ZZZX3834 THROUGH 99ZZZX3839.			2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999100800435	19991008	00435	NE  	1999	10	8	99ZZZX3834       	2	19990830	G	7260	7822651	GEAR            	HAMSTD      	6044T35P10  	SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					LT IDLER AFT	NICKED          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		13584			9251		GEE785592			UPON DISASSEMBLY OF GEARBOX, THE FOLLOWING WAS OBSERVED:  ON AFT SIDE OF BULKHEAD AT THE RT IDLER GEAR OPENING, THERE IS	 A 360 DEGREE GROOVE, .078 INCH DEEP BY .200 INCH WIDE, (PN 775775-31, SET NR 242).  RT IDLER FORWARD TAB WASHER (PN 789	578-1) BROKEN.  BEARINGS REJECTED FOR NICKS/PITS TO ROLLER AND RACE SURFACES.  HSS SO NR 325699 SO.  CUST:  KENDELL.  RE	F:  OPER CNTRL NR 99ZZZX3833 THROUGH 99ZZZX3839.			2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999100800436	19991008	00436	NE  	1999	10	8	99ZZZX3835       	2	19990830	G	7260	7757602	GEAR            	HAMSTD      	6044T35P10  	SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					RT IDLER FWD	PITTED          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		13584			7135		GEE785592			UPON DISASSEMBLY OF GEARBOX, THE FOLLOWING WAS OBSERVED:  ON AFT SIDE OF BULKHEAD AT THE RT IDLER GEAR OPENING, THERE IS	 A 360 DEGREE GROOVE, .078 INCH DEEP BY .200 INCH WIDE, (PN 775775-31, SET NR 242).  RT IDLER FORWARD TAB WASHER (PN 789	578-1) BROKEN.  BEARINGS REJECTED FOR NICKS/PITS TO ROLLER AND RACE SURFACES.  HSS SO NR 325699 SO.  CUST:  KENDELL.  RE	F:  OPER CNTRL NR 99ZZZX3833 THROUGH 99ZZZX3839			2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999100800437	19991008	00437	NE  	1999	10	8	99ZZZX3836       	2	19990830	G	7260	7757602	GEAR            	HAMSTD      		SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					LT IDLER FWD	PITTED          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		13584			7138		GEE785592			UPON DISASSEMBLY OF GEARBOX, THE FOLLOWING WAS OBSERVED:  ON AFT SIDE OF BULKHEAD AT THE RT IDLER GEAR OPENING, THERE IS	 A 360 DEGREE GROOVE, .078 INCH DEEP BY .200 INCH WIDE, (PN 775775-31, SET NR 242).  RT IDLER FORWARD TAB WASHER (PN 789	578-1) BROKEN.  BEARINGS REJECTED FOR NICKS/PITS TO ROLLER AND RACE SURFACES.  HSS SO NR 325699 SO.  CUST:  KENDELL.  RE	F:  OPER CNTRL NR 99ZZZX3833 THROUGH 99ZZZX3839.			2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999100800438	19991008	00438	NE  	1999	10	8	99ZZZX3837       	2	19990903	G	7260	7757583	SHAFT           	HAMSTD      		SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					PROP AFT ROLLER	NICKED          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		13584			TBC00370		GEE785592			UPON DISASSEMBLY OF GEARBOX, THE FOLLOWING WAS OBSERVED:  ON AFT SIDE OF BULKHEAD AT THE RT IDLER GEAR OPENING, THERE IS	 A 360 DEGREE GROOVE, .078 INCH DEEP BY .200 INCH WIDE, (PN 775775-31, SET NR 242).  RT IDLER FORWARD TAB WASHER (PN 789	578-1) BROKEN.  BEARINGS REJECTED FOR NICKS/PITS TO ROLLER AND RACE SURFACES.  HSS SO NR 325699 SO.  CUST:  KENDELL.  RE	F:  OPER CNTRL NR 99ZZZX3833 THROUGH 99ZZZX3839.			2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999100800439	19991008	00439	NE  	1999	10	8	99ZZZX3838       	2	19990903	G	7260	7757573	SHAFT           	HAMSTD      		SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					PROP FWD ROLLER	NICKED          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		13584			TBC00368		GEE785592			UPON DISASSEMBLY OF GEARBOX, THE FOLLOWING WAS OBSERVED:  ON AFT SIDE OF BULKHEAD AT THE RT IDLER GEAR OPENING, THERE IS	 A 360 DEGREE GROOVE, .078 INCH DEEP BY .200 INCH WIDE, (PN 775775-31, SET NR 242).  RT IDLER FORWARD TAB WASHER (PN 789	578-1) BROKEN.  BEARINGS REJECTED FOR NICKS/PITS TO ROLLER AND RACE SURFACES.  HSS SO NR 325699 SO.  CUST:  KENDELL.  RE	F:  OPER CNTRL NR 99ZZZX3833 THROUGH 99ZZZX3839.			2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999100800440	19991008	00440	NE  	1999	10	8	99ZZZX3839       	2	19990903	G	7260	7757652	BLOCK           	HAMSTD      		SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					SLIDER BLOCK	PITTED          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		13584			TBC00336		GEE785592			UPON DISASSEMBLY OF GEARBOX, THE FOLLOWING WAS OBSERVED:  ON AFT SIDE OF BULKHEAD AT THE RT IDLER GEAR OPENING, THERE IS	 A 360 DEGREE GROOVE, .078 INCH DEEP BY .200 INCH WIDE, (PN 775775-31, SET NR 242).  RT IDLER FORWARD TAB WASHER (PN 789	578-1) BROKEN.  BEARINGS REJECTED FOR NICKS/PITS TO ROLLER AND RACE SURFACES.  HSS SO NR 325699 SO.  CUST:  KENDELL.  RE	F:  OPER CNTRL NR 99ZZZX3833 THROUGH 99ZZZX3838.			2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999100800441	19991008	00441	NE  	1999	10	8	99ZZZX3840       	2	19990901	G	7230	772568QQ	BOLT            								PWA   	JT8   	JT8D7B      	52053	NE  					COMPRESSOR	FRACTURED       	B			WG4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19							654747			PMA BOLT, PN 772568QQ, REPLACEMENT FOR OEM BOLT PN 772568, FAILED AFTER 931:47 HOURS AND, 1,361 CYCLES IN SERVICE.  BOLT	 FRACTURED CAUSING HEAD TO BE INGESTED INTO THE N-2 COMPRESSOR DRIVE TURBINE.  BORESCOPE INSPECTIONS REVEALED EXTENSIVE 	DAMAGE TO TURBINE BLADES.									4	F			E2EA				 
1999100800442	19991008	00442	SO  	1999	10	8	99ZZZX3841       	1	19990923	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE	CRACKED         	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		1446 			1194A					BRAKE ASSY, PN 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE TUBE KEY SLOTS.  HEAT STACK	 WARPED.  THIS IS A CONTINUAL DISCREPANCY.  BRAKE ASSEMBLY SHOULD LAST 2,400 CYCLES.  NOTE:  OEM PARTS INSTALLED IN BRAK	E ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION, PN 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
1999100800443	19991008	00443	SO  	1999	10	8	99ZZZX3842       	1	19990923	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE	CRACKED         	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		679  			0578A					BRAKE ASSEMBLY, PN 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN THROUGH AND BINDING IN TORQUE TUBE KEY SLOTS.  HEAT S	TACK WARPED.  THIS IS A CONTINUAL DISCREPANCY.  BRAKE ASSY SHOULD LAST 2,500 CYCLES.  NOTE:  OEM PARTS INSTALLED IN BRAK	E ASSY AND THE MOST RECENT BRAKE CONFIGURATION, PN 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
1999100800444	19991008	00444	SO  	1999	10	8	99ZZZX3843       	1	19990921	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE	CRACKED         	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		1934 			0547A					BRAKE ASSEMBLY, PN 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN IN HALF. NR 2 STATOR CRACKED THROUGH AND BINDING IN T	ORQUE TUBE KEY SLOTS. THIS IS A CONTINUAL DISCREPANCY.  BRAKE ASSEMBLY SHOULD LAST 2,500 CYCLES.  NOTE:  OEM PARTS INSTA	LLED IN BRAKE ASSEMBLY AND THE MOST RECENT BRAKE CONFIGURATION, PN 2-1585,				2	L	7	2 	4T			RT	A31SO   					 
1999100800445	19991008	00445	WP  	1999	10	8	99ZZZX3844       	2	19990924	G	7200		ENGINE          			BEECH 	18    	C45H        	1151018	CE  	GARRTT	TPE331	TPE331*     	01514	WP  					RIGHT	FAILED          	H				O				OTHER                   				X	J		ENGINE FLAMEOUT           	WARNING INDICATION        		AP	APPROACH       	1			SW	99	400WA					AF764	P93007C			DURING THE TURN FROM BASE TO FINAL APPROACH, THE RT ENGINE FLAMED OUT.  THE PILOT MADE AN UNEVENTFUL LANDING.  MAINTENAN	CE PERSONNEL FOUND THE ENGINE INLET DE-ICE VALVE CANNON PLUG LOOSE ALLOWING ICE ACCUMULATION THAT EVENTUALLY WAS INGESTE	D RESULTING IN THE FLAMEOUT.  A VISUAL INSPECTION OF THE FIRST IMPELLER SHOWED NO APPARENT DAMAGE.  THE ENGINE WAS THEN 	RUN WITH ALL INDICATIONS NORMAL.			1	L	7	2 	3R	3	T		A765    	E2WE				 
1999100800447	19991008	00447	CE  	1999	10	8	99ZZZX3846       	1	19990826	G	3242	3052V	BRAKE           	CLEVELAND   		CESSNA	210   	T210N       	2073456	CE  										MLG	MALFUNCTIONED   	B			AW4R	O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			WP	11	1937V					21064753				ON TAXI OUT FOR TAKEOFF, RT BRAKE JAMMED IN APPLIED POSITION.  INVESTIGATION REVEALED PRIMARY CAUSE WAS PISTON HAD EXTEN	DED TOO FAR FROM BRAKE CYLINDER AND HAD JAMMED IN APPLIED POSITION DUE TO EXCESSIVELY WORN LININGS AND UNAPPROVED SHIM B	ETWEEN BRAKE CYLINDER AND BRAKE BACKING PLATES.  BACKING PLATES AND CYLINDERS ALSO SHOWED EVIDENCE OF DAMAGE DUE TO BACK	 PLATE ATTACH BOLT ATTACH BOLTS BEING CONSISTENTLY OVERTORQUED.  PREVENTIVE ACTION WOULD BE TO INSURE TIMELY REPLACEMENT	 OF LININGS AND DAMAGED BRACE PARTS.		1	H	7	1 	3O				3A21    					 
1999100800448	19991008	00448	CE  	1999	10	8	99ZZZX3847       	1	19990902	G	2710		TUBE            			BEECH 	36    	A36         	1151604	CE  										RT AILERON	CHAFED          	B	P		QC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	1127J	386  				E3027				RIGHT AILERON PUSH/PULL TUB FROM BELL CRANK TO RT AILERON RUBBING AFT SPAR TO THE POINT THAT WALL OF TUBE IS WORN ALMOST	 COMPLETELY THROUGH.					1	L	7	1 	3O				3A15    					 
1999100800449	19991008	00449	SO  	1999	10	8	99ZZZX3848       	1	19990901	G	3230	2250901	FITTING         			PIPER 	PA24  	PA24260     	7102406	SO  										RT MLG	DAMAGED         	G	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	260NC	2700 				244855				DURING GEAR INSPECTION, EXCESSIVE MOVEMENT WAS NOTICED.  REMOVED THE SIDE BRACE STUD ASSEMBLY AND DISCOVERED THE SIDE BR	ACE STUD HAD BEEN FORCED IN THE SIDE BRACE ASSY.  THE SIDE BRACE ASSY WAS SEVERELY FRITTERED AWAY.					1	L	7	1 	3O				1A15    					 
1999100800450	19991008	00450	SO  	1999	10	8	99ZZZX3849       	1	19990928	G	2710	62701143	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	923ER	2042 				4496010				DURING A ROUTINE INSPECTION, THE MECHANIC FOUND A SUSPICIOUS AREA ON THE AILERON BALANCE CABLE AT THE OUTBOARD PULLEY, P	N 62713-02.  THERE ARE FOUR SIMILAR PULLIES WHERE THE CABLES EXIT THE FUSELAGE AND ENTER THE WING.  THESE PULLIES WEAR O	N THE CABLES AND CAUSE BROKEN STRANDS.  THESE ARE OFTEN DIFFICULT TO SEE AT FIRST AND MUST BE INSPECTED WITH A BRIGHT LI	GHT AND RUBBED WITH A CLOTH RAG.  THE SAME CONDITION EXISTS WITH THE STABILATOR CABLE AND PULLEY, PN 481-612.			1	L	7	2 	3O			 	A19S0   					 
1999100800451	19991008	00451	SO  	1999	10	8	99ZZZX3850       	1	19990928	G	2710	62701123	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	923ER	2042 				4496010				DURING A ROUTINE INSPECTION, THE MECHANIC FOUND A SUSPICIOUS AREA ON THE AILERON BALANCE CABLE AT THE OUTBOARD PULLEY, P	N 62713-02.  THERE ARE FOUR SIMILAR PULLIES WHERE THE CABLES EXIT THE FUSELAGE AND ENTER THE WING.  THESE PULLIES WEAR O	N THE CABLES AND CAUSE BROKEN STRANDS.  THESE ARE OFTEN DIFFICULT TO SEE AT FIRST AND MUST BE INSPECTED WITH A BRIGHT LI	GHT AND RUBBED WITH A CLOTH RAG.  THE SAME CONDITION EXISTS WITH THE STABILATOR CABLE AND PULLEY, PN 481-612.			1	L	7	2 	3O			 	A19S0   					 
1999100800452	19991008	00452	SO  	1999	10	8	99ZZZX3851       	1	19990928	G	2710	62701124	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	923ER	2042 				4496010				DURING A ROUTINE INSPECTION, THE MECHANIC FOUND A SUSPICIOUS AREA ON THE AILERON BALANCE CABLE AT THE OUTBOARD PULLEY, P	N 62713-02.  THERE ARE FOUR SIMILAR PULLIES WHERE THE CABLES EXIT THE FUSELAGE AND ENTER THE WING.  THESE PULLIES WEAR O	N THE CABLES AND CAUSE BROKEN STRANDS.  THESE ARE OFTEN DIFFICULT TO SEE AT FIRST AND MUST BE INSPECTED WITH A BRIGHT LI	GHT AND RUBBED WITH A CLOTH RAG.  THE SAME CONDITION EXISTS WITH THE STABILATOR CABLE AND PULLEY, PN 481-612.			1	L	7	2 	3O			 	A19S0   					 
1999100800453	19991008	00453	SO  	1999	10	8	99ZZZX3852       	1	19990928	G	2710	62701113	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	923ER	2042 				4496010				DURING A ROUTINE INSPECTION, THE MECHANIC FOUND A SUSPICIOUS AREA ON THE AILERON BALANCE CABLE AT THE OUTBOARD PULLEY, P	N 62713-02.  THERE ARE FOUR SIMILAR PULLIES WHERE THE CABLES EXIT THE FUSELAGE AND ENTER THE WING.  THESE PULLIES WEAR O	N THE CABLES AND CAUSE BROKEN STRANDS.  THESE ARE OFTEN DIFFICULT TO SEE AT FIRST AND MUST BE INSPECTED WITH A BRIGHT LI	GHT AND RUBBED WITH A CLOTH RAG.  THE SAME CONDITION EXISTS WITH THE STABILATOR CABLE AND PULLEY, PN 481-612.			1	L	7	2 	3O			 	A19S0   					 
1999100800454	19991008	00454	CE  	1999	10	8	99ZZZX3853       	1	19990909	G	2434	02373	ALTERNATOR      	ELECTROSYS  		CESSNA	210   	T210M       	2073451	CE  										ENGINE	FAILED          	C				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	17	888Q	1429 	172  			21062855				DURING VFR FLIGHT, ALTERNATOR FAILED AFTER LANDING GEAR RETRACTION.  ALTERNATOR FAILED 5 MINUTES AFTER LANDING GEAR RETR	ACTION DURING CLIMB TO ALTITUDE.  AMMETER AND VOLTMETER INDICATIONS PRIOR TO FAILURE WERE NORMAL.  ALTERNATOR DID NOT CO	ME ON-LINE AFTER COMPLETING ACTIONS AS OUTLINED IN PILOT'S OPERATING HANDBOOK.  AIRCRAFT DIVERTED TO NEAREST AIRPORT, LA	NDED SAFELY.			1	H	7	1 	3O				3A21    					 
1999101500071	19991015	00071	WP  	1999	10	15	99ZZZX3854       	1	19990527	G	3230	369D2630121	DAMPERS         			HUGHES	369   	369D        	4470706	WP  										MLG	WEAK            	B			EOOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	5074R		108  			1151D				BOTH DAMPERS WERE FOUND WEAK WITH FLUID SHOWING AROUND SEALS, SN 3244 AND SN 0887.   REPLACED SEALS AND RE-SERVICED.						1	G	7	1 	3U				H3WE    					 
1999101500072	19991015	00072	WP  	1999	10	15	99ZZZX3855       	1	19990819	G	6220	369A10053	DAMPER PIN      			HUGHES	369   	369D        	4470706	WP  										M/R HUB	LOOSE           	B			EOOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	5074R	366  				1151D				DURING POST-FLIGHT, THE 'GREEN' MAIN ROTOR DAMPER PIN WAS FOUND LOOSE.  IT HAD WORKED UP TO A POINT WHERE THE BALE WAS C	ONTACTING THE DAMPER CLEVIS ALTHOUGH IT WAS STILL ENGAGED ON THE PIN.					1	G	7	1 	3U				H3WE    					 
1999101500073	19991015	00073	GL  	1999	10	15	99ZZZX3856       	2	19990730	G	7532	23053176	BLEED VALVE     			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	INOPERATIVE     	B			EOOR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	5074R	104  			FF30169	1151D	CAE832750			DURING THROTTLE ROLL-ON DURING POWER RECOVERY FROM PRACTICE AUTOROTATION, THE PILOT EXPERIENCED A COMPRESSOR STALL.  REP	LACED BLEED VALVE.					1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999101500074	19991015	00074	WP  	1999	10	15	99ZZZX3857       	1	19990716	G	6220	369A10053	DAMPER PIN      			HUGHES	369   	369D        	4470706	WP  										M/R HUB	LOOSE           	B			EOOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	5074R	259  				1151D				DURING 100-HOUR INSPECTION, THE MAIN ROTOR DAMPER PINS WERE FOUND LOOSE AND ONE, THE 'BALE', WAS NOT ENGAGED PROPERLY. (	THE PIN HAVING RISEN SO HIGH AS TO FORCE THE BALE OFF OF THE INDEX).  INSPECTED, ADJUSTED, AND RE-INSTALLED TWO EACH (RE	D AND YELLOW).				1	G	7	1 	3U				H3WE    					 
1999101500075	19991015	00075	GL  	1999	10	15	99ZZZX3858       	2	19990911	G	7532	23053176	BLEED VALVE     			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	INOPERATIVE     	B			EOOR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	5074R		81   		FF37863	1151D	CAE832750			PILOT ENCOUNTERED NUMEROUS RAPID COMPRESSOR STALLS IN A HIGH POWER SITUATION.  FOUND SIDE SLOP ON BLEED VALVE POPPET AND	 A RATCHETY FEEL DURING MANUAL ACTUATION.  REPLACED BLEED VALVE.					1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999101500076	19991015	00076	GL  	1999	10	15	99ZZZX3859       	2	19990721	G	7420	9048222102	IGNITION LEAD   			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE IGNITION	DAMAGED         	B	P	A	EOOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	5074R				94420080	1151D	CAE832750			(ALLISON EQUIVALENT P/N 6870855) ON INSPECTION, THE CONTACT SLEEVE AT THE 16NOTOR END WS FOUND TO BE MISSING THE CIRCLIP	 RETAINER AND THE CONTACT SLEEVE HAD SLIPPED BACK INTO THE INSULATOR.					1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999101500077	19991015	00077	SW  	1999	10	15	99ZZZX3860       	1	19990908	G	3411	AN58131	TUBE            			BELL  	212   	212         	1181420	SW  										PITOT SYSTEM	CORRODED        	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530B					30702				RUSTED THROUGH TUBING.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999101500161	19991015	00161	EU  	1999	10	15	99ZZZX3888       	1	19990914	G	5510	C55151101051	BUSHING         			UROCOP	EC120 	EC120B      	8680987	EU  										LT HORIZ STAB	LOOSE           	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	120TX	40   				1029				DAILY INSPECTION REVEALED LEFT SUPPORT BUSHING WAS BROKEN AWAY FOR ITS FIXED COMPOSITE POSITION WITHIN THE HORIZONTAL ST	ABILIZER.  NO OTHER DAMAGE WAS FOUND AT EITHER OF THE STABILIZER MOUNT BRACKETS TO THE TAILBOOM, LT AND RT SIDES.  NEW S	ERVICEABLE STABILIZER INSTALLED.  FENESTRON WAS BALANCE CHECKED AT 100 PERCENT FPOG - OUT OF TOLERANCE.  TIPS - BALANCED	 TO .1 IPS.  POSSIBLE CAUSE FOR THE COMPOSITE FAILURE IS SUSPECT TO POOR COMPOSITE ADHESION AND WORKMANSHIP.  RECOMMENDA	TION FOR ENHANCEMENT: INSTALL LIKE RIVETED PLATE TO LOWER BUSHING STABILIZER INTERFACE AS THE TOP (LT AND RT SIDES).		1	G	7	2 	3U			NC	R0001RD 					 
1999101500162	19991015	00162		1999	10	15	99ZZZX3889       	4	19990908	G	3414	MS28045	INDICATOR       			BELL  	204   	UH1H        	1181407	SW  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	51AG				92906	7120178				INDICATING FALSE AIRSPEED.  SLOW TO CHANGE INDICATION.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999101500163	19991015	00163	SW  	1999	10	15	99ZZZX3890       	1	19990907	G	2822	2050606063	PUMP            			BELL  	204   	UH1H        	1181407	SW  										FUEL BOOST	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	51AG				69120	7120178				HEARD NOISE FROM LEFT FUEL CELL.  CHECKED PRESSURE ON BOOST PUMP, FOUND TO BE LOW.  REMOVED AND REPLACED PUMP.						1	G	7	1 	4U				EXPA1G71					 
1999101500164	19991015	00164		1999	10	15	99ZZZX3891       	4	19990908	G	3414	MS28045T2	INDICATOR       			BELL  	204   	UH1H        	1181407	SW  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	51AG				93196	7120178				INDICATING FALSE AIRSPEED, SLOW TO CHANGE INDICATION.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999101500165	19991015	00165		1999	10	15	99ZZZX3892       	4	19990908	G	2340	18486G01	INTERPHONE      			HUGHES	369   	369D        	4470706	WP  										COCKPIT	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	500DC				X96021X	290456D				NO SIDE TONES.  NO INTERCOM.  WILL NOT TRANSMIT.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999101500166	19991015	00166		1999	10	15	99ZZZX3893       	4	19990908	G	3120	102149	HOUR METER      			HUGHES	369   	369D        	4470706	WP  										COCKPIT	SLOW            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	500DC					290456D				HOUR METER RUNS SLOW.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999101500167	19991015	00167	WP  	1999	10	15	99ZZZX3894       	1	19990908	G	7712	369H4551	TACH GENERATOR  			HUGHES	369   	369D        	4470706	WP  										ENGINE RPM	DAMAGED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	500DC				289	2904569				CANNON PLUG BENT AND RIVETS TORN OUT OF HOUSING.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999101500168	19991015	00168	SW  	1999	10	15	99ZZZX3895       	1	19990908	G	7714	32009023	TACH GENERATOR  			BELL  	206   	206B        	1181511	SW  										ENGINE RPM	BROKEN          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	49718				WE3437	1917				N2 TACH GENERATOR HOUSING BROKEN.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999101500169	19991015	00169	SW  	1999	10	15	99ZZZX3896       	1	19990908	G	7714	32005023	TACH GENERATOR  			BELL  	206   	206B        	1181511	SW  										ENGINE RPM	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BX				10946	2872				TACHOMETER/GENERATOR FAILS TO GENERATE SIGNAL.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999101500170	19991015	00170	SW  	1999	10	15	99ZZZX3897       	1	19990907	G	6230	222010403114	RING            		222010400105	BELL  	222   	222         	1182122	SW  										SWASHPLATE	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	29KH	842  			CL0002	47053				DURING C/W BELL SB ASB 222-99-84, DRIVE PIN TORQUE CHECK.  ROTATIONAL TORQUE OF DRIVE PINS WAS FOUND TO BE BELOW MINIMUM	S.  NO REPAIR IS APPROVED AT THIS TIME.  INSTALLED NEW PART.					1	G	7	2 	3U				H9SW    					 
1999101500171	19991015	00171	SW  	1999	10	15	99ZZZX3898       	1	19990915	G	7923	03773804	HOUSING         			BELL  	206   	206B        	1181511	SW  										ENGINE OIL	LOOSE           	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY					2871				DURING REPLACEMENT OF NI-CAD FILTER  (FACET) AT REMOVAL FROM HOUSING AND BYPASS VALVE ASSY, THE BYPASS VALVE ASSY WAS FO	UND UNSECURED FROM THE HOUSING.  REMOVED AND REPLACED HOUSING.					1	G	7	1 	3U				H2SW    					 
1999101500172	19991015	00172	SW  	1999	10	15	99ZZZX3899       	1	19990907	G	2822	2C271	PUMP            			BELL  	206   	206B        	1181511	SW  										FUEL BOOST	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BY				4AD162	2871				ENGINE FUEL PRESSURE NOTICED TO BE LOW.  NOTICED ISOLATED FORWARD PUMP TO BE OFF-LINE.  VERIFIED CURRENT TO PUMP WITH NO	 FLUID OUTPUT.  REMOVED AND REPLACED.					1	G	7	1 	3U				H2SW    					 
1999101500173	19991015	00173	WP  	1999	10	15	99ZZZX3900       	1	19990908	G	6220	J156406	DAMPER          			HUGHES	369   	369E        	4470707	WP  										MAIN ROTOR	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8330P				10650	0330E				MAIN ROTOR DAMPER FAILED 600-HOUR INSPECTION.  STRETCH TEST.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999101500174	19991015	00174		1999	10	15	99ZZZX3901       	4	19990908	G	3120	400240	CLOCK           			HUGHES	369   	369E        	4470707	WP  										COCKPIT	INTERMITTENT    	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8330P				17929	0330E				WORKS INTERMITTENTLY.  INTERNAL BINDING.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999101500175	19991015	00175	SW  	1999	10	15	99ZZZX3902       	1	19990908	G	6330	204001994001	BEARING         			BELL  	212   	212         	1181420	SW  										XMISSON SUPPORT	WORN            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530P					30920				BEARINGS WORN AND POPPING OUT OF SLEEVE.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999101500176	19991015	00176	SW  	1999	10	15	99ZZZX3903       	1	19990908	G	6220	204010425009	TUBE BEARING    			BELL  	212   	212         	1181420	SW  										M/R HEAD	WORN            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530F					30920				BOTH DAMPER TUBES HAVE WORN BEARINGS.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999101500177	19991015	00177		1999	10	15	99ZZZX3904       	4	19990908	G	3416	0900409901	ENCODER         			BELL  	212   	212         	1181420	SW  										ALTIMETER	FAILED          	B			LS1R	K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			EA	13	8530F				16472	30920				SMOKE IS RELEASED FROM PART WHEN OPERATION IS ATTEMPTED.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999101500178	19991015	00178	SW  	1999	10	15	99ZZZX3905       	1	19990914	G	3210	2120304377	STRAP           			BELL  	212   	212         	1181420	SW  										MLG	DETERIORATED    	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530F					30920				RUBBER BUMPERS WERE FOUND DETERIORATED DURING INSPECTION.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999101500179	19991015	00179	SW  	1999	10	15	99ZZZX3906       	1	19990914	G	6710	212001712101	BELLCRANK       			BELL  	212   	212         	1181420	SW  										FLIGHT CONTROL	WORN            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	8530F					30920				DURING PERIODIC INSPECTION, FOUND BEARING WORN AND ROUGH IN OPERATION.  REMOVED AND REPLACED.						1	G	7	1 	4U				H4SW    					 
1999101500180	19991015	00180	SW  	1999	10	15	99ZZZX3907       	1	19990908	G	2821	2050626541	VALVE           			BELL  	204   	UH1H        	1181407	SW  										FUEL CELL	LEAKING         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	52AG					7015746				LEAKING FROM BREAK-AWAY VALVE ON CENTER FUEL CELL AT 'T' ON CROSS FEED LINE.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999101500181	19991015	00181	SW  	1999	10	15	99ZZZX3908       	1	19990908	G	2822	2050606063	PUMP            			BELL  	204   	UH1H        	1181407	SW  										FUEL BOOST	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	52AG				C7934	7015746				FUEL BOOST PUMP INTERMITTENTLY COMES ON AND OFF.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999101500182	19991015	00182	SW  	1999	10	15	99ZZZX3909       	1	19990908	G	6220	206011105001	TRUNNION        			BELL  	206   	206B        	1181511	SW  										M/R HEAD	WORN            	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	9907K				94799	2040				TRUNNION BEARING WORN, REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999101500183	19991015	00183		1999	10	15	99ZZZX3910       	4	19990908	G	3422	5050031904	GYRO            			BELL  	206   	206B        	1181511	SW  										COCKPIT	MALFUNCTIONED   	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	9907K				1105	2040				DIRECTIONAL GYRO WILL NOT HOLD HEADING.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999101500184	19991015	00184	GL  	1999	10	15	99ZZZX3911       	3	19990924	G	6114	B83037	LOCK            			MTSBSI	MU2   	MU2B35      	5780411	CE  						HARTZL	HCB3T	HCB3TN5     	GL  	HUB	WORN            	H	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	11	300RX		500  			572				PROPELLER HAS NEW STYLE BLADE LOCKS.  COTTERPIN THAT HOLDS SPRING AND LOCK IN ASSEMBLY IS FAILING OR WEARING OUT THE HOL	ES IN HOUSING.					1	H	7	2 	3T			RT	A10SW   		6	C	P15EA	 
1999101500185	19991015	00185	NM  	1999	10	15	99ZZZX3912       	1	19990909	G	4930	69254517	VALVE           			AMD   	FALC50	FALCON2000  	2730170	NM  										APU	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	326EW	85   			2673	58				CREW ATTEMPTED TO START APU DURING QUICK TURN AND APU FAILED TO START.  TOPPING ON VALVE ENABLE APU START.  VALVE WAS RE	PLACED WITH NEW WHEN AIRCRAFT RETURNED HOME.  IF APU IS REQUIRED IN CERTAIN CIRCUMSTANCES, IT MAY OR MAY NOT START DUE T	O THE UNRELIABLE VALVE.				2	K	7	3 	4F			RT	A50NM   					 
1999101500186	19991015	00186	NM  	1999	10	15	99ZZZX3913       	1	19990719	G	4930	69254517	VALVE           		GTCP36150   	AMD   	FALC50	FALCON2000  	2730170	NM  										APU	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	17	326EW	80   			2673	58				AFATER LANDING FOLLOWING A LONG FLIGHT AT FL 430, CREW ATTEMPTED TO START APU FOR A QUICK TURN.  APU FAILED TO START.  T	HEREFORE, LEFT NR 2 ENGINE RUNNING FOR CROSSBLEED START.  TROUBLESHOOTING REVEALED THAT FUEL SOLENOID VALVE FAILED TO OP	EN WHEN COMMANDED BY ECU.  IF ENGINES HAD FLAMED OUT, THIS EMERGENCY COMPONENT WOULD NOT HAVE STARTED.  THEREFORE, CREW 	COULD NOT HAVE RESTARTED ENGINES.  WHEN CREW RETURNED TO SBN, APU FUNCTIONAL NORMAL.			2	K	7	3 	4F			RT	A50NM   					 
1999101500188	19991015	00188	CE  	1999	10	15	99ZZZX3915       	1	19990916	G	3230	08421043	BELLCRANK       			CESSNA	310   	310R        	2074245	CE  										NLG	FAILED          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	25	98904	8012 				310R1240				WHEN PILOT SELECTED GEAR DOWN, HEARD LOUD NOISE IN NOSE, HAD 3 GREEN LIGHTS AND NO HORN, LANDED WITHOUT INCIDENT.  FOUND	 NOSE GEAR INBOARD BELLCRANK BROKEN AND BOLT BENT.  GEAR WAS RIGGED TO SPECS 2 MONTHS PRIOR.  SUSPECT GEAR MOTOR BRAKE I	NOPERABLE AND GEAR WENT PAST UPLIMIT SWITCH AND JAMMED IN UP POSITION.  UPLOCK HOOK AND BOLT ALSO BENT.				1	L	7	2 	3O				3A10    					 
1999101500189	19991015	00189	SO  	1999	10	15	99ZZZX3916       	1	19990916	G	2510	7933761	SEAT            		9680609     	PIPER 	PA28  	PA28161     	7102803	SO  										COCKPIT	BROKEN          	B	P		TIMR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	84495	9325 				288216033				DURING ROUTINE INSPECTION, FOUND BROKEN TUBING ON BOTTOM OF SEAT.						1	L	7	1 	3O				2A13    					 
1999101500190	19991015	00190	SO  	1999	10	15	99ZZZX3917       	1	19991004	G	2710	62701143	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	FRAYED          	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	920ER	2637 				4495013				ONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND TO HAVE FRAYED AILERON CABLES.  THE LOCATION OF THE DAMAGE IS AT PULLEYS, PN 62	713-02 AND PN 62713-04.  CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPE	D WITH A CLOTH, SMALL STRANDS CAN BE SEEN AND FELT WHERE THEY ARE BROKEN.  ONCE CABLE IS REMOVED, IT CAN BE BENT TO A SM	ALL RADIUS.  THIS IS WHEN THE FULL EXTENT OF THE DAMAGE CAN BE SEEN.  IN SOME CASES, CABLE WAS AS MUCH AS 40 PERCENT FAI	LED.  FLEET OPER GROUNDED AND REPAIRED THE REMAINING AIRCRAFT.  SUBMITTER STATED BECAUSE THE DAMAGE IS NOT APPARENT WITH	 THE CABLE IN THE INSTALLED CONFIGURATION, IT IS POSSIBLE THE CABLE COULD BE LEFT IN SERVICE TO A POINT WHERE IT FAILS.	1	L	7	2 	3O			 	A19S0   					 
1999101500191	19991015	00191	SO  	1999	10	15	99ZZZX3918       	1	19991004	G	2710	62701123	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	FRAYED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	920ER	2637 				4495013				ONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND TO HAVE FRAYED AILERON CABLES.  THE LOCATION OF THE DAMAGE IS AT PULLEYS, PN 62	713-02 AND PN 62713-04.  CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPE	D WITH A CLOTH, SMALL STRANDS CAN BE SEEN AND FELT WHERE THEY ARE BROKEN.  ONCE CABLE IS REMOVED, IT CAN BE BENT TO A SM	ALL RADIUS.  THIS IS WHEN THE FULL EXTENT OF THE DAMAGE CAN BE SEEN.  IN SOME CASES, CABLE WAS AS MUCH AS 40 PERCENT FAI	LED.  FLEET OPER GROUNDED AND REPAIRED THE REMAINING AIRCRAFT.  SUBMITTER STATED BECAUSE THE DAMAGE IS NOT APPARENT WITH	 THE CABLE IN THE INSTALLED CONFIGURATION, IT IS POSSIBLE THE CABLE COULD BE LEFT IN SERVICE TO A POINT WHERE IT FAILS.	1	L	7	2 	3O			 	A19S0   					 
1999101500192	19991015	00192	SO  	1999	10	15	99ZZZX3919       	1	19991004	G	2710	62701124	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	FRAYED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	920ER	2637 				4495013				ONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND TO HAVE FRAYED AILERON CABLES.  THE LOCATION OF THE DAMAGE IS AT PULLEYS, PN 62	713-02 AND PN 62713-04.  CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPE	D WITH A CLOTH, SMALL STRANDS CAN BE SEEN AND FELT WHERE THEY ARE BROKEN.  ONCE CABLE IS REMOVED, IT CAN BE BENT TO A SM	ALL RADIUS.  THIS IS WHEN THE FULL EXTENT OF THE DAMAGE CAN BE SEEN.  IN SOME CASES, CABLE WAS AS MUCH AS 40 PERCENT FAI	LED.  FLEET OPER GROUNDED AND REPAIRED THE REMAINING AIRCRAFT.  SUBMITTER STATED BECAUSE THE DAMAGE IS NOT APPARENT WITH	 THE CABLE IN THE INSTALLED CONFIGURATION, IT IS POSSIBLE THE CABLE COULD BE LEFT IN SERVICE TO A POINT WHERE IT FAILS.	1	L	7	2 	3O			 	A19S0   					 
1999101500193	19991015	00193	SO  	1999	10	15	99ZZZX3920       	1	19991004	G	2710	62701143	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	FRAYED          	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	926ER	1670 				4496016				ONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND WITH FRAYED AILERON CABLE.  THE LOCATION OF THE DAMAGE IS AT PULLEYS, PN 62713-	02 AND PN 62713-04.  THE CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPE	D WITH A CLOTH, SMALL STRANDS CAN BE SEEN AND FELT WHERE THEY ARE BROKEN.  ONCE THE CABLE IS REMOVED IT CAN BE BENT TO A	 SMALL RADIUS.  THE CABLE WAS AS MUCH AS 4 PERCENT FAILED.  THE FLEET OPERATOR HAS GROUNDED AND THEN REPAIRED THE REMAIN	ING AIRCRAFT.  SUBMITTER STATED BECAUSE THE DAMAGE IS NOT APPARENT WITH THE CABLE IN THE INSTALLED CONFIGURATION, IT IS 	VERY POSSIBLE THE CABLE COULD BE LEFT IN SERVICE TO A POINT WHERE IT FAILS.	1	L	7	2 	3O			 	A19S0   					 
1999101500194	19991015	00194	SO  	1999	10	15	99ZZZX3921       	1	19991004	G	2710	62701123	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	FRAYED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	926ER	1670 				4496016				ONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND WITH FRAYED AILERON CABLE.  THE LOCATION OF THE DAMAGE IS AT PULLEYS, PN 62713-	02 AND PN 62713-04.  THE CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPE	D WITH A CLOTH, SMALL STRANDS CAN BE SEEN AND FELT WHERE THEY ARE BROKEN.  ONCE THE CABLE IS REMOVED IT CAN BE BENT TO A	 SMALL RADIUS.  THE CABLE WAS AS MUCH AS 4 PERCENT FAILED.  THE FLEET OPERATOR HAS GROUNDED AND THEN REPAIRED THE REMAIN	ING AIRCRAFT.  SUBMITTER STATED BECAUSE THE DAMAGE IS NOT APPARENT WITH THE CABLE IN THE INSTALLED CONFIGURATION, IT IS 	VERY POSSIBLE THE CABLE COULD BE LEFT IN SERVICE TO A POINT WHERE IT FAILS.	1	L	7	2 	3O			 	A19S0   					 
1999101500195	19991015	00195	SO  	1999	10	15	99ZZZX3922       	1	19991004	G	2710	62701124	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	FRAYED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	926ER	1670 				4496016				ONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND WITH FRAYED AILERON CABLE.  THE LOCATION OF THE DAMAGE IS AT PULLEYS, PN 62713-	02 AND PN 62713-04.  THE CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPE	D WITH A CLOTH, SMALL STRANDS CAN BE SEEN AND FELT WHERE THEY ARE BROKEN.  ONCE THE CABLE IS REMOVED IT CAN BE BENT TO A	 SMALL RADIUS.  THE CABLE WAS AS MUCH AS 4 PERCENT FAILED.  THE FLEET OPERATOR HAS GROUNDED AND THEN REPAIRED THE REMAIN	ING AIRCRAFT.  SUBMITTER STATED BECAUSE THE DAMAGE IS NOT APPARENT WITH THE CABLE IN THE INSTALLED CONFIGURATION, IT IS 	VERY POSSIBLE THE CABLE COULD BE LEFT IN SERVICE TO A POINT WHERE IT FAILS.	1	L	7	2 	3O			 	A19S0   					 
1999101500196	19991015	00196	SO  	1999	10	15	99ZZZX3923       	1	19991004	G	2710	62701143	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	FRAYED          	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	925ER	2019 				4496012				ONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND WITH FRAYED AILERON CABLES.  LOCATION OF THE DAMAGE IS AT PULLEYS PN 62713-02 A	ND PN 62713-04.  CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPED WITH A	 CLOTH, SMALL STRANDS CAN BE SEEN AND FELT WHERE THEY ARE BROKEN.  ONCE CABLE IS REMOVED, IT CAN BE BENT TO A SMALL RADI	US.  THIS IS WHEN THE FULL EXTENT OF THE DAMAGE CAN BE SEEN.  IN SOME CASES, THE CABLE WAS AS MUCH AS 40 PERCENT FAILED.	  THE FLEET OPERATOR HAS GROUNDED AND THEN REPAIRED REMAINING ACFT.  SUBMITTER STATED BECAUSE DAMAGE IS NOT APPARENT WIT	H CABLE IN THE INSTALLED CONFIGURATION, IT IS POSSIBLE CABLE COULD BE LEFT IN SERVICE TO A POINT WHERE IT FAILS.	1	L	7	2 	3O			 	A19S0   					 
1999101500197	19991015	00197	SO  	1999	10	15	99ZZZX3924       	1	19991004	G	2710	62701123	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	FRAYED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	925ER	2019 				4496012				ONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND WITH FRAYED AILERON CABLES.  LOCATION OF THE DAMAGE IS AT PULLEYS PN 62713-02 A	ND PN 62713-04.  CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPED WITH A	 CLOTH, SMALL STRANDS CAN BE SEEN AND FELT WHERE THEY ARE BROKEN.  ONCE CABLE IS REMOVED, IT CAN BE BENT TO A SMALL RADI	US.  THIS IS WHEN THE FULL EXTENT OF THE DAMAGE CAN BE SEEN.  IN SOME CASES, THE CABLE WAS AS MUCH AS 40 PERCENT FAILED.	  THE FLEET OPERATOR HAS GROUNDED AND THEN REPAIRED REMAINING ACFT.  SUBMITTER STATED BECAUSE DAMAGE IS NOT APPARENT WIT	H CABLE IN THE INSTALLED CONFIGURATION, IT IS POSSIBLE CABLE COULD BE LEFT IN SERVICE TO A POINT WHERE IT FAILS.	1	L	7	2 	3O			 	A19S0   					 
1999101500198	19991015	00198	SO  	1999	10	15	99ZZZX3925       	1	19991004	G	2710	62701124	CONTROL CABLE   			PIPER 	PA44  	PA44180     	7104402	SO  										AILERON	FRAYED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	925ER	2019 				4496012				ONE AIRCRAFT IN FLEET OF EIGHT WAS FOUND WITH FRAYED AILERON CABLES.  LOCATION OF THE DAMAGE IS AT PULLEYS PN 62713-02 A	ND PN 62713-04.  CABLES APPEAR TO BE IN GOOD CONDITION AT FIRST, BUT WHEN INSPECTED WITH A BRIGHT LIGHT AND WIPED WITH A	 CLOTH, SMALL STRANDS CAN BE SEEN AND FELT WHERE THEY ARE BROKEN.  ONCE CABLE IS REMOVED, IT CAN BE BENT TO A SMALL RADI	US.  THIS IS WHEN THE FULL EXTENT OF THE DAMAGE CAN BE SEEN.  IN SOME CASES, THE CABLE WAS AS MUCH AS 40 PERCENT FAILED.	  THE FLEET OPERATOR HAS GROUNDED AND THEN REPAIRED REMAINING ACFT.  SUBMITTER STATED BECAUSE DAMAGE IS NOT APPARENT WIT	H CABLE IN THE INSTALLED CONFIGURATION, IT IS POSSIBLE CABLE COULD BE LEFT IN SERVICE TO A POINT WHERE IT FAILS.	1	L	7	2 	3O			 	A19S0   					 
1999101500199	19991015	00199	EA  	1999	10	15	99ZZZX3926       	2	19990916	G	8530	60828	PIN PLUG        			PIPER 	PA28  	PA28181     	7102807	SO  	LYC   	O360  	O360A4M     	41514	EA  					NR 1 & 2 CYLS	DESTROYED       	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	09	38735	800  				287790581	L2336736A			OWNER NOTICED A SIGNIFICANT DROP IN OIL PRESSURE DURING FLIGHT AND MADE AN IMMEDIATE LANDING AT THE NEAREST AVAILABLE AI	RPORT.  UPON INSPECTION OF THE OIL FILTER, MUCH ALUMINUM WAS FOUND.  UPON REMOVAL OF THE NR 1 AND NR 2 CYLINDERS, IT WAS	 EVIDENT THE PISTON PIN PLUGS WERE DISINTEGRATING.  POSSIBLE CAUSE - LACK OF USE AND MULTIGRADE OIL/SLUDGE BUILD UP CAUS	ING PLUG TO STICK.  PREVENTION - REGULAR OIL ANALYSIS (SOAP) OR CUTTING OPEN FILTERS INSPECTING EVERY FILTER CHANGE.			1	L	7	1 	3O	3	O		2A13    	E286				 
1999101500200	19991015	00200	EA  	1999	10	15	99ZZZX3927       	2	19990929	G	7240	3028332	CASE            			BEECH 	200   	C12C        		CE  	PWA   	PT6   	PT6A41      	52043	EA  					GAS GENERATOR	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7074G	3872 	382  			7322266	PCE81093			FLOW DIVIDERS WERE BEING SWAPPED TO TROUBLESHOOT STARTING PROBLEM AND A CRACK WAS NOTICED AT THE WELD AREA OF THE FLOW D	IVIDER/FUEL NOZZLE MOUNTING BOSS.  WHEN THE BOSS WAS SLIGHTLY SIDE LOADED WITH A ROD, CRACK OPENED UP VERIFYING THE CASE	 IS CRACKED NOT JUST THE PAINT COATING.				1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999101500202	19991015	00202	NM  	1999	10	15	99ZZZX3929       	1	19990825	G	3220	654620036	NLG             			BOEING	737   	737222      	1384473	NM  										NOSE	CORRODED        	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	135TA	53968			044	19940				DURING CORROSION PREVENTION CONTROL PROGRAM INSPECTION ON NOSE LANDING GEAR, DIFFERENT ASSY COMPONENTS WERE FOUND WITH C	ORROSION, GROOVES, AND WORN OUT.					2	L	7	2 	4F				A16WE   					 
1999012900059	19990129	00059	CE  	1999	1	29	99ZZZX393        	1	19990105	G	5321		FLOORBOARDS     			BEECH 	200   	B200        	1152922	CE  										CABIN	CRACKED         	B	P		DINR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	260G	491  				BB1525				CENTER ISLE FLOORBOARDS FORWARD OF SPAR ARE SPLIT DOWN THE CENTER WITH A SINGLE CAMLOC FASTENER TO HOLD EACH SET OF PANE	LS TOGETHER.  PANELS ARE VERY SPONGY FEELING WHEN WALKED ON, AND THE FORWARD PANEL FLEXES DOWN AND RESTS ON THE NON-STRU	CTURAL THIN PLASTIC COVER OVER THE CURRENT LIMITER PANEL.  MFG RECOMMENDED CROSS-BRACES BE INSTALLED AS NEEDED.  ACFT IS	 3 YEARS OLD.			1	L	7	2 	4T				A24CE   					 
1999101500203	19991015	00203	NM  	1999	10	15	99ZZZX3930       	1	19990825	G	3210	654610012	MLG             	MENASCO     		BOEING	737   	737222      	1384473	NM  										LEFT	CORRODED        	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	135TA	53968			MC04270D	19940				DURING CORROSION PREVENTION CONTROL PROGRAM INSPECTION ON LEFT MAIN LANDING GEAR, DIFFERENT ASSY COMPONENTS WERE FOUND W	ITH CORROSION AND GROOVES.  IN ADDITION, THERE WERE SOME COMPONENTS WITH LOOSE BUSHINGS.					2	L	7	2 	4F				A16WE   					 
1999101500204	19991015	00204	NM  	1999	10	15	99ZZZX3931       	1	19990825	G	3210	654610012	MLG             	MENASCO     		BOEING	737   	737222      	1384473	NM  										RIGHT	CORRODED        	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	135TA	53968			MC04220D	19940				DURING CORROSION PREVENTION CONTROL PROGRAM INSPECTION ON RIGHT MAIN LANDING GEAR, DIFFERENT ASSY COMPONENTS WERE FOUND 	WITH CORROSION, GROOVES, AND WORN OUT.  IN ADDITION, THERE WERE SOME COMPONENTS WITH LOOSE BUSHINGS AND MISSING, LOOSE, 	AND BROKEN RIVET.				2	L	7	2 	4F				A16WE   					 
1999101500205	19991015	00205	SW  	1999	10	15	99ZZZX3932       	1	19990908	G	6320	214040805001	SWITCH          			BELL  	204   	UH1H        	1181407	SW  										TRANSMISSION	MALFUNCTIONED   	B			LS1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	51AG					7120178				TRANSMISSION OIL HOT LIGHT COMES ON INTERMITTENTLY WITH TEMPERATURE IN GREEN.  REMOVED AND REPLACED.						1	G	7	1 	4U				EXPA1G71					 
1999102200001	19991022	00001	NM  	1999	10	22	99ZZZX3933       	1	19990908	G	5754		SKIN            			BOEING	727   	727225      	1384077	NM  										LE FLAP	CRACKED         	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	803MA					22434				APPROXIMATELY .6250 INCH CRACK AT LEFT OUTBOARD FOREFLAP LOWER LEADING EDGE ABOVE NR 1 FLAP TRACK.  FOUND DURING SCHEDUL	ED C-MAINTENANCE CHECK.  AREA EXPOSED TO STRESS LOADS AS WELL AS BENDING LOADS.					2	L	7	3 	4F				A3WE    					 
1999102200002	19991022	00002	NM  	1999	10	22	99ZZZX3934       	1	19990908	G	5315		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 400	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	803MA					22434				CABIN FLOORBEAM STA 400 RBL 12 TO RBL 12LT HAS CORROSION AND DAMAGE HOLE.  FOUND DURING SCHEUDLED C-MAINTENANCE CHECK. A	REA EXPOSED TO ENVIRONMENTAL CHANGES AS WELL AS LIQUID SPILLS, ETC.					2	L	7	3 	4F				A3WE    					 
1999102200003	19991022	00003	NM  	1999	10	22	99ZZZX3935       	1	19990908	G	5720		STIFFENER       			BOEING	727   	727225      	1384077	NM  										RT WING	CRACKED         	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	803MA					22434				ONE INCH CRACK AT TOP OF SECOND FROM AFT STIFFENER INSIDE RT WING LE AT INBOARD SIDE OF LEADING EDGE RIB WBL 92.0, ACCES	S CUT-OUT 6402.  FOUND DURING SCHEDULED C-MAINTENANCE CHECK.  AREA EXPOSED TO STRESS LOADS.					2	L	7	3 	4F				A3WE    					 
1999102200004	19991022	00004	NM  	1999	10	22	99ZZZX3936       	1	19990908	G	5320		ANGLE           			BOEING	727   	727225      	1384077	NM  										BS 1150-1180	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	803MA					22434				CABIN AFT LAVATORY (LEFT SIDE) FLOOR SUPPORT ANGLE AT STA 1150 THROUGH STA 1180 LBL 24 HAS CORROSION.  FOUND DURING SCHE	DULED C-MAINTENANCE CHECK.  SUBMITTER SUGGESTED LIQUID SPILLS ARE POSSIBLE CAUSE FOR PROBLEM.					2	L	7	3 	4F				A3WE    					 
1999102200005	19991022	00005	NM  	1999	10	22	99ZZZX3937       	1	19990908	G	5315		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 1030	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	803MA					22434				CABIN FLOORBEAM ST STA 1030, LBL 24 THROUGH RBL 25 HAS CORROSION.  FOUND DURING SCHEDULED C-MAINTENANCE CHECK.  SUBMITTE	R STATED AREA IS EXPOSED TO LIQUID SPILLS.					2	L	7	3 	4F				A3WE    					 
1999102200006	19991022	00006	NM  	1999	10	22	99ZZZX3938       	1	19990908	G	5720		WEB             			BOEING	727   	727225      	1384077	NM  										WING	CRACKED         	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	803MA					22434				LEFT WING LEADING EDGE LBL 92.0 WEB CRACKED 1.5 INCHES DOWN FROM TOP AFT VERTICAL STIFFENER.  ACCESS 6302.  FOUND DURING	 SCHEDULED C-MAINTENANCE CHECK.  SUBMITTER SUGGESTED WING FLEX OR STRESS LOADS POSSIBLE CAUSE.					2	L	7	3 	4F				A3WE    					 
1999102200007	19991022	00007	NM  	1999	10	22	99ZZZX3939       	1	19990908	G	5720		STIFFENER       			BOEING	727   	727225      	1384077	NM  										RT WING	CRACKED         	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	803MA					22434				ONE INCH CRACK AT TOP OF STIFFENER INSIDE RIGHT WING LEADING EDGE AT INBOARD SIDE OF LEADING EDGE RIB WDL 92.0.  FOUND D	URING SCHEDULED C-MAINTENANCE CHECK.  SUBMITTER SUGGESTED AREA SUBJECTED TO STRESS LOADS AND FLEX.					2	L	7	3 	4F				A3WE    					 
1999102200008	19991022	00008	NM  	1999	10	22	99ZZZX3940       	1	19990908	G	5311		FRAME           			BOEING	727   	727225      	1384077	NM  										FUSELAGE	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	803MA					22434				LEFT AFT EXIT HATCH FRAME HAS SIGNS OF CORROSION AT LOWER AFT CORNER.  FOUND DURING SCHEDULED C-CHECK.  SUBMITTER STATED	 AREA EXPOSED TO MOISTURE AND OTHER ELEMENTS.					2	L	7	3 	4F				A3WE    					 
1999102200009	19991022	00009	NM  	1999	10	22	99ZZZX3941       	1	19990908	G	5320		WEB             			BOEING	727   	727225      	1384077	NM  										BS 400	CRACKED         	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	803MA					22434				CABIN FLOOR SUPPORT INTERCOSTAL WEB HAS APPROXIMATELY .25 INCH CRACK AT FORWARD END JUST AFT OF BS 400 AT BL ZERO.  FOUN	D DURING C-MAINTENANCE CHECK.  SUBMITTER SUGGESTED AREA EXPOSED TO HEAVY LOADS, STRESS.					2	L	7	3 	4F				A3WE    					 
1999102200010	19991022	00010	NM  	1999	10	22	99ZZZX3942       	1	19990908	G	5260		AIRSTAIR        			BOEING	727   	727225      	1384077	NM  										BS 1263	CRACKED         	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	803MA					22434				AFT AIRSTAIRS, AREA AT RIGHT, STA 1263 JUST BELOW ACTUATOR ATTACH FITTING, AREA CRACKED.  FOUND DURING C-MAINTENANCE CHE	CK.  OPENING AND CLOSING OF STAIRS CAUSED AREA TO BE UNDER CONSTANT PRESSURE.					2	L	7	3 	4F				A3WE    					 
1999102200011	19991022	00011	NM  	1999	10	22	99ZZZX3943       	1	19990908	G	5720		BEAM            			BOEING	727   	727225      	1384077	NM  										RT WING	CRACKED         	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	803MA					22434				RIGHT WING J-BEAM HAS APPROXIMATELY .3750 INCH CRACK ABOVE NR 8 SPOILER ACTUATOR.  FOUND DURING SCHEDULED C-MAINTENANCE 	CHECK.  SUBMITTER STATED DESIGN FLAW OR WING FLEX CAUSE OF CRACK.					2	L	7	3 	4F				A3WE    					 
1999102200012	19991022	00012	NM  	1999	10	22	99ZZZX3944       	1	19990929	G	5320		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 1130	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	887MA					21857				CABIN FLOORBEAM AT STA 1130 RBL 36 HAS CORROSION AROUND SCREW HOLES.  FOUND DURING SCHEDULED C-MAINTENANCE CHECK.  SUBMI	TTER STATED POSSIBLE CAUSE AS LIQUID SPILLS OR DISSIMILAR METAL.					2	L	7	3 	4F				A3WE    					 
1999102200013	19991022	00013	NM  	1999	10	22	99ZZZX3945       	1	19990929	G	5320		FLOORBEAM       			BOEING	727   	727225      	1384077	NM  										BS 344	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	887MA					21857				CABIN FLOORBEAM STA 344 RBL 24 TO WALL HAS CORROSION.  FOUND DURING SCHEDULED C-MAINTENANCE CHECK.  SUBMITTER STATED POS	SIBLE CAUSE AS LIQUID SPILLS OR DISSIMILAR METAL.					2	L	7	3 	4F				A3WE    					 
1999102200014	19991022	00014	NM  	1999	10	22	99ZZZX3946       	1	19990929	G	5720		BEAM            			BOEING	727   	727225      	1384077	NM  										RT WING	CRACKED         	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	887MA					21857				RIGHT WING TRAILING EDGE J-BEAM CRACKED (.3750 INCH) ABOVE NR 8 SPOILER ACTUATOR.  FOUND DURING SCHEDULED C-MAINTENANCE 	CHECK.  SUBMITTER SUGGESTED POSSIBLE CAUSE AS DESIGN FLAW OR WING FLEXING LOADS.					2	L	7	3 	4F				A3WE    					 
1999102200015	19991022	00015	NM  	1999	10	22	99ZZZX3947       	1	19990929	G	5720		ANGLE           			BOEING	727   	727225      	1384077	NM  										RT WING	CRACKED         	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	887MA					21857				LOWER TRAILING EDGE PANEL BELOW NR 8 SPOILER ACTUATOR (FALSE SPAR) LOWER CHORD ANGLE CRACKED.  FOUND DURING SCHEDULED C-	MAINTENANCE CHECK.  SUBMITTER SUGGESTED POSSIBLE CAUSE AS WING FLEXING LOADS.					2	L	7	3 	4F				A3WE    					 
1999102200016	19991022	00016	NM  	1999	10	22	99ZZZX3948       	1	19990927	G	5320	652427624	TIE             			BOEING	727   	727251      	138408H	NM  										BS 1183	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON TENSION TIES FS 1183 - 29R AND 23L.						2	L	7	3 	4F				A3WE    					 
1999102200017	19991022	00017	NM  	1999	10	22	99ZZZX3949       	1	19990918	G	5320	652427649	TIE             			BOEING	727   	727251      	138408H	NM  										BS 1183	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON TENSION TIE STR 17 FS 1183.						2	L	7	3 	4F				A3WE    					 
1999102200018	19991022	00018	NM  	1999	10	22	99ZZZX3950       	1	19990927	G	5320		WEB             			BOEING	727   	727251      	138408H	NM  										BS 770	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON KEEL BEAM WEB STA 770.						2	L	7	3 	4F				A3WE    					 
1999102200019	19991022	00019	NM  	1999	10	22	99ZZZX3951       	1	19990927	G	5320		ANGLE           			BOEING	727   	727251      	138408H	NM  										BS 812	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON T-ANGLE STA  812 KEEL BEAM.						2	L	7	3 	4F				A3WE    					 
1999102200020	19991022	00020	NM  	1999	10	22	99ZZZX3952       	1	19990927	G	5320		FLOOR PAN       			BOEING	727   	727251      	138408H	NM  										CABIN	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON FLOOR PAN, RT AFT LAVATORY.						2	L	7	3 	4F				A3WE    					 
1999102200021	19991022	00021	NM  	1999	10	22	99ZZZX3953       	1	19990927	G	5320		ANGLE           			BOEING	727   	727251      	138408H	NM  										CABIN	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED LT AFT LAVATORY FORWARD WALL HAT CHANNEL AND SUPPORT ANGLES.						2	L	7	3 	4F				A3WE    					 
1999102200022	19991022	00022	NM  	1999	10	22	99ZZZX3954       	1	19990927	G	5320		CHANNEL         			BOEING	727   	727251      	138408H	NM  										CABIN	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED LT AFT LAVATORY FORWARD WALL HAT CHANNEL AND SUPPORT ANGLES.						2	L	7	3 	4F				A3WE    					 
1999102200023	19991022	00023	NM  	1999	10	22	99ZZZX3955       	1	19990927	G	5320		ANGLE           			BOEING	727   	727251      	138408H	NM  										CABIN	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON RT AFT LAVATORY WALL HAT CHANNEL AND ATTACH ANGLES.						2	L	7	3 	4F				A3WE    					 
1999102200024	19991022	00024	NM  	1999	10	22	99ZZZX3956       	1	19990927	G	5320		CHANNEL         			BOEING	727   	727251      	138408H	NM  										CABIN	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON RT AFT LAVATORY WALL HAT CHANNEL AND ATTACH ANGLES.						2	L	7	3 	4F				A3WE    					 
1999102200025	19991022	00025	NM  	1999	10	22	99ZZZX3957       	1	19990927	G	5347		SEAT TRACK      			BOEING	727   	727251      	138408H	NM  										BS 344-380	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED AT FS 344 - FS 380 (RT) SEAT TRACK.						2	L	7	3 	4F				A3WE    					 
1999102200182	19991022	00182	SW  	1999	10	22	99ZZZX3962       	1	19990901	G	5230	35009099511	BAGGAGE DOOR    			MOONEY	M20   	M20J        	5870219	SW  										NOSE	SEPARATED       	D		A		O				OTHER                   				D			INFLIGHT SEPARATION       			NR	NOT REPORTED   	1			SO	15	57259	1912 				241435				BAGGAGE DOOR CAME OPEN IN-FLIGHT.  CAUSE UNKNOWN.  DOOR LATCH AD HAD BEEN C/W.  NO ACCIDENT OCCURRED.  DOOR WAS REPLACED	 WITH NEW DOOR.					1	L	7	1 	3O				2A3     					 
1999102200183	19991022	00183	SW  	1999	10	22	99ZZZX3963       	1	19990924	G	3230	560011	JOHNSON BAR     			MOONEY	M20   	M20D        	5870210	SW  										NLG	SHEARED         	D		A		O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			SO	15	6830U					201				LANDING GEAR RETRACTION HANDLE ASSY ('JOHNSON BAR') SHEARED ENTIRE CIRCUMFERENCE WHERE HANDLE ATTACHES TO BELLCRANK ARM 	BELOW CABIN FLOORBOARDS.  CRACK WAS FRESH WITH NO INDICATION OF PRIOR EXISTING DAMAGE.  SEPARATION OF HANDLE FROM CRANK 	ASSY OCCURRED AT APPROXIMTELY 5 MPH TAXI RESULTING IN PROPELLER STRIKE AND LOWER NOSE COWL WHEN ALL GEAR RETRACTED.  GEA	R HANDLE WAS STILL DAMAGED IN THE 'DOWN AND LOCKED' POSITION AND THE GEAR INDICATOR LIGHT SHOWED GEAR DOWN.			1	L	7	1 	3O				2A3     					 
1999102200184	19991022	00184	CE  	1999	10	22	99ZZZX3964       	1	19990901	G	3210	458250721	DRAG BRACE      			BEECH 	58    	58          	1152740	CE  										NLG	FAILED          	B		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	58GP	5024 				TH40				FOUND RIGHT ARM OF DRAG BRACE BROKEN JUST FORWARD OF RETRACTION ROD ATTACHMENT.  THIS BRACE WAS FOUND TO BE THE OLD STYL	E, STEEL TUBE TYPE.  THERE WAS SEVERE INTERNAL CORROSION OF THE TUBE THAT WAS NOT DETECTABLE BY NORMAL INSPECTION PROCED	URES.  THE BREAK WAS AT THE LEADING EDGE OF THE CLUSTER WELD AND APPEARS TO HAVE STARTED TO CRACK THERE.  THE NEW STYLE 	DRAG BRACE IS MADE OF ALUMINUM.  SUBMITTER SUGGESTED REPLACEMENT OF THE OLD STYLE WITH THE NEW TO PREVENT ANY FUTURE FAI	LURES.		1	L	7	2 	3O				3A16    					 
1999102200185	19991022	00185	CE  	1999	10	22	99ZZZX3965       	1	19990921	G	2701	9652402915	COLUMN          			BEECH 	36    	A36         	1151604	CE  										CONTROL WHEEL	BROKE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	25	9136Q					E248				REF:  AD 71-24-10 AND BEECH SI 0254-156 REV IV.  AD HAD BEEN C/W ON AIRCRAFT.  UNKNOWN IF ORIGINAL PART.  THE ADAPTER SH	AFT AND ADAPTER PLATE BROKE APART AT WELD.  ALTHOUGH THE CORRECT NEW PART NUMBER HAD BEEN INSTALLED, THE ADDITIONAL WELD	 AS SHOWN IN FIG 4 OF SI HAD NOT BEEN ACCOMPLISHED ON NEW PART.  SUBMITTER RECOMMENDED ALL AIRCRAFT RECEIVE NEW REVISED 	PART NUMBER.			1	L	7	1 	3O				3A15    					 
1999102200186	19991022	00186	SW  	1999	10	22	99ZZZX3966       	1	19990920	G	2560	4530150	ELT             	ARTEX       		GULSTM	560   	560         	0141402	SW  										CABIN	FAILED          	B			AC1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	356WC	1144 			585586	5600432				WHILE PERFORMING A PHASE 18 INSPECTION, THE ELT WAS FOUND INOPERABLE.  INSPECTION OF THE ELT REVEALED A BURNED AREA ON T	HE PRINTED CIRCUIT BOARD APPROXIMATELY THE SIZE OF A NICKEL.  IN ADDITION, THE BATTERY CASE HAD CRACKED IN THE MIDDLE AN	D THE BATTERIES INSIDE HAD CORROSION.  APPARENTLY, PART OF THE PRINTED CIRCUIT BOARD SHORTED OUT AND CAUSED THE BATTERIE	S TO RUN DOWN.  THE ELT HAD NOT ACTIVATED WHEN THE PRINTED CIRCUIT BOARD SHORTED.  SUBMITTER UNSURE WHAT CAUSED THE CASE	 TO CRACK UNLESS IT WAS IN A STRAIN AFTER INSTALL.  THE ELT WAS LAST INSPECTED ON 9-23-98 AND THE BATTERY REPLACED AT TH	AT TIME.  A NEW ELT WAS INSTALLED.	1	H	7	2 	3O				6A1     					 
1999102200187	19991022	00187	WP  	1999	10	22	99ZZZX3967       	1	19990908	G	2842	369D263039	TRANSMITTER     			HUGHES	369   	369E        	4470707	WP  										FUEL SYSTEM	LEAKING         	B			LS1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	13	8330P				1042	0330E				FUEL FOUND ON TOP OF FUEL CELL.  SENDER LEAKING INTERNALLY.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999102200188	19991022	00188	EA  	1999	10	22	99ZZZX3968       	2	19990921	G	7414	10382807	CONDENSER       			ENSTRM	F28   	280F        	3300550	GL  	LYC   	O360  	HIO360F1AD  	41514	EA  					MAGNETO	FAILED          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	01	199TV	42   				1510	L2413451A			PILOT REPORTED A ONE PER REV VIBRATION ON BURP IN HELICOPTER DURING FLIGHT.  DURING A MAGNETO CHECK, ENGINE WOULD CONTIN	UE TO RUN WITH IGNITION IN OFF POSITION.  MAGNETO WAS REMOVED AND SENT TO ARN-AIR FOR INSPECTION.  IT WAS FOUND THAT ONE	 CONDENSER FAILED BURNING OUT THE POINTS.  THE OTHER CONDENSER HAD AN OPEN CIRCUIT AND WOULD HAVE FAILED ALSO.  BOTH CON	DENSERS AND POINTS HAD TO BE REPLACED IN THIS.  MAGNETO DATE CODE:  98-23.			1	G	7	1 	3O	3	O		H1CE    	1E10				 
1999102200189	19991022	00189	NE  	1999	10	22	99ZZZX3969       	2	19990930	G	7250	2292253940	BLADE           		0292253250  	SNIAS 	350   	AS350B2     	8680813	EU  	TMECA 	ARRIEL	ARRIEL1D    		NE  					GAS GENERATOR	FAILED          	D		A		O				OTHER                   				E			VIBRATION/BUFFET          			AP	APPROACH       	1			WP	13	992BH	1661 			ADD0687YC	2889	9414			HELICOPTER WAS ON A FINAL APPROACH TO LANDING SITE ON ISLAND OF KAHOOLAWE, HAWAII.  PILOT EXPERIENCED A YAW TO THE ACFT.	  HE MADE A NORMAL LANDING ON THE HELIPAD AND SHUT DOWN ENGINE.  POST-FLIGHT CHECK REVEALED THE POWER TURBINE BLADES WER	E DAMAGED.  UPON DISASSEMBLY AND INSPECTION OF ENGINE, DETERMINED THE SECOND STAGE GAS GENERATOR TURBINE BLADE BROKE AWA	Y AT THE ROOT AND CAUSED ADDITIONAL DAMAGE TO THE SECOND STAGE GAS GENERATOR BLADES, POWER TURBINE NOZZLE, AND POWER TUR	BINE BLADES.  SIGNIFICANT RUBBING WAS EVIDENT ON COMPRESSOR, GAS GENERATOR, AND POWER TURBINE COMPONENTS.		1	G	7	1 	3U	3	U		H9EU    	E19EU				 
1999102200190	19991022	00190	EU  	1999	10	22	99ZZZX3970       	1	19990913	G	2910	DSQ2018846	SWITCH          			SNIAS 	350   	AS350B      	8680801	EU  										COCKPIT	FAILED          	H				A				UNSCHED LANDING         				L	J		NO TEST                   	WARNING INDICATION        		NR	NOT REPORTED   	1			SW	99	350EC	746  				2354				INSTALLED NEW SWITCH, OPS CHECKED TEST FUNCTION OF SWITCH AND TEST FLEW AIRCRAFT.						1	G	7	1 	3U				H9EU    					 
1999102200191	19991022	00191	EU  	1999	10	22	99ZZZX3971       	1	19990920	G	7732	25W881011001	VIBMETER        			ISRAEL	1125  	ASTRASPX    	4500205	EU  										COCKPIT	STUCK           	B			QRRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	275RA	754  			B120	098				NEEDLE STUCK DURING TEST.  REPLACED WITH SERVICEABLE UNIT.						2	L	7	2 	4F			RT	A16NM   					 
1999102200192	19991022	00192	CE  	1999	10	22	99ZZZX3972       	1	19990823	G	5210	504300377	ROLLER          		1014300323  	BEECH 	200   	200BEECH    	1152920	CE  										PASSENGER DOOR	MISSING         	B			AKGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	05	280SC	5714 				BB664				FOUND THE ROLLER FOR THE TOP FORWARD SIDE BOLT GUIDES MISSING.  THIS ALLOWED THE BOLT TO COME INTO CONTACT WITH THE CABI	N DOOR SIDE FRAME AND CUT A .25 INCH BY .25 INCH SLOT INTO THE FRAME.  AFTER FURTHER INSPECTION OF THE REST OF THE SIDE 	BLOCKS THE TOP AFT BLOCK WAS FOUND WITH THE PIN FOR THE ROLLER MIGRATING OUT.  BOTH BLOCKS AND ROLLER ASSEMBLIES WERE RE	PLACED.  THE DAMAGE TO THE DOOR SIDE FRAME WAS REPAIRABLE THIS TIME WITH LITTLE WORK.  IF IT HAD GONE ON LONGER, THE DAM	AGE TO THE DOOR WOULD HAVE BEEN HARDER TO REPAIR.		1	L	7	2 	4T				A24CE   					 
1999102200193	19991022	00193	EU  	1999	10	22	99ZZZX3973       	1	19990913	G	2435		BEARING         		23079009    	BAG   	JETSTM	JETSTM3101  	1500215	EU  	GARRTT	TPE331	TPE33110U   	01514	WP  					STARTER/GEN	WORN            	B			CWQR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05	411MX		670  		3899	660	42122			STARTER/GENERATOR BEARINGS WORN.  CAUSED RESONANT VIBRATION THAT CRACKED OIL LINE.						2	L	7	2 	4T	4	T	RT	A21EU   	E4WE				 
1999102200194	19991022	00194	CE  	1999	10	22	99ZZZX3974       	1	19990901	G	2460	DDMA50S	CONNECTOR       	COLLINS     	6226290001  	LEAR  	55    	55LEAR      	5170702	CE  										TAILCONE	MISMANUFACTURED 	D	P			K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	19	277AL					104				DURING TROUBLESHOOTING, A TRANSPONDER IDENTS ALL THE TIME.  AVIONICS TECH DETERMINED THERE WAS A SHORT IN CANON PLUG RP7	38.  WHEN PLUG WAS DISASSEMBLED, HE FOUND THE WIRES AND PINS WERE IMPROPERLY INSTALLED WITH WIRE INSULATION CUT BACK TOO	 FAR LEAVING BARE WIRES INSIDE THE PLUG.  SOME WIRES WERE TOUCHING EACH OTHER.  A BRIEF LOG SERCH WAS CONDUCTED, BUT NO 	WORK IN THIS AREA IN THE RECENT PAST WAS DISCOVERED.			2	L	7	2 	4F				A10CE   					 
1999102200195	19991022	00195	WP  	1999	10	22	99ZZZX3975       	1	19990908	G	3150	369AU5143	WARNING UNIT    			HUGHES	369   	369D        	4470706	WP  										COCKIT	MALFUNCTIONED   	B			LS1R	O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			EA	13	369AW				2595	U70117D				EPO BOX HAS ENGINE OUT LIGHT AND WARNING HORN ACTIVATED DURING FLIGHT.  REMOVED AND REPLACED.						1	G	7	1 	3U				H3WE    					 
1999102200196	19991022	00196	NE  	1999	10	22	99ZZZX3976       	2	19990809	G	7250	30740971	ROTOR ASSY      			AMD   	FALC50	FALCON50MYST	2730106	EU  	GARRTT	TFE731	TFE73131C   	01518	NE  					POWER TURBINE	WORN            	B			MJ1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	11	881M					83	P76387			UPON DISASSEMBLY OF ENGINE, 3RD LPT ROTOR ASSY, PN 3074097-1, SN 965332200333 ROTOR, TSN 1,309.6 HOURS, CSN, 921, WAS NO	TED TO HAVE BEEN RUB-DAMAGED ON FORWARD SIDE OF ROTOR DISK JUST INSIDE OF BLADE RETENTION RIVET AREA (FIR TREE).  DAMAGE	 APPEARS TO BE FROM CONTACT WITH 3RD LPT STATOR ASSY SEAL.  STATOR, PN 3072342-4, SN 2-01334-192.  ALLIED SIGNAL AEROSPA	CE, ENGINEERING DEPT., HAS BEEN ADVISED OF THIS CONDITION.  ENG, SN P76387.  TSN:  8,081.5 HOURS.  CSN:  5,635.			2	L	7	3 	4F	4	F		A46EU   	E6WE				 
1999102200197	19991022	00197	NE  	1999	10	22	99ZZZX3977       	2	19990831	G	7230	30770496	DIFFUSER        								GARRTT	TFE731	TFE73131C   	01518	NE  					COMPRESSOR	FRACTURED       	B			UO2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19					IP567		P76239			PIECE BROKEN OUT AT THE4 O'CLOCK POSITION 1.5 INCHES BY 1.0 INCH AREA.  CAUSED DAMAGE TO BACKFACE OF HP IMPELLER.  ALLIE	D SIGNAL HAS BEEN NOTIFIED.  PART WILL BE RETURNED TO ALLIED SIGNAL FOR ENGINEERING EVALUATION.										4	F			E6WE				 
1999102200198	19991022	00198	NE  	1999	10	22	99ZZZX3978       	2	19990812	G	7314	2345119059	BOLT            		GTCP36100A  	AMD   	FALC50	FALCON50MYST	2730106	EU  	GARRTT	TFE731	TFE73131C   	01518	NE  					FUEL PUMP CLAMP	FAILED          	B			UO2R	O				OTHER                   				X	J		ENGINE FLAMEOUT           	WARNING INDICATION        		NR	NOT REPORTED   	1			GL	19	8550A	459  			P373	263				APU SHUT DOWN DURING START.  NOTICED OIL DRIPPING FROM OVERBOARD DRAIN.  INVESTIGATION REVEALED APU FUEL CLAMP BOLT FAIL	ED AND FUEL PUMP DISENGAGED FROM ACCESSORY HOUSING.  BOLT SHOWED PREVIOUS FRACTURE, POSSIBLE OVERTORQUE.  NO DAMAGE TO F	UEL PUMP.  TORQUE IS SUPPOSED TO BE 25 INCHES/POUNDS.				2	L	7	3 	4F	4	F		A46EU   	E6WE				 
1999102200199	19991022	00199	CE  	1999	10	22	99ZZZX3979       	1	19990827	G	2150	11555502615	ROD END         			BEECH 	200   	B200        	1152922	CE  										NR 2 ENGINE	BENT            	B	P	A	DINR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	260G	654  				BB1525				DURING ROUTINE POST-FLIGHT INSPECTION, FOUND ROD-END, PN 115-555026-15 (FOR THE FREON COMPRESSOR BELT TENSIONER), BENT A	PPROXIMATELY 10 DEGREES.  REPLACED PART WITH NEW.					1	L	7	2 	4T				A24CE   					 
1999102200201	19991022	00201	EU  	1999	10	22	99ZZZX3981       	1	19991001	G	3310	ASTARA313	BULB            			AMD   	FALCON	FALCON20    	2730103	EU  										COCKPIT	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	620A					412				THE RIGHT WING VENT VALVE PULSATED AND EVENTUALLY WOULD NOT CLOSE AFTER FUELING OR VENTING OF TANKS.  AN ASTARA 313 BULB	 WAS INSTALLED IN THE 'GREEN' FUEL AUTHORIZATION LIGHT SOCKET.  THIS WORKED FOR AWHILE, THEN APPARENTLY FAILED IN SOME M	ANNER BECAUSE THE BULB STILL ILLUMINATED.  SUBMITTER RECOMMENDED MAKING SURE THE CORRECT BULB IS INSTALLED IN THE FUEL A	UTHORIZATION LIGHTS OF THE FALCON 20, THESE BEING P/N ASTARA 1820			2	L	7	2 	4F			RT	A7EU    					 
1999102200202	19991022	00202	WP  	1999	10	22	99ZZZX3982       	2	19990901	G	7240	8939735	CASE            			MTSBSI	MU2   	MU2B36A     	5780413	CE  	GARRTT	TPE331	TPE3315     	01514	WP  					COMB CHAMBER	FAILED          	G	P			C				ABORTED TAKEOFF         				A			FLAME/FIRE                			TO	TAKEOFF        	1			SW	15	3UN		5281 			720SA	P33039			THE COMBUSTION CASE ASSY FAILED ALONG THE ENTIRE LENGTH OF THE MFG WELD.  AIRCRAFT WAS ON TAKEOFF ROLL RESULTING IN AN A	BORTED TAKEOFF AND FIRE IN THE NACELLE.  NOTE:  LOG BOOK ENTRY 3-25-96 ON OVERTEMP INSP C/W TSO 4,397.0 HOURS APPROX 884	.2 HRS PRIOR TO FAILIURE.				1	H	7	2 	3T	4	T		A10SW   	E4WE				 
1999102200203	19991022	00203	NM  	1999	10	22	99ZZZX3983       	1	19990927	G	5320		SUPPORT         			BOEING	727   	727227      	1384078	NM  										BS 950	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED AT FS 950A-950E, LBL 4, 6, 12, AND 16 ON FLOOR SUPPORTS.						2	L	7	3 	4F				A3WE    					 
1999102200204	19991022	00204	SO  	1999	10	22	99ZZZX3984       	1	19990929	G	3320	AL5112	POWER SUPPLY    			GULSTM	G1159 	G1159       	3953505	SO  										CABIN	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	154C	1611 			2526	253				WHILE THE AIRCRAFT WAS POWERED UP ON THE GROUND, PRIOR TO A TRIP, FLIGHT MECHANIC NOTICED A LARGE AMOUNT OF WHITE SMOKE 	COMING FROM UNDER THE VALANCE PANEL ON LEFT SIDE OF CABIN AND ONE OF THE FLUORESCENT BULBS NOT ILLUMINATING.  CIRCUIT BR	EAKERS FOR ALL FLUORESCENT LIGHTS WERE PULLED AS A PRECAUTION.				2	L	7	2 	4F			RT	A12EA   					 
1999102200205	19991022	00205	WP  	1999	10	22	99ZZZX3985       	1	19990908	G	5314		KEEL BEAM       			DOUG  	DC8   	DC863       	302198A	WP  										BS 730-742	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	950R					45903				KEEL BEAM HAS SURFACE CORROSION, STA 730 AND STA 742 WHERE SKIN WAS OPENED FOR INSPECTION OF AREA.  FOUND DURING SCHEDUL	ED C MAINTENANCE CHECK.  AREA EXPOSED TO ENVIRONMENTAL CHANGES.					2	L	7	4 	4F				4A25    					 
1999102200206	19991022	00206	NM  	1999	10	22	99ZZZX3986       	1	19990927	G	5320		BRACKET         			BOEING	727   	727230      	1384080	NM  										BS 720	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON BRACKET AT STR 26R STA 720B.						2	L	7	3 	4F				A3WE    					 
1999102200207	19991022	00207	NM  	1999	10	22	99ZZZX3987       	1	19990927	G	5320		BRACKET         			BOEING	727   	727230      	1384080	NM  										BS 660	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON BRACKET AT STR 26R STA 660.						2	L	7	3 	4F				A3WE    					 
1999102200208	19991022	00208	NM  	1999	10	22	99ZZZX3988       	1	19990927	G	5320		BRACKET         			BOEING	727   	727230      	1384080	NM  										BS 660	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON BRACKET AT STR 26L STA 660.						2	L	7	3 	4F				A3WE    					 
1999102200209	19991022	00209	NM  	1999	10	22	99ZZZX3989       	1	19990927	G	5320		BRACKET         			BOEING	727   	727230      	1384080	NM  										BS 620	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON BRACKET AT STR 26L STA 620.						2	L	7	3 	4F				A3WE    					 
1999102200210	19991022	00210	NM  	1999	10	22	99ZZZX3990       	1	19990927	G	5320		BRACKET         			BOEING	727   	727230      	1384080	NM  										BS 560	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON BRACKET AT STR 26L STA 560.						2	L	7	3 	4F				A3WE    					 
1999102200211	19991022	00211	NM  	1999	10	22	99ZZZX3991       	1	19990927	G	5320		BRACKET         			BOEING	727   	727230      	1384080	NM  										BS 580	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON BRACKET AT STR 26L STA 580.						2	L	7	3 	4F				A3WE    					 
1999102200212	19991022	00212	NM  	1999	10	22	99ZZZX3992       	1	19990927	G	5320		BRACKET         			BOEING	727   	727230      	1384080	NM  										BS 540	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	3003F					21619				DURING A C-CHECK, CORROSION WAS NOTED ON BRACKET AT STR 26L, STA 540.						2	L	7	3 	4F				A3WE    					 
1999102200213	19991022	00213	NM  	1999	10	22	99ZZZX3993       	1	19990927	G	5347		SEAT TRACK      			BOEING	727   	727230      	1384080	NM  										BS 380-400	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 380 - STA 400, RBL 18.						2	L	7	3 	4F				A3WE    					 
1999102200214	19991022	00214	NM  	1999	10	22	99ZZZX3994       	1	19990927	G	5320		WEB             			BOEING	727   	727230      	1384080	NM  										BS 720	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON WEB OF WING TO BODY FAIRING BS 720F STR 28L - STR 28R (ALSO 4 EACH ATTACH ANGLE	S).					2	L	7	3 	4F				A3WE    					 
1999102200215	19991022	00215	NM  	1999	10	22	99ZZZX3995       	1	19990927	G	5311		FRAME           			BOEING	727   	727230      	1384080	NM  										BS 1090	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON FRAME, BS 1090 AT STR 27R.						2	L	7	3 	4F				A3WE    					 
1999102200216	19991022	00216	NM  	1999	10	22	99ZZZX3996       	1	19990927	G	5315		FLOORBEAM       			BOEING	727   	727230      	1384080	NM  										BS 380	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED AT STA 380 RBL 3, FLOORBEAM UPPER FLANGE.						2	L	7	3 	4F				A3WE    					 
1999102200217	19991022	00217	NM  	1999	10	22	99ZZZX3997       	1	19990927	G	5315		FLOORBEAM       			BOEING	727   	727230      	1384080	NM  										BS 380	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM UPPER FLANGE STA 380 RBL 24.						2	L	7	3 	4F				A3WE    					 
1999102200218	19991022	00218	NM  	1999	10	22	99ZZZX3998       	1	19990927	G	5313		STRINGER        			BOEING	727   	727230      	1384080	NM  										BS 1183	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON STR 26R STA 1183.						2	L	7	3 	4F				A3WE    					 
1999102200219	19991022	00219	NM  	1999	10	22	99ZZZX3999       	1	19990927	G	5320		WEB             			BOEING	727   	727230      	1384080	NM  										BS 950A-950B	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON WEB AT STA 950A - STA 950B APPROX STR 28R.						2	L	7	3 	4F				A3WE    					 
1999102200220	19991022	00220	EU  	1999	10	22	99ZZZX4000       	1	19991005	G	3250	AIR133994	LEVER           		AIR860124   	JETAIR	JETSTM	JETSTM4101  	1500501	EU  										NLG STEERING	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		9834 			APB950368					STEERING INPUT LEVER WAS INSTALLED 180 DEGREES FROM  CORRECT POSITION WHEN RETURNED TO REPAIR BY THE AIRLINE.  THE UNIT 	WAS RETURNED FOR NOT FUNCTIONING WHICH THIS ERROR WOULD CAUSE (CSN 9,083).					2	L	7	2 	4T			RT	A41NM   					 
1999102200221	19991022	00221	NM  	1999	10	22	99ZZZX4001       	1	19990923	G	2722	69778551	SPRING          		65C347517   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		44219	24424		KEO0275					SPRINGS, PN 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT TREATING, AUSTENITE, FATIGUE, AND INCRE	ASED SPRING COIL STRESSES.  SPRINGS, PN 69-77855-1, ARE TO BE REPLACED WITH PN 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLIES	 MANUFACTURED PRIOR TO S/N KEO1730 PER BOEING SL 737-SL-27-090-B.				2	L	7	2 	4F			RT	A16WE   					 
1999102200222	19991022	00222	NM  	1999	10	22	99ZZZX4002       	1	19990917	G	2722	69778551	SPRING          		654997025   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		30412	19051		KEO0826					SPRINGS, P/N 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE, AND INCR	EASED SPRING OIL STRESSES.  SPRINGS, P/N 69-77855-1, ARE TO BE REPLACED WITH P/N 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLI	ES MANUFACTURED PRIOR TO S/N KEO1730 PER BOEING SL 737-SL-27-090-B.				2	L	7	2 	4F			RT	A16WE   					 
1999102200223	19991022	00223	NM  	1999	10	22	99ZZZX4003       	1	19990917	G	2722	69778551	SPRINGS         		654997025   	BOEING	737   	737*        		NM  										HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		19139			KEO1674					SPRINGS, P/N 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE AND INCRE	ASED SPRING COIL STRESSES.  SPRINGS, P/N 69-77855-1 ARE TO BE REPLACED WITH P/N 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLIE	S MANUFACTURED PRIOR TO S/N KEO1730 PER BOEING SL 737-SL-27-090-B.				2	L	7	2 	4F			RT	A16WE   					 
1999102200224	19991022	00224	NM  	1999	10	22	99ZZZX4004       	1	19990922	G	3230	65446924	HOUSING         		65446915    	BOEING	737   	737*        		NM  										MLG MODULE	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01			59229		1080					HOUSING IS CRACKED AT THE BOTTOM OF PRIORITY PORTS.  OVERSTRESSED, FATIGUE.						2	L	7	2 	4F			RT	A16WE   					 
1999102200225	19991022	00225		1999	10	22	99ZZZX4005       	1	19990819	G	3230	2672232	VALVE           	PARKERHANFIN	2670296     															MLG	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					294					BODY IS CRACKED AT UP AND DOWN PORTS.  FATIGUE, OVERSTRESSED.																			 
1999102200226	19991022	00226		1999	10	22	99ZZZX4006       	1	19990819	G	3230	2672232	VALVE           	PARKERHANFIN	2670296     															MLG	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					H633C020					BODY IS CRACKED AT UP AND DOWN PORTS.  FATIGUE, OVERSTRESSED.																			 
1999102200227	19991022	00227	NM  	1999	10	22	99ZZZX4007       	1	19990917	G	2720	3171001003	SENSOR          	MOOG        	33215205    	BOEING	757   	7572G7      	1384963	NM  										RUDDER	DAMAGED         	B	P		IU6R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	01	909AW	1308 			0952	24522				BASE OF LEAD WIRE FOUND PINCHED AND/OR BROKEN AT COIL CAUSING A FAILURE IN THE SENSOR ASSY OF THE RUDDER PCU ASSY.  WIRE	S BEING PINCHED AND/OR CUT DURING INSTALLATION AND THE TORQUING OF CAP P/N 315123-1.  WIRE GAUGE/DIAMETER OF COIL LEADS 	IS TOO SMALL.				2	L	7	2 	4F			RT	A2NM    					 
1999102200228	19991022	00228	NM  	1999	10	22	99ZZZX4008       	1	19990917	G	2720	3171001007	SENSOR          	MOOG        	33215208    	BOEING	757   	7572G7      	1384963	NM  										RUDDER	DAMAGED         	B			IU6R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	01	908AW				2719	24233				BASE OF LEAD WIRE FOUND PINCHED AND/OR BROKEN AT COIL CAUSING A FAILURE IN THE SENSOR ASSY OF THE RUDDER PCU ASSY.  WIRE	S BEING PINCHED AND/OR CUT DURING INSTALLATION AND THE TORQUING OF CAP P/N 315123-1.  WIRE GAUGE/DIAMETER OF COIL LEADS 	IS TOO SMALL.				2	L	7	2 	4F			RT	A2NM    					 
1999102200229	19991022	00229	NE  	1999	10	22	99ZZZX4009       	2	19991007	G	7230		CARBON SEAL     			BOEING	757   	75724APF    	1384969	NM  	PWA   	2037  	PW2040      		NE  					NR 2	FAILED          	B			WA2D	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	426UP	1326 				25457	P717902			TEAR DOWN INSPECTION REVEALED NR 2 CARBON SEAL FRACTURED APPROXIMATELY .250 INCH WIDE BY 2.300 INCHES LONG AND FAILED SE	CTION ADHERED TO SEAL PLATE FACE.  LOCKING TABS OF 6TH DISK TIE RODS LIBERATED, POSSIBLE FRACTURE CAUSE.  P & W ENGINEER	ING E.H., IS CONDUCTING INVESTIGATION.				2	L	7	2 	4F	4	F	RT	A2NM    	E17NE				 
1999102200230	19991022	00230	NE  	1999	10	22	99ZZZX4010       	2	19990811	G	7240	772568QQ	BOLT            								PWA   	JT8   	JT8D9A      	52048	NE  					COMB CHAMBER	FAILED          	B	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		156  					666682			P/N 772568QQ, PMA APPROVED QUALITY MANUFACTURER, PMA NR PQ2163MM, SUPPORT NR 17.  ONE  EACH FAILED UNDER HEAD RELEASING 	HEAD INTO TURBINE AREA CAUSING TURBINE DAMAGE AND PERFORMANCE DETERIORATION.  BORESCOPE INSPECTION REVEALED ONE EACH TUR	BINE BLADE FRACTURED APPROXIMATELY ONE INCH FROM TIP.  ENGINE REMOVED FOR REPAIR.  BOLT FAILED DUE TO CADMIUM EMBRITTLEM	ENT.  ALL BOLTS WHICH ARE SUSPECT ARE BEING REMOVED FROM SERVICE.								4	F			E2EA				 
1999102200231	19991022	00231	EU  	1999	10	22	99ZZZX4011       	1	19990624	G	3246	22X57510	TIRE            			AMD   	FALC10	FALCON10    	2730101	EU  										LT MAIN	FAILED          	G				C				ABORTED TAKEOFF         				O			OTHER                     			TO	TAKEOFF        	1			WP	03	5JY	184  				74				DURING ATTEMPTED TAKEOFF AT OAK, BOTH LEFT MAIN TIRES FAILED AT 100 KNOTS.  TAKEOFF WAS ABORTED.  INSPECTION REVEALED DA	MAGE TO BOTH MAIN WHEELS, LEFT FLAP AND LEFT MAIN LANDING GEAR DOOR.  AIRCRAFT FERRIED AFTER WHEEL AND TIRE ASSEMBLIES R	EPLACED.				2	L	7	2 	4F				A33EU   					 
1999102200233	19991022	00233	CE  	1999	10	22	99ZZZX4013       	1	19990405	G	7602	S12203A	CONTROL CABLE   			CESSNA	210   	210D        	2073414	CE  										MIXTURE CONTROL	FAILED          	H				A				UNSCHED LANDING         				O			OTHER                     			NR	NOT REPORTED   	1			WP	23	2340F	99   				21058540				MIXTURE CABLE BROKE IN-FLIGHT CAUSING FORCED OFF-FIELD LANDING AND SUBSEQUENT INJURIES TO PILOT AND PASSENGER, AND DESTR	UCTION OF THE AIRCRAFT.  MIXTURE CABLE HAD BEEN REPLACED LESS THAN ONE YEAR PRIOR AND 99 FLIGHT HOURS HAD BEEN ACCUMULAT	ED.  THE CABLE SHOWED SIGNS OF BEING RIGGED INCORRECTLY.  AD 85-03-01 AND SL SE 69-16 PERTAIN TO THIS AREA, BUT ARE ONLY	 ONE-TIME COMPLIANCE.			1	H	7	1 	3O			 	3A21    					 
1999102200235	19991022	00235	SO  	1999	10	22	99ZZZX4015       	1	19991004	G	2913	1213HBG310A	PUMP            			PIPER 	PA31  	PA31350     	7103110	SO  										HYDRAULIC SYSTEM	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	11	3587Y	145  			1983	318052121				HYDRAULIC PUMP SHAFT SHEARED.						1	L	7	2 	3O				A20SO   					 
1999102200236	19991022	00236	NE  	1999	10	22	99ZZZX4016       	2	19990927	G	8530		CAMSHAFT        			DOUG  	DC3   	DC3C        	3021457	WP  	PWA   	R1830 	R183092     	52020	NE  					ENGINE	FAILED          	G				E				ENGINE SHUTDOWN         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CR	CRUISE         	1			SW	11	5831B		313  		354578	42100882	354578			IN CRUISE FLIGHT, ENGINE STARTED TO RUN ROUGH.  ENGINE SHUT DOWN AND PROP FEATHERED.  MAINTENANCE FOUND NO COMPRESSION O	N REAR CYLINDERS.  SUBMITTER SUSPECTED REAR CAM FAILURE.  ENGINE TO BE REMOVED AND REPLACED.					2	L	7	2 	4R	4	R		A669    	5E4				 
1999102200237	19991022	00237		1999	10	22	99ZZZX4017       	4	19990921	G	6122	3599043	DRIVE GEAR      	WOODWARD    	210638      															PROPELLER	MISINSTALLED    	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03					1997439					CUSTOMER STATED PROP SYNCRONIZING INOPERATIVE.  FOUND INCORRECT DRIVE GEAR INSTALLED IN COMPONENT.																			 
1999102200238	19991022	00238	NM  	1999	10	22	99ZZZX4018       	1	19990922	G	2720	3171001007	SENSOR          	MOOG        	33215207    	BOEING	757   	757200      	1384950	NM  										RUDDER	DAMAGED         	B	P		IU6R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	01		42024			2723					BASE OF LEAD WIRE FOUND PINCHED AND/OR BROKEN AT COIL CAUSING A FAILURE IN THE SENSOR ASSY OF THE RUDDER PCU ASSY.  WIRE	S BEING PINCHED AND/OR CUT DURING INSTALLATION AND THE TORQUING OF CAP P/N 315123-1.  WIRE GAUGE/DIAMETER OF COIL LEADS 	IS TOO SMALL.				2	L	7	2 	4F			RT	A2NM    					 
1999102200482	19991022	00482	EU  	1999	10	22	99ZZZX4029       	1	19990924	G	6330	FDT14194	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										AFT BAR	LOOSE           	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	333AS	227  			5550	2893				BEARING HAS PLAY, NONE ALLOWED.						1	G	7	1 	3U				H9EU    					 
1999102200483	19991022	00483	SW  	1999	10	22	99ZZZX4030       	1	19990916	G	6220	407010100115	BEARING         		407310102101	BELL  	407   	407         		SW  										MAIN ROTOR	DAMAGED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437AL	1570 	764  		LK3674	53141				DURING DAILY INSPECTION, FOUND ELASTOMERIC EXTRUSION AND SEPARATION.						1	G	7	1 	3U			O	H2SW    					 
1999102200484	19991022	00484	SW  	1999	10	22	99ZZZX4031       	1	19990916	G	6220	407010100115	BEARING         		407310102101	BELL  	407   	407         		SW  										MAIN ROTOR	DAMAGED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437AL	1570 	764  		LK3581	53141				DURING DAILY INSPECTION, FOUND ELASTOMERIC EXTRUSION AND SEPARATION.						1	G	7	1 	3U			O	H2SW    					 
1999102200485	19991022	00485	SW  	1999	10	22	99ZZZX4032       	1	19990916	G	6220	407010100115	BEARING         		407310102101	BELL  	407   	407         		SW  										MAIN ROTOR	DAMAGED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437AL	1570 	764  		LK3538	53141				DURING DAILY INSPECTION, FOUND ELASTOMERIC EXTRUSION AND SEPARATION.						1	G	7	1 	3U			O	H2SW    					 
1999102200486	19991022	00486	SW  	1999	10	22	99ZZZX4033       	1	19990918	G	6510	407340340101	DISC PACK       		407040302101	BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	B	P		ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437AL	77   	28   		RNFS2938	53141				DURING 50-HOUR INSPECTION, FOUND NR 7 DISC PACK CRACKED AT AFT DISC.  IT IS CRACKED IN 3 LOCATIONS ON AFT DISC.  DISC PA	CK WAS 76.8 HOURS TT ON AIRCRAFT.					1	G	7	1 	3U			O	H2SW    					 
1999102200487	19991022	00487	SW  	1999	10	22	99ZZZX4034       	1	19990917	G	6510	40640316101	ADAPTER         		407040325101	BELL  	407   	407         		SW  										SPLINE	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457AL	2320 			AFS940	53151				DURING PHASE 1 INSPECTION, SECTION II ITEM 2 CLEANING SPLINES ON BLOWER SHAFT AND ADAPTER.  SPLINES HAVE SLIGHT STEP WOR	N INTO THEM AT FLANGED END OF ADAPTER.  THIS SMALL STEP PREVENTS ADAPTER FROM SLIDING FREELY ON BLOWER SHAFT SPLINES WHE	N SUBJECT TO TORSIONAL LOAD OF DRIVESHAFT TURNING.				1	G	7	1 	3U			O	H2SW    					 
1999102200488	19991022	00488	SW  	1999	10	22	99ZZZX4035       	1	19990902	G	6210	206015001107	BLADE           			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3188P				A2402	45778				DURING DAILY INSPECTION, FOUND TRAILING EDGE EXTRUSION CORRODED.						1	G	7	1 	3U				H2SW    					 
1999102200490	19991022	00490	SW  	1999	10	22	99ZZZX4037       	1	19990901	G	6710	206001190001	TUBE            			BELL  	206   	206L1       	1182107	SW  										CYCLIC	CRACKED         	B	P	A	ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3179V				A1901137	45782				DURING DAILY INPSECTION, FOUND CRACK ON MAIN BODY OF CONTROL TUBE.						1	G	7	1 	3U				H2SW    					 
1999102200491	19991022	00491	SW  	1999	10	22	99ZZZX4038       	1	19990918	G	6310	206040106001	SPRING          		206040015103	BELL  	206   	206B        	1181511	SW  										MAIN DRIVE	FAILED          	B	P	A	ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	209AL	5594 	310  		A909	1044				FORWARD COUPLING BECAME DISLODGED FROM PLATE AND WORE HOLES THROUGH THE PLATE.  THIS ALSO CAUSED DAMAGE TO THE TRANSMISS	ION FLANGE NUT PN 206-040-047-001.  SHOP TEARDOWN REVEALED ONE END OF THE SPRING HAD BROKEN OFF CAUSING THE SPRING TO SH	IFT.				1	G	7	1 	3U				H2SW    					 
1999102200492	19991022	00492	EU  	1999	10	22	99ZZZX4039       	1	19990924	G	6330	FDT14193	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										FRONT BAR	LOOSE           	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	333AS	520  			5426	2893				BEARING HAS PLAY, NONE ALLOWED.						1	G	7	1 	3U				H9EU    					 
1999102200777	19991022	00777	CE  	1999	10	22	99ZZZX4040       	1	19990820	G	3710		HOSE            			CESSNA	172   	172P        	2072436	CE  										VACUUM SYSTEM	CRACKED         	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	07	99157	2630 				17276412				COMPLETE VACUUM SYSTEM FAILURE, BOTH NORMAL SYSTEM AND STANDBY SYSTEM.  THE FAILURE WAS CAUSED BY DETERIORATION OF VACUU	M HOSES.  HOSES TO THE ATTITUDE INDICATOR AND DIRECTIONAL GYRO WERE SO BRITTLE THAT BENDING THE NOSE WOULD RESULT IN COM	PLETE BREAK-UP, AND FLAKING OF THE HOSE.  INSPECTION OF THREE OTHER 172'S OF THIS MODEL REVEALED THE IDENTICAL CONDITION	 OF VACUUM HOSES.  REVIEW OF MAINTENANCE RECORDS REVEALED THAT THESE HOSES HAD NEVER BEEN REPLACED AND WERE APPARENTLY I	NSTALLED AT THE DATE OF MANUFACTURE - 1978.		1	H	7	1 	3O			NT	3A12    					 
1999102200778	19991022	00778	SO  	1999	10	22	99ZZZX4041       	1	19990928	G	5280	4665300	HINGE           		4752931     	PIPER 	PA31  	PA31350     	7103110	SO  										RT MLG DOOR	FAILED          	B		A	UJDR	A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			EA	05	728CA	5798 				317752035				UPON TAKEOFF, PILOT NOTED LANDING GEAR FAILED TO FULLY RETRACT AS INDICATED BY GEAR UNLOCKED LIGHT ILLUMINATION.  LANDIN	G GEAR RECYCLED WITH SAME RESULT.  COPILOT WAS ABLE TO VISUALLY ASCERTAIN GEAR WAS NOT FULLY RETRACTED.  GEAR WAS SELECT	ED DOWN AND A NON-EVENTFUL LANDING MADE.  INSP OF GEAR DISCLOSED RT MLG INBD DOOR WAS DAMAGED AND BEING HELD IN PLACE BY	 ONLY AFT HINGE AND HYD ACTUATOR.  20 PERCENT OF SPOT WELDS ON DOOR ASSY HAD SEPARATED RESULTING IN THE DOOR SKIN BEING 	PEALED BACK.  THE HYD ACTUATOR, DOOR HINGE BRACKETS, AND WW STRUCTURE WERE DAMAGED, RT INBD LANDING GEAR DOOR FWD HINGE 	HAD CRACKED IN HALF.  FAILURE OF THE HINGE CAUSED SUBSEQUENT DAMAGE TO ADJACENT ACFT STRUCTURES AND COMPONENTS.	1	L	7	2 	3O				A20SO   					 
1999102200779	19991022	00779	CE  	1999	10	22	99ZZZX4042       	1	19990901	G	5730		SKIN            			BEECH 	35    	V35B        	1151548	CE  										RT WING	CORRODED        	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	13	651PC					D9192				AIRCRAFT EQUIPPED WITH TRS ALCOHOL WING ANTI-ICE SYSTEM IAW STC NR SA2239CE.  ANNUAL INSPECTION REVEALED CORROSION ON EX	TERIOR OF BOTTOM RT WING UNDERNEATH THE TRS BLADDER TANK.  REMOVAL OF WING SKIN REVEALED EXCESSIVE CORROSION DUE TO MOIS	TURE TRAPPED IN THE STYROFOAM TANK LINER.  MOISTURE IS DUE TO CONDENSATION AND LACK OF AIR CIRCULATION WITHIN THE COMPAR	TMENT.  OPERATOR INSTALLED AN ALUMINUM TANK LINER WHICH ALSO ALLOWS AIR CIRCULATION AND REPLACED THE WING SKIN.			1	L	7	1 	3O				3A15    					 
1999102200781	19991022	00781	EU  	1999	10	22	99ZZZX4044       	1	19990914	G	5510		BUSHING         		C55151101051	UROCOP	EC120 	EC120B      	8680987	EU  										HORIZONTAL STAB	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	120TX	40   			1029	1029				DAILY INSPECTION REVEALED LEFT SUPPORT BUSHING WAS BROKEN AWAY FROM ITS FIXED COMPOSITE POSITION WITHIN THE HORIZONTAL S	TABILIZER.  NO OTHER DAMAGE WAS FOUND AT EITHER OF THE STABILIZER MOUNT BREAKERS TO THE TAILBOOM, (LT AND RT SIDES).  NE	W SERVICEABLE STABILIZER INSTALLED.  FENESTRON WAS BALANCE CHECKED AT 100 PERCENT FPOG - OUT OF TOLERANCE. 7 IPS - BALAN	CED TO 1 IPS.			1	G	7	2 	3U			NC	R0001RD 					 
1999102200782	19991022	00782	EU  	1999	10	22	99ZZZX4045       	1	19990925	G	6510	1053180301	SHAFT           			BOLKMS	117   	BK117A1     	5626010	EU  										TAIL ROTOR	WORN            	B			BAQR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	03	39257				51181	S7027				TAIL ROTOR PEDALS BINDING IN FULL LEFT PEDAL POSITION.  NO BINDING AT FLIGHT IDLE, BINDING INCREASES AS ROTOR RPM INCREA	SE.  TAIL ROTOR OUTPUT SHAFT SPLINES THAT DRIVE TAIL ROTOR SLIDING SLEEVE, PN 105-31765, EXTREMELY WORN, NO DAMAGE TO SL	IDING SLEEVE DRIVE SPLINES.  SUBMITTER SUSPECTED WITH INCREASE OF CENTRIFUGAL FORCE, TAIL ROTOR SLIDING SLEEVE WAS TWIST	ING CAUSING BINDING.			1	G	7	2 	3U				H13EU   					 
1999102200783	19991022	00783	WP  	1999	10	22	99ZZZX4046       	2	19991009	G	7530	321378811	VALVE           			BRAERO	DH125 	BAE125800A  	1500285	EU  	GARRTT	TFE731	TFE7315R    	01518	WP  					BLEED AIR	FAILED          	D				A				UNSCHED LANDING         				N			FALSE WARNING             			NR	NOT REPORTED   	1			SO	15	75CS	7079 				258066				AIRCRAFT RETURNED TO BASE AFTER NO REAR BAY OVERHEAT LIGHT ILLUMINATED.  UPON INVESTIGATION, FOUND THE MIXING VALVE HAD 	SEPARATED AT THE FLANGE POINTED OUT IN THE ENCLOSED ILLUSTRATION.  THE VALVE SEPARATION ALLOWED HP AIR TO LEAK, ILLUMINA	TING THE OVERHEAT WARNING.  REPLACEMENT OF THE VALVE SOLVED THE PROBLEM.				2	L	7	2 	4F	4	F	RT	A3EU    	E6WE				 
1999102200785	19991022	00785		1999	10	22	99ZZZX4048       	2	19990929	G	8530	653877	LIFTER          			AMTR  		LANCAIRIV   			CONT  		TSIO550E    							CYLINDER	PITTED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99							803097			FACTORY NEW ENGINE DIS-ASSEMBLED FOR BALANCING.  PITTING FOUND ON 6 INTAKE AND 2 EXHAUST LIFTER FACES.									0 										 
1999102200786	19991022	00786		1999	10	22	99ZZZX4049       	4	19991015	G	2562	SRB10	ELT             																	CABIN	FAILED          	B			VW3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	09					2365					DURING THE FUNCTIONAL TESTING OF THE ELT, IT DID NOT TRANSMIT ANY SIGNALS.  THE BATTERY WAS REPLACED WITH A BATTERY THAT	 TESTED OKAY ON OTHER ELT'S, BUT IT WOULD STILL NOT TRANSMIT.  ELT STOWED ON 10-MAN LIFE RAFT, B.F. GOODRICH,  P/N 5A321	0-10511, S/N 10R211.																	 
1999102200787	19991022	00787		1999	10	22	99ZZZX4050       	4	19991018	G	2562	SRB10	ELT             																	CABIN	FAILED          	B			VW3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	09					2367					DURING THE FUNCTIONAL TESTING OF THE ELT, IT DID NOT TRANSMIT ANY SIGNALS.  THE BATTERY WAS REPLACED WITH A BATTERY THAT	 TESTED OKAY ON OTHER ELT'S, BUT IT WOULD STILL NOT TRANSMIT.  ELT STOWED ON 10-MAN LIFE RAFT, BF GOODRICH, P/N 5A3210-1	0511, S/N 10R214.																	 
1999102200788	19991022	00788		1999	10	22	99ZZZX4051       	4	19991018	G	2562	SRB10	ELT             																	CABIN	FAILED          	B			VW3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	09					2361					DURING FUNCTIONAL TESTING OF THE ELT, IT DID NOT TRANSMIT ANY SIGNALS.  THE BATTERY WAS REPLACED WITH A BATTERY THAT TES	TED OKAY ON OTHER ELT'S, BUT IT WOULD STILL NOT TRANSMIT.  ELT STOWED ON 10-MAN LIFE RAFT, B. F. GOODRICH, P/N 513210-10	511, S/N 10R209.																	 
1999102200789	19991022	00789		1999	10	22	99ZZZX4052       	4	19991018	G	2562	SRB10	ELT             																	CABIN	FAILED          	B			VW3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	09					10R216					DURING FUNCTIONAL TESTING OF THE ELT, IT DID NOT TRANSMIT ANY SIGNALS.  THE BATTERY WAS REPLACED WITH A BATTERY THAT TES	TED OKAY ON OTHER ELT'S, BUT WOULD STILL NOT TRANSMIT.  ELT STOWED ON 10-MAN LIFE RAFT, P/N 5A3210-10511, S/N 10R216.																		 
1999102200790	19991022	00790	EA  	1999	10	22	99ZZZX4053       	2	19990827	G	7414	4250	MAGNETO         	SLICK       		CESSNA	172   	172M        	2072418	CE  	LYC   	O320  	O320E2D     	41508	EA  					ENGINE	FAILED          	B			BNGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	61612	1646 			0070670	17264675	RL4247627A			RIGHT MAGNETO FAILED.  MAJOR WORK ON BOTH MAGS APPROXIMATELY 850 HOURS AGO.  NO  MENTION OF POINTS OR CONDENSOR AT THAT 	TIME.  500-HOUR INSPECTIONS C/W APPROXIMATELY 200 HOURS AGO.  APPEARS MAG HAD 1,646 HOURS SINCE NEW.					1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999102200791	19991022	00791	EU  	1999	10	22	99ZZZX4054       	1	19990929	G	3233	AIR400390	SEAL            		AIR864141   	SAAB  	SF340 	340B        	7860101	EU  										NLG ACTUATOR	FAILED          	B			FW1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	03	424XJ	5271 			LK9700483	340B424				PREMATURE FAILURE OF GLAND SEAL.  PART HAD 5,945 CSN ON 24,000 CYCLE OVERHAUL SCHEDULE.  PART WAS BUILT NEW 2Q97, MFG OF	 APPLIANCE AND SEAL HAS BEEN NOTIFIED.					2	L	7	2 	4T			RT	A52EU   					 
1999102200792	19991022	00792	CE  	1999	10	22	99ZZZX4055       	1	19990416	G	3231	08411066	BELLCRANK       			CESSNA	310   	310R        	2074245	CE  										MLG DOOR	BROKE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	37256					310R0977				THE RT MAIN GEAR IDLER BELLCRANK WAS FOUND BROKEN AT JUST AFTER THE WEBBING PORTION OF THE CASTING THAT SUPPORTS THE CUR	VED ARM OF THE BELLCRANK.  SUBMITTER STATED THIS SPECIFIC FAILURE IS THE THIRD ONE SEEN AND THE SECOND ONE REPAIRED IN 2	 MONTHS.  ALL FAILURES HAVE BEEN TO THE RT MAIN GEAR BELLCRANK.				1	L	7	2 	3O				3A10    					 
1999102200793	19991022	00793	CE  	1999	10	22	99ZZZX4056       	1	19990824	G	5540	51310103	BEARING PLATE   			CESSNA	414   	414A        	2075907	CE  										RUDDER	MISINSTALLED    	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	58H	6264 				414A0314				LOWER RUDDER BEARING PLATE, INSTALLED BY MANUFACTURER, IS UPSIDE DOWN ALLOWING BEARING TO MOVE DOWN FROM RUDDER WEIGHT. 	 THIS CAUSES RUDDER TO FAIRING INTERERENCE (TOP OF HORIZONTAL) AND SEVERE RUBBING OF UPPER RUDDER PIVOT BRACKET TO UPPER	 BEARING.  (UPPER BRACKET).  MUST REMOVE AND REPLACE LOWER BEARING SUPPORT ASSY.				1	L	7	2 	3O				A7CE    					 
1999102200794	19991022	00794	SO  	1999	10	22	99ZZZX4057       	1	19991012	G	3213	4041304	FORK ASSY       			PIPER 	PA31  	PA31310     	7103103	SO  										LT MLG	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	405PA	13825				31424				AIRCRAFT PARKED.  NOTICED LT WHEEL TILTED INBOARD AT TOP.  BRAKE DISC HAD CONTACTED FORK.  REMOVED WHEEL TO INVESTIGATE,	 FOUND AXLE HAD CRACKED HALF WAY AROUND.  AIRCRAFT HAD FLOWN DAY BEFORE.  CRACK SEEMED TO HAVE STARTED AT VERY BOTTOM. N	OT BELIEVED TO BE CAUSED FROM BOUNCED LANDING.  "STRESS CORROSION AND AGE" CRACK IS RIGHT IN SEAM WHERE BOSS AND BEARING	 AREAS NEED A CLOSE VISUAL INSPECTION.			1	L	7	1 	3O			RT	A20SO   					 
1999102200795	19991022	00795		1999	10	22	99ZZZX4058       	4	19990901	G	3452	AT50U	TRANSPONDER     	NARCO       	47971       	PIPER 	PA28  	PA28151     	7102805	SO  										COCKPIT	MALFUNCTIONED   	C				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	4320F					287715016				TRANSPONDER MALFUNCTIONS, MODE-C INOPERABLE.						1	L	7	1 	3O				2A13    					 
1999102200796	19991022	00796	EA  	1999	10	22	99ZZZX4059       	2	19990927	G	8530		STUD            			PIPER 	PA28  	PA28R200    	7102811	SO  	LYC   	O360  	IO360C1C    	41514	EA  					NR 3 CYLINDER	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	01	9455N	1814 	143  			28R35170	L623051A			ROUGH ENGINE IN-FLIGHT.  FOUND BROKEN CYLINDER HOLD DOWN STUDS NR 3 CYLINDER TOP RIGHT, BOTTOM RIGHT AND INSIDE, .3750 I	NCH STUDS ADJACENT ALSO BROKEN.  OVERHAULED 8-18-93.  PULLED AILERON AND CYLINDERS AND FOUND CYLINDER HOLD-DOWN BOLTS NO	T PROPERLY TORQUED.				1	L	7	1 	3O	3	O		2A13    	1E10				 
1999102200797	19991022	00797	SO  	1999	10	22	99ZZZX4060       	1	19990930	G	8011	PS1432C	HOUSING         		MZ4218      	PIPER 	PA28  	PA28161     	7102803	SO  										MOUNT FLANGE	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	8330S				92281824	288116144				DURING ANNUAL INSPECTION, FOUND ALTERNATOR SUPPORT STRUT ATTACH FLANGE ON STARTER NOSE HOUSING BROKEN.  BOLT WAS TIGHT, 	BUT SUPPORT STRUT DID NOT ALIGN CORRECTLY ON FLANGE.  IF WASHER HAD BEEN PLACED UNDER SUPPORT STRUT AT FLANGE, THIS WOUL	D HAVE CORRECTED ALIGNMENT.				1	L	7	1 	3O				2A13    					 
1999102200798	19991022	00798	EA  	1999	10	22	99ZZZX4061       	2	19990802	G	8530	LW16511	CAMSHAFT        			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					NR 2 CYLINDER	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EU	01	6473D	118  				17272822	L618776T			DURING REPAIR OF CYLINDER NR 2, FOUND HYDRAULIC LIFTER OF INLET VALVE CYLINDERS NR 2 AND 1 DAMAGED.  SPALLING OF SURFACE	 RUNNING ON THE CAMSHAFT.  CAMSHAFT COVER INLET VALVE CYLINDERS NR 2 AND 1 HAD MATERIAL DAMAGED.  ENGINE TSO 118 HOURS.					1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999102200799	19991022	00799	SW  	1999	10	22	99ZZZX4062       	1	19990901	G	2810		FUEL CELL       			MOONEY	M20   	M20S        	5870226	SW  										WING	LEAKING         	B			W45R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	2810	10   				300007				FUEL LEAK UNDER FORWARD WING WALK, TWO INBOARD SCREWS.						1	L	7	1 	3O			RT	2A3     					 
1999102200801	19991022	00801	NM  	1999	10	22	99ZZZX4063       	1	19991001	G	2710	654484511	MANIFOLD        		654476118   	BOEING	737   	737*        		NM  										AILERON PCU	CRACKED         	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		48187	3290 		3114					MANIFOLD ASSY IS CRACKED APPROXIMATELY 80 PERCENT OF THE FILTER PORT CIRCUMFERENCE AND EXTENDS THROUGH TO THE THREADED A	REA.  FATIGUE, MISHANDLED, OVERPRESSURED AND/OR OVERTORQUED.					2	L	7	2 	4F			RT	A16WE   					 
1999102200802	19991022	00802	NM  	1999	10	22	99ZZZX4064       	1	19990930	G	2761	65C268631	HOUSING         		65C268641   	BOEING	737   	737300      	1384610	NM  										ACTUATOR	CRACKED         	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01			17785		0070					INNER BORE OF HOUSING IS CRACKED IN TWO LOCATIONS POSSIBLY DUE TO FATIGUE.						2	L	7	2 	4F			RT	A16WE   					 
1999102200803	19991022	00803	NM  	1999	10	22	99ZZZX4065       	1	19990930	G	2740	69778551	SPRINGS         		65C3475111  	BOEING	737   	737*        		NM  										HORIZ STABILIZER	SHATTERED       	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		34671	14692		KEO0641					SPRINGS, PN 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM POSSIBLY DUE TO FATIGUE AND INCREASED SPRING COIL STRES	SES.  SPRINGS, PN 69-77855-1, ARE TO BE REPLACED WITH P/N 69-77855-2 SPRINGS ON ACTUATOR ASSEMBLIES MANUFACTURED PRIOR T	O S/N KEO1730 PER BOEING SL 737-SL-27-090-B.				2	L	7	2 	4F			RT	A16WE   					 
1999102200804	19991022	00804	CE  	1999	10	22	99ZZZX4066       	1	19990929	G	8000	S29431	RELAY           			CESSNA	500   	550         	2076604	CE  										STARTED	FAILED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2734K	4491 			CH92407	5500595				DURING ENGINE START, START BUTTON DID NOT ILLUMINATE.  TROUBLESHOOTING LED TO THE START RELAY. WHEN RELAY WAS OPENED UP,	 WIRE FOR INDICATING LIGHT WAS BROKEN OFF OF CONTACTOR.  WIRE IS ATTACHED TO MOVING CONTACTS AND OVER TIME IT APPARENTLY	 WORK-HARDENED AND BROKE.				1	L	7	2 	4F				A22CE   					 
1999102200805	19991022	00805	EU  	1999	10	22	99ZZZX4067       	1	19991005	G	3250	AD5312A83	ROLL PIN        		AIR860122   	JETAIR	JETSTM	JETSTM4101  	1500501	EU  										NLG STEERING	CRACKED         	B			FW1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03					APB94666					SPLIT PIN CRACKED LENGTHWISE SUCH THAT IT COULD BE REMOVED BY HAND.  LOSS OF PIN WHEN INSTALLED IN AIRCRAFT WOULD RESULT	 IN LOSS OF STEERING.					2	L	7	2 	4T			RT	A41NM   					 
1999102200806	19991022	00806	CE  	1999	10	22	99ZZZX4068       	1	19991008	G	3240	50030964	BRAKE ASSY      	GOODYEARAERO		LEAR  	25    	25D         	5170514	CE  										MLG	MISOVERHAULED   	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99					APR6939					PART INSTALLED ON AIRCRAFT, BUT WHEN THROUGH-BOLTS WERE TORQUED, BRAKE ASSY (ROTORS) WOULD NOT MOVE FREELY.  FOUND DISTA	NCE BETWEEN BACKPLATE AND PRESSURE PLATE TO BE UNEVEN AROUND THE CIRCUMFERENCE WITH THE ASSY INSTALLED AND TORQUED.  BOT	TOM OF ASSY HAD GREATER DISTANCE THAN TOP.  UNKNOWN EXACTLY WHAT CAUSED SUSPECTED DEFECT.  RETURNED FRESHLY OVERHAULED B	RAKE ASSY TO SUPPLIER.  INSTALLED DIFFERENT OVERHAULED ASSY.			2	L	7	2 	4J				A10CE   					 
1999102200807	19991022	00807	SO  	1999	10	22	99ZZZX4069       	2	19991006	G	8530	639615	ROCKER ARM      		64197CP     	CESSNA	172   	172G        	2072420	CE  	CONT  	O300  	O300D       	17022	SO  					NR 4 CYLINDER	CRACKED         	H				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			SW	17	3255L		206  		01	17253924	33631D5D			APPROXIMATELY 2 MILES FROM AN AIR FIELD, THE ENGINE BEGAN TO RUN ROUGH.  LANDED WITHOUT INCIDENT. INSPECTION REVEALED TH	E NR 4 CYLINDER EXHAUST ROCKER ARM HAD CRACKED AND SEPARATED, ON THE BOTTOM INBOARD SIDE, IN THE BUSHING AREA.  THE BUSH	ING WAS NOT DAMAGED.  NO OTHER PART IN THE CYLINDER WAS DAMAGED.  INSTALLED A RE-CERTIFIED ROCKER ARM.  RUN-UP AND TEST 	FLIGHT CHECKED OK.			1	H	7	1 	3O	3	O	NT	3A12    	E253				 
1999102200808	19991022	00808	EA  	1999	10	22	99ZZZX4070       	2	19990802	G	8530	LW16812	LIFTER          			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					NR 2 CYLINDER	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EU	01	6473D	118  				17272822	L618776T			DURING REPAIR OF CYLINDER NR 2, FOUND HYDRAULIC LIFTER OF INLET VALVE CYLINDERS NR 2 AND 1 DAMAGED.  SPALLING OF SURFACE	 RUNNING ON THE CAMSHAFT.  CAMSHAFT COVER INLET VALVE CYLINDERS NR 2 AND 1 HAD MATERIAL DAMAGED.  ENGINE TSO 118 HOURS.					1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999102900018	19991029	00018	SW  	1999	10	29	99ZZZX4079       	1	19990915	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	SPREAD          	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	487AL				RNFS7672	53204				FOUND NR 4 DISC  PACK SPREAD JUST BEYOND LIMITS DURING 25-HOUR INSPECTION.  FOUND NR 4 DISC PACK SPREAD BEYOND LIMITS. R	EMOVED NR 3 TAIL ROTOR DRIVESHAFT TO BLOWER SPLINE ADAPTER TO ENSURE IT STILL CONTAINED PROPER AMOUNT OF LUBRICANT.  IT 	DID, BUT FOUND THE SPLINE ADAPTER P/N 406-040-316-101 HAD A STEP WORN IN IT.  REPLACED THE SPLINE ADAPTER.				1	G	7	1 	3U			O	H2SW    					 
1999102900023	19991029	00023	EU  	1999	10	29	99ZZZX4081       	1	19990908	G	3240	133593	STATOR          	BFGOODRICH  	215412      	BRAERO	DH125 	HS125700A   	4230170	EU  										BRAKE ASSEMBLY	CRACKED         	B	P		COZR	K				NONE                    				S	Z		AFFECT SYSTEMS            	SIGNIFICANT FAILURE REPORT		IN	INSP/MAINT     	1			WP	27	215RS	131  			131	NA0215				ON REMOVAL OF MAIN WHEEL ASSEMBLY, NOTED THE BRAKE IN THE LEFT NR 2 POSITION WAS SET WHILE ALL OTHER BRAKES WERE IN THE 	OFF POSITION.  INSPECTION OF THE BRAKE FOUND THE NR 2 STATOR DISK (NEXT TO THE TORQUE PLATE) CRACKED.  BF GOODRICH HAS I	SSUED SB 2-1541-32-2 ABOUT THIS PROBLEM FOR BRAKE ASSEMBLIES WITH MORE THAN 500 LANDINGS.  THIS BRAKE HEAT STACK ONLY HA	D 126 LANDINGS SINCE NEW (TSN ZERO).  BRAKE ASSEMBLY SENT TO BF GOODRICH FOR EVALUATION.   LANDINGS:  126.			2	L	7	2 	4F				A3EU    					 
1999121000001	19991210	00001	SO  	1999	12	10	99ZZZX4084       	1	19990923	G	6123	4049A	PUMP            			MARSH 	S2F   	S2F3S       	3951007	SO  										FEATHERING	FAILED          	B			IL3R	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			WP	07	425DF	16   			79901	152825				DURING PRODUCTION FLIGHT TESTING, THE LEFT ENGINE WAS SHUT DOWN SEVERAL TIMES IN-FLIGHT.  ON THE 6TH TIME, THE PROPELLER	 WOULD NOT UNFEATHER ALLOWING AN ENGINE RESTART.  PILOT HAD TO MAKE SINGLE ENGINE LANDING.  UNFEATHER PUMP WAS REPLACED 	AND SYSTEM OPERATED NORMALLY.  PUMP IS BEING RETURNED TO WELSON.				2	H	0	2 	4O			RT	A51NM   					 
1999102900769	19991029	00769	GL  	1999	10	29	99ZZZX4087       	2	19990911	G	7250	6889069	COUPLING        			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					N2 TURBINE	MISMANUFACTURED 	B			EOPR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	01	3194P					45788	CAE860263			SUBMITTER SUSPECTED MIS-MANUFACTURED PART.  SPLINES ARE MACHINED THROUGH SEAL RING GROOVES.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999102900770	19991029	00770		1999	10	29	99ZZZX4088       	4	19991016	G	2562	EBC102A	ELT             			AMTR  		KR2         												CABIN	MISINSTALLED    	G				O				OTHER                   				W			INADEQUATE Q C            			NR	NOT REPORTED   	1			SO	03	85ES	141  			12642	6457				FOLLOWING AN ACCIDENT, THE EMERGENCY LOCATOR TRANSMITTER (ELT) DID NOT AUTOMATICALLY ACTIVATE.  UPON COMBING THE WRECKAG	E AND FINDING THE ELT, THE REASON WHY IT DID NOT FUNCTION WAS THE ACTUATING SWITCH ARM WAS LOCKED IN THE 'OFF' POSITION 	BY THE SHIPPING SCREW.  MOREOVER, THIS PROBLEM MAY NOT HAVE BEEN DISCOVERED DURING THE LAST ANNUAL INSPECTION.  SUBMITTE	R SUGGESTED AN AD TO COMPLETELY REMOVE THE SHIPPING LOCK ON INITIAL ELT INSTALLATION AND AN INSPECTION OF ALL IN-SERVICE	 UNITS TO ENSURE THE SAME CONFIGURATION.					0 										 
1999102900772	19991029	00772	SW  	1999	10	29	99ZZZX4089       	1	19990927	G	6320		GEARBOX         			BELL  	212   	212         	1181420	SW  										ENGINE	MAKING METAL    	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	5017H	13281	2545 		CPGD1804	30930				HEAVY TO MODERATE NOISE AND VIBRATION IN-FLIGHT.  EXCESSIVE METAL IN FILTER (C-BOX).						1	G	7	1 	4U				H4SW    					 
1999102900773	19991029	00773	SW  	1999	10	29	99ZZZX4090       	1	19990921	G	6520	AN126420	STUD            		204040012013	BELL  	204   	UH1H        	1181407	SW  										TAIL ROTOR	FAILED          	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	13	32800		408  		A132581	6616854				MOUNTING STUDS, 6 EACH, FAILED SUB-SURFACE AT 90 DEGREE GEARBOX MOUNTING FLANGE (APPARENT TENSILE FAILURE).  SUBMITTER S	USPECTED PREVIOUS VIBRATORY OR OVER-TORQUE DAMAGE TO MOUNTING STUDS.					1	G	7	1 	4U				EXPA1G71					 
1999102900774	19991029	00774	GL  	1999	10	29	99ZZZX4091       	2	19991007	G	7323	23037870	GOVERNOR        			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					ENGINE	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	10729				25799	2876	834865			SLOW TO RECOVER FROM N2 DROOP.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999102900775	19991029	00775		1999	10	29	99ZZZX4092       	4	19991014	G	2200	8241631	POTENTIOMETER   	HAMSTD      		SKRSKY	S76   	S76         	8143010	NE  										AFCS	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5402T	1175 			8002860	760140				FEEDBACK POTENTIOMETER EXPERIENCED PREMATURE FAILURE.  SUBMITTER STATED POTENTIOMETER SHOULD LAST UNTIL OVERHAUL, 3,000 	HOURS.  COMP P/N 76900-01802-106.					1	G	7	2 	3U				H1NE    					 
1999102900776	19991029	00776		1999	10	29	99ZZZX4093       	4	19991005	G	2200	8241631	POTENTIOMETER   			SKRSKY	S76   	S76         	8143010	NE  										AFCS	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	5402T	4579 	285  		85110259	760140				FEEDBACK POTENTIOMETER HAD PREMATURE FAILURE, SUBMITTER STATED SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS.  CAUSES A	CTUATOR TO KICK IN-FLIGHT.  COMP P/N 76900-01802-106.					1	G	7	2 	3U				H1NE    					 
1999102900780	19991029	00780	EU  	1999	10	29	99ZZZX4094       	1	19991010	G	7720	704A37642043	TRANSMITTER     			SNIAS 	350   	AS350B      	8680801	EU  										ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	61CU					1636				TRANSMITTER UNIT FAILED WITHIN .3 HOUR.						1	G	7	1 	3U				H9EU    					 
1999102900786	19991029	00786	SO  	1999	10	29	99ZZZX4095       	2	19991013	G	8550	0024100143	PAN             			BEECH 	36    	A36         	1151604	CE  	CONT  	O550  	IO550B      		SO  					ENGINE	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	3249D	425  				E2949	675978			DURING AN ANNUAL INSPECTION, THE P/N 002-410014-3, 'PAN', LOCATED AT THE FORWARD NOSE COWL AREA BELOW THE ENGINE CRANKSH	AFT FLANGE, AND ABOVE THE AIR FILTER, HAD LARGE CRACKS WITH A HOLE APPROXIMATELY 2 INCHES BY 4 INCHES FROM WHERE CRACKED	 PIECES FELL/BROKE AWAY.				1	L	7	1 	3O	3	O		3A15    	E3SO				 
1999102900787	19991029	00787	EA  	1999	10	29	99ZZZX4096       	2	19991008	G	7414		GEAR            	BENDIX      		CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					MAGNETO	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	03	5624G	4033 	425  			172773563	L826176T			DISTRIBUTOR GEARS IN MAGNETO BROKE DURING TAKEOFF.  RETURNED TO FIELD.  NOTIFIED ELECTRO SYSTEMS, INC., OF MAGNETO MALFU	NCTION.					1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999102900788	19991029	00788	EA  	1999	10	29	99ZZZX4097       	2	19991008	G	7414	10400184	CONTACT         	BENDIX      		PIPER 	PA31  	PA31310     	7103103	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					MAGNETO	FAILED          	B			KC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03	879F	50   			3273915	317812026	L506861A			NYLON CAM FOLLOWER MELTED WHERE IT CONTACTED THE CONTACT POINT LEAF SPRING.  THE CAM FOLLOWER WOULD NO LONGER OPEN THE C	ONTACT POINTS, AND THE LEFT MAGNETO FAILED.  SUBMITTER STATED POSSIBLE CAUSE, POOR CONDENSER GROUND.  REF: TCM IGNITION 	BULLETIN SB 651.  COMPONENT P/N D6LN3200 10-682910-13.				1	L	7	1 	3O	3	O	RT	A20SO   	E14EA				 
1999102900789	19991029	00789	CE  	1999	10	29	99ZZZX4098       	1	19991020	G	2910	5217840150	HOSE            			CESSNA	177   	177RG       	2073709	CE  										NLG WW	FAILED          	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	11	1521H	2663 				177RG0698				HOSE BLEW APART AT FITTING WHILE IN-FLIGHT.  SHOWED NO OUTWARD SIGNS OF FAILURE.  LOSS OF ALL HYDRAULIC FLUID.  SUBMITTE	R SUGGESTED MANDATORY REPLACEMENT TIME OF HOSES BE ESTABLISHED BY MANUFACTURER.					1	H	7	1 	3O				A20CE   					 
1999102900790	19991029	00790	NE  	1999	10	29	99ZZZX4099       	2	19991006	G	7230	2A0003	BEARING         								IAE   	V2500 	V2500A1     		NE  					COMPRESSOR	SPALLED         	B			RA1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05		297  			PGGUAK6566		V0170			ENGINE WAS REMOVED DUE TO M50 MATERIAL ON THE MAG CHIP DETECTORS.  DISASSEMBLY OF THE ENGINE REVEALED THE NR 4 BEARING E	XHIBITED SPALLING DAMAGE ON THE OUTER RACE.  THE BEARING WAS SUBMITTED TO THE LAB FOR ANALYSIS.										4	F			E311NE				 
1999012900091	19990129	00091	EU  	1999	1	29	99ZZZX410        	1	19990102	G	2822	1C454	PUMP            	AIRBORNE    		SNIAS 	350   	AS350B2     	8680813	EU  										ENGINE	MALFUNCTIONED   	D		A		A				UNSCHED LANDING         				J			WARNING INDICATION        			NR	NOT REPORTED   	1			WP	13	972BH				3AP8	2804				JANUARY 2, 1999, AT APX 16:30 HOURS, WHILE ON A ROUTINE SIGHTSEEING FLIGHT, PILOT EXPERIENCED A FUEL FILTER CAUTION LIGH	T.  COLLECTIVE MOVEMENTS CREATED FLUCTUATIONS IN FUEL PRESSURE AND NO ROTOR RPM DROOP.  PILOT LANDED AT BEST SITE AVAILA	BLE AT MAUNA KEA RESORT HELIPAD WITHIN TEN MINUTES OF LIGHT ILLUMINATION.  INSPECTION OF ACFT TANK SUMP - FUEL WAS FOUND	 CLEAN.  FUEL AT THE AIRFRAME FUEL FILTER WAS DARK IN COLORING.  PROBLEM CONFIRMED TO BE FROM ELECTRIC BOOST PUMP.  REPL	ACED FUEL BOOST PUMP AND FUEL CONTROL REGULATOR.  SUBMITTER STATED POSSIBLE INTERNAL SEAL LEAKAGE AND BRUSH MATERIAL FLU	SHED INTO SYSTEM AND RECOMMENDED THAT AIRBORNE EVALUATE PUMP SEALS.	1	G	7	1 	3U				H9EU    					 
1999102900791	19991029	00791	NE  	1999	10	29	99ZZZX4100       	2	19990924	G	7230	2A0003	BEARING         								IAE   	V2500 	V2500A1     		NE  					COMPRESSOR	SPALLED         	B			RA1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05		300  			PGGUAK6427		V0184			ENGINE WAS REMOVED DUE TO M50 MATERIAL ON THE MAG CHIP DETECTORS.  DISASSEMBLY OF THE ENGINE REVEALED THE NR 4 BEARING E	XHIBITED SPALLING DAMAGE ON THE OUTER RACE.  THE BEARING WAS SUBMITTED TO THE LAB FOR ANALYSIS.										4	F			E311NE				 
1999102900792	19991029	00792		1999	10	29	99ZZZX4101       	4	19991012	G	2561	PO723105	LIFE VEST       	EAAEROMARINE	KSD35       															CABIN	FAILED          	B			KQ1R	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	07					F80261					LIFE VEST FAILED TWO PSI PRESSURE TESTS IAW MM  25-60-7.  DOM:  SEPT 1986.																			 
1999102900793	19991029	00793	EA  	1999	10	29	99ZZZX4102       	2	19991013	G	8500		ENGINE          			PIPER 	PA46  	PA46350P    		SO  	LYC   	O540  	TIO540AE2A  	41532	EA  					NOSE	MAKING METAL    	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	126SR	526  			B9064	4622036	RL492061A			OIL SAMPLE SHOWS AMS6270 STEEL FROM CAMSHAFT, EMS-91 CAST IRON FROM TAPPETS AND ALUMINUM ALLOY WORN 5 PERCENT TIN CONTEN	T FROM BEARING INSERTS.  OIL TIME SINCE LAST CHANGE, 20.2 HOURS.  RECENT CHANGE OUT OF OIL SUMP AND TURBO SUPPORT BRACKE	T RIGHT SIDE.  SUBMITTER STATED SIMILAR PROBLEMS ON OTHER TIO-520-AE2A.				1	L	7	1 	3O	3	O	RT	A25SO   	E14EA				 
1999102900794	19991029	00794		1999	10	29	99ZZZX4103       	4	19991014	G	2562	MN1300	BATTERY         	AMERIKING   	AK450       	PIPER 	PA28  	PA28R200    	7102811	SO  										ELT	DISCHARGED      	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	9423N				355271	28R35135				ANNUAL CHECK OF ELT TRANSMITTER SHOWED NO SIGNAL OVER AM RADIO PER ACTION NOTICE A8150.3.  FOUND ONE OF THE SIX 'D' CELL	 BATTERIES HAD VERY LOW VOLTAGE.  ALL BATTERIES LABELED 'BEST IF INSTALLED BY JAN 2001'.  REPLACED BATTERIES, CHECKED OK	.				1	L	7	1 	3O				2A13    					 
1999102900795	19991029	00795	SO  	1999	10	29	99ZZZX4104       	1	19991007	G	5740	1418200	FITTING         			PIPER 	PA18  	PA18A150    	7101837	SO  										RT WING	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	3088Z	12934				187142				SEVERE CORROSION OF LIFT STRUT ATTACH FITTING.  FRONT OF FRONT SPAR IN RIGHT WING LOCATED UNDER LEADING EDGE COVERING CA	USED BY LACK OF ACCESS FOR INSPECTION.					1	H	7	1 	3O				1A2     					 
1999102900796	19991029	00796	CE  	1999	10	29	99ZZZX4105       	1	19990523	G	2434	01501237	MOUNT           			PIPER 	PA24  	PA24180     	7102402	CE  										ALTERNATOR	LOOSE           	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	09	6017P					241112				INBOARD MOUNT BEGAN WORKING AND EVENTUALLY CAUSED LOSS OF ALTERNATOR BELT TENSION.  ALTERNATOR WAS PREVIOUSLY INSTALLED 	UNDER STC SA 334SW.					1	L	7	1 	3O			NT	1A15    					 
1999102900797	19991029	00797	SW  	1999	10	29	99ZZZX4106       	1	19990927	G	2810		FUEL CELL       			BELL  	47    	47G3B1      	1181028	SW  										FUSELAGE	CONTAMINATED    	H	L			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	80SD					3679				THE REFUELING TRUCK HOSE INTERNALLY DECOMPOSED LEACHING A GUM-LIKE RESIN INTO FUEL WITHIN THE HOSE.  THE FUEL, WHEN PUMP	ED INTO AIRCRAFT'S FUEL TANK, WAS THEN FED TO THE CARBURETOR WHERE RESIN THEN ATOMIZED CLOGGING THE CARB JETS AND RESULT	ING IN A POWER DEGRADATION DURING TAKEOFF.  THE OWNER/OPERATOR AND 2 PASSENGERS WERE DEPARTING A SMALL CLEARING, ON APRI	L 19, 1998, WHEN HELICOPTER BEGAN TO LOSE MANIFOLD PRESSURE AND RPM.  A RAPID DESCENT FOLLOWED, AND WHILE ATTEMPTING A P	EDAL TURN TO REACH A CLEAR AREA, ROTORCRAFT STRUCK TREES AND IMPACTED THE GROUND.  PILOT AND PASSENGERS EXITED WITHOUT I	NJURIES AND A POST-CRASH FIRE CONSUMED ROTORCRAFT WITHIN APPROX 5 MINUTES AFTER THE ACCIDENT.	1	G	7	1 	3O				2H3     					 
1999102900799	19991029	00799	EU  	1999	10	29	99ZZZX4108       	1	19991011	G	5610	343017183	WINDOW          			ISRAEL	1124  	1124A       	4500103	EU  										COCKPIT	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	50HS	1860 				412				PER IAI MM, CHAPTER 5-20-02, PAGE 202, PARA D(4), THIS PART NUMBERED SIDE WINDOW IS NO LONGER INSPECTED AT 800-HOUR INTE	RVALS.  THIS WINDOW CRACKED AT A MOUNT BOLT HOLE AT THE PILOT'S DV WINDOW.  CRACK WAS DETECTED WITH A PRISM.  SUBMITTER 	RECOMMENDED ALL COCKPIT SIDE WINDOWS BE PRISM INSPECTED AT 800-HOUR INTERVALS. SUBMITTER STATED THIS IS THE THIRD AIRPLA	NE WITH THIS P/N WINDOW FOUND CRACKED.  PART TC:  1,184.			2	M	7	2 	4F				A2SW    					 
1999102900800	19991029	00800	CE  	1999	10	29	99ZZZX4109       	1	19991005	G	2913	99123921	PUMP            		MC145474    	CESSNA	525   	525         	2076601	CE  										LT ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	25	888RA	718  			440B	5250135				PUMP FAILED TO PRODUCE HYDRAULIC PRESSURE.						1	L	7	2 	4F			RT	A1WI    					 
1999102900801	19991029	00801	NE  	1999	10	29	99ZZZX4110       	2	19991007	G	7230	5003204023	BLADE           								PWA   	JT8   	JT8D17A     	52049	NE  					ENGINE	BROKEN          	B			RA1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05					35		P709500			ENGINE WAS REMOVED FROM SERVICE DUE TO IN-FLIGHT SHUTDOWN.  THE ENGINE SUFFERED LPT CONTAINED FAILURE.											4	F			E2EA				 
1999110500004	19991105	00004	SO  	1999	11	5	99ZZZX4115       	1	19991019	G	2500		INSULATION      			GULSTM	GV    	GULFSTREAMGV	3980116	SO  										CABIN	BURNED          	H				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			SW	99	77CP					565				IN-FLIGHT SMOKE IN THE CABIN.  NO DAMAGE TO THE AIRCRAFT.  UNDER FLOOR INSULATION WAS FOUND BURNED BECAUSE OF CLOSE PROX	IMITY TO AN ANTI-ICE DUCT.  INSULATION REMOVED AND OPERATION CONTINUED.  GULFSTREAM IS IN THE PROCESS OF EVALUATING AND 	WILL ISSUE A CUSTOMER BULLETIN WHICH WILL REQUIRE INSPECTION OF THE FLEET AND A CORRECTIVE ACTION.				2	L	7	2 	4F			RT	A12EA   					 
1999102900806	19991029	00806	NE  	1999	10	29	99ZZZX4116       	1	19990921	G	2400	8241631	POTENTIOMETER   	HAMSTD      		SKRSKY	S76   	S76         	8143010	NE  										ELECTRICAL	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5403C	6502 	1714 		79J9713	760141				FEEDBACK POTENTIOMETER PREMATURE FAILURE, SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS.  SUBMITTER STATED CAUSED ACTUA	TOR TO KICK IN-FLIGHT.  COMP P/N 7690001802106.					1	G	7	2 	3U				H1NE    					 
1999102900807	19991029	00807	NE  	1999	10	29	99ZZZX4117       	1	19990724	G	2400	8241631	POTENTIOMETER   	HAMSTD      		SKRSKY	S76   	S76         	8143010	NE  										ELECTRICAL	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5414X	7888 	1063 		8410991	760152				FEED BACK POTENTIOMETER PREMATURE FAILURE, SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS.  SUBMITTER STATED CAUSED ACTU	ATOR TO KICK IN-FLIGHT.  COMP P/N 7690001802106					1	G	7	2 	3U				H1NE    					 
1999102900808	19991029	00808	EU  	1999	10	29	99ZZZX4118       	1	19991010	G	7720	704A37142043	TRANSMITTER     			SNIAS 	350   	AS350B      	8680801	EU  										ENGINE	READIS LOW      	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	61CU					1636				LOW PRESSURE READING AT INSTALLATION.						1	G	7	1 	3U				H9EU    					 
1999102900809	19991029	00809	EU  	1999	10	29	99ZZZX4119       	1	19991018	G	7720	704A37642043	TRANSMITTER     			SNIAS 	350   	AS350B      	8680801	EU  										ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	61CU					1636				PRESSURE TRANSMITTER UNIT FAILED WITHIN .1 HOUR.						1	G	7	1 	3U				H9EU    					 
1999102900810	19991029	00810	EU  	1999	10	29	99ZZZX4120       	1	19991018	G	7720		TRANSMITTER     			SNIAS 	350   	AS350B      	8680801	EU  										ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	61CU					1636				PRESSURE TRANSMITTER UNIT FAILED WITHIN 1.1 HOURS.						1	G	7	1 	3U				H9EU    					 
1999102900812	19991029	00812	SO  	1999	10	29	99ZZZX4122       	1	19991013	G	5751		BALANCE WEIGHT  			PIPER 	PA28  	PA28140     	7102802	SO  										AILERON	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	6279					2821148				DISSIMILAR METAL CORROSION BETWEEN OUTBOARD AILERON RIB AND BALANCE WEIGHT BRACE (ATTACHMENT) HELD BY ONLY 9 EACH MS 204	70-AD-3 RIVETS.  RUST AND CORROSION CAUSED RIVETS TO SHEAR.					1	L	7	1 	3O				2A13    					 
1999110500060	19991105	00060	CE  	1999	11	5	99ZZZX4125       	1	19990901	G	3610	312312201	BLEED VALVE     			BEECH 	200   	200BEECH    	1152920	CE  										ENGINE	STICKING        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	401HC	3531 			9B955	BB1294				BLEED VALVE STICKING AT HIGH POWER SETTINGS INTERMITTENTLY.						1	L	7	2 	4T				A24CE   					 
1999110500061	19991105	00061	CE  	1999	11	5	99ZZZX4126       	1	19990930	G	2500		SEAT SUPPORT    			CESSNA	310   	310R        	2074245	CE  										COCKPIT	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	5499J	12236				310R0297				WHILE INSPECTING COPILOT SEAT FOR LOOSENESS, FOUND AFT SEAT TRACK ROLLER WEBS, LEFT AND RIGHT, CRACKED.   P/N'S 0811990-	1, 0811990-2.  ALSO, FOUND LEFT ROLLER BRACKET SUPPORT, P/N 0811992-1 CRACKED.  REPLACED WITH NEW PARTS AND TIGHTENED BO	LTS ON ROLLERS AND SEAT WAS TIGHTER IN TRACKS.				1	L	7	2 	3O				3A10    					 
1999110500062	19991105	00062	NE  	1999	11	5	99ZZZX4127       	2	19990928	G	7230	12788	IMPELLER        			AYRES 	S2    	S2R         	7630202	CE  	PWA   	R1340 	R1340AN1    	52016	NE  					COMPRESSOR	BROKEN          	G				A				UNSCHED LANDING         				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			GL	15	8417V		958  			2177R	19618			CONDUCTING AERIAL APPLICATION, ENGINE SUDDENLY LOST POWER, EMERGENCY LANDING.  INSPECTION DISCLOSED IMPELLER HAD FAILED 	WHICH RESTRICTED AIRFLOW.					1	L	7	1 	3R	3	R	NC	A4SW    	5E2				 
1999110500063	19991105	00063	EA  	1999	11	5	99ZZZX4128       	2	19990827	G	7314		PUMP            								LYC   	O290  	O290D2      	41506	EA  					OIL SYSTEM	CRACKED         	D	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	01										OBSOLETE PUMP BODY.  CRACK WAS COMPLETELY THROUGH BODY.											3	O			E229				 
1999110500064	19991105	00064		1999	11	5	99ZZZX4129       	4	19990912	G	2312	SX165	TRANSCEIVER     			BEECH 	36    	A36         	1151604	CE  										NAV COMM	MALFUNCTIONED   	B			CNZ2	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			WP	01	364DF				58039	E3091				SQUAWK - BURNING SMELL IN CABIN AND NR 2 NAV/COMM STOPPED WORKING.  CONFIRMED PROBLEM.  REMOVED NR 2 KX165 NAV/COMM P/N 	069-1025-25, S/N 58039.  FOUND F401 OPEN IN POWER SUPPLY CIRCUIT.  POWER SUPPLY INPUT SHORTED TO GROUND.  TROUBLESHOT PO	WER SUPPLY CIRCUIT.  TRACED PROBLEM TO SHORTED POWER TRANSFORMER.  REPLACED T400 AND F401  (P/N 019-06019-000) AND (P/N 	036-00058-0006).  MADE MINOR ADJUSTMENTS TO VOR/LOC CONVERTER.  FUNCTION TESTED UNIT PER MM.  UNIT TESTED GOOD.  RE-INST	ALLED UNIT IN AIRCRAFT.  NAV/COMM CHECKED GOOD.		1	L	7	1 	3O				3A15    					 
1999012900096	19990129	00096	GL  	1999	1	29	99ZZZX413        	2	19990112	G	7323	2526146	SPOOL BUSHING   	BENDIX      	252469211   	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					GOVERNOR	FAILED          	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	376AL	388  			84360022S	760002				GOVERNOR REMOVED FOR TORQUE FLUCTUATION.  UPON INSPECTION IN SHOP, FOUND BALL BEARING THAT FELL OUT OF GOVERNOR COVER WH	ILE STILL ASSEMBLED.  SPLIT GOVERNOR BODY IN SHOP AND DISCOVERED SPOOL BUSHING HAD FAILED.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999110500065	19991105	00065		1999	11	5	99ZZZX4130       	4	19991013	G	2350	JJ033	MIC JACK        			CESSNA	182   	182Q        	2072732	CE  										COCKPIT	LOOSE           	B			LX5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	811LL					18266165				PILOT REPORTED LOOSING RECEIVE FUNCTION ON RADIO.  MIC SOCKET FOUND LOOSE BEHIND PEDESTAL.  SECURED SOCKET.  OPS CHECKED	 OK.					1	H	7	1 	3O			NT	3A13    					 
1999110500066	19991105	00066	NM  	1999	11	5	99ZZZX4131       	1	19991007	G	5320		INTERCOSTAL     			BOEING	727   	727225      	1384077	NM  										BS 360	CRACKED         	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	8840E					20383				DURING CONFORMITY  INSPECTION, AN INTERCOSTAL WAS FOUND CRACKED AT STA 360, S16L.						2	L	7	3 	4F				A3WE    					 
1999110500067	19991105	00067	NM  	1999	11	5	99ZZZX4132       	1	19991007	G	5320		INTERCOSTAL     			BOEING	727   	727227      	1384078	NM  										BS 360	CRACKED         	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING CONFORMITY INSPECTION, AN INTERCOSTAL WAS FOUND CRACKED AT STA 360, S16L.						2	L	7	3 	4F				A3WE    					 
1999110500068	19991105	00068	NM  	1999	11	5	99ZZZX4133       	1	19991007	G	5320		INTERCOSTAL     			BOEING	727   	727227      	1384078	NM  										BS 360	CRACKED         	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING CONFORMITY INSPECTION, AN INTERCOSTAL WAS FOUND CRACKED AT STA 360, S16L.						2	L	7	3 	4F				A3WE    					 
1999110500069	19991105	00069		1999	11	5	99ZZZX4134       	4	19991013	G	3140	6228588105	EICAS           			BOEING	747   	74745E      	1384947	NM  										COCKPIT	FAILED          	H				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			WP	03	409EV	4539 			4027	28097				PILOT REPORTED SMOKE IN COCKPIT AND UPPER EICAS DISPLAY UNIT BLANKED OUT DURING ROUTE FROM TPE/DXB ON 10-13-99.  CREW TR	IPPED UPPER EICAS  DUAL CIRCUIT BREAKER AND AIRCRAFT RETURNED TO TPE.  MAINTENANCE CHECKED, FOUND UPPER EICAS DISPLAY UN	IT INTERNAL BURNT OR ARCING.  WIRE AND CONNECTORS CHECKED NORMAL.  REPLACED A NEW EICAS DISPLAY UNIT PER MM 31-61-02.  A	IRCRAFT RETURNED TO SERVICE.			2	L	7	4 	4F			RT	A20WE   					 
1999110500070	19991105	00070	NE  	1999	11	5	99ZZZX4135       	2	19991008	G	7250	2A0851	SEAL            								IAE   	V2500 	V2500A1     		NE  					NR 4 BEARING	CRACKED         	B			KB1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03					0198					PART RECEIVED FROM WESTFIELD GAGE FOR FLUORESCENT PENETRANT INSPECTION IAW INTERNATIONAL AERO ENGINE V2500 PROPULSION SY	STEM ENGINE MANUAL, REVISION 38, SECTION 70-23-01, INSPECTION CHECK-01, TASK 70-23-01-230-501.  PART REJECTED AT FPI DUE	 TO A CRACK ON TOP FLAT APPROXIMATELY .500 INCH LONG AS MARKED ON PART.  PART WAS TAGGED WITH REJECT SYMBOL.									4	F			E311NE				 
1999110500071	19991105	00071	SO  	1999	11	5	99ZZZX4136       	1	19991004	G	7120	6711957	MOUNT           			PIPER 	PA28  	PA28R200    	7102811	SO  										ENGINE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	4559X					28R7635089				DURING A REPAIR ON THE ELECTRIC FUEL PUMP, NOTICED WELDS WERE CRACKED AT THE BASE OF THE TWO VERTICAL ENGINE MOUNT SUPPO	RTS LOCATED DIRECTLY ABOVE THE GEAR DOOR RETRACT SUPPORT.  SUBSEQUENT REMOVAL OF THE ENGINE, PAINT, AND A DYE PENETRANT 	INSPECTION REVEALED THE WELDS WERE COMPELTELY BROKEN AROUND THE CIRCUMFERENCE OF EACH WELD AT THE BASE OF THE WELDS AND 	THE MATING HORIZONTAL TUBE HAND CRACKS DIRECTLY BELOW THE VERTICAL TUBE WELDS.  THOSE CRACKS EXTENDED THROUGH 25 PERCENT	 TO 50 PERCENT OF THE DIAMETER OF THE HORIZONTAL TUBE. THE CRACKS WERE MASKED BY PAINT AND WERE NOT VISIBLE DURING PRIOR	 INSPECTIONS.	1	L	7	1 	3O				2A13    					 
1999110500075	19991105	00075	CE  	1999	11	5	99ZZZX4140       	1	19991011	G	8011	631847	SHAFT GEAR      			CESSNA	421   	421C        	2076016	CE  										STARTER	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	49TD					421C0025				AFTER A FLIGHT FROM CPK TO FRANKFORT, KY, PILOT TRIED TO START THE RIGHT ENGINE AND IT WOULD NOT START.  A MECHANIC TRIE	D TO START IT ALSO AND ONLY THE STARTER MOTOR WOULD SPIN.  THE MECHANIC REMOVED THE STARTER GEAR AND FOUND THE TEETH GON	E.  ENGINE WAS PLACED ON ORDER FOR REPLACEMENT.				1	L	7	2 	3O				A7CE    					 
1999110500076	19991105	00076	SO  	1999	11	5	99ZZZX4141       	1	19990817	G	8011		STARTER         	BENDIX      	MZ4222R     	PIPER 	PA28  	PA28180     	7102808	SO  										ENGINE	ENGAGED         	G				C				ABORTED TAKEOFF         				R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			GL	23	44547					287405259				ON TAKEOFF, AIRCRAFT LOST POWER.  PILOT ELECTED TO LAND ON REMAINING RUNWAY.  AIRCRAFT IMPACTED EARTH DIKE AT END OF RUN	WAY. INVESTIGATION FOUND THAT BENDIX STARTER WAS ENGAGED.					1	L	7	1 	3O				2A13    					 
1999110500077	19991105	00077	SO  	1999	11	5	99ZZZX4142       	1	19991011	G	2910	633871	LINE            			PIPER 	PA34  	PA34200T    	7103406	SO  										HYDRAULIC SYSTEM	CHAFED          	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	99	81TH	493  				347870178				493 HRS SFRM.  UPPER DECK LINE WAS TIGHT TO INT. MANIFOLD PIPE, P/N 631875 AND WAS FOUND CHAFED APPROXIMATELY 75 PERCENT	.  PART WAS REPLACED.					1	L	7	2 	3O				A7SO    					 
1999110500078	19991105	00078		1999	11	5	99ZZZX4143       	4	19991018	G	2562	ELT10	ELT             	NARCO       																CABIN	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19					A269407					SUBMITTER STATED FOUND SEVERAL OF ELT - PULL-OUT ANTENNA RUSTED.																			 
1999110500079	19991105	00079	SO  	1999	11	5	99ZZZX4144       	1	19990728	G	2720	6342005	PEDAL BAR       			PIPER 	PA28  	PA28140     	7102802	SO  										RUDDER CONTROL	CRACKED         	H	S			O				OTHER                   				O			OTHER                     			LD	LANDING        	1			SW	99	15868	4221 				287325182				THE STUDENT PILOT DISCOVERED DURING A CROSS-WING LANDING THAT THERE WAS NO LEFT RUDDER PEDAL CONTROL.  AFTER LANDING, TA	XIING TO THE LEFT WAS ALMOST IMPOSSIBLE.  INSPECTION REVEALED THE RUDDER PEDAL BAR WAS CRACKED BEHIND THE PILOT'S RIGHT 	PEDAL.				1	L	7	1 	3O				2A13    					 
1999110500080	19991105	00080	NE  	1999	11	5	99ZZZX4145       	2	19990928	G	7412	90497703	EXCITER BOX     			CESSNA	500   	560CESSNA   	2076750	CE  	PWA   	JT15  	JT15D5      	52112	NE  					LT ENGINE	MALFUNCTIONED   	B	L		AC1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	01	356WC	464  				5600432				PILOT INITIATED START CYCLE ON LT ENGINE, ROTATION ACHIEVED, FUEL INTRODUCED, NO IGNITION AND ENG FAILED TO START.  MX I	NVEST REVEALED THERE NO AUDIBLE SNAP FROM IGNITERS.  FOUND IGNITERS WET WITH FUEL.  A NON-BURST MODE EXCITER BOX INSTALL	ED AND ACFT DISPATCHED.  IGNITERS REMOVED, FND WORN  CLOSE TO MAX.  SPARE EXCITER BOX REMOVED AND ORIG RE-INSTALLED.  IG	NITION, BOTH PLUGS FIRED, WOULD NOT FIRE WET.  2 NEW IGNITER PLUGS INSTALLED, CHECKED DRY, THEY FIRED.  3 DROPS OF FUEL 	APPLIED, IGNITERS WOULD FIRE WET.  NON-BURST MODE BOX INSTALLED AND 1 OF OLD IGNITERS ATTACHED AND WET WITH FUEL, IGNITE	R FIRED.  IGNITER PLUGS, 231 HRS SINCE INSTALLED.  INSTALLED NEW IGNITER PLUGS ON LT ENG AND RT SIDE LUGS CHANGED.	2	L	7	2 	4F	4	F	RT	A22CE   	E25EA				 
1999110500081	19991105	00081	NE  	1999	11	5	99ZZZX4146       	2	19990928	G	7412		IGNITERS        			CESSNA	500   	560CESSNA   	2076750	CE  	PWA   	JT15  	JT15D5      	52112	NE  					LT ENGINE	WORN            	B			AC1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	01	356WC	464  				5600432				PILOT INITIATED START CYCLE ON LT ENGINE, ROTATION ACHIEVED, FUEL INTRODUCED, NO IGNITION AND ENG FAILED TO START.  MX I	NVEST REVEALED THERE NO AUDIBLE SNAP FROM IGNITERS.  FOUND IGNITERS WET WITH FUEL.  A NON-BURST MODE EXCITER BOX INSTALL	ED AND ACFT DISPATCHED.  IGNITERS REMOVED, FND WORN  CLOSE TO MAX.  SPARE EXCITER BOX REMOVED AND ORIG RE-INSTALLED.  IG	NITION, BOTH PLUGS FIRED.  2 NEW IGNITER PLUGS INSTALLED, CHECKED DRY, THEY FIRED, IGNITERS WOULD FIRE WET.  NON-BURST M	ODE BOX INSTALLED AND 1 OF OLD IGNITERS ATTACHED AND WET WITH FUEL, IGNITER FIRED.  IGNITER PLUGS, 231 HRS SINCE INSTALL	ED.  INSTALLED NEW IGNITER PLUGS ON LT ENG AND RT SIDE LUGS CHANGED.	2	L	7	2 	4F	4	F	RT	A22CE   	E25EA				 
1999110500082	19991105	00082	EA  	1999	11	5	99ZZZX4147       	2	19991001	G	7414	M3485	BEARING         	SLICK       	4370        	PIPER 	PA28  	PA28161     	7102803	SO  	LYC   	O320  	O320D3G     	41508	EA  					MAGNETO	LOOSE           	B	P		DINR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	8269Z	209  			97120934	288116039	L786739A			MAGNETO WAS SQUAWKED FOR EXCESSIVE MAG DROP ON RUN-UP.  NOTED UNUSUAL INDICATIONS ON MAG TIMING INDICATOR LIGHTS.  PULLE	D MAG AND DISASSEMBLED.  FOUND BEARING CAP ASSY (M3485) LOOSE.  THE POINTS MOUNT TO THIS CAP.  THE ENTIRE INSIDE OF THE 	MAG WAS COVERED IN BLACK SOOT, THE DISTRIBUTOR BLOCK, DISTRIBUTOR GEAR, AND POINTS WERE ALL DESTROYED.				1	L	7	1 	3O	3	O		2A13    	E274				 
1999110500083	19991105	00083	NE  	1999	11	5	99ZZZX4148       	2	19990924	G	7260	3020052	SEAL            			ISRAEL	1124  	1124        	4500102	EU  	GARRTT	TFE731	TFE73131G   	01518	NE  					GEARBOX	LEAKING         	C				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			K	J		FLUID LOSS                	WARNING INDICATION        		NR	NOT REPORTED   	1			WP	23	624KM					227	P75103C			ONE HOUR INTO FLIGHT, THE RIGHT ENGINE 'ENGINE OIL PRESS LOW' LIGHT CAME ON.  ENGINE THRUST WAS REDUCED AND EMERGENCY CH	ECK LIST WAS ACCOMPLISHED.  AFTER 2 MINUTES, THE RIGHT ENGINE WAS SHUT DOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS 	MADE AT KLAS.  UPON INSPECTION, A FAILED HYDRAULIC PUMP ACCESSORY GEARBOX SHAFT SEAL WAS FOUND THAT CAUSED LOSS OF OIL. 	 RECURRENCE CONTROL:  NONE.  ISOLATED FAILURE.			2	M	7	2 	4F	4	F		A2SW    	E6WE				 
1999110500084	19991105	00084	CE  	1999	11	5	99ZZZX4149       	1	19991016	G	3222	5082020475	BRACE           		97820000613 	BEECH 	200   	200BEECH    	1152920	CE  										NLG	CORRODED        	B			L5NR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	25	946CE				BB0545	BB540				HEAVILY CORRODED IN CYLINDER BORE.  CORROSION FILLED IN WITH PUTTY.  SUBMITTER STATED CAUSE AS DISSIMILAR METALS AND MOI	STURE.					1	L	7	2 	4T				A24CE   					 
1999110500085	19991105	00085	SO  	1999	11	5	99ZZZX4150       	1	19991012	G	2450		CIRCUIT BREAKER 			PIPER 	PA31  	PA31350     	7103110	SO  										COCKPIT	FAILED          	H				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			SW	99	200AK					318052180				WHILE ADJUSTING PANEL AND INSTRUMENT LIGHTS BRIGHTER, A LARGE STREAM OF SMOKE CAME FROM THE AVIONICS CIRCUIT BREAKER PAN	EL AREA.  SHUT OFF MASTER AND SMOKE STOPPED.  FOUND 'PANEL LIGHT' CIRCUIT BREAKER TRIPPED, WAS THEN DETERMINED THAT IT W	AS OKAY TO TURN MASTER ON.  FOUND A FAILED LAMP AND ASSOCIATED CIRCUIT BOARD MELTED AND CHARRED, SLIGHT RESIDUE OF GYLCO	L AND POSSIBLE WATER.			1	L	7	2 	3O				A20SO   					 
1999110500086	19991105	00086	CE  	1999	11	5	99ZZZX4151       	1	19991011	G	3246	D302104	WHEEL           		99101941    	CESSNA	414   	414         	2075908	CE  										NLG	FAILED          	B			VA1R	O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			SW	19	220RH	3685 	6    			4140905				WHEEL FLANGE, PN D30210-4, SEPARATED FROM HUB ASSY.  PN D30321 AND TUBE BLOW-OUT ON LANDING ROLL-OUT AFTER MAINT TEST FL	IGHT AT THIS REPAIR STATION.  A NEW TIRE HAD BEEN INSTALLED AT CRS BUER634C BEFORE A FERRY FLIGHT TO ACT FOR ENG OVERHAU	L.  FLIGHT TIME SINCE TIRE INSTALLATION WAS 5.6 HOURS WITH THREE LANDINGS.  THE SIX SCREWS PN A1368-1 WHICH RETAIN WHEEL	 FLANGE TO HUB HAD PULLED THREADS OUT OF HUB AND SEPARATED.  TOTAL THREADED SHANK LENGTH OF PN A1638-1 SCREW IS ONE INCH	.  SCREWS PENETRATE HUB MORE THAN .7 INCH WHEN TIGHT.  DEPTH OF THREAD DAMAGE IN HUB MEASURED .4 INCH IN THREE HOLES, .3	 INCH IN ONE HOLE, AND .2 INCH IN TWO REMAINING HOLES.  THIS INDICATES SCREWS HAD BACKED OUT AT TIME OF FINAL FAILURE.	1	L	7	2 	3O			RT	A7CE    					 
1999110500087	19991105	00087	EU  	1999	11	5	99ZZZX4152       	1	19991005	G	2400		HARNESS         			SOCATA	TB10  	TB10TOBAGO  	8680696	EU  										COCKPIT	CHAFED          	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01	55437					1229				MAIN POWER WIRING HARNESS PASSED THROUGH 2 INCH DIAMETER HOLE IN HORIZONTAL ALUMINUM INSTRUMENT PANEL SUPPORT STRUCTURE.	  THIS HOLE IS LOCATED BEHIND FIREWALL APROXIMATELY 10 INCHES AND APPROXIMATELY 1 INCH FROM PILOT'S SIDE OF FUSELAGE WAL	L.  THIS HOLE WAS NOT INSULATED WITH RUBBER OR NYLON GROMMET MATERIAL AND WIRE HARNESS HAD RUBBED THROUGH THE INSTALLATI	ON AT APPROXIMATELY 10 WIRES AGAINST SHARP METAL EDGES OF THE HOLE.			1	L	7	1 	3O			RT	A51EU   					 
1999110500088	19991105	00088	SO  	1999	11	5	99ZZZX4153       	2	19991028	G	8530	2542	BEARING         			BOEING	75    	E75         	1380120	CE  	CONT  	R670  	W6706A      	17016	SO  					NR 2 CYLINDER	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	23	1343M	637  				758445	16821			APPROX 15 MINUTES AFTER TAKEOFF FROM A RE-FUELING STOP ON A LONG CROSS-COUNTRY FLIGHT, OIL TEMP BEGAN A RAPID RISE AND O	IL PRESSURE FELL TO 0-21 PSI (FLUCTUATING).  AN OFF-FIELD LANDING WAS MADE WITH THE AIRCRAFT NOSEING OVER NEAR THE END O	F THE LANDING ROLL.  UPON CHECKING THE MAIN AND SCAVENGING OIL SCREENS, LARGE PIECES OF METAL WERE FOUND IN THE SCAVENGI	NG SCREEN AND IT WAS ALMOST COMPLETELY BLOCKED.  NR 2 CYL WAS PULLED AND THE BALL BEARING CAGES WERE COMPLETELY GONE WIT	H EXTENSIVE PEENING DAMAGE EVIDENT IN THE CRANKCASE.  THE METAL RECOVED FROM THE SCAVENGE SUMP SCREEN WAS IDENTIFIED AS 	PARTS OF THE BEARING CAGES.  UNABLE TO DETERMINE THE CAUSE OR SEQUENCE OF THE FAILURES.	1	Q	7	1 	3R	3	R		A743    	E162				 
1999110500089	19991105	00089	CE  	1999	11	5	99ZZZX4154       	1	19991005	G	7810		DATA PLATE      	WALLCOLMNY  	CE50002     	CESSNA	182   	182G        	2072716	CE  										NR 2 EXH RISER	DETACHED        	C	L			C				ABORTED TAKEOFF         				R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			SO	21	6YJDK	7    			WCC0905515	18255494				PARTIAL POWER LOSS AT FULL THROTTLE WAS EXPERIENCED ON ACFT REGISTERED, 6Y-JDK, PRIOR TO THE COMMENCEMENT OF TAKEOFF ROL	L AT KIRKVINE AERODROME IN JAMACIA.  SEVERAL FULL POWER CHKS ACHIEVED ONLY 2,350 RPM INSTEAD OF THE REQUISITE 2,600 RPM.	  ACFT RETURNED TO RAMP WHERE ANOTHER FULL POWER RUN-UP WAS ATTEMPTED AND MAX RPM SUCCESSFULLY ACHIEVED.  ACFT WAS SHUT 	DOWN.  INVEST BY MAINT REVEALED THE DATA PLATE FROM A RECENTLY INSTALLED LT EXHAUST STACK HAD BECOME DETACHED AND LOCATI	ON OF PLATE WORKED ITS WAY TO THE INDUCTION AIRBOX WHERE IT PARTIALLY BLOCKED CARB AIR INTAKE THAT MANIFESTED ITSELF AS 	PARTIAL POWER LOSS.	1	H	7	1 	3O			NT	3A13    					 
1999110500090	19991105	00090	CE  	1999	11	5	99ZZZX4155       	1	19991018	G	2822		PUMP            			CESSNA	172   	172S        	2072439	CE  										FUEL BOOST	MALFUNCTIONED   	D	L			C				ABORTED TAKEOFF         				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		TO	TAKEOFF        	1			NM	03	949SP					172S8145				NEW 172S CONDUCTING FLIGHT TRAINING AT AIRFIELD ABOVE 6,000 FEET WITH DENSITY ALTITUDE AT 9,000 FEET AND AMBIENT TEMP AP	PROXIMATELY 89 DEGREES FAHRENHEIT.  TAXI AND RUN-UP CHECKS SATISFACTORY.  ON TAKEOFF ROLL, PILOT REPORTED POWER LOSS AND	 REJECTED TAKEOFF.   AIRCRAFT RETURNED TO MAINT AND SHUT DOWN.  APPROX 20 MINUTES LATER, MAINT ATTEMPTED TO START ENGINE	, WITH BOOST PUMP ON, MIXT AND THROTTLE FULL OPEN.  NO FUEL FLOW COULD BE ATTAINED DUE TO FUEL VAPORIZATION.  AFTER ALLO	WING ENGINE TO COOL SUFFICIENTLY, ENGINE START AND RUN-UP WERE NORMAL.		1	H	7	1 	3O			NT	3A12    					 
1999110500091	19991105	00091	EA  	1999	11	5	99ZZZX4156       	2	19991005	G	7314		PUMP            			CESSNA	172   	172S        	2072439	CE  	LYC   	IO360 	IO360L2A    		EA  					FUEL SYSTEM	MALFUNCTIONED   	D	L			O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			NM	03	948SP					172S8144	L2812651A			NEW 172S CONDUCTING FLIGHT TRAINING AT AIRFIELD ABOVE 6,000 FEET WITH AMBIENT TEMP OF 80 DEGREES FAHRENHEIT.  ON 3RD SOR	TIE OF THE DAY, ACFT TAXIED TO RUN-UP AREA AND COMMENCED ENGINE RUN-UP.  AT 1,800 RPM, ENGINE WAS RE-LEANED FOR PEAK RPM	 AND RPM FLUCTUATED BETWEEN 1,500 AND 1,900 RPM.  ENGINE WAS POPPING, HISSING, AND BACKFIRING AND WOULD NOT RUN ABOVE 1,	900 RPM.  ENG WAS OPERATED FOR ONE MINUTE IAW LYC SI 1498 TO REMOVE FUEL VAPORIZATION WITH NO SUCCESS AND RETURNED FOR M	AINTENANCE.  SUBMITTER STATED THE PROBLEM WAS VAPORIZATION OF FUEL DUE TO EXCESSIVE HEAT.  ENG ALLOWED TO COOL 3 HRS AND	 OPER CHK'D SATISFACTORY.  CESSNA NOTIFIED.	1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999110500092	19991105	00092	EU  	1999	11	5	99ZZZX4157       	1	19991019	G	3233	AIR485021	HOUSING         		256471AG    	BRAERO	DH125 	HS125700B   	1500205	EU  										MLG ACTUATOR	BROKEN          	G				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			SO	05	34GG				LK0416	257034				APPEARS ACTUATOR BROKE AT BOLT MOUNT ON ACTUATOR HOUSING WHEN LANDING GEAR WAS RETRACTED OR EXTENDED.  FAILURE OF THE AC	TUATOR CAUSED LT GEAR TO REMAIN IN THE WHEELWELL DURING EMERGENCY LANDING.  PILOT FOLLOWED ALL EMERGENCY PROCEDURES.  PA	RT TOTAL CYCLES:  92.				2	L	7	2 	4F				A3EU    					 
1999110500093	19991105	00093	EU  	1999	11	5	99ZZZX4158       	1	19990909	G	5280	F10A291002401	HINGE           		F10A29100240	AMD   	FALC10	FALCON10    	2730101	EU  										NLG DOOR	FAILED          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	23	77SF	7408 				141				THE PILOT REPORTED THERE WAS AN ABNORMAL 'THUMP' NOISE COMING FROM THE NOSE GEAR AREA WHEN THE GEAR WAS RETRACTED ON SEV	ERAL OCCASIONS.  AN INVESTIGATION REVEALED THE CENTER RT NOSE LANDING GEAR DOOR BELLCRANK/HINGE WAS BROKEN IN HALF.  AN 	INSPECTION OF THE ENTIRE NOSE GEAR AND WHEELWELL AREA SHOWED NO FURTHER DAMAGE.  METAL FATIGUE IS THE SUSPECTED CAUSE OF	 THIS FAILURE.  SUBMITTER SUGGESTED CLOSE INSPECTION OF THESE HINGES BE MADE ANY TIME LANDING GEAR WORK IS PERFORMED AS 	WELL AS DURING ALL PRE AND POST-FLIGHT INSPECTIONS.		2	L	7	2 	4F				A33EU   					 
1999110500094	19991105	00094		1999	11	5	99ZZZX4159       	4	19990920	G	2200	8241631	POTENTIOMETER   	HAMSTD      		SKRSKY	S76   	S76A        	8143006	NE  										AFCS	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5401G	4113 	721  		89120612	760137				FEEDBACK POTENTIOMETER PREMATURE FAILURE, SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS.  SUBMITTER STATED CAUSED ACTUA	TOR TO KICK IN-FLIGHT.  COMPONENT P/N 7690001802106.					1	G	7	2 	3U				H1NE    					 
1999110500095	19991105	00095	CE  	1999	11	5	99ZZZX4160       	1	19990921	G	5610	KPP3DH	RELAY           			CESSNA	210   	P210N       	2073454	CE  										WINDSHIELD HEAT	FAILED          	H	S			O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	23	323DC	4000 				P21000384				THIS RELAY SUPPLIES POWER TO THE WINDSHIELD HEATING PANEL AND IS CONTROLLED BY A CONTROL BOX.  THE WINDSHIELD PANEL WENT	 OPAQUE ON AN IFR FLIGHT IN ICING CONDITIONS AND STAYED OPAQUE THROUGHOUT THE FLIGHT EVEN WHEN THE ICE HAD MELTED FROM T	HE REST OF THE WINDSHIELD WHEN FLYING IN WARMER AIR.  THERE IS NO LIGHT ON INSTRUMENT PANEL TO SHOW WINDSHIELD HEAT IS O	N.  THE CIRCUIT BREAKER CANNOT BE TRIPPED.  THE RELAY STUCK AND THE PILOT HAD NO WAY TO TURN OFF THE PANEL WHICH CAUSED 	IT TO OVERHEAT/GO OPAQUE.		1	H	7	1 	3O				3A21    					 
1999110500096	19991105	00096	NE  	1999	11	5	99ZZZX4161       	2	19991028	G	7230	1B3055	CASE            								PWA   	2037  	F117PW100   		NE  					DIFFUSER	CRACKED         	B			WA2D	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		3318 			DGUSAA0098		P170046			ENGINE REMOVED FOR CRACK AT 17TH STAGE BLEED BOSS, APPROXIMATELY 5 INCHES LONG.  CASE HAS BEEN FORWARDED TO PRATT & WHIT	NEY MATERIAL LAB FOR INVESTIGATION.  PART  TOTAL CYCLES, 2,134.										4	T			E17NE				 
1999110500097	19991105	00097	SO  	1999	11	5	99ZZZX4162       	1	19990927	G	2434	85532003	BEARING         			PIPER 	PA28  	PA28181     	7102807	SO  										PULLEY	FROZEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	4148P	485  				2843177				DURING A ROUTINE INSPECTION, THE ALTERNATOR BELT IDLER PULLEY BEARING WAS FOUND FROZEN.						1	L	7	1 	3O				2A13    					 
1999110500765	19991105	00765	NM  	1999	11	5	99ZZZX4168       	1	19991006	G	5315		FLOORBEAM       			BOEING	727   	727251      	138408H	NM  										BS 344	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM UPPER T-CHORD LBL 24 AT STA 344.						2	L	7	3 	4F				A3WE    					 
1999110500766	19991105	00766	NM  	1999	11	5	99ZZZX4169       	1	19991006	G	3230	66129761	PIN             			BOEING	727   	727251      	138408H	NM  										LT MLG	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON LEFT MAIN LANDING GEAR LOWER TORSION LINK PIN RETAINING PIN.						2	L	7	3 	4F				A3WE    					 
1999110500767	19991105	00767	NM  	1999	11	5	99ZZZX4170       	1	19991006	G	5315		FLOORBEAM       			BOEING	727   	727227      	1384078	NM  										BS 328	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM AT STA 328 LBL 45.5.						2	L	7	3 	4F				A3WE    					 
1999110500768	19991105	00768	NM  	1999	11	5	99ZZZX4171       	1	19991006	G	5240		FRAME           			BOEING	727   	7272K5      		NM  										SERVICE DOOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	369FA					21851				DURING A C-CHECK, CORROSION WAS NOTED ON A/C BAY STA 740 DOOR FRAME, LEFT.						2	L	7	3 	4F			RT	A3WE    					 
1999110500769	19991105	00769	NM  	1999	11	5	99ZZZX4172       	1	19991008	G	2560	65659723	BRACKET         			BOEING	727   	727251      	138408H	NM  										GIRT BAR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	266US					19985				DURING A C-CHECK, CORROSION WAS NOTED ON GIRT BAR BASES NR 1 GALLEY.						2	L	7	3 	4F				A3WE    					 
1999110500770	19991105	00770	CE  	1999	11	5	99ZZZX4173       	1	19991025	G	3260	1013646287	SWITCH          			BEECH 	B300  	B300        	1159232	CE  										NLG	MALFUNCTIONED   	B			LX5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	991LL	1733 				FL142				THE RED LIGHT IN THE LANDING GEAR HANDLE, 'GEAR UNSAFE LIGHT', WOULD NOT EXTINGUISH WITH LANDING GEAR IN FULLY RETRACTED	 POSITION.  JACKED AIRCRAFT, CHECKED ALL UP AND LOCK SWITCHES, AND ASSOCIATED WIRING.  CYCLED LANDING GEAR THROUGH TEN C	OMPLETE EXTENSION/RETRACTION CYCLES.  COULD NOT DUPLICATE.  NO PROBLEMS FOUND.  REPLACED UPLOCK SWITCHES ON ALL 3 LANDIN	G GEAR.  PERFORMED TEST FLIGHT.  OPS CHECK WAS GOOD.			2	L	7	2 	4T			RT	A24CE   					 
1999110500771	19991105	00771	CE  	1999	11	5	99ZZZX4174       	1	19991025	G	3260	10136462811	SWITCH          			BEECH 	B300  	B300        	1159232	CE  										MLG	MALFUNCTIONED   	B			LX5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	991LL	1733 				FL142				THE RED LIGHT IN THE LANDING GEAR HANDLE, 'GEAR UNSAFE LIGHT', WOULD NOT EXTINGUISH WITH LANDING GEAR IN FULLY RETRACTED	 POSITION.  JACKED AIRCRAFT, CHECKED ALL UP AND LOCK SWITCHES, AND ASSOCIATED WIRING.  CYCLED LANDING GEAR THROUGH TEN C	OMPLETE EXTENSION/RETRACTION CYCLES.  COULD NOT DUPLICATE.  NO PROBLEMS FOUND.  REPLACED UPLOCK SWITCHES ON ALL 3 LANDIN	G GEAR.  PERFORMED TEST FLIGHT.  OPS CHECK WAS GOOD.			2	L	7	2 	4T			RT	A24CE   					 
1999111100117	19991111	00117	SO  	1999	11	11	99ZZZX4178       	1	19991001	G	3211	67040013	TRUNNION        			PIPER 	PA28  	PA28R200    	7102811	SO  										LT MLG	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	55599	5662 				28R7335256				IN THE COURSE OF A 100-HOUR INSPECTION, FOUND THE RT GEAR LOOSE.  ON CLOSER INSPECTION, THE LEFT FORWARD ATTACH FITTING 	WAS FOUND TO BE MOVING IN ALL DIRECTIONS.  REMOVED THE LANDING GEAR AND FOUND THE ENTIRE NUTPLATE HAD BROKEN LOOSE.  THI	S ALLOWED THE TRUNNION TO ELONGATE THE HOLES IN THE SPAR WEB AND THE TRUNNION.  THE AIRCRAFT IS USED FOR TRAINING, BUT T	HERE WAS NO REPORT OF UNUSUAL NOISE OR VIBRATION.  ALL MAIN GEAR TRUNNION BOLTS WERE CHECKED, ONE AFT BOLT ON BOTH GEARS	 WAS FOUND LOOSE.  SUBMITTER STATED POSSIBLE CAUSE, THE BOLTS CAME LOOSE WHICH THEN BROKE THE NUTPLATE.		1	L	7	1 	3O				2A13    					 
1999111100118	19991111	00118	SO  	1999	11	11	99ZZZX4179       	1	19991020	G	2820		LINE            			PIPER 	PA28  	PA28151     	7102805	SO  										FUEL SYSTEM	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	151SF					287415411				FOUND COPPER LINE FROM FUEL SELECTOR TO MAIN FUEL LINE CORRODED SEVERELY AND LEAKING.  CORROSION WAS AROUND B-NUT ALSO. 	 REPLACED LINE.					1	L	7	1 	3O				2A13    					 
1999111100119	19991111	00119	GL  	1999	11	11	99ZZZX4180       	1	19991029	G	7810		EXHAUST STACK   			DIAMON	DA20  	DA20C1      	2990001	GL  	CONT  	O240  	IO240B      	17063	SO  					ENGINE	SEPARATED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	212CS	20   				C0048	806978			SUBMITTER STATED THEY HAVE ENCOUNTERED MULTIPLE EXHAUST STACK FAILURES ON FLEET OF KATANA DA-20-C1.  THE SEPARATION OCCU	RRING AT THE EXHAUST PORT ATTACH FLANGE.  AT THIS POINT, FLEET HAS BEEN GROUNDED UNTIL ALL STACKS HAVE BEEN INSPECTED AN	D A CAUSE HAS BEEN DETERMINED.  TOTAL TIME ON AFFECTED PARTS IS LESS THAN 200 HOURS.				1	L	7	1 	3O	3	O	NT	TA4CH   	E7SO				 
1999111100120	19991111	00120	CE  	1999	11	11	99ZZZX4181       	1	19991025	G	2434	3536901817	BRACE           			BEECH 	35    	M35         	1151526	CE  										ALTERNATOR	CRACKED         	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	681V	3614 				D6392				ALTERNATOR FAILED EN ROUTE.  INSPECTION REVEALED THE FIELD WIRE BROKE LOOSE FROM ALTERNATOR MOST LIKELY DUE TO A CRACKED	 ALTERNATOR SUPPORT BRACE BEING CRACKED ALLOWING THE ALTERNATOR TO VIBRATE.					1	L	7	1 	3O				3A15    					 
1999111100121	19991111	00121	CE  	1999	11	11	99ZZZX4182       	1	19991014	G	2432	406607000	INSULATOR       	BFGOODRICH  	PS823B      	LEAR  	24    	24D         	5170311	CE  										BATTERY	FAILED          	B	P		JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	37HT				3653	243				ONE POSITIVE CELL TAB IS SHORTED TO BASE NEGATIVE. AN IN-SERVICE FAILURE FOUND DURING ROUTINE SERVICE/INSPECTION.  SUBMI	TTER STATED INADEQUATE INSULATORS INSTALLED ON CELLS.					2	L	7	2 	4J				A10CE   					 
1999111100122	19991111	00122	CE  	1999	11	11	99ZZZX4183       	1	19990125	G	3232	508101334	BRACKET         			BEECH 	90    	C90A        	1152911	CE  										MLG DOOR	FAILED          	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	27	480JA	5461 				LJ1178				THE MOUNTING BRACKET IS DEPICTED ON 32-10-10, PAGE 6, ITEM 42 OF KING AIR C90A PARTS CATALOG.  THE LT OTBD LANDING GEAR 	DOOR TORQUE TUBE ASSY MOUNTING BRACKET FAILED WHICH PREVENTED THE LT MLG FROM OBTAINING THE FULL UP POSITION.  EXAM OF F	AILED BRACKET INDICATED  IT HAD BEEN CRACKED FOR SOME TIME.  THE CRACK EXTENDS PARALLEL IN THE BEND RADIUS ON THE LEG WI	TH SINGLE BOLT HOLE.  SIMILAR CRACKS WERE FND IN 4 FLEET ACFT BY VISUAL INSP.  ONE CRACKED BRACKET FOUND BY MAGNETIC PAR	TICAL INSP AFTER PAINT REMOVAL.  ALL ACFT HAVE TT EXCESS OF 5,000 HRS AND 11,000 LANDINGS.  SUBMITTER STATED GREATER ATT	ENTION SHOULD BE PAID TO THIS AREA DURING EACH INSPECTION OF HIGH TIME AIRCRAFT.	1	L	7	2 	3T			RT	3A20    					 
1999111100123	19991111	00123	NE  	1999	11	11	99ZZZX4184       	2	19990601	G	7250	718708	BLADE           		800705      	BOEING	747   	747*        		NM  	PWA   	JT9   	JT9D7AH     	52054	NE  					TURBINE	FAILED          	B			WA2D	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03					D63019CN		P662255CN			ENGINE REMOVED POS 2 AT ANCHORAGE, AK 6-1-98 DUE LOW PRESSURE TURBINE FAILURE.  ENGINE RECEIVED FOR MAINTENANCE 1-11-99.	  DISASSEMBLY INSPECTION REVEALED AN APPARENT 5TH STAGE TURBINE BLADE FAILURE.  THE FAILED BLADES WILL BE FORWARDED TO P	RATT & WHITNEY FOR ANALYSIS.  NOTE:  SUBMITTER STATED THIS WAS A FULLY CONTAINED FAILURE.				2	L	7	4 	4F	4	F	RT	A20WE   	E20EA				 
1999111100124	19991111	00124	SW  	1999	11	11	99ZZZX4185       	1	19990917	G	6710	41002413	BEARING         		214076147001	BELL  	214   	214B        	1182100	SW  										SERVO ACTUATOR	DAMAGED         	B			B80R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	CFWQU				1074					BEARING DAMAGED IN THE SERVO ACTUATOR.						2	G	7	1 	4U				H6SW    					 
1999111100125	19991111	00125	SW  	1999	11	11	99ZZZX4186       	1	19990917	G	6710	41002404	CYLINDER        		214076147001	BELL  	214   	214B        	1182100	SW  										SERVO ACTUATOR	DAMAGED         	B			B80R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	CFWQU				1074					CYLINDER ON SERVO ACTUATOR IS DAMAGED.						2	G	7	1 	4U				H6SW    					 
1999111100128	19991111	00128	NM  	1999	11	11	99ZZZX4187       	1	19991008	G	5320		WEB             			BOEING	727   	727230      	1384080	NM  										BS 1170	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	303FV					21619				DURING A C-CHECK, CORROSION WAS NOTED ON SHEAR WEB AT STA 1150 AND STA 1170, LEFT SIDE.						2	L	7	3 	4F				A3WE    					 
1999121000005	19991210	00005	SO  	1999	12	10	99ZZZX4188       	1	19990921	G	2500	9904110002	MONITOR         		SRLQ14AAB   	GULSTM	GV    	GV          		SO  										CABIN	FAILED          	B				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			TX	TAXI/GRND HDL  	1			GL	23	920DC	496  			9803053	534				CABIN COMPARTMENT AFT TV SCREEN CAUGHT FIRE DURING TAXI FOR TAKEOFF.  FORWARD GALLEY HALON FIRE EXTINGUISHER USED TO PUT	 OUT FLAME.  SUBMITTER STATED AT THIS TIME, THE CAUSE OF THE MONITOR FAILURE IS UNDETERMINED.					2	L	7	2 	4F			RT	A12EA   					 
1999111100129	19991111	00129	EU  	1999	11	11	99ZZZX4189       	1	19990930	G	3411	257SF231	RESERVOIR       			BRAERO	DH125 	BAE125800A  	1500285	EU  										SATIC SYSTEM	CORRODED        	B	P		JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	803X	4138 				258127				S8 STATIC DRAIN SYSTEM HAS CORRODED LINE, P/N 25-7SF207-209, AND RESERVOIR, P/N 257SF231.  THE STATIC DRAIN SYSTEM HAS B	EEN MAINTAINED PER MAINTENANCE SCHEDULE ACCORDING TO OWNER/OPERATOR. OWNER HAS HAD THIS ACFT SINCE NEW.  THIS DEFECT WAS	 FOUND DURING COMPLETION OF SB 34-3282 MODIFICATION OF PITOT/STATIC AND STALL VENT DRAIN VALVES.  CUSTOMER OPTED TO C/W 	SB BY MODIFYING FROM THE INSIDE PER SB.			2	L	7	2 	4F			RT	A3EU    					 
1999111100131	19991111	00131	SO  	1999	11	11	99ZZZX4191       	1	19990818	G	2133	13048221	SELECTOR        			GULSTM	G1159 	GIV         	3980115	SO  										COCKPIT	FAILED          	G		A		O				OTHER                   				O			OTHER                     			LD	LANDING        	1			WP	07	99GA				77466	1198				CABIN PRESSURIZATION SELECTOR.  LANDING ALTITUDE TAPE FAILED.  TAPE/RHEOSTAT SLIPPED INTERNALLY.  TAPE DISPLAYED DIFFERE	NT ALT THAN WAS ACTUALLY BEING CONTROLLED; THERE WAS APPROX 1,000 FOOT ERROR.  ERROR CAUSED CABIN ALT AT LANDING TO BE A	PPROX 1,400 FEET BELOW FIELD ELEV.  THE CONCERN IS THE ACFT IS PRESSURIZED GREATER THAN NORMAL AND PLUG TYPE EMERG EXIT 	WINDOWS AND DOORS CANNOT BE OPENED UNTIL PRESSURIZATION IS EQUALIZED.  SUBMITTER STATED THERE IS NO KNOWN IN-SERVICE MAI	NT OR INSP THAT CAN PREVENT THIS.  FAILURE EVIDENT TO CREW AND AFM PROCEDURES COVER MANUAL PRESS CNTRL TO EQUALIZE CABIN	 PRESS.  ENG EVAL OF INTERNAL COUPLING OF TAPE-TO-RHEOSTAT SHOULD BE DONE TO SEE IF DESIGN IMPROVEMENTS NEED TO BE MADE.	2	L	7	2 	4F			RT	A12EA   					 
1999111100133	19991111	00133	CE  	1999	11	11	99ZZZX4193       	1	19991026	G	7500	035A63221	TUBE            			MTSBSI	MU2   	MU2B60      	5780460	CE  	GARRTT	TPE331	TPE33110    	01514	WP  					BLEED AIR	CRACKED         	D	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	157CA					1558SA	P36182C			AIRCAFT IN FOR INSPECTION.  FOUND BLEED AIR TUBE CRACKED AT WELD FOR MOUNT FLANGE TO ENGINE.  SUBMITTER STATED THIS IS 4	TH CONSECUTIVE AIRCRAFT IN FOR INSPECTION THAT ONE OR TWO WERE CRACKED.					1	H	7	2 	3T	4	T	RT	A10SW   	E4WE				 
1999111100134	19991111	00134	CE  	1999	11	11	99ZZZX4194       	1	19991001	G	2435		GENERATOR       	LEARSIEGLER 		BEECH 	100   	B100        	1152919	CE  										LT ENGINE	FAILED          	D				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SO	05	86TR		753  		3709	BE22				PILOT REPORTED LEFT GENERATOR FAILED IN-FLIGHT.  AFTER RE-SETTING LEFT GENERATOR.  BOTH GENERATORS WENT OFF-LINE.  IT WA	S ALSO REPORTED THAT RIGHT OR LEFT GENERATOR WORKED ALONE, BUT REGARDLESS OF WHICH ONE WAS ON-LINE, BRINGING THE SECOND 	GENERATOR ON-LINE CAUSED BOTH FAIL LIGHTS TO ILLUMINATE.  LEFT GENERATOR WS REPLACED WITH SERVICEABLE UNIT AND THIS SOLV	ED THE PROBLEM.			1	L	7	2 	4T				A14CE   					 
1999111100136	19991111	00136	CE  	1999	11	11	99ZZZX4196       	1	19991015	G	3213	05411541	STEP            		054115644   	CESSNA	172   	172G        	2072420	CE  										RT STRUT	SHEARED         	G	P	A		O				OTHER                   				O			OTHER                     			LD	LANDING        	1			GL	15	4621L	5218 				17254616				UPON LANDING, THE RIGHT SPRING STRUT SHEARED OFF JUST ABOVE THE AXLE.  THE STRUT REVEALED SOMEONE HAD WELDED THE FOOT ST	EP TO THE STRUT.  THE WELD PENETRATION POINTS SET UP STRESS ULTIMATELY CAUSING THE STRUT TO SHEAR.  THE LEFT STRUT INSPE	CTED ALSO HAD BEEN WELDED ON IN THE SAME AREA.				1	H	7	1 	3O			NT	3A12    					 
1999111100137	19991111	00137	SW  	1999	11	11	99ZZZX4197       	1	19990804	G	7820	630045503	MUFFLER         			MOONEY	M20   	M20J        	5870219	SW  										EXHAUST SYSTEM	SEPARATED       	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	644DD		10   			240664				FOUND RISER FROM NR 2 CYLINDER HAD DEPARTED FROM MUFFLER WHILE TROUBLESHOOING ROUGH RUNNING ENGINE.  MUFFLER HAD BEEN RE	PAIRED 10 HOURS PRIOR TO THIS FLIGHT.					1	L	7	1 	3O				2A3     					 
1999111100138	19991111	00138		1999	11	11	99ZZZX4198       	1	19990928	G	3213		STRUT           			AMTR  		FLYBABY1A   												MLG	CRACKED         	D	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	09	3249					7216				RIGHT SIDE LANDING, GEAR 'V' STRUT FAILURE.  FRACTURED THROUGH 2  PLYS INSIDE.  FRACTURED THROUGH ONE PLY OUTSIDE AND IN	NER PLY SEPARATED ABOUT 4 INCHES.  SPLIT FROM 2 BOLT HOLES THROUGH 3 PLYS.  INSPECTION OF FUSELAGE MOUNTS AND AREA SHOWE	D NO STRAIN FOR FRACTURES AFTER INCIDENT.  STRUT MET REQUIREMENTS OF ORIGINAL DESIGN.							0 										 
1999111100139	19991111	00139	EA  	1999	11	11	99ZZZX4199       	1	19990517	G	7110	22850219108	PIN             			CNDAIR	CL600 	CL6002B16   	1900305	EA  										RT ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01	601VH	3280 				5043				UPON PRE-FLIGHT, NOTICED NR 9 BLOCKER DOOR STANDING STRAIGHT UP IN THE BYPASS SECTION.  (THE DOOR SHOULD BE FLUSH WITH T	HE T/R STOWED).  THE BLOCKER DOOR ACTUATING ARM WAS DISCONNECTED FROM THE BLOCKER DOOR.  THE PIN AND CLIP FELL OUT ALLOW	ING THE ARM TO BECOME DISCONNECTED FROM THE BLOCKER DOOR.  REPLACED BENT BLOCKER DOOR WITH NEW CLIP AND PIN.				2	L	7	2 	4F			RT	A21EA   					 
1999111100140	19991111	00140	SW  	1999	11	11	99ZZZX4200       	1	19991021	G	6730	212076004101	ACTUATOR        			BELL  	412   	412EP       	1182205	SW  										MAIN ROTOR	FAILED          	B			GS1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	03	60506	15   			HR3334H	36237				ACTUATOR FAILED.  REPLACED WITH NEW ACTUATOR FROM BELL HELICOPTER.						1	G	7	2 	4U				H4SW    					 
1999111100141	19991111	00141	EU  	1999	11	11	99ZZZX4201       	1	19990917	G	5302	350A2300000203	FRAME           			SNIAS 	350   	AS350B1     	8680811	EU  										TAIL BOOM	CRACKED         	B	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	213LA	11994			TB2553	2126				DURING 100-HOUR INSPECTION, FOUND TAIL BOOM APPROXIMATELY 6 INCHES LONG AT AFT HANGER BEARING SUPPORT.  ALSO, RIVETS ATT	ACHING HANGER BEARING SUPPORT TO TAIL BOOM LOOSE AND WORKING.					1	G	7	1 	3U				H9EU    					 
1999111100142	19991111	00142		1999	11	11	99ZZZX4202       	4	19990824	G	2200	8241631	POTENTIOMETER   	HAMSTD      		SKRSKY	S76   	S76         	8143010	NE  										AFCS	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99	5403C	4524 	2224 		90030873	760141				FEEDBACK POTENTIOMETER PREMATURE FAILURE, SUBMITTER STATED SHOULD LAST UNTIL OVERHAUL TIME OF 3,000  HOURS.  CAUSES ACTU	ATOR TO KICK IN-FLIGHT.  COMPONENT P/N 769000180210L.					1	G	7	2 	3U				H1NE    					 
1999111100143	19991111	00143	GL  	1999	11	11	99ZZZX4203       	2	19991007	G	7250	6810063	BEARING         		CAT33903    	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE SECTION	FAILED          	B			M6IR	A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			SO	13	6624N	966  				3169	CAE833330			NR 6 AND NR 7 BEARINGS FAILED IN THE TURBINE.  CAUSE UNKNOWN.  FAILURE OCCURRED DURING NORMAL OPERATION.  WHILE IN CRUIS	E FLIGHT, ENGINE CHIP LIGHT ILLUMINATED AND IMMEDIATE LANDING INITIATED.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999111100144	19991111	00144	GL  	1999	11	11	99ZZZX4204       	2	19991007	G	7250	6873741	BEARING         		CAT33903    	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE SECTION	FAILED          	B			M6IR	A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			SO	13	6624N	966  				3169	CAE833330			NR 6 AND NR 7 BEARINGS FAILED IN THE TURBINE.  CAUSE UNKNOWN.  FAILURE OCCURRED DURING NORMAL OPERATION.  WHILE IN CRUIS	E FLIGHT, ENGINE CHIP LIGHT ILLUMINATED AND IMMEDIATE LANDING INITIATED.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999111100145	19991111	00145	SW  	1999	11	11	99ZZZX4205       	1	19991026	G	2841	407375006101	INDICATOR       			BELL  	407   	407         		SW  										FUEL QUANTITY	FAILED          	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	407WH	65   				53027				REPLACED FUEL QUANTITY INDICATOR WITH NEW INDICATOR FROM BELL HELICOPTER DUE TO FAILURE.						1	G	7	1 	3U			O	H2SW    					 
1999111100146	19991111	00146	SO  	1999	11	11	99ZZZX4206       	1	19991011	G	2823	491947	VALVE           			PIPER 	PA28  	PA28181     	7102807	SO  										FUEL SELECTOR	LEAKING         	H				O				OTHER                   				K	B		FLUID LOSS                	SMOKE/FUMES/ODORS/SPARKS  		NR	NOT REPORTED   	1			GL	19	4144K	845  			5245	2843145				PILOT REPORTED FUEL SMELL FROM CABIN DURING FLIGHT.  AIRCRAFT WAS LOOKED AT BY MAINTENANCE AND THE FUEL SELECTOR WAS FOU	ND LEAKING FUEL.  UPON FURTHER INVESTIATION, THE SNAP RING ON THE FUEL SELECTOR HANDLE SIDE OF THE UNIT WAS FOUND MISSIN	G.  THIS ALLOWED THE INNER VALVE ASSY TO START MOVING OUT OF THE HOUSING ALLOWING FUEL TO LEAK PAST THE O-RING.  INSPECT	ED ALL LIKE AIRCRAFT IN THE FLEET FOR THE SAME DEFECT.  NONE FOUND.			1	L	7	1 	3O				2A13    					 
1999111100241	19991111	00241	CE  	1999	11	11	99ZZZX4207       	1	19991013	G	3222		STRUT           			CESSNA	172   	172S        	2072439	CE  										NLG	LEAKING         	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SO	05	963AC	31   				172S8259				1999 CESSNA 172S NLG STRUT LEAKED DOWN AFTER 31 HOURS SINCE NEW.  UPON EVALUATION, DISCOVERED NLG STRUT ASSY TO BE PRACT	ICALLY EMPTY OF FLUID.  SERVICED PER MM.  ACFT TT:  31.0 HOURS.					1	H	7	1 	3O			NT	3A12    					 
1999111100242	19991111	00242	EA  	1999	11	11	99ZZZX4208       	2	19991101	G	7322	105217	LOCK PLATE      			CESSNA	172   	172M        	2072418	CE  	LYC   	O320  	O320E2D     	41508	EA  					CARBURETOR	FAILED          	D	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	01	9627Q	900  			75083313	17265711				BODY TO BOWL SCREWS LOOSE.  ONE LOCK PLATE MISSING WITH SCREW STILL IN HOLE.  ALL LOCK PLATES BROKEN ALLOWING SCREWS TO 	LOOSEN AND BOWL TO SEPARATE.  LOCK PLATES BAD.					1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999111100243	19991111	00243	CE  	1999	11	11	99ZZZX4209       	1	19991101	G	7820	175400125	MUFFLER         			CESSNA	172   	172M        	2072418	CE  										EXHASUT	LEAKING         	D				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	01	9627Q	800  			NEE082376	17265711				MUFFLERS ONLY LAST 500 TO 800 HOURS BEFORE EXHAUST STARTS LEAKING AT TAILPIPE JUNCTION TO MUFFLER CAN.  TAILPIPE NEEDS T	O BE WELDED INSIDE MUFFLER CAN TO CLOSE CAM JUNCTION.					1	H	7	1 	3O			NT	3A12    					 
1999111100244	19991111	00244	SO  	1999	11	11	99ZZZX4210       	1	19991019	G	2750	30681	FLAP LEVER      			MAULE 	M5    	M5235C      	5460135	SO  										COCKPIT	FAILED          	D	P	A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	01	9236E					7142C				FLAP LEVER FAILED WHILE EXTENDING FLAPS BEYOND THE 20 DEGREE SETTING.  SUBMITTER STATED THIS IS THE SECOND TIME THIS FAI	LURE OCCURRED ON THIS AIRCRAFT.  INITIAL FAILURE OCCURRED AT APPROX 400 HRS TT AIRFRAME WITH PN 3068 STRAIGHT LEVER INST	ALLED.  SECOND FAILURE OCCURRED AT APPROX 1,950 HRS TT INSTALLED.  FAILURE OCCURS AT THE POINT WHERE THE LOCK ROD PROTRU	DES FROM LEVER AT THE .25 INCH HOLE FORWARD OF THE WELDED BEARING PLATE.			1	H	7	1 	3O				3A23    					 
1999111100245	19991111	00245	SO  	1999	11	11	99ZZZX4211       	1	19991021	G	2434	73965009	BELT            			PIPER 	PA28  	PA28235     	7102810	SO  										ALTERNATOR	WORN            	B			BAYR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	9181D					2811029				BELT STARTED TO WEAR IN ONE SPOT ABOUT 6 INCHES LONG AND STARTED TO TURN IN FLYWHEEL GROOVE.						1	L	7	1 	3O				2A13    					 
1999111100246	19991111	00246	CE  	1999	11	11	99ZZZX4212       	1	19991028	G	7602	C2995070201	CONTROL CABLE   			CESSNA	185   	A185E       	2072818	CE  										MIXTURE CONTROL	FAILED          	H				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			SO	15	85PR					18501777				AIRCRAFT GRADUALLY LOST POWER AND CRASHED.  INVESTIGATION FOUND THE THREADED END OF THE MIXTURE CABLE WAS FOUND SEPARATE	D FROM THE ROD END IN THE ENGINE COMPARTMENT.  THE TIPS OF THE ELEVEN THREADS ON THE END OF THE CABLE WERE WORN SO THAT 	IT COULD BE INSERTED IN THE ROD END WITH LITTLE RESISTANCE.  THE JAM NUT WAS FOUND ON THE GOOD THREADS ADJACENT TO THE W	ORN THREADS.  THE ROD END COULD BE SECURELY THREADED ON TO THE SERVICEABLE THREADS.			1	H	7	1 	3O			 	3A24    					 
1999111100247	19991111	00247	CE  	1999	11	11	99ZZZX4213       	1	19991019	G	2140	22540151	CORE            			CESSNA	182   	TR182       	2072735	CE  										HEATER	DETERIORATED    	G		A		A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			WP	17	756LE	1313 				R18201101				THE HEATER CORE END CPA FAILED DUE TO EXCESSIVE  DETERIORATED METAL.  THE HOT GASSES ENTERED THE DUCT RISER-HOSE-CONTROL	 VALVE CAUSING SMOKE IN THE COCKPIT.  THE PILOT WAS FLYING AT 11,000 MSL AND SHUT DOWN THE ENGINE.  PERFORMED AN EMERGEN	CY LANDING CRASHING THE AIRPLANE ON A ROAD.  AIRCRAFT RECORDS WERE NOT DOCUMENTED FOR THE LAST DETAILED VISUAL AND AIR L	EAK TEST AT 50 HOURS.			1	H	7	1 	3O				3A13    					 
1999111100248	19991111	00248	CE  	1999	11	11	99ZZZX4214       	1	19991102	G	7120	71503	MOUNT           			BBAVIA	8     	8KCAB       	2110612	CE  										ENGINE	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	5057G	2276 				54679				ENGINE MOUNT TUBE WAS FOUND BROKEN IN TWO WHERE IT CROSSES ABOVE MAGNETOS CAUSING EXCESSIVE FLEXING OF ENGINE IN MOUNT. 	 AIRCRAFT WAS USED AS AN AEROBATIC TRAINER.					1	H	7	1 	3O				A21CE   					 
1999111100251	19991111	00251	SO  	1999	11	11	99ZZZX4217       	2	19991018	G	8500		ENGINE          			CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  					FORWARD	FAILED          	D				A				UNSCHED LANDING         				Y			ENGINE STOPPAGE           			NR	NOT REPORTED   	1			AL	05	496K		352  			U2063953	814908R			IN-FLIGHT FAILURE OF ENGINE.  APPARENT BROKEN CRANKSHAFT.  NOTE:  AD 99-09-17 C/W BY FACTORY.  INSTALLATION OF NEW CRANK	SHAFT 5-26-99.  NO DAMAGE TO AIRCRAFT DUE TO SUCCESSFUL EMERGENCY LANDING.					1	H	7	1 	3O	3	O		A4CE    	E5CE				 
1999111100252	19991111	00252	CE  	1999	11	11	99ZZZX4218       	1	19991027	G	3110		LIGHT           	AMERIKING   	AK950KLN90B 	BEECH 	1900  	1900C       	1154161	CE  										SWITCH	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	41UE				90639	UC41				'GPS' MODE LIGHT OUT AFTER 726 HOURS/70 DAYS OF OPERATION.						2	L	7	2 	4T			RT	A24CE   					 
1999111100254	19991111	00254	CE  	1999	11	11	99ZZZX4220       	1	19991029	G	5320	04320049	BRACKET         			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  					FUSELAGE	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	25339					15280603				PERFORMED A DETAILED INSPECTION OF BRACKET, PN 0432004-9, CRACKS WERE FOUND ALONG TOP PART OF BRACKET ON THE WELD AREA, 	ONE CRACK 2 INCHES LONG,THE OTHER CRACK, 1.25 INCHES LONG.  ALSO, CRACKS WERE FOUND ALONG RIVNUT HOLES AND BOLT HOLE ON 	THE MAJORITY OF THE BOLT HOLES.  INSPECTED SEVERAL BRACKETS FROM SALVAGE YARDS AND ALL OF THEM WERE CRACKED.  ALL CRACKS	 WERE HIDDEN.  SUBMITTER STATED BRACKET MUST BE REMOVED, CLEANED, AND ZYGLO.			1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999111100255	19991111	00255	EA  	1999	11	11	99ZZZX4221       	2	19991108	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B			BF8R	O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		CR	CRUISE         	1			WP	07	470ER	707  				17280614	L2783651A			DURING NORMAL CRUISE OPERATIONS, THE ENGINE EXPERIENCED A 2 SECOND POWER LOSS, ABOUT 250 RPM.  THE ENGINE WAS THOROUGHLY	 INSPECTED AND NO SUSPECT ITEMS WERE FOUND.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999111100256	19991111	00256	EA  	1999	11	11	99ZZZX4222       	2	19991108	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B		A	BF8R	O				OTHER                   				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			WP	07	429ER	1230 				17280608	L2776851A			DURING NORMAL CRUISE OPERATION, THE ENGINE EXPERIENCED MOMENTARY ROUGHNESS.  THE ENGINE WAS THOROUGHLY INSPECTED AND NO 	SUSPECT ITEMS WERE FOUND					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999111100257	19991111	00257	EA  	1999	11	11	99ZZZX4223       	2	19991108	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B		A	BF8R	O				OTHER                   				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			WP	07	478ER	1022 				17280623	L2779151A			DURING NORMAL CRUISE OPERATIONS, THE ENGINE EXPERIENCED MOMENTARY ROUGHNESS.  THE ENGINE WAS THOROUGHLY INSPECTED AND NO	 SUSPECT ITEMS WERE FOUND.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999111100258	19991111	00258	EA  	1999	11	11	99ZZZX4224       	2	19991108	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B		A	BF8R	O				OTHER                   				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			WP	07	486ER	832  				172806672	L2804051A			DURING NORMAL CRUISE OPERATIONS, THE ENGINE EXPERIENCED MOMENTARY ROUGHNESS.  THE ENGINE WAS THOROUGHLY INSPECTED AND NO	 SUSPECT ITEMS WERE FOUND.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999111100259	19991111	00259	EA  	1999	11	11	99ZZZX4225       	2	19991108	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B		A	BF8R	O				OTHER                   				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CL	CLIMB          	1			WP	07	477ER	856  				17280622	L2803951A			DURING NORMAL CLIMB, THE ENGINE EXPERIENCED MOMENTARY ROUGHNESS (2 SECONDS).  THE ENGINE WAS THOROUGLY INSPECTED AND NO 	SUSPECT ITEMS WERE FOUND.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999111100260	19991111	00260	EA  	1999	11	11	99ZZZX4226       	2	19991108	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B		A	BF8R	O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		CR	CRUISE         	1			WP	07	406ER	1547 				17280297	L2731951A			DURING NORMAL CRUISE OPERATIONS, THE ENGINE EXPERIENCED A 2 SECOND POWER LOSS.  THE ENGINE WAS THOROUGHLY INSPECTED AND 	NO SUSPECT ITEMS WERE FOUND.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999111100261	19991111	00261	EA  	1999	11	11	99ZZZX4227       	2	19991108	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B		A	BF8R	O				OTHER                   				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			WP	07	403ER	2005 				17280245	L2720751A			DURING NORMAL CRUISE OPERATIONS, THE ENGINE EXPERIENCED MOMENTARY ROUGHNESS (2 SECONDS).  THE ENGINE WAS THOROUGHLY INSP	ECTED AND NO SUSPECT ITEMS WERE FOUND.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999111100262	19991111	00262	CE  	1999	11	11	99ZZZX4228       	1	19991004	G	2820	05503623	ELBOW           			CESSNA	172   	172S        	2072439	CE  										FUEL SYSTEM	LEAKING         	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NM	03	494SP	409  				172S8035				DURING PHASE I INSPECTION, FOUND FUEL LEAKING OUT OF AIR INLET ELBOW ADAPTER.  ADAPTER OVERBOARD DRAIN IS RIVETED AND SE	ALED TO ELBOW.  SEALANT MISSING AROUND ONE RIVET AND FUEL LEAKS OUT OF ADAPTER BASE INTO ENGINE COWLING.					1	H	7	1 	3O			NT	3A12    					 
1999111100266	19991111	00266	CE  	1999	11	11	99ZZZX4231       	1	19990902	G	3000	105881	DRAIN HEATER    			CESSNA	650   	650         	2076802	CE  										GALLEY	FAILED          	B	P	A	HAXR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	11	4612Z					6500203				NEW GALLEY DRAIN, PN 105881, WAS INSTALLED.  WHEN ELECTRICAL POWER WAS APPLIED, THE HEATER/DRAIN BURNED OUT.  IT SEEMS T	HE HEATER WAS SHORTED OUT INTERNALLY.					2	L	7	2 	4F				A9NM    					 
1999121000008	19991210	00008	SO  	1999	12	10	99ZZZX4232       	1	19991026	G	2435		WIRE            			GULSTM	GV    	GV          	3980116	SO  										GENERATOR	CHAFED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	83M					557				INSPECTION OF RIGHT ENGINE INTEGRATED DRIVE GENERATOR FEEDER WIRE REVEALED A CHAFE CONDITION BETWEEN THE WIRES AND THE F	IRE LOOP BRACKET AT THE 6 O'CLOCK POSITION.  DAMAGE TO THE WIRE INSULATION IS WITHIN LIMITS.  SPACERS WERE ADDED TO WIRE	 BUNDLE CLAMPS TO GIVE PROPER CLEARANCE BETWEEN WIRE BUNDLE AND FIRE LOOP BRACKET.				2	L	7	2 	4F			RT	A12EA   					 
1999121000009	19991210	00009	SO  	1999	12	10	99ZZZX4233       	1	19991026	G	2435		WIRE            			GULSTM	GV    	GV          	3980116	SO  										GENERATOR	CHAFED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	93M					567				INSPECTION OF RIGHT INTEGRATED DRIVE GENERATOR FEEDER WIRES REVEALED A CHAFE CONDITION BETWEEN THE WIRES AND THE FIRE LO	OP BRACKET AT THE 6 O'CLOCK POSITION.  DAMAGE TO THE WIRE INSULATION IS WITHIN LIMITS.  SPACERS WERE ADDED TO WIRE BUNDL	E CLAMPS TO GIVE PROPER CLEARANCE BETWEEN WIRE BUNDLE AND FIRE LOOP BRACKET.				2	L	7	2 	4F			RT	A12EA   					 
1999111100267	19991111	00267	SO  	1999	11	11	99ZZZX4234       	1	19991015	G	3250	72674003	SPRING          			PIPER 	PA42  	PA42        	7104202	SO  										NLG STEERING	BROKEN          	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	03	112BC	4080 				428001027				FIVE OUT OF SIX SPRING STEEL PLATES WERE BROKEN ON LEFT SIDE OF ASSEMBLY AND CHAFING ON PITOT/STATIC RIGID LINES AND LEF	T SIDE OF WHEELWELL.					1	L	7	2 	4T				A23SO   					 
1999111100268	19991111	00268	SO  	1999	11	11	99ZZZX4235       	1	19991015	G	3250	72674002	SPRING          			PIPER 	PA42  	PA42        	7104202	SO  										NLG STEERING	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	03	112BC	4080 				428001027				FIVE OUT OF SIX SPRING STEEL PLATES WERE BROKEN ON LEFT SIDE OF ASSEMBLY AND CHAFING ON PITOT/STATIC RIGID LINES AND LEF	T SIDE OF WHEELWELL.					1	L	7	2 	4T				A23SO   					 
1999111100269	19991111	00269	CE  	1999	11	11	99ZZZX4236       	1	19991021	G	7920	AE7059761	HOSE            			CESSNA	425   	425         	2076018	CE  										ENGINE OIL	FAILED          	H		A		K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CE	07	50JN	118  				4250232				SIDE WALL OF RIGHT OIL COOLER HOSE, PN AE705976, FAILED WHERE HOSE MAKES A SHARP BEND WHEN INSTALLED.  HOSE FAILED WITH 	NO SIGNS OF PREVIOUS LEAKAGE.  CESSNA RECOMMENDED INSTALLATION OF LONGER OIL HOSE, PN AE7013002K0204.  HOSE INSTALLATION	 REQUIRES FORM 337 FIELD APPROVAL.  FIVE HOURS PRIOR TO THIS FAILURE, THE LEFT HOSE WAS CHANGED DUE TO LEAKAGE.  CURRENT	LY, THE ACFT HAS PN AE7013002K0204 ON LEFT AND RIGHT ENGINES.  IT APPEARS FAILURES COULD BE THE RESULT OF THE SHARP BEND	 THE HOSE MAKES WHEN INSTALLED OR FAULTY MANUFACTURING.  THIS ACFT HAD TO SHUT THE RIGHT ENGINE DOWN WHEN THE FAILURE OC	CURRED IN-FLIGHT.	1	L	7	2 	3T			RT	A7CE    					 
1999111100271	19991111	00271	CE  	1999	11	11	99ZZZX4238       	1	19991021	G	3211	VTB0816	BEARING         			LEAR  	35    	35A         	5170602	CE  										TRUNNION	CRACKED         	B	P	A	WTXR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	37FA	11784				091				DURING REMOVAL OF RIGHT MAIN LANDING GEAR ASSY FOUND OUTER HOUSING OF FORWARD TRUNNION BEARING CRACKED COMPLETELY THROUG	H.  INSTALLED NEW ONE.  BALL WAS EXTREMELY LOOSE IN HOUSING.  LANDINGS:  8,189.					2	L	7	2 	4F				A10CE   					 
1999111100272	19991111	00272	CE  	1999	11	11	99ZZZX4239       	1	19991004	G	3213	9981002815	BRACE           			BEECH 	200   	200BEECH    	1152920	CE  										MLG STRUT	CRACKED         	B			T4OR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	208MS					BB400				FOUND BOTH MAIN LANDING GEAR STRUT BRACES CRACKED AT ATTACH LUG FOR UPPER TORQUE KNEE.  CRACKS ARE APPROXIMATELY .50 INC	H LONG, BOTH ON LEFT UPPER SIDE OF LUG.					1	L	7	2 	4T				A24CE   					 
1999111100273	19991111	00273	CE  	1999	11	11	99ZZZX4240       	1	19990929	G	2434	646853	BRUSHES         		649304      	BEECH 	36    	A36         	1151604	CE  										ALTERNATOR	WORN            	B				O				OTHER                   				H	J		ELECT. POWER LOSS-50 PC   	WARNING INDICATION        		LD	LANDING        	1			EA	23	2032K					E1351				AIRCRAFT LANDED, NO POWER.  BATTERY DEAD.  ALTERNATOR QUIT ONE HOUR PRIOR TO LANDING (BAD WEATHER).  FOUND ALTERNATOR BR	USHES WORN TO  SPRINGS, WORKING INTERMITTENTLY.  INSTALLED NEW BRUSHES, CHECKED OK.  TOTAL TIME UNKNOWN.					1	L	7	1 	3O				3A15    					 
1999111100274	19991111	00274	SO  	1999	11	11	99ZZZX4241       	1	19990920	G	3213	756555	VALVE           			PIPER 	PA42  	PA42        	7104202	SO  										MLG DOOR	STICKING        	B			EASR	O				OTHER                   				J			WARNING INDICATION        			LD	LANDING        	1			EA	23	29TF	6372 			WTC3124	425501003				DURING LANDING GEAR EXTENSION, LEFT AND RIGHT LANDING GEAR WOULD NOT EXTEND.  AN ATTEMPT TO EXTEND THE GEAR WAS MADE USI	NG EMERGENCY BLOW-DOWN SYSTEM.  THE RIGHT GEAR CAME DOWN, BUT NOT THE LEFT.  THE LEFT GEAR EVENTUALLY CAME DOWN.  ACFT W	AS PLACED ON JACKS AND A GEAR RETRACTION TEST WAS COMPLETED.  PROBLEM COULD NOT BE DUPLICATED.  POSSIBLE CAUSE WAS THE I	NBD GEAR DOOR SOLENOID MOMENTARILY STUCK IN THE DOOR CLOSED POSITION.  THE DOOR SOLENOID WAS REPLACED AND GEAR RETRACTIO	N TEST WAS COMPLETED WITH NO PROBLEMS.  IT WAS ALSO DETERMINED A WIRE TO THE LEFT GEAR BLOW-DOWN BOTTLE WAS BROKEN RESUL	TING IN THE INABILITY OF THE LEFT GEAR BEING EXTENDED USING THE EMERGENCY BLOW-DOWN SYSTEM. THE WIRE WAS REPAIRED.	1	L	7	2 	4T				A23SO   					 
1999111100275	19991111	00275	SW  	1999	11	11	99ZZZX4242       	1	19991018	G	2731	50001150913425	CONTROL CABLE   			GULSTM	690TP 	690B        	7630516	SW  										ELEVATOR TRIM	FRAYED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	01	11HY	5371 				11403				CABLE FOR TRIM CONTROL AT THE COLLINS AUTOPILOT ELEVATOR TRIM SERVO WAS FOUND FRAYED APPROXIMATELY 90 PERCENT THROUGH.						1	H	7	2 	3T			 	2A4     					 
1999121000010	19991210	00010	SO  	1999	12	10	99ZZZX4243       	1	19991026	G	2435		WIRE            			GULSTM	GV    	GV          	3980116	SO  										GENERATOR	CHAFED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	73M					547				INSPECTION OF RIGHT ENGINE INTEGRATED DRIVE GENERATOR FEEDER WIRES REVEALED A CHAFE CONDITION BETWEEN THE WIRE AND THE F	IRE LOOP BRACKET AT THE 6 O'CLOCK POSITION.  SPACER WAS ADDED TO WIRE BUNDLE CLAMPS TO GIVE PROPER CLEARANCE BETWEEN WIR	E BUNDLE AND FIRE LOOP BRACKET.				2	L	7	2 	4F			RT	A12EA   					 
1999111900240	19991119	00240	EU  	1999	11	19	99ZZZX4244       	1	19990809	G	4930	2345119059	CLAMP           		38826008    	AMD   	FALC50	FALCON50MYST	2730106	EU  										FUEL CONTROL	FAILED          	D	P			K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	99	9550A	399  			16395	265				THE T-HEAD BOLT ON CLAMP THAT HOLDS THE FUEL CONTROL TO THE APU BROKE LETTING THE CLAMP SPLIT AND FUEL CONTROL TO COME O	FF OF APU.					2	L	7	3 	4F				A46EU   					 
1999111900241	19991119	00241	EU  	1999	11	19	99ZZZX4245       	1	19990806	G	4930	2345119059	CLAMP           		38826008    	AMD   	FALC50	FALCON50MYST	2730106	EU  										FUEL CONTROL	FAILED          	D	P			K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	99	8550A				15234	263				THE T-HEAD BOLT ON CLAMP THAT HOLDS THE FUEL CONTROL TO THE APU BROKE LETTING THE CLAMP SPLIT AND FUEL CONTROL TO COME O	FF THE APU.					2	L	7	3 	4F				A46EU   					 
1999111900243	19991119	00243	NE  	1999	11	19	99ZZZX4247       	2	19991030	G	7200		ENGINE          			LEAR  	25    	25          	5170506	CE  	GE    	CJ610 	CJ6106      	30006	NE  					LEFT	FLAMED OUT      	H				O				OTHER                   				X	J		ENGINE FLAMEOUT           	WARNING INDICATION        		CL	CLIMB          	1			WP	21	800GG	7690 	4564 			008	251162A			DURING CLIMB-OUT, THE LEFT ENGINE EXPERIENCED A FLAME OUT.  THE FLIGHT CREW SAID THEY HEARD A POP AND EXPERIENCED ENGINE	 INDICATIONS ON THE LEFT ENGINE ROLL BACK.  THEY DESCENDED AND PROCEEDED TO COMPLETE EMERGENCY AND NORMAL CHECK LISTS. T	HEY CONCLUDED THE FLAME OUT WAS DUE TO AN OPERATIONAL ERROR AND RESTARTED THE ENGINE AND CONTINUED THE FLIGHT WITHOUT IN	CIDENT.			2	L	7	2 	4J	4	J		A10CE   	1E16				 
1999111900244	19991119	00244		1999	11	19	99ZZZX4248       	1	19990826	G	2910	90002	PISTON          																	HYDRAULIC SYSTEM	CRACKED         	B	S		XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01					BI662					HYDRAULIC PISTON CRACK DETECTED DURING MAGNETIC PARTICLE INSPECTION.  REF:  CALIF PRECISION HYDRAULICS P.O. NR 67296.																			 
1999111900245	19991119	00245	CE  	1999	11	19	99ZZZX4249       	1	19991022	G	3230	05412024	BUSHING         			CESSNA	172   	172R        	2072401	CE  										RT  MLG	FAILED          	B			WIWR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	852CP	199  				17280485				DURING A ROUTINE INSPECTION OF THE AIRFRAME, THE RIGHT MAIN LANDING GEAR MOUNT BUSHING INNER MATERIAL WAS FOUND PRESSED 	COMPLETELY OUT OF THE BUSHING.  POSSIBLE CAUSE OF FAILURE WAS DUE TO IMPROPER FIT BETWEEN LANDING GEAR LEG OUTSIDE DIAME	TER AND BUSHING MATERIAL INSIDE DIAMETER.  INSTALLATION OF BUSHING REQUIRED EXCESSIVE FORCE CAUSING A BREAKDOWN OF THE A	DHESION BETWEEN THE BUSHING MATERIAL OUTSIDE DIAMETER AND THE BUSHING INSIDE DIAMETER.  THE BUSHING MATERIAL WILL THEN L	OOSEN AND EVENTUALLY WORK ITSELF COMPLETELY OUT OF THE BUSHING.		1	H	7	1 	3O			NT	3A12    					 
1999111900246	19991119	00246	CE  	1999	11	19	99ZZZX4250       	1	19991028	G	3246		BOLT            			CESSNA	150   	152         	2071835	CE  										TAILWHEEL	WRONG PART      	H				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			GL	17	49079	945  	533  			15281138				CESSNA 152 TEXAS TAIL DRAGGER CONVERSION. TAILWHEEL HALVE SEPARATED AFTER LANDING DUE TO IMPROPER LENGTH BOLTS (TOO SHOR	T).  INSTALLED CORRECT LENGTH BOLTS AFTER INSPECTING WHEEL HALVES.					1	H	7	1 	3O			NT	3A19    					 
1999111900247	19991119	00247	SO  	1999	11	19	99ZZZX4251       	2	19991027	G	8530	CLASS717	CYLINDER        			CESSNA	210   	210G        	2073430	CE  	CONT  	O520  	IO520A      	17032	SO  					ENGINE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	210DT		572  			21058884	11224471AR			DURING INSPECTION, FOUND GREASE LIKE FLUID ON INDUCTION TUBES AND WHERE CYLINDER AND HEAD ATTACH.  REMOVED AND SENT TO O	VERHAUL SHOP.  REPORTED CRACKED HEAD WILL COME OFF SOON.  REMOVED AND REPLACED CYLINDER.  SUBMITTER RECOMMENDED CHECKING	 THIS LOCATION AT CYLINDER O/H AND KEEP TRACK OF CYLINDER AND HEAD TOTAL TIME.				1	H	7	1 	3O	3	O		3A21    	E5CE				 
1999111900248	19991119	00248	CE  	1999	11	19	99ZZZX4252       	1	19990810	G	2450	CM358950	CIRCUIT BREAKER 			CESSNA	402   	402C        	207590R	CE  										COCKPIT	FAILED          	C				O				OTHER                   				B	J		SMOKE/FUMES/ODORS/SPARKS  	WARNING INDICATION        		NR	NOT REPORTED   	1			NE	01	26514					402C0344				CREW DECLARED EMERGENCY EN ROUTE ACK/BOS WHEN SMOKE CAME FROM AFT SIDE PANEL AFTER RE-SETTING AVIONICS MASTER SWITCH, FO	R AVIONICS FAILURE.  USING EMERGENCY AVIONIC SWITCH, RESUMED COMMUNICATIONS WITH BOS.  APPROACH, LANDED WITHOUT INCIDENT	.  MAINTENANCE REPLACED AVIONICS MASTER SWITCH.  SYSTEM CHECKED OK.				1	L	7	2 	3O				A7CE    					 
1999111900249	19991119	00249	SO  	1999	11	19	99ZZZX4253       	2	19991001	G	8500		ENGINE          			CESSNA	140   	140A        	2071604	CE  	CONT  	C90   	C9012F      	17009	SO  					FORWARD	MALFUNCTIONED   	D				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			GL	23	3797V					15218	40773812			ENGINE LOST POWER.  AIRCRAFT UPSIDE DOWN IN CORN FIELD FOR 3 DAYS.  FLIPPED AIRCRAFT OVER, DISMANTLED, AND HAULED BACK T	O AIRPORT (PTK).  DIALED CRANKSHAFT, OK.  INSTALLED USED SERVICEABLE PROPELLER.  HOOKED UP AUXILIARY FUEL TANK TO LEFT W	ING.  STARTED ENGINE AND RUN-UP FOR 10 MINUTES.  CHECKED MAG DROPS, OK.  FULL THROTTLE RUN-UP (GOOD).  DISMANTLED CARBUR	ETOR.  CHECKED FLOAT, OK.  NO UNUSUAL CONTAMINENTS.  TORE DOWN BOTH MAGS.  SAW NOTHING UNUSUAL.  COULD NOT FIND ANYTHING	 UNUSUAL ANYWHERE.  SUBMITTER SUSPECTED FUEL CONTAMINATION OR CARBURETOR ICE.		1	H	7	1 	3O	3	O		5A2     	E252				 
1999111900250	19991119	00250	EU  	1999	11	19	99ZZZX4254       	1	19990922	G	6120	4507032	FLYWEIGHT       	WOODWARD    	8210263     	BAG   	JETSTM	JETSTM3201  	1500217	EU  										GOVERNOR	FAILED          	B			EY2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	03					2488866A					FLYWEIGHT CAME APART.  FLYWEIGHT HAS SEVERAL DIFFERENT PARTS.  SUBMITTER STATED HARD TO SAY WHAT SPECIFIC PART THAT WAS 	DEFECTIVE					2	L	7	2 	4T			RT	A56EU   					 
1999111900251	19991119	00251		1999	11	19	99ZZZX4255       	4	19991030	G	2562	AK450	ELT             	AMERIKING   																CABIN	MISMANUFACTURED 	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	09										ALL REMOTE SWITCHES WIRED WRONG FROM MANUFACTURER.																			 
1999111900252	19991119	00252	SW  	1999	11	19	99ZZZX4256       	1	19991101	G	5752	047041430000	BEARING         		KFC150      	MOONEY	M20   	M20K        	5870220	SW  										AILERON TRIM	FROZEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	11	252AE	1532 				251111				CUSTOMER COMPLAINED TRIM WAS VERY STIFF TO OPERATE MANUALLY.  INSPECTION FOUND THIS BEARING FROZEN AND NOT ALLOWING TRIM	 TORQUE TUBE TO ROTATE FREELY.  ASSEMBLY WAS REPLACED AND TRIM SYSTEM OPERATION RESTORED.					1	L	7	1 	3O				2A3     					 
1999111900253	19991119	00253	EA  	1999	11	19	99ZZZX4257       	2	19991108	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B		A	BF8R	A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			WP	07	411ER	2076 				17280262	L2779851A			DURING NORMAL CRUISE, THE ENGINE EXPERIENCED MOMENTARY ROUGHNESS.  THE ENGINE WAS THOROUGHLY INSPECTED AND NO SUSPECT IT	EMS WERE FOUND.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999111900254	19991119	00254	EA  	1999	11	19	99ZZZX4258       	2	19991108	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B		A	BF8R	A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			WP	07	480ER	834  				17280624	L2779551A			DURING NORMAL CRUIISE AT 3,500 FEET, THE ENGINE EXPERIENCED MOMENTARY ROUGHNESS.  THE ENGINE WAS THOROUGHLY INSPECTED AN	D NO SUSPECT ITEMS WERE FOUND.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999111900255	19991119	00255	EA  	1999	11	19	99ZZZX4259       	2	19991028	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B		A	BF8R	A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			WP	07	486ER	1069 				17280670	L2804051A			DURING NORMAL CRUISE, THE CREW EXPERIENCED MOMENTARY ENGINE ROUGHNESS.  THE ENGINE WAS THOROUGHLY INSPECTED AND NO SUSPE	CT ITEMS WERE FOUND.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999012900076	19990129	00076	SO  	1999	1	29	99ZZZX426        	1	19990105	G	7921	8522650	COOLER          	LORINORDAM  	AP07AU0G03  	PIPER 	PA28  	PA28151     	7102805	SO  										ENGINE OIL	LEAKING         	D	S			K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	03	32388		80   		81M221	287515143				THE OIL COOLER APPEARS TO HAVE TWO PIECES OF METAL COME TOGETHER WHERE THE OIL COOLER SEPARATED AND OIL POURED OUT.  PIP	ER P/N OF COOLER IS 455-165.					1	L	7	1 	3O				2A13    					 
1999111900256	19991119	00256	EA  	1999	11	19	99ZZZX4260       	2	19991108	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B		A	BF8R	A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	NR	NOT REPORTED   	1			WP	07	458ER	1389 				17280613	L2777551A			WHILE DOING GROUND REFERENCE MANEUVERS, THE ENGINE RAN ROUGH FOR SEVERAL SECONDS.  A THOROUGH INSPECTION WAS PERFORMED O	N ALL ENGINE SYSTEMS AND NO SUSPECT ITEMS WERE FOUND.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999111900257	19991119	00257	EA  	1999	11	19	99ZZZX4261       	2	19991108	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B		A	BF8R	A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			WP	07	475ER	1047 				17280670	L2786551A			DURING NORMAL CRUISE, CREW EXPERIENCED MOMENTARY ENGINE ROUGHNESS.  THE ENGINE WAS THOROUGHLY INSPECTED AND NO SUSPECT I	TEMS WERE FOUND.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999111900258	19991119	00258	EA  	1999	11	19	99ZZZX4262       	2	19991108	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B			BF8R	A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CL	CLIMB          	1			WP	07	422ER	1055 				17280639	L2779851A			DURING NORMAL CLIMB, THE ENGINE EXPERIENCED MOMENTARY ROUGHNESS (2 SECONDS).  THE ENGINE WAS THOROUGHLY INSPECTED AND NO	 SUSPECT ITEMS WERE FOUND.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999112500290	19991125	00290	CE  	1999	11	25	99ZZZX4300       	1	19991025	G	5523	35524554	BRACKET         			BEECH 	33    	F33A        	1151425	CE  										ELEVATOR TRIM	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	21	48RK	1019 				CE1396				TENSION BRACKET FOR ELEVATOR TRIM INDICATOR CABLE BROKE AND CAUSED TRIM SYSTEM TO BIND COMPLETELY, MAKING TRIM SYSTEM UN	MOVABLE.					1	L	7	1 	3O				3A15    					 
1999112500291	19991125	00291	CE  	1999	11	25	99ZZZX4301       	1	19991029	G	5312	24120072	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										BS 75-90	CORRODED        	A			H5GR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	6117R	5052 				172RG0087				BULKHEAD, PN 2412007-2, FROM STA 75.33 TO STA 90.00.  THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST P	IPE EMISSIONS.  SUBMITTER SUGGESTED A LONGER TAILPIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT.  INSPE	CTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION.  AIRCRAFT TT 5,052.5 HOURS.				1	H	7	1 	3O				3A17    					 
1999112500292	19991125	00292	CE  	1999	11	25	99ZZZX4302       	1	19991029	G	5312	24120072	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										BS 90-108	CORRODED        	A			H5GR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	6117R	5052 				172RG0087				BULKHEAD, PN 2412017-2, FROM STA 90.00 TO STA 108.00.  THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST 	PIPE EMISSIONS.  SUBMITTER SUGGESTED A LONGER TAILPIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT.  INSP	ECTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION.  AIRCRAFT TT 5,052.5 HOURS.				1	H	7	1 	3O				3A17    					 
1999112500293	19991125	00293	CE  	1999	11	25	99ZZZX4303       	1	19991029	G	5320	24110332	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										FUSELAGE	CORRODED        	A			H5GR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	6117R	5052 				172RG0087				FORWARD BUMPER ASSEMBLIES PN 2411033-2.  THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST PIPE EMISSIONS	.  SUBMITTER SUGGESTED A LONGER TAILPIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT.  INSPECTION OF LIKE	 MODEL AIRCRAFT REVEALED SIMILAR CORROSION.  AIRCRAFT TT 5,052.5 HOURS.				1	H	7	1 	3O				3A17    					 
1999112500294	19991125	00294	CE  	1999	11	25	99ZZZX4304       	1	19991029	G	5312	24110111	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										BS 75	CORRODED        	A			H5GR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	6117R	5052 				172RG0087				BULKHEAD, PN 2411011-1 AND DOUBLER PN 2411013-2 AT STA 75.33.   THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE	 EXHAUST PIPE EMISSIONS.  SUBMITTER SUGGESTED A LONGER TAILPIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRA	FT.  INSPECTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION.  AIRCRAFT TT 5,052.5 HOURS.				1	H	7	1 	3O				3A17    					 
1999112500295	19991125	00295	CE  	1999	11	25	99ZZZX4305       	1	19991029	G	5320	124120201	TUNNEL          			CESSNA	172   	172RG       	2072438	CE  										BS 108	CORRODED        	A			H5GR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	6117R	5052 				172RG0087				TUNNEL ASSEMBLY PN 12412020-1 AFT OF STA 108.0 AFT UPPER CORNER.   THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENG	INE EXHAUST PIPE EMISSIONS.  SUBMITTER SUGGESTED A LONGER TAILPIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIR	CRAFT.  INSPECTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION.  AIRCRAFT TT 5,052.5 HOURS.				1	H	7	1 	3O				3A17    					 
1999112500296	19991125	00296	CE  	1999	11	25	99ZZZX4306       	1	19991029	G	5315	24120191	FLOORBOARD      			CESSNA	172   	172RG       	2072438	CE  										BS 90-108	CORRODED        	A			H5GR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	6117R	5052 				172RG0087				FLOORBOARD PN 2412019-1 FROM STA 90.00 TO STA 108.00.  THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST 	PIPE EMISSIONS.  SUBMITTER SUGGESTED A LONGER TAILIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT.  INSPE	CTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION.  AIRCRAFT TT 5,052.5 HOURS.				1	H	7	1 	3O				3A17    					 
1999112500297	19991125	00297	CE  	1999	11	25	99ZZZX4307       	1	19991029	G	5320	24110105	BULKHEAD        			CESSNA	172   	172RG       	2072438	CE  										BS 65-90	CORRODED        	A			H5GR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	6117R	5052 				172RG0087				BULKHEAD, PN 2411010-5 FROM STA 65.33 TO STA 90.0.   THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST PI	PE EMISSIONS.  SUBMITTER SUGGESTED A LONGER TAILIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT.  INSPECT	ION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION.  AIRCRAFT TT 5,052.5 HOURS.				1	H	7	1 	3O				3A17    					 
1999112500298	19991125	00298	CE  	1999	11	25	99ZZZX4308       	1	19991029	G	5320	24120162	COVER           			CESSNA	172   	172RG       	2072438	CE  										BS 108	CORRODED        	A			H5GR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	6117R	5052 				172RG0087				RIGHT HAND COVER ASSEMBLY PN 2412016-2 AT STA 108.   THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST PI	PE EMISSIONS.  SUBMITTER SUGGESTED A LONGER TAILIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT.  INSPECT	ION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION.  AIRCRAFT TT 5,052.5 HOURS.				1	H	7	1 	3O				3A17    					 
1999112500299	19991125	00299	EU  	1999	11	25	99ZZZX4309       	2	19991025	G	8550	72346	OIL SUMP        			PIPER 	PA36  	PA36300     	7103612	SO  	RROYCE	TAY   	TAY6118     		EU  					ENGINE	LEAKING         	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	17	59650	6777 	253  		230A3	367760060	76442			PILOT STATED AFTER ENGINE SHUT DOWN, THAT OIL WAS DRAINING FROM INTAKE SYSTEM.  UPON FURTHER INVESTIGATION, FOUND THE NR	 3 CYLINDER INTAKE EXTENSION PIPE HAD FALLEN OUT OF ITS SWAGED RECEPTACLE AND CHAFED A HOLE IN THE BOTTOM OF THE OIL SUM	P.  AFTER REMOVAL OF OIL SUMP, FOUND THE PROBLEM HAD OCCURRED BEFORE BECAUSE THERE WAS A WELD AT THE SAME SPOT.  ALSO, A	FTER REMOVAL OF THE OIL SUMP, THE SUMP SWASHPLATE WAS FOUND WITH TWO BREAKS AT ATTACH POINTS, AND MULTIPLE CRACKS AT ATT	ACH POINTS.		1	L	7	1 	3O	4	F		A10SO   	E25NE				 
1999112500300	19991125	00300		1999	11	25	99ZZZX4310       	4	19991109	G	2565	312611026	HOSE            	BFGOODRICH  	5WA23030G201															ESCAPE SLIDE	WRONG PART      	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	19					FF004					EVACUATION SLIDE/RAFT RECEIVED WITH INCORRECT HOSES.  CORRECT HOSES P/N SHOULD BE 720111-101.  NOTE:  THIS UNIT WAS LAST	 OVERHAULED IN 6-98.																		 
1999112500301	19991125	00301	EA  	1999	11	25	99ZZZX4311       	2	19991109	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTION     	B		A	BF8R	O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			WP	07	405ER	2001 				17280285	L2732551A			WHILE IN CRUISE AT 1,000 FEET, THE CREW EXPERIENCED A 1 TO 2 SECOND HESITATION.  A COMPLETE INSPECTION OF THE ENGINE, RE	LATED COMPONENTS AND SYSTEMS DID NOT DISCLOSE ANY ABNORMALITIES.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999112500302	19991125	00302	CE  	1999	11	25	99ZZZX4312       	1	19991105	G	2710	S3784	PULLEY          			CESSNA	172   	172N        	2072434	CE  										AILERON	SEPARATED       	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	75803					17267962				FOLLOWING WIND STORM, DISCOVERED BROKEN AILERON INPUT CONTROL ROD ON LT AILERON.  FURTHER INSP REVEALED ZERO TENSION ON 	AILERON CONTROL CABLES.  DISCOVERED RT UPPER AILERON PULLEY THRU-BOLT COMPLETELY BACKED OUT OF PULLEY.  PULLEY, BOLT, NU	T, AND BUSHING FELL OUT OF HEADLINER AREA WHEN HEADLINER WAS REMOVED.  PULLEY THRU-BOLT WAS AN 4-14 VICE AN 4-15 AS REQU	ESTED BY PARTS MANUAL.  LOGS AND CONDITION OF GENERAL AREA INDICATE NO WORK PERFORMED THAT WOULD HAVE AFFECTED PULLEY AS	SY.  SUSPECT SHORTER BOLT WAS INSTALLED AT TIME OF MFG.  ELONGATION OF BOLT HOLES INDICATED BOLT WAS LOOSE AND WORKING F	OR SOME TIME.	1	H	7	1 	3O			NT	3A12    					 
1999112500303	19991125	00303	CE  	1999	11	25	99ZZZX4313       	1	19991024	G	2750	16952404717	CONTROL CABLE   			BEECH 	23    	C23         	1151242	CE  										TE FLAP	FRAYED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	13	66345	7420 				N2208				DURING ANNUAL INSPECTION, THE FLAP CABLE WAS FOUND FRAYED AROUND TORQUE TUBE.  THIS COULD NOT BE EASILY SEEN UNTIL FLAPS	 WERE LOWERED AND CABLE CLEANED.					1	L	7	1 	3O				A1CE    					 
1999112500304	19991125	00304	CE  	1999	11	25	99ZZZX4314       	1	19991029	G	5311	085112141	FRAME           			CESSNA	340   	340A        	2076405	CE  										ENGINE BAY	CORRODED        	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	5171J	2068 				340A0006				CORROSION HAS EATEN AWAY ABOUT 2 SQUARE INCHES ON THE TOP OF THE 0851121-41 LT OUTBOARD BEAM ASSY BEHIND THE CANTED WEB 	AND IN FRONT OF THE FIREWALL.  THE HEADS OF SEVERAL RIVETS ARE ALSO MISSING IN THIS AREA.  EXHAUST GASSES AND HIGH TEMPE	RATUES IN THIS AREA SEEM TO BE THE REASON FOR THE CORROSION.				1	L	7	2 	3O				3A25    					 
1999112500305	19991125	00305	SO  	1999	11	25	99ZZZX4315       	1	19991013	G	2710	3547603	PUSHROD         			PIPER 	PA32  	PA32301T    	7103209	SO  										AILERON	FRACTURED       	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	8192Q					328024020				WHEN PILOT CHECKED CONTROLS AT RUN-UP, THE LT AILERON PUSHROD BROKE AT FIRST THREAD FLUSH WITH FACE OF ROD END JAM NUT. 	 SUBMITTER NOT SURE IF CAUSE WAS INTERGRANULAR CORROSION OR A MFG DEFECT.  BOTH LT AND RT PUSHRODS AS WELL AS STABILATOR	 PUSHROD (WHICH IS OF SIMILAR CONSTRUCTION) WILL BE REPLACED WITH NEW PARTS.  THE THREADED PORTION OF THIS ASSY IS DIFFI	CULT TO INSPECT WITHOUT COMPLETE DISASSY.			1	L	7	1 	3O				A3SO    					 
1999112500306	19991125	00306	NM  	1999	11	25	99ZZZX4316       	1	19991015	G	3240	B2701	VALVE BODY      	SARGENT     	B270014     	BOEING	727   	727         	UTILSYS	NM  										BRAKE	CRACKED         	B	P		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					7401					BODY IS CRACKED IN BRAKE AND PRESSURE PORTS.  WEAK POINT IN BODY, FATIGUE AND/OR OVERSTRESSED.						2	L	7	3 	4J			RT	A3WE    					 
1999112500308	19991125	00308	CE  	1999	11	25	99ZZZX4318       	1	19991020	G	2730	1155240463	BELLCRANK       			BEECH 	99    	C99         	1154006	CE  										ELEVATOR	LOOSE           	B	S	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	6656N	330  				U213				FOUND ELEVATOR BELLCRANK ASSY LOOSE ON SHAFT.  TAPER PINS COULD NOT BE TIGHTENED ANY FURTHER WITH RUNNING OUT OF HEAD DE	PTH CLEARANCE.  SEEMS THAT THE HOLES WERE DRILLED TOO LARGE OR ELONGATED.  TAPER PIN P/N 115-524046-3.					1	L	7	2 	3T				A14CE   					 
1999112500309	19991125	00309	CE  	1999	11	25	99ZZZX4319       	1	19991102	G	2120	66001122	BLOWER          	ELECTROMECH 		LEAR  	35    	35A         	5170602	CE  										AIR DIST	FAILED          	B			DINR	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			EA	17	258G		106  		1092	443				CABIN AIR BLOWER SN 1092 INSTALLED 712-99.  FAILED 10-29-99 WITH ONLY 106 HRS TSO.  (STARTED MAKING NOISE THEN LOCKED UP	 AND CREATED BURNING SMELL IN CABIN).  REPLACEMENT BLOWER SN 1102 INSTALLED 11-2-99 AND IT DID NOT LAST FIVE MINUTES.  (	BEGAN MAKING NOISE AND VIBRATING WITHIN THE FIRST MINUTE OF OPERATION, THEN ABOUT FOUR MINUTES LATER HAD PROGRESSED TO V	ERY VIOLENT NOISE AND VIBRATIONS AND THE FANS BEGAN TO RUB THE HOUSINGS).  DISABLED THIS BLOWER AND A THIRD BLOWER IS ON	 ORDER.		2	L	7	2 	4F				A10CE   					 
1999112500310	19991125	00310	CE  	1999	11	25	99ZZZX4320       	1	19991102	G	2120	66001122	BLOWER          	ELECTROMECH 		LEAR  	35    	35A         	5170602	CE  										AIR DIST	FAILED          	B			DINR	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			EA	17	258G		106  		1102	443				CABIN AIR BLOWER SN 1092 INSTALLED 712-99.  FAILED 10-29-99 WITH ONLY 106 HRS TSO.  (STARTED MAKING NOISE THEN LOCKED UP	 AND CREATED BURNING SMELL IN CABIN).  REPLACEMENT BLOWER SN 1102 INSTALLED 11-2-99 AND IT DID NOT LAST FIVE MINUTES.  (	BEGAN MAKING NOISE AND VIBRATING WITHIN THE FIRST MINUTE OF OPERATION, THEN ABOUT FOUR MINUTES LATER HAD PROGRESSED TO V	ERY VIOLENT NOISE AND VIBRATIONS AND THE FANS BEGAN TO RUB THE HOUSINGS).  DISABLED THIS BLOWER AND A THIRD BLOWER IS ON	 ORDER.		2	L	7	2 	4F				A10CE   					 
1999112500311	19991125	00311	CE  	1999	11	25	99ZZZX4321       	1	19991102	G	2120	1005540443	DUCT            		1005540441  	BEECH 	100   	B100        	1152919	CE  										AIR DIST	LEAKING         	E		A		O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			CE	03	4490M	6965 				BE64				FLIGHT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE.  TROUBLESHOOTING REVEALED THE AIR CONDITIONING NOSE DISTRIBUTION DUC	T LEAKING.  THE 'CROSSOVER DUCT' (WELDED ALUMINUM SECTION) CRACKED AND SEPARATED 10.2 INCHES LONG AT THE UPPER FORWARD L	ATERIAL WELD.  THIS PORTION OF THE DISTRIBUTION DUCTING IS NOT ACCESSIBLE FOR INSPECTION WITH CURRENT INSPECTION PROCEDU	RES.			1	L	7	2 	4T				A14CE   					 
1999112500312	19991125	00312	EU  	1999	11	25	99ZZZX4322       	1	19991104	G	7500	BAS2452502	CLAMP           			BRAERO	DH125 	BAE125800A  	1500285	EU  										LT ENGINE	FAILED          	D	S			O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	21	290EC	4930 				258172				CLAMP PN BAS-245-25-2 ITEM 65 OF IPC DRAWING NR 21-10-05-05 FAIELD AT ASSY JOINT CAUSING LP BLEED AIR LEAK AT SLEEVE ITE	M 70 OF IPC DRAWING NR 21-10-05-05.  LP BLEED AIR LEAK CAUSED SLEEVE TO DETERIORATE TO POINT WHERE IT ALSO NEEDED TO BE 	REPLACED.				2	L	7	2 	4F			RT	A3EU    					 
1999112500313	19991125	00313	CE  	1999	11	25	99ZZZX4323       	1	19991026	G	5520	NAS110438D	BOLT            			LEAR  	35    	35A         	5170602	CE  										AILERON	BENT            	B	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	98AC	3584 				301				AILERON BOLT FOUND BENT.  THIS IS A LIFE-LIMIT PART TO BE REPLACED EVERY 3,600 HOURS.						2	L	7	2 	4F				A10CE   					 
1999112500314	19991125	00314	CE  	1999	11	25	99ZZZX4324       	1	19991005	G	2913	D007966166	PUMP            			CESSNA	750   	750         	2076810	CE  										HYDRAULIC SYSTEM	LEAKING         	B			CNQR	O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		NR	NOT REPORTED   	1			CE	07	950QS	1160 			M035	7500050				HYDRAULIC VOLUME LOW 'A' SYSTEM IN-FLIGHT AT FL 410, SHUT DOWN 'A' HYDRAULIC SYSTEM.  FOUND 3 EACH SMALL PIN HOLES IN HY	DRAUIC PUMP HOUSING.  REPLACED ENGINE DRIVEN HYDRAULIC PUMP.					2	L	7	2 	4J			RT	T00007WI					 
1999112500315	19991125	00315	CE  	1999	11	25	99ZZZX4325       	1	19991025	G	2761	6F305B	RESTRICTOR      			RKWELL	NA265 	NA26565     	7630107	CE  										SPOILER	FAILED          	B			KI2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	01	82CR	6380 				46549				SPOILERS ACTUATED IN THE FAST MODE IN BOTH 'AIT' AND 'GROUND AUTO' POSITIONS.  IN-FLIGHT ACTIVATION CAUSED FAST ACTUATIO	N AND SUDDEN ALTITUDE LOSS.  DETERMINED THAT RESTRICTOR THAT WAS INSTALLED PER SABRELINER S.O.K. 81-5 HAD FAILED INTERNA	LLY AND ALLOWED FLUID TO PASS UNRESTRICTED.  SUBMITTER RECOMMENDED VISUAL  INSPECTION EACH 4,000 LANDINGS.				2	L	7	2 	4J				A2WE    					 
1999112500316	19991125	00316	EU  	1999	11	25	99ZZZX4326       	2	19991028	G	7230		BLADE           			GULSTM	G1159 	GIV         	3980115	SO  	RROYCE	TAY   	TAY6118     		EU  					HP COMPRESSOR	DAMAGED         	H	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	1SL	5420 				1167	76442			SUBJECT ENGINE REMOVED FROM AIRCRAFT, NR 2 POSITION, IN APRIL, 1997, FOR A MID-LIFE AND CALENDAR REWORK IAW NMSB70-1050 	REV 3 APPENDICES I & II.  THE ENGINE WAS REPAIRED AT ROLLS ROYCE CANADA, MONTREAL.  THE ENGINE WAS RE-INSTALLED AND COMP	LETED A FURTHER 1,685 HRS AND 777 CYCLES IN OPERATION BEFORE REMOVAL WAS REQUIRED FOLLOWING REPORTS OF VIBRATION AND SUB	SEQUENT BORESCOPE INSPECTIONS REVEALING DAMAGE TO THE STAGE 12 HP COMPRESSOR ROTOR BLADES.  IT WAS REPORTED THE ENGINE H	AD BEEN IN THE VICINITY OF SEVERE WEATHER AT THE TIME OF THE INCREASED LEVELS OF VIBRATION.  ENGINE REMOVED AND CONSIGNE	D TO DALLAS AIRMOTIVE FOR INVESTIGATION AND REPAIR.	2	L	7	2 	4F	4	F	RT	A12EA   	E25NE				 
1999120400299	19991204	00299	WP  	1999	12	4	99ZZZX4332       	1	19991011	G	6320	6894171	SEAL            			HUGHES	369   	369D        	4470706	WP  										GEARBOX	DELAMINATED     	B			EOOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	5074R	13826	4880 		CAG32934	1151D				DURING REMOVAL OF TURBINE SECTION, A PREVIOUSLY REPAIRED AREA AROUND THE TURBINE SEAL BOSS ON THE GEARBOX COVER HAD DELA	MINATED.  REPLACED GEARBOX.					1	G	7	1 	3U				H3WE    					 
1999120400300	19991204	00300	GL  	1999	12	4	99ZZZX4333       	2	19991006	G	7240	A23056108	COMBUSTION LINER			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	CRACKED         	B			EOOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	5074R	442  			95A01	1151D	CAE832750			DURING REPLACEMENT OF TURBINE, THE COMBUSTION LINER WAS FOUND CRACKED AT THE EXPANSION SLOTS AT THE DOUBLE LIP AND THE F	UEL NOZZLE FERRULE HAS A DEEP STEP WORN AT THE 6 O'CLOCK POSITION.					1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999121100717	19991211	00717	NM  	1999	12	11	99ZZZX4344       	1	19991117	G	5311		FRAME           			BOEING	727   	727227      	1384078	NM  										BS 1163	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT STA 1163 STR 13 AND STR 14L.						2	L	7	3 	4F				A3WE    					 
1999121100718	19991211	00718	NM  	1999	12	11	99ZZZX4345       	1	19991117	G	5311		FRAME           			BOEING	727   	727227      	1384078	NM  										BS 420	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	79754					21363				DURING A C-CHECK, CORROSION WAS NOTED ON LOWER FRAME STA 420 R-1 DOOR.						2	L	7	3 	4F				A3WE    					 
1999121100719	19991211	00719	NM  	1999	12	11	99ZZZX4346       	1	19991117	G	5320		SHEAR TIE       			BOEING	727   	727227      	1384078	NM  										BS 680	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED AT BL ZERO STA 680 SHEAR TIE.						2	L	7	3 	4F				A3WE    					 
2000012100005	20000121	00005	NM  	2000	1	21	99ZZZX4347       	1	19991117	G	5330		SKIN            			BOEING	727   	727227      	1384078	NM  										BS 500	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED ON SKIN AT STA 500 STR 27R.						2	L	7	3 	4F				A3WE    					 
1999121100720	19991211	00720	NM  	1999	12	11	99ZZZX4348       	1	19991117	G	5313		STRINGER        			BOEING	727   	727227      	1384078	NM  										BS 500	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED ON STR 27R STA 500.						2	L	7	3 	4F				A3WE    					 
1999121100722	19991211	00722	NM  	1999	12	11	99ZZZX4350       	1	19991117	G	5313		STRINGER        			BOEING	727   	727227      	1384078	NM  										BS 1010-1030	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED ON STR LBL 20 STA 1010 - STA 1030.						2	L	7	3 	4F				A3WE    					 
1999121100723	19991211	00723	NM  	1999	12	11	99ZZZX4351       	1	19991117	G	5320		SHEAR TIE       			BOEING	727   	727227      	1384078	NM  										BS 720	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED AT STA 720 ON SHEAR TIE BL ZERO.						2	L	7	3 	4F				A3WE    					 
1999121100724	19991211	00724	NM  	1999	12	11	99ZZZX4352       	1	19991117	G	5350		SKIN            			BOEING	727   	727227      	1384078	NM  										BS 950F-970	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED ON SKIN APPROXIMATELY LBL 20 STA 950F - STA 970.						2	L	7	3 	4F				A3WE    					 
1999121100725	19991211	00725	NM  	1999	12	11	99ZZZX4353       	1	19991117	G	5320		WEB             			BOEING	727   	727227      	1384078	NM  										BS 950F-970	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED ON WEB AT STA 950F - STA 970 APPROXIMATELY LBL 20.						2	L	7	3 	4F				A3WE    					 
1999121100726	19991211	00726	NM  	1999	12	11	99ZZZX4354       	1	19991117	G	5315		FLOORBEAM       			BOEING	727   	727227      	1384078	NM  										BS 328	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED ON FLOORBEAM STA 328 LBL 45.5.						2	L	7	3 	4F				A3WE    					 
1999121100727	19991211	00727	NM  	1999	12	11	99ZZZX4355       	1	19991117	G	5347		SEAT TRACK      			BOEING	727   	727227      	1384078	NM  										BS 950D	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 950D RBL 45.5.						2	L	7	3 	4F				A3WE    					 
1999121100728	19991211	00728	NM  	1999	12	11	99ZZZX4356       	1	19991021	G	5330		SKIN            			BOEING	727   	727225      	1384077	NM  										BS 333-360	MISREPAIRED     	B			VN4R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	19	887MA					21857				PREVIOUS DOUBLER REPAIR AT FORWARD RIGHT JACK PAD AREA, STR 19R TO STR 24R STA 333 TO STA 360 DO NOT HAVE PROVISIONS FOR	 JACK PAD (HOLES).  FOUND DURING SCHEDULED C-MAINTENANCE CHECK.					2	L	7	3 	4F				A3WE    					 
1999121100729	19991211	00729	NM  	1999	12	11	99ZZZX4357       	1	19991023	G	5315		FLOORBEAM       			BOEING	727   	727221      	1384071	NM  										CABIN	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	370PA					22542				CORROSION ON TOP OF FLOORBEAM RBL 24 INCH TO LBL 45 INCH.  FOUND DURING SCHEDULED CPCP INSPECTION.  AREA EXPOSED TO LIQU	ID SPILLS AND ENVIRONMENTAL CHANGES.					2	L	7	3 	4F				A3WE    					 
1999121100730	19991211	00730	NM  	1999	12	11	99ZZZX4358       	1	19991025	G	5311		FRAME           			BOEING	727   	727221      	1384071	NM  										BS 910	CRACKED         	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	370PA					22542				CRACK IN FRAME AT FS 910 AND STR 14R.  FOUND DURING SCHEDULED CPCP INSPECTION.  AREA SUBJECT TO STRESS AND TWISTING LOAD	S.					2	L	7	3 	4F				A3WE    					 
1999121100731	19991211	00731	NM  	1999	12	11	99ZZZX4359       	1	19991022	G	5315		FLOORBEAM       			BOEING	727   	727221      	1384071	NM  										BS 1050	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	370PA					22542				CORROSION ON TOP OF FLOORBEAM AT SCREW HOLES BS 1050 LBL 55 INCH.  FOUND DURING SCHEDULED CPCP INSPECTION.  AREA EXPOSED	 TO LIQUID SPILLS AND ENVIRONMENTAL CHANGES.					2	L	7	3 	4F				A3WE    					 
1999121100732	19991211	00732	NM  	1999	12	11	99ZZZX4360       	1	19991025	G	5210		SKIN            			BOEING	727   	727221      	1384071	NM  										PASSENGER DOOR	CRACKED         	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	370PA					22542				L1 DOOR LOWER AFT CORNER OUTER SKIN CRACKED.  FOUND DURING SCHEDULED CPCP INSPECTION.  AREA SUBJECT TO STRESS AND BENDIN	G LOADS.					2	L	7	3 	4F				A3WE    					 
1999121100733	19991211	00733	NM  	1999	12	11	99ZZZX4361       	1	19991022	G	5330		SKIN            			BOEING	727   	727221      	1384071	NM  										BS 294	DENTED          	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	370PA					22542				RIGHT FUSELAGE SKIN AT STA 294 JUST ABOVE AND FORWARD OF NOSE JACK PAD, AREA DISHED AND DENTED.  FOUND DURING SCHEDULED 	CPCP INSPECTION.  INTERIOR AREA EXPOSED TO LAVATORY LEAKS.					2	L	7	3 	4F				A3WE    					 
1999121100734	19991211	00734	NM  	1999	12	11	99ZZZX4362       	1	19991022	G	5315		FLOORBEAM       			BOEING	727   	727221      	1384071	NM  										BS 380	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	370PA					22542				FLOORBEAM HAD CORROSION AT BS 380, BL ZERO TO RBL 65 INCH.  FOUND DURING SCHEDULED CPCP INSPECTION.  AREA EXPOSED TO LIQ	UID SPILLS AND ENVIRONMENTAL CHANGES.					2	L	7	3 	4F				A3WE    					 
1999121100735	19991211	00735	NM  	1999	12	11	99ZZZX4363       	1	19991022	G	5315		FLOORBEAM       			BOEING	727   	727221      	1384071	NM  										BS 344	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	370PA					22542				CORROSION ON TOP OF FLOORBEAM BS 344 TO BL ZERO TO RBL 65 INCH.  FOUND DURING SCHEDULED CPCP INSPECTION.  AREA EXPOSED T	O LIQUID SPILLS AND ENVIRONMENTAL CHANGES.					2	L	7	3 	4F				A3WE    					 
1999121100736	19991211	00736	NM  	1999	12	11	99ZZZX4364       	1	19991022	G	5315		FLOORBEAM       			BOEING	727   	727221      	1384071	NM  										BS 400	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	370PA					22542				FLOORBEAM HAD CORROSION RBL 21 INCH TO LBL 21 INCH AT BS 400.  FOUND DURING SCHEDULED CPCP INSPECTION.  AREA EXPOSED TO 	LIQUID SPILLS AND ENVIRONMENTAL CHANGES.					2	L	7	3 	4F				A3WE    					 
1999121100737	19991211	00737	NM  	1999	12	11	99ZZZX4365       	1	19991022	G	5315		FLOORBEAM       			BOEING	727   	727221      	1384071	NM  										BS 420	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	370PA					22542				CABIN FLOORBEAM HAD CORROSION AT SCREW HOLES BL ZERO TO RBL 10 INCH, BS 420.  FOUND DURING SCHEDULED CPCP INSPECTION.  A	REA EXPOSED TO LIQUID SPILLS AND ENVIRONMENTAL CHANGES.					2	L	7	3 	4F				A3WE    					 
1999121100738	19991211	00738	NM  	1999	12	11	99ZZZX4366       	1	19991022	G	5315		FLOORBEAM       			BOEING	727   	727221      	1384071	NM  										BS 1090	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	370PA					22542				CABIN FLOORBEAM HAD CORROSION AND SEVERAL DOUBLE DRILLED HOLES, BS 1090 RBL 10 INCH TO LBL 24 INCH.  FOUND DURING SCHEDU	LED CPCP INSPECTION.  AREA EXPOSED TO LIQUID SPILLS AND ENVIRONMENTAL CHANGES.					2	L	7	3 	4F				A3WE    					 
1999121100739	19991211	00739	NM  	1999	12	11	99ZZZX4367       	1	19991022	G	5315		FLOORBEAM       			BOEING	727   	727221      	1384071	NM  										BS 344	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	370PA					22542				CABIN FLOORBEAM HAD CORROSION ON TOP AROUND HOLES BS 344, BL ZERO, AND LBL 65 INCH.  FOUND DURING SCHEDULED CPCP INSPECT	ION.  AREA EXPOSED TO LIQUID SPILLS AND ENVIRONMENTAL CHANGES.					2	L	7	3 	4F				A3WE    					 
1999121100740	19991211	00740	NM  	1999	12	11	99ZZZX4368       	1	19991023	G	5315		FLOORBEAM       			BOEING	727   	727221      	1384071	NM  										BS 1110	CORRODED        	B			VN4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	370PA					22542				CORROSION ON TOP OF FLOORBEAM BS 1110 RBL 24 INCH TO LBL 24 INCH.  FOUND DURING SCHEDULED CPCP INSPECTION.  AREA EXPOSED	 TO LIQUID SPILLS AND ENVIRONMENTAL CHANGES.					2	L	7	3 	4F				A3WE    					 
1999121100741	19991211	00741	NM  	1999	12	11	99ZZZX4369       	1	19990928	G	5730		SKIN            			BOEING	747   	747124      	1384874	NM  										WING	CORRODED        	B	L		XYJY	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	33	602FF					19734				DURING MAINTENANCE C-CHECK, BEJ FOUND SEVERE CORROSION ON THE UPPER SURFACE OF THE WING CENTER SECTION (WCS) UPPER SKIN 	AT BS 1110, LBBL 11.33, AND BETWEEN UPPER STR S18C AND STR S19C.					2	L	7	4 	4F				A20WE   					 
1999121100742	19991211	00742	NM  	1999	12	11	99ZZZX4370       	1	19990929	G	5711		SPAR            			BOEING	747   	747124      	1384874	NM  										WS 444-520	CORRODED        	B	L		XYJY	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	33	602FF					19734				DURING MAINTENANCE C-CHECK, BEJ FOUND SEVERE CORROSION ON THE REAR SURFACE OF VERTICAL LEG OF THE LEFT WING REAR SPAR UP	PER CHORD AT WS 550, WS 520, AND WS 444.					2	L	7	4 	4F				A20WE   					 
1999121100743	19991211	00743	NM  	1999	12	11	99ZZZX4371       	1	19991016	G	5315		FLOORBEAM       			BOEING	747   	747124      	1384874	NM  										BS 1400	CRACKED         	B	P		XYJY	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	33	602FF					19734				FOUR CRACKS WERE FOUND BY AMECO C-CHECK ON FLOORBEAM WEB AT BS 1400, LBL 99 - LBL 121 IN M/D.  SIZE 3.2 INCHES, 4 INCHES	 1.5 INCHES, AND 1.5 INCHES.					2	L	7	4 	4F				A20WE   					 
1999121100744	19991211	00744	NM  	1999	12	11	99ZZZX4372       	1	19990920	G	5311		FRAME           			BOEING	747   	747124      	1384874	NM  										BS 1480	CRACKED         	B	L		XYJY	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	33	602FF					19734				WHILE PERFORMING MODIFICATION PER THE SB 747-5342390, A CRACK OF 3 INCHES WAS FOUND IN STA 1480 LOWER BULKHEAD, RT FRAME	 WEB AFTER REMOVAL OF THE AFTER WEB SPACE.					2	L	7	4 	4F				A20WE   					 
1999121100745	19991211	00745	NM  	1999	12	11	99ZZZX4373       	1	19991016	G	5315		FLOORBEAM       			BOEING	747   	747124      	1384874	NM  										BS 1420	CRACKED         	B	P		XYJY	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	33	602FF					19734				FOUR CRACKS WERE FOUND BY AMECO C-CHECK ON FLOOR BEAM WEB AT BS 1420, LBL 99 - LBL 121 IN M/D.  SIZE:  5 INCHES, 3 INCHE	S, 1 INCH AND .0.5 INCH.					2	L	7	4 	4F				A20WE   					 
1999121100746	19991211	00746	NM  	1999	12	11	99ZZZX4374       	1	19991016	G	5315		FLOORBEAM       			BOEING	747   	747124      	1384874	NM  										BS 1400	CRACKED         	B	P		XYJY	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	33	602FF					19734				THREE CRACKS WERE FOUND BY AMECO C-CHECK ON FLOORBEAM WEB AT BS 1400, LBL 99 - LBL 121, IN M/D.  SIZE:  12 INCHES, 2.5 I	NCHES, AND 2 INCHES.					2	L	7	4 	4F				A20WE   					 
1999121100747	19991211	00747	NM  	1999	12	11	99ZZZX4375       	1	19991016	G	5315		FLOORBEAM       			BOEING	747   	747124      	1384874	NM  										BS 1400	CRACKED         	B	P		XYJY	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	33	602FF					19734				FOUR CRACKS WERE FOUND BY AMECO C-CHECK ON FLOORBEAM WEB AT BS 1400, RBL 99 - RBL 121.  SIZE:  2 INCHES, 2 INCHES, 1 INC	H AND 1 INCH.					2	L	7	4 	4F				A20WE   					 
1999121100748	19991211	00748	NM  	1999	12	11	99ZZZX4376       	1	19991117	G	5320		INTERCOSTAL     			BOEING	727   	727227      	1384078	NM  										BS 360	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	70755					21366				DURING A C-CHECK, CORROSION WAS NOTED AT STR 16L, STA 360 (INTERCOSTAL).						2	L	7	3 	4F				A3WE    					 
1999121100994	19991211	00994	NM  	1999	12	11	99ZZZX4378       	1	19991101	G	3250	22470000019	DRIVE SPIDER    			ISRAEL	1125  	1125        		NM  										NLG STEERING	FAILED          	D	P			O				OTHER                   				E			VIBRATION/BUFFET          			TX	TAXI/GRND HDL  	1			NE	03	1125K	4864 				035				UPON LANDING ROA, FLT CREW EXPERIENCED SEVERE VIB'S FROM NLG.  ACFT STOPPED IN THE NORMAL MANNER AND ALL TAXI AND STEERI	NG INPUTS NORMAL.  UPON INSP OF NLG, NOTED LT NLG WHEEL DRIVE SPIDER, PN 2247.0000.019, CRACKED COMPLETELY THRU ALONG IT	S LONGITUDINAL AXIS.  PINCH BOLT NUT, AN310-5, WAS BACKED OFF APPROX THE THICKNESS OF THE NUT ITSELF WITH THE COTTER PIN	 SHEARED.  VISUAL INSP OF TORSION DRIVE AXLE ALLOWING KEYED DRIVE AXLE TO ROTATE WITHIN WHEEL DRIVE SPIDER.  WHEN THIS O	CCURRED, THE KEY, PN 2247.09000.020, CONTAINED WITHIN THE WHEEL DRIVE SPIDER, RODE UP AND OUT OF THE TORSION DRIVE AXLE 	KEYWAY SHEARING KEY'S ATTACHMENT SCREW, MS24693C51, EXERTING FORCE ON THE WHEEL DRIVE SPIDER TO SEVER ONE LEG OF ASSY.	2	L	7	2 	4F			RT	A16NM   					 
1999121100996	19991211	00996	EU  	1999	12	11	99ZZZX4379       	1	19991111	G	7932	761672	TRANSMITTER     			AIRBUS	320   	A320232     	3930326	EU  										NR 2 ENGINE	FAILED          	B			OZZR	E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			N			FALSE WARNING             			CL	CLIMB          	1			WP	21	619AW					525				AIRCRAFT TOOK OFF FROM BENTONVILLE AIRPORT (XNA).  UPON CLIMB-OUT, THE NR 2 ENGINE EXPERIENCED AN INDICATED OIL QUANTITY	 LOSS.  THE CREW ELECTED TO SHUT DOWN NR 2 ENGINE AND DECLARED AN IN-FLIGHT EMERGENCY.  AIRCRAFT LANDED WITHOUT INCIDENT	.  THE SYSTEM WAS TROUBLESHOT AND FOUND TO BE A BAD OIL QUANTITY TRANSMITTER.				2	L	7	2 	4F			RT	A28NM   					 
1999121100997	19991211	00997		1999	12	11	99ZZZX4380       	1	19991103	G	3246	2606347	WHEEL           	BENDIX      	26035617    															MLG	BROKEN          	B			YF4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					B3901					FOUND BROKEN SPOKES IN INBOARD WHEEL HALF.  SUBMITTER SUGGESTED POSSIBLY DUE TO HARD LANDING.																			 
1999121100998	19991211	00998		1999	12	11	99ZZZX4381       	4	19991112	G	2300	097001040038	CAPACITOR       	BENDIX      	KR87        	BEECH 	58    	58P         	1152744	CE  										RADIO	FAILED          	B			ACOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	69CL				18226	TJ444				COMPONENT FAILURE CAUSES RECEIVER TO LOSE STORED FREQUENCY AND TIMER INFORMATION.  THIS FACILITY HAS SEEN TWO IDENTICAL 	FAILURES IN PAST YEAR.					1	L	7	2 	3O				A23CE   					 
1999121100999	19991211	00999	CE  	1999	12	11	99ZZZX4382       	1	19991014	G	3233	12810061	ACTUATOR        			CESSNA	210   	T210K       	2073447	CE  										MLG	RUPTURED        	D				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			SW	01	1450C				224	T21059318				AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT OR EXTEND.  AN EMERGENCY LANDING WAS PERFORMED WITH GEAR IN THE INTERMEDIA	TE POSITION.  POST-FLIGHT INSPECTION REVEALED THE ACTUATOR HAD RUPTURED AT THE FORGING SEAM FROM FORE TO AFT.  NEW ACTUA	TOR WAS INSTALLED AND SYSTEM WORKED OK.				1	H	7	1 	3O				3A21    					 
1999121101000	19991211	01000	SO  	1999	12	11	99ZZZX4383       	1	19991027	G	2810	CCA1550	DRAIN VALVE     			PIPER 	PA28  	PA28161     	7102803	SO  										GASCOLATOR	FAILED          	H				C				ABORTED TAKEOFF         				Y	J		ENGINE STOPPAGE           	WARNING INDICATION        		TO	TAKEOFF        	1			GL	03	81023					288016108				ON TAKEOFF, AIRCRAFT ENGINE QUIT, AN EMERGENCY LANDING WAS DECLARED AND LANDED WITHOUT INCIDENT.  THE CFI (FLIGHT INSTRU	CTOR) INSPECTED AIRCRAFT AND FOUND THE GASCOLATOR DRAW VALVE WAS STUCK OPEN AND FUEL WAS DRAINING ON THE TAXIWAY.  INSPE	CTION OF VALVE SHOWED SIGNS OF VARNISHING AND WAS STIFF TO OPERATE.				1	L	7	1 	3O				2A13    					 
1999121101001	19991211	01001	SO  	1999	12	11	99ZZZX4384       	2	19991109	G	8520	643626105	PIN             		649898      						CONT  	O520  	TSIO520NB   	17040	SO  					CRANKSHAFAT	MISSING         	B			VA1R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	19					I139915N					PURCHASED NEW CRANKSHAFT P/N 649898 FROM TELEDYNE CONTINENTAL AND RECEIVED WITH COUNTERWEIGHT PIN PN 643626-105 MISSING 	ON REAR COUNTERWEIGHT ASSY PN 639195.  SUBMITTER RECOMMENDED THOROUGH INSPECTION ON ANY NEW PART OR ASSY.										3	O			E8CE				 
1999121101002	19991211	01002	SO  	1999	12	11	99ZZZX4385       	2	19991109	G	8520	629757	TUBE            		649898      						CONT  	O520  	TSIO520NB   	17040	SO  					CRANKSHAFT	MISSING         	B			VA1R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	19					F179903N					PURCHASED NEW CRANKSHAFT PN 649898 FROM TELEDYNE CONTINENTAL AND RECEIVED WITH ALL OIL SUPPLY TUBES MISSING PN 629757 TU	BE.  ALSO, FOUND LOOSE TUBE ON ANOTHER CRANKSHAFT.  SUBMITTER SUGGESTED A THOROUGH INSPECTION OF ANY NEW PART OR ASSY.										3	O			E8CE				 
1999121101003	19991211	01003	SO  	1999	12	11	99ZZZX4386       	2	19991109	G	8530	654650A4	CYLINDER        			CESSNA	182   	182P        	2075816	CE  	CONT  	O470  	O470U       	17026	SO  					NR 1	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	23	952CC	1031 				18263638	470757			DURING A ROUTINE 100-HOUR INSPECTION, EXCESSIVE LEAKAGE WAS FOUND GOING PAST THE PISTON RINGS ON THE NR 1 CYLINDER.  THE	 REMOVED CYLINDER IS FOUND TO BE WORN OUT AND HAD A NEGATIVE CHOICE.					1	H	7	1 	3O	3	O	NT	TA13    	E273				 
1999121101004	19991211	01004	EU  	1999	12	11	99ZZZX4387       	1	19991107	G	3213	LP880420041	AXLE            		LP8804200360	WSK   	150A  	PZL150A     	05625QK	EU  										NLG	FAILED          	D				O				OTHER                   				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			SW	09	150AD	376  				03930057				AIRCRAFT LANDED AND DEVELOPED NOSE WHEEL SHIMMY AND NOSE GEAR AXLE BROKE.  THE AXLE WAS PREVIOUSLY REPLACED 10-18-95.  T	HE AXLE IS HOLLOW AT THE POINT OF FAILURE AND IT APPEARS TO HAVE HAD AN OLD CRACK THAT COULD HAVE BEEN DETECTED DURING A	 REPETITIVE INSPECTION.				1	L	7	1 	3O			NT	A69EU   					 
1999121101005	19991211	01005	SO  	1999	12	11	99ZZZX4388       	2	19991102	G	8530	654650	CYLINDER        			CESSNA	182   	182Q        	2072732	CE  	CONT  	O470  	O470U       	17026	SO  					NR 6	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	23	954CC	989  				18265290	813337R			DURING A ROUTINE 100-HOUR INSPECTION, EXCESSIVE LEAKAGE IS FOUND GOING PAST THE PISTON RINGS ON THE NR 6 CYLINDER.  THE 	TOP TWO PISTON RING GAPS ARE FOUND ALIGNED AND THERE IS A NEGATIVE CHOKE IN THE CYLINDER.					1	H	7	1 	3O	3	O	NT	3A13    	E273				 
1999121101006	19991211	01006	CE  	1999	12	11	99ZZZX4389       	1	19991027	G	8120		BEARING         		4078109001  	CESSNA	340   	340A        	2076405	CE  										TURBOCHARGER	FAILED          	B			GMNR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	11	340MM		746  		TH08A67	340A0635				INNER BEARING FAILURE OF LEFT TURBO CAUSING TURBO CASE TO SPLIT AROUND INNER CIRCUMFERENCE.						1	L	7	2 	3O				3A25    					 
1999121101007	19991211	01007	SO  	1999	12	11	99ZZZX4390       	1	19991115	G	7922	53E22144A	VALVE           			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					ENGINE OIL	FAILED          	H				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			SW	99	44AC	433  			97792	318052147	L283568A			RIGHT ENGINE REPORTED AS HAVING OIL TEMPERATURES NEAR RED LINE IN CRUISE.  REPLACED BYPASS VALVE AND TEST FLIGHT SHOWED 	NORMAL TEMPS.  FOUND REMOVED VALVE WAS STUCK IN THE CLOSED POSITION.					1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999121101008	19991211	01008	CE  	1999	12	11	99ZZZX4391       	1	19991030	G	3220	3222	SPRING          	SCOTT       		CESSNA	305   	305A        	2074002	CE  										TAIL WHEEL	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	5198G	400  				21831				SPRING, PN 3222, BROKE AT BEND CAUSING TAIL WHEEL STEERING TO RIGHT TO BE INAFFECTIVE.						1	H	7	1 	3O				5A5     					 
1999121101009	19991211	01009	CE  	1999	12	11	99ZZZX4392       	1	19991025	G	2820		LINE            			BEECH 	MU300 	400A        	1155402	CE  										FUEL SYSTEM	DISCONNECTED    	B			JAVR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NE	01	3337J	1400 				RK159				B-NUT FOR ENGINE FUEL FEED LINE IN LEFT COLLECTOR TANK WAS TOTALLY DISCONNECTED.  NUT WAS FOUND AT REAR END OF LINE DURI	NG INSPECTION.  NUT TIGHTENED AND OPS CHECKED OK.					2	H	7	2 	4F			RT	A16SW   					 
1999121101010	19991211	01010	CE  	1999	12	11	99ZZZX4393       	1	19991008	G	3240	1338931	STATOR          			CESSNA	500   	550         	2076604	CE  										BRAKE	FAILED          	B				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			NE	03	202CE		445  		1085	5500097				RIGHT BRAKE LOCKED UP DURING TAXI - LOGAN INT'L.  AIRCRAFT STOPPED FOR CLEARANCE.  PILOT ATTEMPTED TO TAXI, AIRCRAFT WOU	LD NOT MOVE.  REQUIRED A DOLLY AND TOW TO MOVE.  INSPECTION OF THE ASSY FOUND THE INBOARD STATOR CRACKED ACROSS THE WIDT	H AND HAD OPENED UP.  THE CRACKED EDGE CAUGHT THE WHEEL DRIVE KEY PREVENTING ROTATION.  LANDINGS:  511.				1	L	7	2 	4F				A22CE   					 
1999121101014	19991211	01014	SO  	1999	12	11	99ZZZX4396       	1	19990823	G	3250	JL15014	ACTUATOR        		JL19571     	LKHEED	1329  	132925      	5263125	SO  										NLG STEERING	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	400MP				18UD14	5228				BECAUSE OF PREVIOUS FAILURES OF THIS UNIT, CUSTOMER REQUESTED A TEAR-DOWN AND INSPECTION OF THIS UNIT.  FOUND EXCESSIVE 	CORROSION AND THE END CAP WAS CRACKED.  SUBMITTER STATED THERE HAVE BEEN 5 PREVIOUS FAILURES OF THIS PART WITH EXTENSIVE	 DAMAGE DONE TO S/N 5210.				2	L	7	4 	4F				2A1SO   					 
1999121101015	19991211	01015	NE  	1999	12	11	99ZZZX4397       	2	19991103	G	7321	32447681013	FCU             			BEECH 	200   	B200        	1152922	CE  	PWA   	PT6   	PT6A42      	52043	NE  					FUEL SYSTEM	LEAKING         	B			T4OR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NE	03	500LP				A69057	BB1141	PLE93625			FOUND FUEL LEAKING OUT OF IDLE CUT-OFF SHAFT OF FUEL CONTROL UNIT.						1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999121101016	19991211	01016	EA  	1999	12	11	99ZZZX4398       	2	19991013	G	7321	324475519184	FCU             			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  					FUEL SYSTEM	LEAKING         	B			T4OR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NE	03	703KH	4746 	1744 		A45242	BB703	PCE81653			FOUND FUEL LEAKING OUT OF IDLE CUT-OFF SHAFT OF FCU.						1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999121101017	19991211	01017		1999	12	11	99ZZZX4399       	4	19991101	G	2216	MS24187D1	RELAY           			ISRAEL	1125  	ASTRASPX    	4500205	EU  										AFCS	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	11	500M	1105 				091				PART FAILED, CAUSED AUTOPILOT LOSS OF NOSE UP TRIM.  NORMAL TRIM WAS NOT EFFECTED.						2	L	7	2 	4F			RT	A16NM   					 
1999121101018	19991211	01018	EA  	1999	12	11	99ZZZX4400       	1	19990923	G	5320	600908311	BRACKET         		600908209   	CNDAIR	CL600 	CL6001A11   	1900302	EA  										FUSELAGE	CRACKED         	B	S		SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	491DB	8695 				1049				INSPECTION OF THE ADG BAY REVEALED THE ATTACH BRACKET, IN TWO PLACES, TO BE CRACKED.  REMOVED AND REPLACED WITH A NEW BR	ACKET.  LANDINGS:  4,672.					2	L	7	2 	4F			RT	A21EA   					 
1999121101019	19991211	01019	SW  	1999	12	11	99ZZZX4401       	1	19990827	G	6230	406040036107	BEARAING        			BELL  	407   	407         		SW  										M/R MAST	MAKING METAL    	B			CYXR	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			CE	01	407LG	462  				53143				PILOTS REPORTED MAIN ROTOR TRANS. CHIP LIGHT CAME ON.  CHIP PLUGS INSPECTED AND FOUND METAL PARTICLES ON UPPER CHIP DETE	CTOR.  HELICOPTER FLOWN AGAIN AND AFTER A FEW HOURS, THE LIGHT CAME ON AGAIN.  CHIP PLUGS INSPECTED AND FOUND METAL ON U	PPER PLUG.  MAST ASSY REPLACED.  CAUSE WAS FAULTY BEARING.				1	G	7	1 	3U			O	H2SW    					 
1999121101020	19991211	01020	GL  	1999	12	11	99ZZZX4402       	2	19990809	G	7230		BEARING         		CAC444186   	BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					NR 2	MAKING METAL    	B			CYXR	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			CE	01	407LG	456  				53143	CAE847161			ENGINE CHIP LIGHT CAME ON.  CHIP PLUGS INSPECTED AND FOUND EXCESSIVE METAL PARTICLES ON BOTH PLUGS.  FERRY PERMIT WAS IS	SUED BY FSDO FOR FLIGHT FROM MANCHESTER, IA TO CEDAR RAPIDS, IA.  ENGINE WAS REMOVED AND SENT IN FOR REPAIR.  CAUSE UNKN	OWN.				1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999121101021	19991211	01021	SW  	1999	12	11	99ZZZX4403       	1	19991115	G	2840	407375016101	SIGNAL CONDITION			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					FUEL SYSTEM	INTERMITTENT    	B			CYXR	O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			CE	01	407LG	531  				53143	CAE847161			PILOTS REPORTED AN INTERMITTENT PROBLEM WITH THE RIGHT FUEL TRANSFER CAUTION LIGHT COMING ON AND THE FUEL QUANTITY GAUGE	 GOING BLANK.  SUBMITTER STATED PROBLEM WAS IN PN 407-375-016-101 SIGNAL CONDITIONER.  DEFECT CAUSE UNKNOWN.					1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999121101022	19991211	01022	GL  	1999	12	11	99ZZZX4404       	2	19991021	G	7240	6870992	COMBUST CASE    			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	CRACKED         	B			CYXR	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			CE	01	206AW	10418	387  			2861	CAE830502			PILOTS REPORTED LOW POWER AND HIGH TOT.  TROUBLESHOOTING FOUND A LARGE CRACK (APPROX 3 INCHES LONG) IN THE ARM PIT AREA 	WHERE IT IS REINFORCED WITH A BRAZED ON SCREEN, RIGHT HAND SIDE. PART REMOVED AND SENT IN FOR POSSIBLE REPAIR.  SUBMITTE	R STATED CAUSE IS POSSIBLEMETAL FATIGUE.				1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999121101023	19991211	01023		1999	12	11	99ZZZX4405       	4	19991111	G	2200	8241631	POTENTIOMETER   	HAMSTD      		SKRSKY	S76   	S76A        	8143006	NE  										AFCS	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	72649	9546 	292  		8312644	760292				SUBMITTER STATED POTS WEAR OUT LONG BEFORE THE OVERHAUL OF 3,000.00 HOURS.  FEEDBACK POT PREMATURE FAILURE, SHOULD LAST 	UNTIL OVERHAUL TIME OF 3,000 HOURS.  CAUSED ACTUATOR TO KICK IN-FLIGHT.  COMPONENT P/N 7690001802106.					1	G	7	2 	3U				H1NE    					 
1999121101025	19991211	01025	EA  	1999	12	11	99ZZZX4407       	2	19991129	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B			BF8R	O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			WP	07	477ER	1184 	901  			17280622	L2803951A			THE PILOT REPORTED A MOMENTARY POWER LOSS.  THERE WERE TWO SUCCESSIVE PERIODS OF POWER LOSS EACH TIME THE ENGINE RESTART	ED.  A COMPLETE INSPECTION OF THE ENGINE AND ENGINE SYSTEMS FOUND NO ABNORMALITIES.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999121101026	19991211	01026	SO  	1999	12	11	99ZZZX4408       	2	19991122	G	8520	646743	PISTON          		652955A1    	MOONEY	M20   	M20K        	5870220	SW  	CONT  	O360  	TSIO360LB   	17025	SO  					ENGINE	FAILED          	B				O				OTHER                   				F			FLT CONT AFFECTED         			NR	NOT REPORTED   	1			NM	02	4822H	1800 				250229	247081R			AIRCRAFT LOST POWER IN CLIMB AND MADE AN OFF-FIELD LANDING.  FOUND CYLINDER NR 1 BROKEN APPROXIMATELY 2 INCHES UP FROM B	ASE AND SEPARATED FROM CYLINDER BASE.  NR 1 PISTON FOUND BROKEN THROUGH PISTON PIN BORE.  UPPER HALF OF PISTON REMAINED 	IN CYLINDER WHILE LOWER HALF OF PISTON WAS GROUND UP IN ENGINE.  PISTON PIN REMAINED INTACT IN ROD.  SUBMITTER SUSPECTED	 PISTON FAILED AND SUBSEQUENTLY CAUSED CYLINDER BARREL TO FAIL AS IT WAS KNOCKED AROUND BY THE ROD/PIN.			1	L	7	1 	3O	3	O		2A3     	E9CE				 
1999012900714	19990129	00714	SW  	1999	1	29	99ZZZX441        	1	19990101	G	5510	407023800119	ANGLE           		407023800101	BELL  	407   	407         		SW  										HORIZ STABILIZER	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	497AL	1460 				53172				DURING DAILY INSPECTION FOUND CRACK IN BEND RADIUS.						1	G	7	1 	3U			O	H2SW    					 
1999121101029	19991211	01029	SO  	1999	12	11	99ZZZX4411       	1	19991027	G	2821		SEAL            			PIPER 	PA22  	PA22108     	7102204	SO  										GASCOLATOR	FAILED          	G		A		K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	09	4905Z					228490				THE SWOLLEN RUBBER SEAL CAUSED A FUEL LEAK AT THE GASCOLATOR RESULTING IN AN IN-FLIGHT FIRE.  THE AIRPLANE WAS BEING OPE	RATED IAW AN STC FOR AUTO FUEL.  THE SWOLLEN SEAL WAS POSSIBLY CAUSED BY THE AUTO FUEL'S AFFECT TO RUBBER BASED PRODUCTS	.  OWNER ADMITTED NOT TESTING FUEL FOR ALCOHOL IAW THE STC INSTRUCTIONS.  INCIDENT NR IEA092000004.				1	H	7	1 	3O				1A6     					 
1999121101030	19991211	01030	CE  	1999	12	11	99ZZZX4412       	1	19991116	G	8011		GEAR            	CONT        	EQ66R2      	CESSNA	421   	421B        	2076014	CE  										STARTER	DAMAGED         	B			EKIR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	421KP	348  				421B0142				STARTER ADAPTER SHAFT GEAR AT BEARING END IN ENGINE AND NEEDLE BEARING IN ENGINE DAMAGED.  NO EVIDENCE OF LACK OF LUBRIC	ATION.  NEEDLE BEARING DESTROYED AND CASE DAMAGED.  SUBMITTER STATED THIS IS THE THIRD FAILURE OF THE EQ6642 ADAPTER IN 	THE LAST 2 YEARS.				1	L	7	2 	3O				A7CE    					 
1999121101031	19991211	01031	EU  	1999	12	11	99ZZZX4413       	1	19991209	G	5754		BRACKET         			AMD   	FALC10	FALCON10    	2730101	EU  										LE FLAP	DAMAGED         	B			UO2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	47RK					162				SLAT (OUTBOARD) NR 3 RAIL MOUNT BRACKET ATTACHED TO SLAT RUBBING LEADING EDGE CAUSING DAMAGE TO THE BRACKET.  THIS HAS A	LSO BEEN NOTICED ON FALCON10, SN 131.					2	L	7	2 	4F				A33EU   					 
1999121101032	19991211	01032	SO  	1999	12	11	99ZZZX4414       	2	19991029	G	8530		GUIDE           			CESSNA	421   	421B        	2076014	CE  	CONT  	O520  	GTSIO520H   	17032	SO  					EXHAUST VALVE	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	420GC	829  				421B0494	231370R			NR 5 EXHAUST VALVE GUIDE FAILED AND ALLOWED CRANKCASE PRESSURE TO BLOW OIL OUT THE BREATHER.  VALVE GUIDE PARTICLES DAMA	GED TURBO.  CHANGED CYLINDER AND TURBO.  ENGINE CONVERTED TO 1,600 TBO BY STC 09059SC AT WESTERN SKYWAYS.					1	L	7	2 	3O	3	O		A7CE    	E7CE				 
1999121101033	19991211	01033	CE  	1999	12	11	99ZZZX4415       	1	19991026	G	7810		SLIP JOINT      			CESSNA	421   	421B        	2076014	CE  										EXHAUST	DEFORMED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	420GC					421B0464				MAIN EXHAUST SLIP JOINT WAS BULGED AND DEFORMED INTERNALLY, NOT REAL VISIBLE FROM OUTSIDE.  SLIP JOINT WOULD NOT MOVE IN	 EITHER DIRECTION.  REPLACED WITH K9910314.1.  THE BAD SLIP JOINT WAS A SEALLESS TYPE PART NR 8, MFG UNKNOWN.					1	L	7	2 	3O				A7CE    					 
1999121101035	19991211	01035	GL  	1999	12	11	99ZZZX4417       	3	19990806	G	6114		HUB             			BEECH 	33    	F33A        	1151425	CE  						HARTZL	HCC3Y	PHCC3YF1    	GL  	PROPELLER	CRACKED         	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05	8240T	8240 	1982 			CE1542		EE1687		PROPELLER HUB CRACKED ABOUT 1.5 INCHES REAR SIDE COMING FROM STUD MOUNT HOLE TO CENTER WHERE THE BLADE SHANK IS ATTACHED	.  PART SENT TO HARTZELL.					1	L	7	1 	3O				3A15    		5	C	P25EA	 
2000012100009	20000121	00009	CE  	2000	1	21	99ZZZX4418       	1	19991116	G	2420		TERMINAL END    			BEECH 	100   	B100        	1152919	CE  										GENERATOR WIRE	FAILED          	D				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SO	05	86TR					BE22				PILOT REPORTED THAT LEFT GENERATOR FAILED IN-FLIGHT.  RE-SETTING LEFT GENERATOR CAUSED RIGHT GENERATOR TO FAIL.  PILOT C	OULD USE EITHER GENERATOR ALONE, BUT NOT BOTH AT THE SAME TIME.  MAINTENANCE FOUND A BAD TERMINAL END CONNECTING WIRE NR	 P7A12 TO TERMINAL D OF RIGHT GENERATOR.  REPLACING BAD TERMINAL END REPAIRED THE PROBLEM.				1	L	7	2 	4T				A14CE   					 
1999121101036	19991211	01036	EA  	1999	12	11	99ZZZX4419       	2	19991209	G	8550	SL18109AS	GEAR            			PIPER 	PA18  	PA18150     	7101828	SO  	LYC   	O320  	O320A2B     	41508	EA  					OIL PUMP	CRACKED         	D	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	83622	1627 				187709104	L4705227A			OIL PUMP CRACKED.  KIT INSTALLED (LOG BOOK ENTRY) 12-19-86.						1	H	7	1 	3O	3	O		1A2     	E274				 
1999121101037	19991211	01037	CE  	1999	12	11	99ZZZX4420       	1	19991011	G	2434	333800091	ALTERNATOR      			BEECH 	P35   	P35         	1151530	CE  										ENGINE	FAILED          	B			FTKR	O				OTHER                   				J			WARNING INDICATION        			LD	LANDING        	1			GL	19	8585M					D7207				UPON LANDING, THE MAIN AND NOSE LANDING GEAR COLLAPSED.  PILOT REPORTED ELECTRICAL SYSTEM PROBLEMS.  CHECK OUT OF ELECTR	ICAL SYSTEM REVEALED THE ALTERNATOR WAS NOT WORKING.					1	L	7	1 	3O			RT	3A15    					 
1999121101038	19991211	01038	EU  	1999	12	11	99ZZZX4421       	1	19991209	G	2130		LINE            			AMD   	FALC50	FALCON900   	2700160	EU  										CABIN PRESSURE	CHAFED          	B	P		UO2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	922JW					36				PRESSURIZATION LINE IN HARD CONTACT WITH GALLEY UPPER ATTACH BRACKET AT FRAME 6.  ORIGINAL INTERIOR INSTALLATION FAILED 	TO RELOCATE LINE TO PREVENT INTERFERENCE.					2	L	7	3 	4F			RT	A46EU   					 
1999121101039	19991211	01039		1999	12	11	99ZZZX4422       	4	19991104	G	6122	9696001117	LINE            			BEECH 	58    	58          	1152740	CE  										LT ENGINE	CHAFED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	13	9239Q					TH139				FOUND HARD LINE FROM PROPELLER GOVERNOR TO PROPELLER ACCUMULATOR.  LINE ATTACHED TO FIREWALL FITTING WAS CHAFING ON AIR 	DUCT TO THROTTLE BODY.  RE-ROUTED LINE TO CLEAR HOSE.					1	L	7	2 	3O				3A16    					 
1999121101041	19991211	01041	GL  	1999	12	11	99ZZZX4424       	1	19991110	G	7810	19148410R	COLLECTOR       			BLANCA	17    	1730A       	1220433	GL  										EXHAUST	SEPARATED       	B		A	ZU4R	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			SO	09	93568					7630633				OPERATOR REPORTED STRONG EXHAUST SMELL IN COCKPIT.  REMOVED COWL AND FOUND THE RIGHT EXHAUST BROKEN AT THE COLLECTOR OUT	LET.  ATTEMPTED A WELD REPAIR, BUT FOUND THE BASE METAL DETERIORATED BEYOND REPAIR.  INSTALLED AN EXCHANGE UNIT.  TOTAL 	TIME ON PART UNKNOWN.  THIS PART APPEARED TO HAVE BEEN PARTIALLY CRACKED BEFORE BREAKING, BUT BECAUSE OF DESIGN, WAS UND	ETECTABLE.			1	L	7	1 	3O				A18CE   					 
1999121101042	19991211	01042	CE  	1999	12	11	99ZZZX4425       	1	19991011	G	2121	66082672	MOTOR           			LEAR  	35    	35A         	5170602	CE  										BLOWER	FAILED          	H		A		A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			GL	05	950SP				2319	35A450				PILOTS NOTICED COCKPIT BLOWER SEEMED TO BE SHUT OFF.  KNOB INDICATED IT WAS ON HIGH.  SHUT OFF BLOWER AND IMMEDIATELY TU	RNED IT BACK ON.  A FEW SECONDS LATER, A PUFF OF SMOKE CAME FROM COCKPIT .  IMMEDIATELY TURNED OFF BLOWER AND DIVERTED T	O DENVER.  TECH VERIFIED BLOWER MOTOR WAS THE CAUSE.  HE CUT OUT AND SCRAPPED BLOWER MOTOR WIRES, DEFERRED BLOWER MOTOR 	PER MEL.  AIRCRAFT WAS FUELED AND BACK IN THE AIR IN APPROXIMATELY 15 HOURS.			2	L	7	2 	4F				A10CE   					 
1999121101045	19991211	01045	SW  	1999	12	11	99ZZZX4428       	1	19991101	G	6510	206061432121	HOUSING         		407040303105	BELL  	407   	407         		SW  										T/R BLOWER	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	527AL	1870 			513	53211				DURING DAILY INSPECTION, FOUND CRACKED BLOWER HOUSING AND WORN SPLINES.						1	G	7	1 	3U			O	H2SW    					 
1999121101046	19991211	01046	CE  	1999	12	11	99ZZZX4429       	1	19991117	G	3246	21A06000020	PIVOT SHAFT     			CESSNA	172   	172N        	2072434	CE  										NLG WHEEL	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	15	5342D	34   				17272531				RIGHT NOSE GEAR PIVOT SHAFT ON WIPAIRE 2100 FLOATS.  WORN OUT IN 34 HOURS AND SHIMMIES BADLY.  INSTALLED NEW SHAFT AND T	IRE.					1	H	7	1 	3O			NT	3A12    					 
1999012900718	19990129	00718	NM  	1999	1	29	99ZZZX443        	1	19990108	G	5311		FRAME           			BOEING	727   	727259      	138408J	NM  										BS 970	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON FRAME, SHEAR TIE, AND SPLICE ANGLE STA 970, STR 28L - STR 28R.						2	L	7	3 	4F				A3WE    					 
1999121101048	19991211	01048	SO  	1999	12	11	99ZZZX4431       	1	19991122	G	2530	CRONSTONTC71	FOOD WARMER     			GULSTM	G1159 	GIV         	3980115	SO  										GALLEY	SHORT           	H				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			SW	99	53M	5319 			1089	1089				ON CLIMB-OUT, SMOKE NOTICED COMING FROM THE FOOD WARMER.  THE PROBLEM WAS DETERMINED TO BE FLUID LEAKING FROM ONE OF THE	 HOT PLATES ON TO THE OVEN RAILS CAUSING THE BOTTOM RAIL TO SHORT TO GROUND.  SUBMITTER STATED IF THE BOTTOM OF THE OVEN	 WAS MADE OF A NON-CONDUCTIVE MATERIAL, THERE WOULD BE NO PATH TO GROUND.				2	L	7	2 	4F			RT	A12EA   					 
1999121101049	19991211	01049	SO  	1999	12	11	99ZZZX4432       	2	19991107	G	8520	A50303A2	CRANKSHAFT      			CESSNA	172   	172A        	2072404	CE  	CONT  	O300  	O300A       	17022	SO  					ENGINE	FAILED          	H				A				UNSCHED LANDING         				O			OTHER                     			NR	NOT REPORTED   	1			SW	07	7638T					47238	10919DJA			CRANKSHAFT BROKEN AT NR 6 CONNECTING ROD PIN.  OFF-AIRPORT LANDING WITH NO DAMAGE OR INJURY.						1	H	7	1 	3O	3	O		3A12    	E253				 
1999121101050	19991211	01050	SO  	1999	12	11	99ZZZX4433       	2	19991114	G	7414	10382584	POINTS          	BENDIX      	S6RN1225    	BEECH 	33    	E33         	1151422	CE  	CONT  	O550  	IO550B      		SO  					MAGNETO	LOOSE           	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01	7135N					CD1139	281935R			FOUND STATIONARY CONTACT ON THE MAGNETO, BREAKER POINTS LOOSE.  THE CONTACT WAS ABLE TO MOVE APPROXIMATELY .0625 INCH. T	HERE WERE 142.7 HOURS ON THE LT MAGNETO POINTS AT THE TIME OF DISCOVERY AND 157.1 ON THE RT MAGNETO POINTS.  (THE CONDIT	ION ON THE RT MAGNETO WAS FOUND APPROXIMATELY 2 WEEKS AFTER THE LEFT).				1	L	7	1 	3O	3	O		3A15    	E3SO				 
1999121101052	19991211	01052	CE  	1999	12	11	99ZZZX4435       	1	19991116	G	5510	169660001603	SPAR            			BEECH 	23    	C23         	1151242	CE  										STABILATOR	CRACKED         	B			YEBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	05	5167M					M2043				SPAR HAS CRACKS RADIATING OUT FROM CUT-OUTS FOR HINGE ATTACH POINT ON RIGHT SIDE.  TIME IN SERVICE UNKNOWN.						1	L	7	1 	3O				A1CE    					 
1999121101053	19991211	01053	SW  	1999	12	11	99ZZZX4436       	1	19991022	G	6210	206101200133	BLADE           			BELL  	206   	206B        	1181511	SW  										MAIN ROTOR	DAMAGED         	B		A	DFUR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	09	67662	2769 			A1946	5186				MAIN ROTOR BLADE FACTORY INSTALLED WEIGHT DISLODGED DURING OPERATION STRIKING MAIN ROTOR BLADE TIP CAP.  TIP CAP TRAILIN	G EDGE WAS BENT OUTBOARD APPROXIMATELY 30 DEGREES AND APPROXIMATELY ONE INCH OF WEIGHT PROTRUDED THROUGH OUTBOARD END OF	 SPAR.  UPPER AND LOWER MAIN ROTOR BLADE SKIN BALLOONED OUT FROM FORCE OF WEIGHT IMPACT.  MAIN ROTOR BLADE WAS RETURNED 	TO BELL HELICOPTER FOR INVESTIGATION.			1	G	7	1 	3U				H2SW    					 
1999121101054	19991211	01054	EU  	1999	12	11	99ZZZX4437       	1	19991021	G	2422	ASH6641PF	INVERTER        			BRAERO	DH125 	BAE125800A  	1500285	EU  										NR 1	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	17	500J	3122 			EK919	258216				INVERTER FAILED AFTER FLYING LOW LEVEL IN A RAIN STORM.  AFTER DRYING OUT, INVERTER STARTED WORKING.  PART REMOVED FROM 	SERVICE.  NOTE:  SUBMITTER STATED RAYTHEON HAS NOT YET ISSUED A BULLETIN WHICH WOULD RECTIFY THIS PROBLEM.					2	L	7	2 	4F			RT	A3EU    					 
1999121101055	19991211	01055	EU  	1999	12	11	99ZZZX4438       	1	19990929	G	2422	ASH6641PF	INVERTER        			BRAERO	DH125 	BAE125800A  	1500285	EU  										NR 2	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	17	500J	3108 			EK920	258216				INVERTER FAILED AFTER AIRCRAFT SPENT OVERNIGHT OUTSIDE IN RAIN STORM.  AFTER DRYING OUT, INVERTER STARTED WORKING.  PART	 REMOVED FROM SERVICE.					2	L	7	2 	4F			RT	A3EU    					 
1999121101056	19991211	01056		1999	12	11	99ZZZX4439       	4	19990713	G	2200	8241631	POTENTIOMETER   	HAMSTD      		SKRSKY	S76   	S76         	8143010	NE  										AFCS	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5447C	8052 	1204 		8107102	760180				FEEDBACK POT PREMATURE FAILURE.  SUBMITTER STATED SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS.  CAUSED ACTUATOR TO KI	CK IN-FLIGHT.  COMPONENT PN 7690002802106.					1	G	7	2 	3U				H1NE    					 
1999012900719	19990129	00719	NM  	1999	1	29	99ZZZX444        	1	19990108	G	5312		BULKHEAD        			BOEING	727   	727227      	1384078	NM  										BS 304	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	76753					21249				DURING A C-CHECK, CORROSION WAS NOTED ON THE BULKHEAD AT STA 304.  (ONE AT FLOOR LEVEL - OTHER NEAR CENTER.)						2	L	7	3 	4F				A3WE    					 
1999121101057	19991211	01057	EA  	1999	12	11	99ZZZX4440       	2	19991209	G	8520		CONNECTING ROD  			CESSNA	172   	172RG       	2072438	CE  	LYC   	O360  	O360F1A6    	41514	EA  					ENGINE	FAILED          	D				O				OTHER                   				F			FLT CONT AFFECTED         			NR	NOT REPORTED   	1			SO	13	5244V	6287 	2343 		L1052636A	172RG0481	L1052636A			AIRCRAFT ENGINE SEIZED IN-FLIGHT AND CRACKED LEFT ENGINE CASE HALF.  WEATHER CONDITIONS DID NOT EFFECT OUTCOME.  ENGINE 	HAS BEEN 50-HOUR, 100-HOUR, AND ANNUALIZED ITS ENTIRE LIFE.  OIL ANALYIS WAS TAKEN LAST.  NO ABNORMAL SIGNS OF WEAR.  PO	SSIBLE CAUSE SHOWED SEIZURE OF NR 4 CONNECT ROD ON CRANKSHAFT.				1	H	7	1 	3O	3	O		3A17    	E286				 
1999121101058	19991211	01058	CE  	1999	12	11	99ZZZX4441       	1	19990810	G	2720	24670011	RUDDER PEDAL    			CESSNA	172   	172RG       	2072438	CE  										COCKPIT	BROKEN          	B			WIWR	O				OTHER                   				F			FLT CONT AFFECTED         			NR	NOT REPORTED   	1			WP	07	6623Z	6263 				172RG0240				THE LT FOOT AND BRAKE PEDAL WELD ASSY FAILED DURING ROUTINE LOCAL FLIGHT.  INSP OF RUDDER BAR REVEALED A BROKEN PILOT SI	DE LT RUDDER PEDAL ATTACH TUBE AT WELD LINE.  THE TUBE BROKE COMPLETELY AWAY FROM RUDDER BAR AT THE WELD.  POSSIBLE CAUS	E MAY BE METAL FATIGUE ON RUDDER BAR DUE TO STRESS APPLIED ON WELD THROUGH NORMAL RUDDER PEDAL OPERATION OVER A LONG PER	IOD OF TIME.  SUBMITTER SUGGESTED INSPECTION CRITERIA BE OUTLINED TO PREVENT FAILURE OF PART.			1	H	7	1 	3O				3A17    					 
1999121101059	19991211	01059	CE  	1999	12	11	99ZZZX4442       	1	19991105	G	5530	04310093	FITTING         			CESSNA	150   	152         	2071835	CE  										VETICAL STAB	CRACKED         	B		A	SVIR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03	6249H	11738				15284146				LEFT HAND AFT VERTICAL STABILZIER ATTACH FITTING FOUND CRACKED.						1	H	7	1 	3O			NT	3A19    					 
1999121101060	19991211	01060	CE  	1999	12	11	99ZZZX4443       	1	19991008	G	7603	63255535	THROTTLE ARM    			BEECH 	58    	58          	1152740	CE  										RT ENGINE	WORN            	B			BSYR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	07	696BD					TH352				CLT - RIGHT ENGINE WOULD NOT RETARD THROTTLE.  FOUND ARM WORN WHERE CABLE ATTACHES TO FUEL SERVO.  REMOVED AND REPLACED 	THROTTLE ARM.  OPS GOOD.					1	L	7	2 	3O				3A16    					 
1999121800001	19991218	00001	EU  	1999	12	18	99ZZZX4446       	1	19991111	G	2150	TBL215	BLOWER          			BRAERO	DH125 	BAE125800A  	1500285	EU  										ACM	FAILED          	D				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			CR	CRUISE         	1			EA	25	682B	4961 				258144				WHILE AIRCRAFT WAS IN CRUISE FLIGHT, CREW SMELLED ELECTRICAL BURNING ODOR.						2	L	7	2 	4F			RT	A3EU    					 
1999121800002	19991218	00002	EU  	1999	12	18	99ZZZX4447       	1	19991020	G	2913	AP09V0303	PUMP            	ABEX        		AMD   	FALC10	FALCON10    	2730101	EU  										LT ENGINE	FAILED          	B	L		EA2R	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SW	17	711FJ		158  		AH49557A	149				IN 12-98 THIS S/N PUMP WAS INSTALLED ON ACFT AS REPLACEMENT.  IN 9-99, THIS PUMP FAILED DURING RETURN TRIP.  AFTER REMOV	AL, PUMP CHECKED AND FOUND SHAFT ROTATING BUT NOT CONNECTED TO INTERNAL PUMP, SUSPECTED A SHEARED INTERNAL SHAFT.  PUMP 	RETURNED TO VENDOR.  VENDOR INDICATED INTERNAL SPLINE SHAFT HAD BEEN WORN OUT AND SHAFT HAD DECOUPLED.  VENDOR BLAMED EN	G FOR FAILURE.  SUBMITTER REJECTED THAT EXPLANATION BECAUSE EXTERNAL SHAFT WAS INTACT AND THE BUILT-IN SHEAR POINT ON SH	AFT WAS INTACT.  SUBMITTER BELIEVED PUMP HAD INTERNAL PROBLEM WHICH CAUSED EXCESSIVE WEAR ON INTERNAL SPLINES.  PREVIOUS	 REPAIR/OH INDICATED SAME TYPE PROBLEM.	2	L	7	2 	4F			 	A33EU   					 
1999121800003	19991218	00003	CE  	1999	12	18	99ZZZX4448       	2	19990902	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4128X	37   	18   		70187709	3449112	321497			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.  THIS SERVO HAS 379 HRS TT SINCE NE	W.  18 HRS SINCE PRECISION REPAIRED SERVO AT ATCA.					1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800004	19991218	00004	CE  	1999	12	18	99ZZZX4449       	2	19990902	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4128X	173  	17   		70190610	3449112	321497			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999012900720	19990129	00720	NM  	1999	1	29	99ZZZX445        	1	19990108	G	5313	655624539	STRINGER        			BOEING	727   	727259      	138408J	NM  										BS 950-990	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON STR 27L, STA 950 - STA 990.						2	L	7	3 	4F				A3WE    					 
1999121800005	19991218	00005	CE  	1999	12	18	99ZZZX4450       	2	19990928	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4128X	41   	17   		70165006	3449112	321497			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800006	19991218	00006	CE  	1999	12	18	99ZZZX4451       	2	19990928	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	A		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4128X	156  			70167603	3449112	321497			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800007	19991218	00007	CE  	1999	12	18	99ZZZX4452       	2	19990907	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4142N	166  	15   		70141606	3449128	322265			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800008	19991218	00008	CE  	1999	12	18	99ZZZX4453       	2	19990910	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4142N	398  	9    		70164908	3449128	322265			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800009	19991218	00009	CE  	1999	12	18	99ZZZX4454       	2	19990915	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4142N	174  			70190610	3449128	322265			ENGIEN RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800010	19991218	00010	CE  	1999	12	18	99ZZZX4455       	2	19990827	G	7322	RSA5AD2	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4142N	26   	7    		70156408	3449128	322265			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  REMOVED SERVO FROM ENGINE AND INSPECTED IDLE MIXTURE PLATE FOR GALLING.	  PLATE WAS FOUND GALLED.  SERVO SENT TO PRECISION FOR REPAIR.  THIS SERVO HAS 36 HRS TT SINCE NEW.  7 HRS SINCE PRECISI	ON REPAIRED SERVO AT FACTORY.				1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800011	19991218	00011	CE  	1999	12	18	99ZZZX4456       	2	19990910	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4142N	398  	9    		70164908	3449128	322265			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800012	19991218	00012	CE  	1999	12	18	99ZZZX4457       	2	19990916	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4142N	955  	25   		70140210	3449128	322021			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800013	19991218	00013	CE  	1999	12	18	99ZZZX4458       	2	19990825	G	7314	35328803	PUMP            			PIPER 	PA28  	PA28181     	7102807	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL SYSTEM	FAILED          	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4133K	36   				2843205				PUMP SHORTED OUT AND BURNED THE WIRES WHERE THEY GO IN TO THE PUMP.  WIRES ON THIS PUMP ARE TOO SHORT AND PULL ON CASE.						1	L	7	1 	3O	3	O		2A13    	E9CE				 
1999121800014	19991218	00014	CE  	1999	12	18	99ZZZX4459       	2	19990806	G	7314	35328803	PUMP            			PIPER 	PA28  	PA28181     	7102807	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL SYSTEM	FAILED          	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4133K	191  				2843205				PUMP SHORTED OUT AND BURNED THE WIRES WHERE THEY GO IN TO THE PUMP.  WIRES N THIS PUMP ARE TOO SHORT AND PULL ON CASE. D	ATE ON PART IS 06-0799.					1	L	7	1 	3O	3	O		2A13    	E9CE				 
1999012900721	19990129	00721	NM  	1999	1	29	99ZZZX446        	1	19990108	G	5313	655833872	STRINGER        			BOEING	727   	727259      	138408J	NM  										BS 950-1009	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON STR 28R, STA 950 - STA 1009.						2	L	7	3 	4F				A3WE    					 
1999121800015	19991218	00015	CE  	1999	12	18	99ZZZX4460       	2	19990917	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4177R	473  	30   		70159210	3449046	321427			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.  THIS SERVO HAS 473 HRS TT SINCE NE	W.  30 HRS SINCE PRECISION REPAIRED SERVO AT ATCA.					1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800016	19991218	00016	CE  	1999	12	18	99ZZZX4461       	2	19990827	G	7322	RSA5AD2	SERVO           			PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4177R	1179 	1    		70140106	3449046	321424			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  REMOVED SERVO FROM ENGINE AND INSPECTED IDLE MIXTURE PLATE FOR GALLING.	  PLATE WAS FOUND GALLED.  SERVO SENT TO PRECISION FOR REPAIR.  THIS SERVO HAS 1,179 HRS TT SINCE NEW.  1 HR SINCE PRECI	SION REPAIRED SERVO AT FACTORY.				1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800017	19991218	00017	CE  	1999	12	18	99ZZZX4462       	2	19990827	G	7322	RSA5AD2	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4177R	151  	1    		70141606	3449046	321679			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  REMOVED SERVO FROM ENGINE AND INSPECTED IDLE MIXTURE PLATE FOR GALLING.	  PLATE WAS FOUND GALLED.  SERVO SENT TO PRECISION FOR REPAIR.  THIS SERVO HAS 151 HRS TT SINCE NEW.  1 HR SINCE PRECISI	ON REPAIRED SERVO AT ATCA.				1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800018	19991218	00018	CE  	1999	12	18	99ZZZX4463       	2	19991105	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4177R	955  			70140210	3449046	321679			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800019	19991218	00019	CE  	1999	12	18	99ZZZX4464       	2	19991105	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4177R	547  			70164908	3449046	321679			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800020	19991218	00020	CE  	1999	12	18	99ZZZX4465       	2	19990917	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4177R	30   			70140106	3449046	321679			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800021	19991218	00021	CE  	1999	12	18	99ZZZX4466       	2	19990827	G	7322	RSA5AD2	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	9299E	443  			70159210	349043	321424			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  REMOVED SERVO FROM ENGINE AND INSPECTED IDLE MIXTURE PLATE FOR GALLING.	  PLATE WAS FOUND GALLED.  SERVO SENT TO PRECISION FOR REPAIR. THIS SERVO HAS 443 HRS TT SINCE NEW.  ZERO HRS SINCE PREC	ISION REPAIRED SERVO AT FACTORY.				1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800022	19991218	00022	CE  	1999	12	18	99ZZZX4467       	2	19990827	G	7322	RSA5AD2	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	9299E	398  	4    		70141710	3449043	321687			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  REMOVED SERVO FROM ENGINE AND INSPECTED IDLE MIXTURE PLATE FOR GALLING.	  PLATE WAS FOUND GALLED.  SERVO SENT TO PRECISION FOR REPAIR.  THIS SERVO HAS 398 HRS TT SINCE NEW.  4 HRS SINCE PRECIS	ION REPAIRED SERVO AT FACTORY.				1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800023	19991218	00023	CE  	1999	12	18	99ZZZX4468       	2	19991008	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	9299E	457  	1    		70141710	3449043	321424			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800024	19991218	00024	CE  	1999	12	18	99ZZZX4469       	2	19991012	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	9299E	34   	4    		70140106	3449043	321424			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999012900722	19990129	00722	NM  	1999	1	29	99ZZZX447        	1	19990108	G	5313	655624540	STRINGER        			BOEING	727   	727259      	138408J	NM  										BS 950C-990	CORROSION       	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON STR 28L, STA 950C - STA 990.						2	L	7	3 	4F				A3WE    					 
1999121800025	19991218	00025	CE  	1999	12	18	99ZZZX4470       	2	19990929	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	9299E	36   			70190606	3449043	321687			ENGIEN RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SEVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800026	19991218	00026	CE  	1999	12	18	99ZZZX4471       	2	19990907	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	07	9299E	34   			70190607	3449043	321687			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800027	19991218	00027	CE  	1999	12	18	99ZZZX4472       	2	19990825	G	7322	RSA5AD2	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	9299E	52   	4    		70165002	3449043	321424			ENGINE RAN RICH BELOW 1,600 RPM. ENGINE WOULD DIE ON ROLL-OUT ON RUNWAY.  REMOVED SERVO FROM ENGINE AND INSPECTED IDLE M	IXTURE PLATE FOR GALLING.  PLATE WAS FOUND GALLED.  SERVO SENT TO PRECISION FOR REPAIR.  THIS SERVO HAS 52 HRS TT SINCE 	NEW.  4 HRS SINCE PRECISION REPAIRED SERVO AT ATCA.				1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800028	19991218	00028		1999	12	18	99ZZZX4473       	4	19990722	G	3416		HOSE            			PIPER 	PA28  	PA28181     	7102807	SO  										ALTIMETER	CRACKED         	G				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			WP	07	4133D	1506 				2843117				PERFORMING 2 YEAR CERTIFICATION BLIND ENCODER AND TRANSPONDER FAILED LEAK TEST.  INSPECTION OF THE HOSE FROM THE ALTIMET	ER TO THE BLIND ENCODER WAS FOUND CRACKED AND SPLIT. NEW HOSE INSTALLED.					1	L	7	1 	3O				2A13    					 
1999121800029	19991218	00029		1999	12	18	99ZZZX4474       	4	19990722	G	3416		HOSE            			PIPER 	PA28  	PA28181     	7102807	SO  										ALTIMETER	CRACKED         	G				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			WP	07	4166H	1506 				2843119				PERFORMING 2 YEAR CERTIFICATION BLIND ENCODER AND TRANSPONDER FAILED LEAK TEST.  INSPECTION OF THE HOSE FROM THE ALTIMET	ER TO THE BLIND ENCODER WAS FOUND CRACKED AND SPLIT.  NEW HOSE INSTALLED.					1	L	7	1 	3O				2A13    					 
1999121800030	19991218	00030	SO  	1999	12	18	99ZZZX4475       	2	19990708	G	8530	635448	CYLINDER        			CESSNA	210   	210D        	2073414	CE  	CONT  	O520  	IO520A      	17032	SO  					NR 3	FAILED          	D				A				UNSCHED LANDING         				O			OTHER                     			NR	NOT REPORTED   	1			GL	05	446G	4804 	86   			21058453	1104504A			CYLINDER HEAD SEPARATED DURING FLIGHT.  ACFT MADE PRECAUTIONARY LANDING.  POST-INCIDENT INSP REVEALED NR 3 CYL HEAD SEPA	RATED BETWEEN ITS COOLING FINS.  HEAD CRACKED, SEPARATED AT THREADS THAT SECURE CYL HEAD TO BARREL.  EVIDENCE OF A 3 INC	H CRACK NEAR EXH PORT WITH EVIDENCE OF FRETTING, DEPOSITS ON COOLING FINS NEAR ORIG CRACK AREA.  CRACK EXTENDED AROUND E	NTIRE HEAD.  BARREL REMAINED INTACT WITH LOWER PORTION OF HEAD ATTACHED.  PISTON REMAINED IN BARREL UNDAMAGED.  EXTERNAL	 VISUAL INSP OF ORIG CRACK WOULD HAVE BEEN DIFFICULT TO DETECT DUE TO DENSE PLACEMENT OF COOLING FINS AND LOCATION OF CR	ACKED AREA NEXT TO NR 1 CYL.  FAILED CYL AND NR 1 REMOVED 9.13 HRS EARLIER IN ORDER TO ACCOMPLISH AD 99-09-17/CSB 99-3A.	1	H	7	1 	3O	3	O		3A21    	E5CE				 
1999121800031	19991218	00031	CE  	1999	12	18	99ZZZX4476       	2	19990927	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4123C	456  	23   		70141710	3449042	321676			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800032	19991218	00032	CE  	1999	12	18	99ZZZX4477       	2	19990916	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4123C	938  	18   		70141701	3449042	321421			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800033	19991218	00033	CE  	1999	12	18	99ZZZX4478       	2	19990913	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4123C	49   			70185009	3449042	321676			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR. THIS SERVO HAS 49 HRS TT SINCE NEW.	  ZERO HRS SINCE PRECISION REPAIRED SERVO AT ATCA.					1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800034	19991218	00034	CE  	1999	12	18	99ZZZX4479       	2	19990827	G	7322	RSA5AD2	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4123C	930  			70140210	3449042	321676			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  REMOVED SERVO FROM ENGINE AND INSPECTED IDLE MIXTURE PLATE FOR GALLING,	 PLATE WAS FOUND GALLED.  SERVO SENT TO PRECISION FOR REPAIR.  THIS SERVO HAS 930 HRS TT SINCE NEW.  ZERO HRS SINCE PREC	ISION REPAIRED SERVO AT FACTORY.				1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999012900723	19990129	00723	NM  	1999	1	29	99ZZZX448        	1	19990108	G	5311		FRAME           			BOEING	727   	727259      	138408J	NM  										BS 990	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON FAIL SAFE CHORD AND SPLICE STA 990 AFT SIDE ABOVE STR 28L.						2	L	7	3 	4F				A3WE    					 
1999121800035	19991218	00035	CE  	1999	12	18	99ZZZX4480       	2	19990827	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4123C				70187709	3449042	321676			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  REMOVED SERVO FROM ENGINE AND INSPECTED IDLE MIXTURE PLATE FOR GALLING,	 PLATE WAS FOUND GALLED. SERVO SENT TO PRECISION FOR REPAIR.  THIS SERVO HAS ZERO HRS TT SINCE NEW.  ZERO HRS SINCE PREC	ISION REPAIRED SERVO AT FACTORY.				1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800036	19991218	00036	CE  	1999	12	18	99ZZZX4481       	2	19990827	G	7320	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4123C				70187709	3449042	321676			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  REMOVED SERVO FROM ENGINE AND INSPECTED IDLE MIXTURE PLATE FOR GALLING,	 PLATE WAS FOUND GALLED.  SERVO SENT TO PRECISION FOR REPAIR.  THIS SERVO HAS ZERO HOURS TT SINCE NEW.  ZERO HRS SINCE P	RECISION REPAIRED SERVO AT FACTORY.				1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800037	19991218	00037	CE  	1999	12	18	99ZZZX4482       	2	19990916	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4123C	27   			70167604	349042	321676			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800038	19991218	00038	CE  	1999	12	18	99ZZZX4483       	2	19990904	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4123C	27   			70167604	3449042	321676			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800039	19991218	00039	CE  	1999	12	18	99ZZZX4484       	2	19990904	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4123C	27   	6    		70167604	3449042	321676			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800040	19991218	00040	CE  	1999	12	18	99ZZZX4485       	2	19990916	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4123C	938  	18   		70141701	3449042	321421			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO RPECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800041	19991218	00041	CE  	1999	12	18	99ZZZX4486       	2	19990928	G	7322	RSA5AD	SERVO           	PRECISION   		PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360RB   	17025	CE  					FUEL INJECTOR	FAILED          	G		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	4123C	41   	17   		70165006	3449042	321421			ENGINE RAN RICH, UNABLE TO ADJUST IDLE MIXTURE.  SERVO SENT TO PRECISION FOR REPAIR.						1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999121800042	19991218	00042	CE  	1999	12	18	99ZZZX4487       	1	19990928	G	3230	AN412	BOLT            			BEECH 	58    	58P         	1152744	CE  										NLG	SHEARED         	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	3684Y					TJ298				NOSE GEAR RETRACT ARM FORWARD BOLT THAT ATTACHES THE ARM TO NOSE GEAR DRAG LEG RETRACT MECHANISM SHEARED CAUSING THE GEA	R TO ONLY RETRACT PARTIALLY.  THIS ALSO CAUSED THE UP AND DOWN SWITCH ARM TO BREAK AT ITS PIVOT POINT AS IT WAS ATTEMPTI	NG TO RETRACT THE GEAR WITH THE AN3 ATTACH BOLT.  AIRCRAFT HAD EXPERIENCED A HARD LANDING APROXIMATELY 300 HOURS PRIOR.				1	L	7	2 	3O				A23CE   					 
1999121800044	19991218	00044	CE  	1999	12	18	99ZZZX4489       	1	19991117	G	3246	314901	WHEEL           			CESSNA	500   	560CESSNA   	2076750	CE  										RT MLG	MISMANUFACTURED 	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	07	326QS	184  			3352	5600526				WHEEL WAS DISASSEMBLED FOR TIRE REPLACEMENT.  DURING INSPECTION, FOUND THAT NO HOLES HAD BEEN DRILLED INTO WHEEL HALF IN	SIDE DIAMETER FOR THERMAL RELIEF.  THERMAL RELIEF PLUGS, AND BORES WERE INSTALLED NORMALLY.  FIRST TIRE REPLACEMENT SINC	E NEW.				2	L	7	2 	4F			RT	A22CE   					 
1999012900724	19990129	00724	NM  	1999	1	29	99ZZZX449        	1	19990108	G	5313	65564417	STRINGER        			BOEING	727   	727259      	138408J	NM  										BS 950-1009	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON STR 29L, STA 950 - STA 1009.						2	L	7	3 	4F				A3WE    					 
1999121800045	19991218	00045	WP  	1999	12	18	99ZZZX4490       	1	19991112	G	2460		INVERTER        			CVAC  	340   	34032       	2422706	WP  										E/E BAY	FAILED          	H				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			CR	CRUISE         	1			GL	23	3427				1638	90				AIRCRAFT WAS IN LEVEL CRUISE FLIGHT VFR PART 91.  CREW NOTICED SMOKE IN CABIN/COCKPIT.  EMERGENCY PROCEDURES INITIATED. 	 AIRCRAFT LANDED AT ANN ARBOR AIRPORT WITHOUT INCIDENT.  OVERHAULED INVERTER INSTALLED.  OPERATIONAL CHECK PERFORMED.  A	IRCRAFT RETURNED TO SERVICE.				2	L	7	2 	4R				6A6     					 
1999121800047	19991218	00047	SO  	1999	12	18	99ZZZX4492       	1	19991027	G	7120	8621202	MOUNT           			PIPER 	PA44  	PA44180     	7104402	SO  										ENGINE	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	19	39693	4973 				447995025				DURING INSPECTION, FOUND RT ENGINE MOUNT BROKEN AT TOP LEFT HAND JUST BELOW LORD MOUNT.  CHECKED LT ENGINE AND FOUND CRA	CK AT SAME LOCATION.					1	L	7	2 	3O				A19S0   					 
1999121800048	19991218	00048	CE  	1999	12	18	99ZZZX4493       	1	19991110	G	2913	66070661	PUMP            			LEAR  	60    	60LEAR      	5170707	CE  										HYDRAULIC SYSTEM	FAILED          	B	L			O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			GL	11	234FX	520  			K0294A	151				HYDRAULIC PUMP FAILED INTERNALLY AND CONTAMINATED ENTIRE HYDRAULIC SYSTEM.  PRESSURE AND RETURN FILTERS FULL OF METAL. F	OUND TRACES OF METAL AT ALL ACTUATORS.  AIRCRAFT WAS IN-FLIGHT, HAD LOW PRESSURE LIGHT ON RT SIDE.  LANDED SAFELY.  CAUS	E UNKNOWN.  PREVENTION - NONE AVAILABLE UNTIL CAUSE CONCLUDED.  SYSTEM FLUSHED, OPS CHECKED AND FILTERS RE-CHECKED.				2	L	7	2 	4F			RT	A10CE   					 
1999121800049	19991218	00049	CE  	1999	12	18	99ZZZX4494       	1	19991012	G	2140	12502081	SCROLL          			CESSNA	500   	550         	2076604	CE  										HEATER	DAMAGED         	B			GMNR	F				ACTIVATE FIRE EXT.      				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			SO	11	229MC	2190 				5500229				AFT EVAPORATOR SCROLL ASSY OVER HEATED AND BURNED A HOLE THROUGH IT IN-FLIGHT.  A FLAME WAS SEEN AND WAS PUT OUT WITH PO	RTABLE FIRE EXTINGUISHER.  UPON INSPECTION, A SALT PACK WAS DISCOVERED WEDGED AGAINST A RESISTOR ASSY INSIDE OF SCROLL A	SSY AND CAUSED A HOT SPOT.				1	L	7	2 	4F				A22CE   					 
1999121800050	19991218	00050	WP  	1999	12	18	99ZZZX4495       	2	19991115	G	7260	8968061	GEAR            			CASA  	C212  	C212CD      	2410209	EU  	GARRTT	TPE331	TPE33110    	01514	WP  					GEARBOX	FAILED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	23	204PA	9079 	2945 			309	37600			THE NUT SECURING BEARING TO IDLER GEAR PN 896806-1 LOOSENED CAUSING GEAR TO BIND IN GEARCASE.  THIS BINDING CAUSED THE N	R 1 IDLER IN THE TORQUE SENSOR TO SHEER WHICH RESULTED IN ENGINE SHUT DOWN.					2	H	7	2 	4T	4	T	RT	A43EU   	E4WE				 
1999121800051	19991218	00051	EU  	1999	12	18	99ZZZX4496       	1	19991112	G	5302	1053025151	FRAME           		10530101    	BOLKMS	105   	BO105S      	5626006	EU  										TAIL BOOM	CRACKED         	B	S		DFMR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	03	2784F	9805 				S621				DURING MAINTENANCE INSPECTION, FOUND FRAME 10L CRACKED LEFT SIDE APPROXIMATELY 2 INCHES LONG RUNNING FROM INSIDE LIP LAT	ERALLY OUTBOARD.					1	G	7	2 	3U				H3EU    					 
1999121800052	19991218	00052	SO  	1999	12	18	99ZZZX4497       	1	19991213	G	3230	95829JJ	TORQUE LINK     			PIPER 	PA34  	PA34200T    	7103406	SO  										NLG	FAILED          	D				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			EA	17	18TP	31   			958290J	347970431				ON ROLL-OUT AT 8 TO 10  KNOTS, NOSE GEAR UNLOCKED.						1	L	7	2 	3O				A7SO    					 
1999121800053	19991218	00053	EA  	1999	12	18	99ZZZX4498       	2	19991027	G	7322	MA4SPA	FLOAT BOWL      			CESSNA	172   	172M        	2072418	CE  	LYC   	O320  	O320E2D     	41508	EA  					CARBURETOR	LOOSE           	B				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			GL	19	13628		75   			17262891	L4723127A			PILOT REPORTED ENGINE WOULD NOT IDLE.  REMOVED COWLING.  FOUND FLOAT BOWL LOOSE.  THREE LOCK TABS MISSING.  THE FOURTH L	OCK TAB CRACKED.  ALL BOLTS VERY LOOSE.					1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999121800054	19991218	00054	CE  	1999	12	18	99ZZZX4499       	1	19991102	G	2730	25CF221527	CONTROL CABLE   			RAYTHN	DH125 	HAWKER800XP 	7150012	CE  										RT ELEVATOR	MISMANUFACTURED 	C		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	07	1102U					258343				DURING ROUTINE INSPECTION OF UNDER FLOOR PANEL AREA, THE ELEVATOR CONTROL CABLES WERE FOUND DAMAGED.  THE DAMAGE IS IN T	HE SAME AREA OF THE CABLE ON ALL FOUR AIRCRAFT.  CABLES APPEAR TO BE INCORRECTLY MANUFACTURED.  A FULL STRAND (7 WIRES) 	APPEARS TO BE UNRAVELING AFT OF THE CABLE RIGID REINFORCEMENT TUBE.				2	L	7	2 	4F			RT	A3EU    					 
1999012900725	19990129	00725	NM  	1999	1	29	99ZZZX450        	1	19990108	G	5311		FRAME           			BOEING	727   	727259      	138408J	NM  										BS 116	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT STA 1166, STR 27L - STR 27R.						2	L	7	3 	4F				A3WE    					 
1999121800055	19991218	00055	CE  	1999	12	18	99ZZZX4500       	1	19991102	G	2730	25BCF1051A	CONTROL CABLE   			RAYTHN	DH125 	HAWKER800XP 	7150012	CE  										LT ELEVATOR	MISMANUFACTURED 	C		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	07	1102U					258343				DURING ROUTINE INSPECTION OF UNDER FLOOR PANEL AREA, THE ELEVATOR CONTROL CABLES WERE FOUND DAMAGED.  THE DAMAGE IS IN T	HE SAME AREA OF THE CABLE ON ALL FOUR AIRCRAFT.  CABLES APPEAR TO BE INCORRECTLY MANUFACTURED.  A FULL STRAND (7 WIRES) 	APPEARS TO BE UNRAVELING AFT OF THE CABLE RIGID REINFORCEMENT TUBE.				2	L	7	2 	4F			RT	A3EU    					 
1999121800056	19991218	00056	CE  	1999	12	18	99ZZZX4501       	1	19991102	G	2730	25CF221527	CONTROL CABLE   			RAYTHN	DH125 	HAWKER800XP 	7150012	CE  										RT ELEVATOR	MISMANUFACTURED 	C		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	07	23204	25   				258346				DURING ROUTINE INSPECTION OF UNDER FLOOR PANEL AREA, THE ELEVATOR CONTROL CABLES WERE FOUND DAMAGED.  THE DAMAGE IS IN T	HE SAME AREA OF THE CABLE ON ALL FOUR AIRCRAFT.  CABLES APPEAR TO BE INCORRECTLY MANUFACTURED.  A FULL STRAND (7 WIRES) 	APPEARS TO BE UNRAVELING AFT OF THE CABLE RIGID REINFORCEMENT TUBE.				2	L	7	2 	4F			RT	A3EU    					 
1999121800057	19991218	00057	CE  	1999	12	18	99ZZZX4502       	1	19991102	G	2730	25BCF1051A	CONTROL CABLE   			RAYTHN	DH125 	HAWKER800XP 	7150012	CE  										LT ELEVATOR	MISMANUFACTURED 	C		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	07	23204	25   				258346				DURING ROUTINE INSPECTION OF UNDER FLOOR PANEL AREA, THE ELEVATOR CONTROL CABLES WERE FOUND DAMAGED.  THE DAMAGE IS IN T	HE SAME AREA OF THE CABLE ON ALL FOUR AIRCRAFT.  CABLES APPEAR TO BE INCORRECTLY MANUFACTURED.  A FULL STRAND (7 WIRES) 	APPEARS TO BE UNRAVELING AFT OF THE CABLE RIGID REINFORCEMENT TUBE.				2	L	7	2 	4F			RT	A3EU    					 
1999121800058	19991218	00058	CE  	1999	12	18	99ZZZX4503       	1	19991102	G	2730	25CF221527	CONTROL CABLE   			RAYTHN	DH125 	HAWKER800XP 	7150012	CE  										RT ELEVATOR	MISMANUFACTURED 	C		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	07	23207	25   				258350				DURING ROUTINE INSPECTION OF UNDER FLOOR PANEL AREA, THE ELEVATOR CONTROL CABLES WERE FOUND DAMAGED.  THE DAMAGE IS IN T	HE SAME AREA OF THE CABLE ON ALL FOUR AIRCRAFT.  CABLES APPEAR TO BE INCORRECTLY MANUFACTURED.  A FULL STRAND (7 WIRES) 	APPEARS TO BE UNRAVELING AFT OF THE CABLE RIGID REINFORCEMENT TUBE.				2	L	7	2 	4F			RT	A3EU    					 
1999121800059	19991218	00059	CE  	1999	12	18	99ZZZX4504       	1	19991102	G	2730	25BCF1051A	CONTROL CABLE   			RAYTHN	DH125 	HAWKER800XP 	7150012	CE  										LT ELEVATOR	MISMANUFACTURED 	C		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	07	23207	25   				258350				DURING ROUTINE INSPECTION OF UNDER FLOOR PANEL AREA, THE ELEVATOR CONTROL CABLES WERE FOUND DAMAGED.  THE DAMAGE IS IN T	HE SAME AREA OF THE CABLE ON ALL FOUR AIRCRAFT.  CABLES APPEAR TO BE INCORRECTLY MANUFACTURED.  A FULL STRAND (7 WIRES) 	APPEARS TO BE UNRAVELING AFT OF THE CABLE RIGID REINFORCEMENT TUBE.				2	L	7	2 	4F			RT	A3EU    					 
1999121800060	19991218	00060	CE  	1999	12	18	99ZZZX4505       	1	19991102	G	2730	25CF221527	CONTROL CABLE   			RAYTHN	DH125 	HAWKER800XP 	7150012	CE  										RT ELEVATOR	MISMANUFACTURED 	C		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	07	2321V	25   				258353				DURING ROUTINE INSPECTION OF UNDER FLOOR PANEL AREA, THE ELEVATOR CONTROL CABLES WERE FOUND DAMAGED.  THE DAMAGE IS IN T	HE SAME AREA OF THE CABLE ON ALL FOUR AIRCRAFT.  CABLES APPEAR TO BE INCORRECTLY MANUFACTURED.  A FULL STRAND (7 WIRES) 	APPEARS TO BE UNRAVELING AFT OF THE CABLE RIGID REINFORCEMENT TUBE.				2	L	7	2 	4F			RT	A3EU    					 
1999121800061	19991218	00061	CE  	1999	12	18	99ZZZX4506       	1	19991102	G	2730	25BCF1051A	CONTROL CABLE   			RAYTHN	DH125 	HAWKER800XP 	7150012	CE  										LT ELEVATOR	MISMANUFACTURED 	C		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	07	2321V	25   				258353				DURING ROUTINE INSPECTION OF UNDER FLOOR PANEL AREA, THE ELEVATOR CONTROL CABLES WERE FOUND DAMAGED.  THE DAMAGE IS IN T	HE SAME AREA OF THE CABLE ON ALL FOUR AIRCRAFT.  CABLES APPEAR TO BE INCORRECTLY MANUFACTURED.  A FULL STRAND (7 WIRES) 	APPEARS TO BE UNRAVELING AFT OF THE CABLE RIGID REINFORCEMENT TUBE.				2	L	7	2 	4F			RT	A3EU    					 
1999121800062	19991218	00062	WP  	1999	12	18	99ZZZX4507       	2	19991026	G	7250	30727121	BLADE           								GARRTT	TFE731	TFE73122B   	01518	WP  					HP TURBINE	DAMAGED         	B			UO2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	19		2364 					P89403			CUSTOMER FOUND METAL IN TAILPIPE.  ENGINE WAS SENT TO GARRETT SPI FOR REPAIR.  DURING TEAR DOWN, EXTENSIVE DAMAGE WAS NO	TED THROUGHOUT THE LPT MODULE.  FURTHER TEAR DOWN REVEALED ALL HPT BLADES WERE BROKEN APPROXIMATELY ONE-HALF SPAN.  ONE 	BLADE WAS SEPARATED AT ONE-THIRD SPAN FROM BLADE PLATFORM.  SUSPECT HPT BLADE SEPARATION.									4	F			E6WE				 
1999121800063	19991218	00063	GL  	1999	12	18	99ZZZX4508       	1	19991213	G	2910	000AE9040232	LINE            			AMTR  	F10   	FALCONARF10 		GL  										HYDRAULIC SYSTEM	CHAFED          	B			UO2R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			GL	19	HBUME					131				RUDDER SERVO HYDRAULIC LINES CHAFING EACH OTHER CAUSING LEAK.  THIS HAS BEEN NOTICED ON F10, S/N 162, ALSO.  S/N 131 HAD	 HOLE WORN INTO HARD LINE P/N F10A755401 FROM BRAIDED LINE, P/N 000AE90-4-0232.  BRAIDED LINE NEEDS TO BE REPOSITIONED A	ND POSSIBLY SOME TYPE OF CHAFE PROTCTION ADDED.				1	L	7	1 	3O				EXPA1L71					 
1999121800064	19991218	00064	NM  	1999	12	18	99ZZZX4509       	1	19990618	G	2510	C23PU696701	CORD REEL       		C23PM620001 	BOEING	747   	747*        		NM  										CABIN	FAILED          	B			UWCR	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			NM	01										CORD REEL FAILED.						2	L	7	4 	4F			RT	A20WE   					 
1999012900726	19990129	00726	NM  	1999	1	29	99ZZZX451        	1	19990108	G	5314	65564418	KEEL BEAM       			BOEING	727   	727259      	138408J	NM  										FUSELAGE	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON STR 29R, KEEL BEAM CHORD FORWARD OF AFT CARGO DOOR.						2	L	7	3 	4F				A3WE    					 
1999121800065	19991218	00065	SO  	1999	12	18	99ZZZX4510       	1	19991122	G	3260	1CH214	SWITCH          			PIPER 	PA31  	PA31350     	7103110	SO  										RT MLG	INOPERATIVE     	H				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			SO	17	36BM	3591 				318262008				PILOT REPORTED RT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED AND THE LANDING GEAR SELECTOR DID NOT RETURN TO NEU	TRAL WITH NORMAL OR EMERGENCY HAND PUMP OPERATION.  AFTER AN UNEVENTFUL LANDING WAS MADE, ACFT DELIVERED TO MAINT.  MAIN	T DETERMINED THE RT MLG DOWN AND LOCKED SWITCH WAS DEFECTIVE PREVENTING A GREEN GEAR INDICATION AND PREVENTING THE INNER	 LANDING GEAR DOORS FROM CLOSING.  A NEW SWITCH WAS INSTALLED IAW THE PIPER MM. THE GEAR WAS OPERATIONALLY CHECKED AND T	HE ACFT RETURNED TO SERVICE.  THE SWITCH APPEARED TO BE THE ORIGINAL ONE INSTALLED AT BUILD.  SUSPECT SWITCH FAILED DUE 	TO NORMAL WEAR AND TEAR.	1	L	7	2 	3O				A20SO   					 
1999121800066	19991218	00066	CE  	1999	12	18	99ZZZX4511       	1	19991116	G	3233	2307006166	HOSE            			LEAR  	35    	35A         	5170602	CE  										MLG ACTUATOR	LEAKING         	B			NVIR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	30GJ					320				PILOT COMPLAINED OF HYDRAULIC LEAK IN WHEELWELL AREA.  INVESTIGATION DISCLOSED MAIN GEAR ACTUATOR HOSE LEAKING AT B-NUT.	  CLEANED, OPERATED SYSTEM TO VERIFY, FOUND FLUID COMING FROM B-NUT CRACK.  FURTHER INVESTIGATION DISCLOSED B-NUT TO BE 	CRACKED END TO END AND SEPARATING AT CRACK.  HOSE IDENTIFICATION TAG INDICATED A MANUFACTURE DATE OF 3-15-99, (7 MONTHS 	OLD).  CALLED STRATOFLEX FT. WORTH, WHO REQUESTED THE HOSE FOR FURTHER INVESTIGATION.  REPLACED HOSE WITH NEW.  SERVICED	 AND OPERATED SYSTEM.  NO LEAKS WITH NEW HOSE.		2	L	7	2 	4F				A10CE   					 
1999121800067	19991218	00067	CE  	1999	12	18	99ZZZX4512       	1	19991018	G	5620	9942000197	SEAT TRACK      			BEECH 	200   	200BEECH    	1152920	CE  										CABIN	CORRODED        	B		A		K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NE	05	330BR					BB115				UPON ENTERING AIRCRAFT, NOTICED A VERY STRONG MILDEW ODOR.  AFTER THE PRELIMINARY INSPECTION WAS DONE AND DURING THE DIS	ASSEMBLY OF THE INTERIOR, FOUND THE PROBLEM TO BE SEVERAL LEAKING CABIN WINDOWS.  THEN THE SEAT RAILS WERE FOUND SEVEREL	Y CORRODED AROUND THE MOUNTING SCREWS.  ONE, UPON REMOVAL, BROKE INTO TWO PIECES.				1	L	7	2 	4T				A24CE   					 
1999121800068	19991218	00068	CE  	1999	12	18	99ZZZX4513       	1	19991018	G	5347		WINDOW          			BEECH 	200   	200BEECH    	1152920	CE  										CABIN	LEAKING         	B		A		K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			NE	05	330BR					BB115				UPON ENTERING AIRCRAFT, NOTICED A VERY STRONG MILDEW ODOR.  AFTER THE PRELIMINARY INSPECTION WAS DONE AND DURING THE DIS	ASSEMBLY OF THE INTERIOR, FOUND THE PROBLEM TO BE SEVERAL LEAKING CABIN WINDOWS.  THEN THE SEAT RAILS WERE FOUND SEVEREL	Y CORRODED AROUND THE MOUNTING SCREWS.  ONE, UPON REMOVAL, BROKE INTO TWO PIECES.				1	L	7	2 	4T				A24CE   					 
1999121800070	19991218	00070		1999	12	18	99ZZZX4515       	4	19991122	G	2562		SWITCH          			CESSNA	172   	172R        	2072401	CE  										ELT	MALFUNCTIONED   	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	2745M	691  			326702	17280586				FUNCTION TESTED ELT SYSTEM DURING 100-HOUR INSPECTION.  ELT COULD NOT BE ACTIVATED BY REMOTE SWITCH OR COPILOT'S  INSTRU	MENT PANEL.  INSTALLED SERVICEABLE ELT AND OPERATED NORMALLY, HOWEVER, RED LAMP ON REMOTE SWITCH DID NOT ILLUMINATE.  IN	STALLED NEW SWITCH AND ALL FUNCTIONS CHECKED NORMAL.  MASTER SWITCH ON ORIGINAL ELT AND THE G-SWITCH BOTH SEEMED TO OPER	ATE CORRECTLY WITH UNIT REMOVED FROM AIRCRAFT.  ELT MODEL, 3000-11.  SWITCH, P/N 2019-10.			1	H	7	1 	3O			NT	3A12    					 
1999121800071	19991218	00071	CE  	1999	12	18	99ZZZX4516       	1	19991112	G	2910		SHUT-OFF VALVE  			LEAR  	35    	35LEAR      	5170600	CE  										HYDRAULIC SYSTEM	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			GL	05	111WB					003				DURING A RECENT 300/600 HOUR INSPECTION, THE HYDRAULIC FIREWALL SHUT-OFF VALVES WERE FOUND WIRED BACKWARDS.  WHEN THE LE	FT FIREWALL T-HANDLE WAS PULLED, THE RT HYDRAULIC SHUT-OFF VALVE WOULD CLOSE AND VISA VERSA.					2	L	7	2 	4F				A10CE   					 
1999121800072	19991218	00072	EA  	1999	12	18	99ZZZX4517       	2	19991213	G	8520		BUSHING         								LYC   	O540  	TIO540J2BD  	41532	EA  					CONNECTING ROD	MISINSTALLED    	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	99			1044 				266768K			ALL CONNECTING ROD BUSHINGS FOUND CRACKED.  FOUND BUSHINGS INSTALLED AT 90 DEGREE ANGLE VICE 45 DEGREE ANGLE PER SERVICE	 INSTRUCTION.  THIS WAS AN ICELANDIC AIRCRAFT.  HOWEVER, THE ENGINES WERE OVERHAULED BY LYCOMING.										3	O			E14EA				 
1999121800073	19991218	00073	EU  	1999	12	18	99ZZZX4518       	1	19991110	G	3233	AIR400390	GLAND SEAL      		AIR864141   	SAAB  	SF340 	340B        	7860101	EU  										NLG	FAILED          	B			FW1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	03		6044 			LK9701292					PREMATURE FAILURE OF GLAND SEAL.  PART HAD 3,473 CSN ON 24,000 CYCLE OVERHAUL SCHEDULE.  PART WAS BUILT NEW, 4Q97.  MFG 	OF APPLIANCE AND SEAL HAS BEEN NOTIFIED.					2	L	7	2 	4T			RT	A52EU   					 
1999121800074	19991218	00074	EA  	1999	12	18	99ZZZX4519       	2	19991122	G	8530	71895P10	VALVE SEAT      			HELIO 	H295  	H295        	4300802	CE  	LYC   	O480  	GO480G1D6   	41527	EA  					ENGINE	SEPARATED       	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	PKUCD	2    				1246	L44837			THE EXHAUST VALVE SEAT WAS FOUND TO HAVE COME OUT FOLLOWING THE ENGINE TEST STAND RUN AND PRIOR TO THE INITIAL INSTALLAT	ION RUN ON THE AIRCRAFT.  A 'RATTLE' WAS NOTED AS THE ENGINE WAS TURNED THROUGH BY HAND.  THE CYLINDER OVERHAUL SHOP HAS	 BEEN ALERTED AND OTHER CYLINDERS OF THE SAME BATCH CHECKED.  THE CYLINDER WAS MACHINED TO ACCEPT A P-20 SEAT, BUT A P-1	0 WAS INSTALLED.			1	H	7	1 	3O	3	O		1A8     	E275				 
1999012900727	19990129	00727	NM  	1999	1	29	99ZZZX452        	1	19990108	G	5320		WEB             			BOEING	727   	727259      	138408J	NM  										BS 1166	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON WEB AT STA 1166 BETWEEN STR 28 AND STR 29R.						2	L	7	3 	4F				A3WE    					 
1999121800183	19991218	00183	CE  	1999	12	18	99ZZZX4520       	1	19991123	G	5730	052309510	SKIN            			CESSNA	172   	172S        	2072439	CE  										LT WING	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP					172S8035				DURING FIRST PHASE 3 INSPECTION, FOUND LT UPPER WING TRAILING EDGE SKIN ASSY CRACKED.  THE 3RD RIVET FROM INBOARD TRAILI	NG EDGE HAD A 1 INCH CRACK EMANATING FROM THE RIVET HEAD.  REPLACED TRAILING EDGE SKIN AND RE-PAINTED.					1	H	7	1 	3O			NT	3A12    					 
1999121800184	19991218	00184	CE  	1999	12	18	99ZZZX4521       	1	19991020	G	3230	1053840023	CYLINDER        			BEECH 	76    	76          	1153005	CE  										MLG	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	2009Y	3771 				ME74				THE MAIN LANDING GEAR RETRACT CYLINDER PISTON ROD HAS EXTERNAL THREADS TO ACCEPT A ROD END.  THE PISTON ROD FAILED AT TH	E THREADS.  RECOMMEND THE THREADED PORTION OF THE PISTON ROD BE CLEANED AND INSPECTED AT REGULAR INTERVALS.					1	L	7	2 	3O				A29CE   					 
1999121800186	19991218	00186		1999	12	18	99ZZZX4523       	1	19991201	G	3242	7010FS9545708	SEAL            		50105201    															BRAKE	FAILED          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		1469 			JUNE981364					BRAKE ASSEMBLY, P/N 50-10520-1, FAILED PREMATURELY.  THREE EACH PISTONS LEAKING FROM INSULATOR AREA.  PISTONS INTERNALLY	 FILLED WITH FLUID.  EVIDENCE OF T-SEAL FAILURE.  THIS IS A CONTINUAL DISCREPANCY.  FACTORY NEW BRAKE ASSEMBLY.																		 
1999121800187	19991218	00187	SO  	1999	12	18	99ZZZX4524       	1	19991130	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE ASSY	FAILED          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		1729 			0434A					BRAKE ASSEMBLY, P/N 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN AND BINDING IN TORQUE TUBE KEY SLOTS. THIS IS A CONT	INUAL DISCREPANCY.  BRAKE ASSY SHOULD LAST 2,500 CYCLES.					2	L	7	2 	4T			RT	A31SO   					 
1999121800188	19991218	00188	NM  	1999	12	18	99ZZZX4525       	1	19991203	G	3242	2445902	CARRIER         	BFGOODRICH  	21565       	DHAV  	DHC8  	DHC8*       		NM  										BRAKE ASSY	FAILED          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					0054					BRAKE ASSEMBLY PN 2-1565 FAILED PREMATURELY.  NR 2 CARRIER AND LINING ASSY BROKEN IN HALF.  THIS IS A CONTINUAL DISCREPA	NCY.					2	H	7	2 	4T			RT	A13NM   					 
1999121800189	19991218	00189	SO  	1999	12	18	99ZZZX4526       	1	19991130	G	3242	1331096	STATOR          	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										BRAKE ASSY	FAILED          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19		604  			0244					BRAKE ASSEMBLY, P/N 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN IN TWO PIECES.  STATOR TANGS BROKEN AND BINDING IN T	ORQUE TUBE KEY SLOTS DAMAGING BEYOND SERVICEABLE LIMITS.  THIS IS A CONTINUAL DISCREPANCY.  BRAKE ASSY SHOULD LAST 2,500	 CYCLES.				2	L	7	2 	4T			RT	A31SO   					 
1999121800190	19991218	00190	EU  	1999	12	18	99ZZZX4527       	1	19991202	G	2435	P6048233	ARMATURE        	AUXILEC     	8260121     	AEROSP	ATR72 	ATR72       		EU  										STARTER/GEN	FAILED          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19			1756 		SRC810504					STARTER/GENERATOR P/N 8260-121 FAILED.  ARMATURE DRIVE END COPPER BAND FAILED CAUSING CATASTROPHIC DAMAGE TO STATOR AND 	SPEED SENSOR.  UNIT IS MADE BY A FOREIGN MANUFACTURER.					2	H	7	2 	4T			RT						 
1999121800191	19991218	00191	CE  	1999	12	18	99ZZZX4528       	1	19991129	G	5540		BRACKET         			CESSNA	150   	152         	2071835	CE  										RUDDER	WORN            	D	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	16	48877	6600 				15281022				BOLT HOLES ELONGATED OVER TIME ALLOWING RUDDER FOOT TO CONTACT TAIL AND RUB.  REPLACED UPPER AND LOWER BRACKETS.  NR 5 U	PPER AND LOWER RUDDER BRACKET (HINGE), P/N 0451028-1 AND -2 LOWER; -5 AND -6 UPPER.					1	H	7	1 	3O			NT	3A19    					 
1999012900728	19990129	00728	NM  	1999	1	29	99ZZZX453        	1	19990108	G	5230	655612910	FITTING         			BOEING	727   	727259      	138408J	NM  										AFT CARGO DOOR	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON AFT CARGO DOOR FITTING STR 27R.						2	L	7	3 	4F				A3WE    					 
1999121800195	19991218	00195		1999	12	18	99ZZZX4532       	1	19990928	G	2432	RG380E44	BATTERY         																	E/E BAY	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05					CBC276943					BATTERY WILL NOT TAKE A CHARGE.  REMOVED AND REPLACED.																			 
1999121800196	19991218	00196		1999	12	18	99ZZZX4533       	1	19990825	G	6320	1171206301	GEAR            																	TRANSMISSION	CORRODED        	B			TI1R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	05					KA0969					NEW PART - CORROSION PITTING ON BEARING RACE OF NEW GEAR.  REMOVED AND REPLACED.																			 
1999121800197	19991218	00197		1999	12	18	99ZZZX4534       	1	19990921	G	3340	A7151	HOUSING         																	LIGHT	DENTED          	B			TI1R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	05										RECEIVED NEW PART DAMAGED, DENTED.  REMOVED AND REPLACED.																			 
1999121800198	19991218	00198		1999	12	18	99ZZZX4535       	1	19990909	G	6420	105317261	LAMINATES       																	TAIL ROTOR	SEPARATING      	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05					51275					NEW DEFECTIVE - ONE STRAP HAD SEPARATIONS - RMA R021892.  REMOVED AND REPLACED.																			 
1999121800200	19991218	00200	CE  	1999	12	18	99ZZZX4537       	1	19990827	G	5315	10542000047	STRINGERS       			BEECH 	76    	76          	1153005	CE  										FUSELAGE	CRACKED         	B	S	A	BF8R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	3726D	8988 				ME353				DURING A SCHEDULED INSPECTION, MOVEMENT OF THE FLOOR WAS OBSERVED WHEN THE RUDDER PEDALS WERE MOVED FORE AND AFT BY HAND	. THIS WAS FOUND ON BOTH SIDES. THE PEDALS AND TORQUE TUBES WERE REMOVED AND THE FLOOR REMOVED IN THE LOCAL AREA.  ONCE 	THE FLOOR WAS REMOVED, THE MECHANIC FOUND STRINGERS P/N 105-420000-47 (RT SIDE) AND P/N 169-400005-473 (LT SIDE), CRACKE	D.  THESE CRACKS, APPROXIMATELY 1 INCH LONG, COINCIDE WITH THE LOCATION WHERE THE RUDDER PEDAL TORQUE TUBE BRACKETS ARE 	ATTACHED TO THE FLOOR STRUCTURE.  APPROPRIATE REPAIRS WERE MADE TO THE STRINGERS AND THE FLOOR REPLACED WITH NEW SHEET M	ETAL.	1	L	7	2 	3O				A29CE   					 
1999121800201	19991218	00201	CE  	1999	12	18	99ZZZX4538       	1	19990827	G	5315	169400005473	STRINGERS       			BEECH 	76    	76          	1153005	CE  										FUSELAGE	CRACKED         	B	S	A	BF8R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	3726D	8988 				ME353				DURING A SCHEDULED INSPECTION, MOVEMENT OF THE FLOOR WAS OBSERVED WHEN THE RUDDER PEDALS WERE MOVED FORE AND AFT BY HAND	. THIS WAS FOUND ON BOTH SIDES. THE PEDALS AND TORQUE TUBES WERE REMOVED AND THE FLOOR REMOVED IN THE LOCAL AREA.  ONCE 	THE FLOOR WAS REMOVED, THE MECHANIC FOUND STRINGERS P/N 105-420000-47 (RT SIDE) AND P/N 169-400005-473 (LT SIDE), CRACKE	D.  THESE CRACKS, APPROXIMATELY 1 INCH LONG, COINCIDE WITH THE LOCATION WHERE THE RUDDER PEDAL TORQUE TUBE BRACKETS ARE 	ATTACHED TO THE FLOOR STRUCTURE.  APPROPRIATE REPAIRS WERE MADE TO THE STRINGERS AND THE FLOOR REPLACED WITH NEW SHEET M	ETAL.	1	L	7	2 	3O				A29CE   					 
1999121800202	19991218	00202	WP  	1999	12	18	99ZZZX4539       	1	19991129	G	2560	SWD230305100	GIRT ASSY       	BFGOODRICH  	SWD230300201	DOUG  	DC10  	DC1030F     	3023504	WP  										CABIN	UNAPPROVED PART 	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	19					PM0028A					GIRT ASSY WAS MADE FROM AN UNKNOWN FABRIC AND IDENTIFIED WITH THE MANUFACTURER'S (BFG) P/N SWD230305-100, AND WITHOUT TH	E MANUFACTURER'S INSPECTION STAMP AND INSPECTION DATE.  THIS PART IS NOT PER THE MANUFACTURER'S DRAWING AND IS CONSIDERE	D A SUSPECTED UNAPPROVED PART.				2	L	7	3 	4F			RT	A22WE   					 
1999012900729	19990129	00729	NM  	1999	1	29	99ZZZX454        	1	19990108	G	5311		FRAME           			BOEING	727   	727259      	138408J	NM  										BS 950E	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON FRAME AT FS 950E, STR 27R.						2	L	7	3 	4F				A3WE    					 
1999121800203	19991218	00203	WP  	1999	12	18	99ZZZX4540       	1	19991129	G	2560	SWD230105103	GIRT ASSY       		SWD230100101	DOUG  	DC10  	DC1030F     	3023504	WP  										CABIN	UNAPPROVED PART 	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	19					AA601					GIRT BAR FLAP ASSY WAS MADE FROM AN UNKNOWN FABRIC AND IDENTIFIED WITH THE MANUFACTURER'S (BFG) P/N SWD230105-103, AND W	ITHOUT THE MANUFACTURER'S INSPECTION STAMP AND INSPECTION DATE. THIS PART IS NOT PER THE MANUFACTURER'S DRAWING AND IS C	ONSIDERED A SUSPECTED UNAPPROVED PART.				2	L	7	3 	4F			RT	A22WE   					 
1999121800204	19991218	00204	WP  	1999	12	18	99ZZZX4541       	1	19991129	G	2560	SWD230305102	GIRT ASSY       		SWD230300201	DOUG  	DC10  	DC1030F     	3023504	WP  										CABIN	UNAPPROVED PART 	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03					FF010					GIRT ASSY (LOWER) WAS MADE FROM AN UNKNOWN FABRIC AND IDENTIFIED WITH THE MANUFACTURER'S (BFG) P/N SWD230305-102 AND WIT	HOUT THE MANUFACTURER'S INSPECTION STAMP AND INSPECTION DATE.  THIS PART IS NOT PER THE MANUFACTURER'S DRAWING AND IS CO	NSIDERED A SUSPECTED UNAPPROVED PART.				2	L	7	3 	4F			RT	A22WE   					 
1999121800205	19991218	00205		1999	12	18	99ZZZX4542       	1	19991022	G	6230	1171260901	BEARING         																	M/R MAST	CORRODED        	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05					T33					FOUND PITTING ON INNER RACES ON INITIAL INSPECTION.  REMOVED AND REPLACED.																			 
1999121800206	19991218	00206		1999	12	18	99ZZZX4543       	1	19991013	G	5330	230031593101	PANEL           																	FUSELAGE	MISMANUFACTURED 	B			TI1R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	05										AFT SCREW HOLES DO NOT LINE UP TO AIRCRAFT.  REMOVED AND REPLACED.																			 
1999121800207	19991218	00207		1999	12	18	99ZZZX4544       	1	19991013	G	5330	230031592101	PANEL           																	FUSELAGE	MISMANUFACTURED 	B			TI1R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	05										AFT SCREW HOLES DO NOT LINE UP WITH AIRFRAME.  REMOVED AND REPLACED.																			 
1999121800209	19991218	00209	SO  	1999	12	18	99ZZZX4546       	2	19991122	G	8520	535661	CAMSHAFT        			CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  					ENGINE	MAKING METAL    	B			CY4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	7318Q	1948 	213  		473105	U20603074	247849R			FERROUS MATERIAL FOUND IN OIL FILTER.  ENGINE DISASSEMBLED, PROBLEM FOUND TO BE FAILED CAMSHAFT AND LIFTER BODIES.						1	H	7	1 	3O	3	O		A4CE    	E5CE				 
1999121800210	19991218	00210	SO  	1999	12	18	99ZZZX4547       	2	19991122	G	8520	SA535661	CAMSHAFT        			CESSNA	182   	182Q        	2072732	CE  	CONT  	O470  	O470S       	17026	SO  					ENGINE	MAKING METAL    	B			CY4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	79JP	2142 	118  		473054	18267081	469049			FERROUS MATERIAL FOUND IN OIL FILTER.  ENGINE DISASSEMLBED, PROBLEM FOUND TO BE FAILED CAM AND LIFTER BODIES.						1	H	7	1 	3O	3	O	NT	3A13    	E273				 
1999121800211	19991218	00211	SO  	1999	12	18	99ZZZX4548       	2	19991202	G	8530	635448	CYLINDER        			BEECH 	33    	F33A        	1151425	CE  	CONT  	O520  	IO520BB     	17032	SO  					NR'S 2 & 4	WORN            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	6624B	304  				CE1034	809514R			AT 303.67 HOURS, THESE CYLINDERS HAD WORN OUT BORES AND EXHAUST VALVE GUIDES WORN BEYOND SERVICEABLE LIMITS.  THE ENGINE	 WAS FACTORY REBUILT/ZERO TIMED 1995.					1	L	7	1 	3O	3	O		3A15    	E5CE				 
1999121800212	19991218	00212	SO  	1999	12	18	99ZZZX4549       	2	19990921	G	8540	534728	SUPPORT PIN     			CESSNA	421   	421C        	2076016	CE  	CONT  	O520  	GTSIO520N   	17032	SO  					LT ENGINE	FAILED          	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	6VH					421C0156				FOREIGN OBJECT DAMAGE WITHIN LEFT ENGINE ASSEMBLY CAUSED IDLER GEAR SUPPORT PIN BETWEEN MAGNETO DRIVES TO SHEAR CAUSING 	MOUNT STUDS TO BREAK AND THE GEAR IT RIDES ON TO ROTATE AND BECOME UNMESHED.  IT AFFECTED MAGNETO TIMING AND CAUSED ENGI	NE TO LOSE POWER AND START RUNNING ROUGH.				1	L	7	2 	3O	3	O		A7CE    	E7CE				 
1999121800213	19991218	00213	WP  	1999	12	18	99ZZZX4550       	1	19991110	G	6410	36124	CUFF            			HILLER	UH12  	UH12E       	4360122	WP  										CONTROL BLADE	FAILED          	G		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	13	5388V		2845 		10653	2099				CONTROL ROTOR CUFF SPLIT IN TWO AT THE INBOARD BOLT HOLE.  OUTBOARD SECTION AND CONTROL ROTOR TUBE ASSEMBLY SEPARATED FR	OM HELICOPTER CAUSING LOSS OF CONTROL.  CRACK APPEARS TO HAVE STARTED AT INBOARD BOLT HOLE.  BOTH HALVES OF CUFF SENT TO	 NTSB LAB FOR ANALYSIS.  LIFE LIMIT:  6,860 HOURS.  AIRCRAFT TT:  22,145.3 HOURS.				1	G	7	1 	3O				4H11    					 
1999121800214	19991218	00214	EU  	1999	12	18	99ZZZX4551       	1	19991110	G	6420	60102RSIMT33CA	BEARING         		350A33200405	SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	ROUGH           	B			S88R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	21	5202Y	500  			MA0843	3085				DURING A 500-HOUR INSPECTION, C/W SB 05.00.29 (EUROCOPTER).  DURING THE ROTATIONAL TORQUE CHECK OF THE BEARING, IT WAS F	OUND TO BE ROUGH DURING ROTATION.  DID NOT DISASSEMBLE, BUT APPEARED TO HAVE VERY LITTLE LUBRICATION.  REF:  W.O. NR 000	134.				1	G	7	1 	3U				H9EU    					 
1999121800215	19991218	00215	NE  	1999	12	18	99ZZZX4552       	1	19991018	G	2400	8241631	POTENTIOMETER   	HAMSTD      	769000180210	SKRSKY	S76   	S76         	8143010	NE  										ELECTRICAL	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5402T	4551 	1853 		81092477	760140				FEEDBACK POTENTIOMETER PREMATURE FAILURE.  SUBMITTER STATED SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS.  CAUSED ACTU	ATOR TO KICK IN-FLIGHT.  COMPONENT P/N 7690001802106.					1	G	7	2 	3U				H1NE    					 
1999121800216	19991218	00216	EU  	1999	12	18	99ZZZX4553       	1	19991110	G	3230	200920604	GLAND NUT       	MESSIER     		STBROS	SD3   	SD360       	8100606	EU  										RT MLG	FAILED          	C				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	366MQ				DRG823282	SH3639				GLAND NUT FAILED CAUSING THE SHOCK STRUT TO SEPARATE AND NOT SUPPORT THE AIRCRAFT ON LANDING.						2	H	7	2 	4T				A41EU   					 
1999121800219	19991218	00219	SO  	1999	12	18	99ZZZX4556       	2	19991122	G	8520	535661	CAMSHAFT        			CESSNA	180   	180         	2072602	CE  	CONT  	O470  	O470L       	17026	SO  					ENGINE	FAILED          	B			CY4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	9269T	2039 	80   		473071	50769	8808530L4			FERROUS MATERIAL FOUND IN OIL FILTER.  ENGINE DISASSEMBLED, PROBLEM FOUND TO BE FAILED CAMSHAFT AND LIFTER BODIES.						1	H	7	1 	3O	3	O	NC	5A6     	E273				 
1999121800220	19991218	00220		1999	12	18	99ZZZX4557       	1	19991124	G	3233	11581002917	NUT ASSY        																	MLG ACTUATOR	FAILED          	B			JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09										THREADS PULLED OUT FROM INSIDE OF NUT ASSY DURING TESTING OF MLG ACTUATOR.																			 
1999121800221	19991218	00221		1999	12	18	99ZZZX4558       	1	19991109	G	2820	223902001	VALVE           		223900011   															FUEL SYSTEM	MISREPAIRED     	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	23					407					CHECK VALVE ASSEMBLY, AS RECEIVED BACK FROM THAI AIRWAYS INT'L LTD, HAD THE END OF THE VALVE EXPOXIED CLOSED RENDERING T	HE ASSY USELESS.																		 
1999020500002	19990205	00002	EA  	1999	2	5	99ZZZX456        	2	19990104	G	7321	3010454	FCU             		3010457     	BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  					LT ENGINE	OUT OF ADJUST   	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	777XS	9604 	435  			BB126	PCE80815			INVESTIGATED LEFT ENGINE CONTROL LINKAGE AND FOUND POWER CONTROL LEVER WOULD NOT RETARD WITH POWER CONTROL CABLE MOVEMEN	T.  LUBRICATED PIVOT POINTS, CHECKED ADJUSTMENTS AND RIGGING, PERFORMED ENGINE RUN CHECKS, NO DEFECTS NOTED.					1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999121800224	19991218	00224		1999	12	18	99ZZZX4561       	4	19990914	G	2312	4000106010	CONTROL HEAD    																	COCKPIT	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05		2052 								CONTROL HEAD CANNOT PROGRAM PRESETS.  REMOVED AND REPLACED.																			 
1999121800232	19991218	00232	GL  	1999	12	18	99ZZZX4569       	2	19991001	G	7321		O-RING          	BENDIX      	252464429   	AEROSP	AS355 	AS355E      	8680805	EU  	ALLSN 	250C  	250C20      	03013	GL  					FCU	FAILED          	B			ALGR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	372E				325174	5208				UPON DISASSEMBLY OF UNIT, FOUND O-RING HARD AND BRITTLE.  ALL O-RINGS BRITTLE AND HARD - POSSIBLE EXTREME HEAT.						1	G	7	2 	3U	3	U		H11EU   	E4CE				 
1999020500003	19990205	00003	NE  	1999	2	5	99ZZZX457        	3	19990112	G	6111	A32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		457  						HL277		PROPELLER S/N HL277 WAS RETURNED FOR LOOSE BLADE.  AFTER DISASSEMBLY, INSPECTION REVEALED 2 LOOSE AND 2 BROKEN A-3204-1 	PRELOAD SET SCREWS.  THE B-3368 LOCKNUTS WERE STILL ATTACHED TO THE INBOARD SECTION OF THE A-3204-1 SCREWS.  THE SCREWS 	WERE REMOVED, SENT TO HARTZELL ENGINEERING FOR EVALUATION AND REPLACED FOR NEW.				2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999121800233	19991218	00233	EU  	1999	12	18	99ZZZX4570       	1	19990912	G	7931	6607A2114	SWITCH          			BOLKMS	105   	BO105LSA3   	5626020	EU  										OIL PRESSURE	FAILED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	8118Y	204  			W65389	2017				UNIT FAILED AFTER 203.9 HOURS OF USE.  REMOVED AND REPLACED.						1	G	7	2 	3U				H3AU    					 
1999121800234	19991218	00234	EU  	1999	12	18	99ZZZX4571       	1	19990927	G	2913	L290M20A1015	PUMP            			UROCOP	EC135 	EC135P1     	8680990	EU  										HYDRAULIC SYSTEM	LEAKING         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	911SV	282  			0152	0070				SPLINES SHOW ABNORMAL WEAR.  SHAFT SEAL LEAKING.  REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999121800235	19991218	00235	GL  	1999	12	18	99ZZZX4572       	2	19990801	G	7261	222340091101	PUMP            			BELL  	230   	230         	1182149	SW  	ALLSN 	250C  	250C30      	03013	GL  					OIL SYSTEM	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	4UV	2467 			0018	23019				LOW OIL PRESSURE - PARTS SUPPORT AIRCRAFT.  REMOVED AND REPLACED.						1	G	7	2 	3U	3	U	NC	H9SW    	E1GL				 
1999121800236	19991218	00236		1999	12	18	99ZZZX4573       	4	19991013	G	2312	069102525	TRANSCEIVER     		KX165       	BELL  	222   	222U        	1182140	SW  										COCKPIT	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	222HX				60745	47533				SEVERAL DIGITS MISSING ON DISPLAY.  REMOVED AND REPLACED.						1	G	7	2 	3U				H9SW    					 
1999121800237	19991218	00237	SW  	1999	12	18	99ZZZX4574       	1	19990920	G	3340	206810501	MOTOR           			BELL  	206   	206L3       	1182108	SW  										SEARCH LIGHT	INOPERATIVE     	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	206AZ	1    			555	51007				ROTATIONAL MOTOR INOPERATIVE.  TURN SOLENOID OPERATES, ALL OTHER FUNCTIONS OKAY.  REMOVED AND REPLACED.						1	G	7	1 	3U				H2SW    					 
1999121800238	19991218	00238	EU  	1999	12	18	99ZZZX4575       	1	19991103	G	2910	105450121	HYDRAULIC PACK  			BOLKMS	105   	BO105LSA3   	5626020	EU  										HYDRAULIC SYSTEM	LEAKING         	B			TI1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	05	8118Y	673  			6002	2017				LOW PRESSURE SEALS ON SYSTEM.  ONE RESERVOIR LEAKING.  ALSO, PERFORMED 6-MONTH AND 1-YEAR INSPECTIONS.  REMOVED AND REPL	ACED.					1	G	7	2 	3U				H3AU    					 
1999121800239	19991218	00239	EU  	1999	12	18	99ZZZX4576       	1	19991004	G	2150	JBS8803	MIXING VALVE    			UROCOP	EC135 	EC135P1     	8680990	EU  										HEATER	STICKING        	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	911SV	192  			052	0070				SHUT-OFF VALVE STICKS IN OPEN POSITION ON NR 2 SIDE.  REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999121800240	19991218	00240	NE  	1999	12	18	99ZZZX4577       	2	19990922	G	7230	410102050	IMPELLER        			BOLKMS	117   	BK117A3     	5626015	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					COMPRESSOR	CHAFED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	118LL	597  			SA435	7097				HEAVY RUB ON IMPELLER AT AREA 2.421 INCH - 2.419 INCH DIAMETER.  REMOVED AND REPLACED.						1	G	7	2 	3U	3	U		H13EU   	E5NE				 
1999121800241	19991218	00241	SW  	1999	12	18	99ZZZX4578       	1	19990908	G	6520	406040406101	CASE            		407040400115	BELL  	407   	407         		SW  										T/R GEARBOX	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407AL	3616 	1376 		AFS749	53044				PRE-FLIGHT INSPECTION FOUND MOUNTING PADS WORN BEYOND LIMITS IN BHT 407 CR&O MANUAL.  ONE EACH DOW ALIGNMENT PIN BROKEN.	  FURTHER TEAR-DOWN REVEALED HIGH GEAR BACKLASH AND SCARING OF THE GEAR TEETH.  POSSIBLY DUE TO  LOW OR ABSENCE OF OIL A	T THE SAME TIME.  HIGH VIBRATION CAUSED GEARBOX TO LOOSEN UP.				1	G	7	1 	3U			O	H2SW    					 
1999121800242	19991218	00242	NE  	1999	12	18	99ZZZX4579       	2	19990905	G	7530	430110209	ACTUATOR        			BOLKMS	117   	BK117A3     	5626015	EU  	LYC   	LTS101	LTS101650B1 	41560	NE  					MODULATOR	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	1140H	422  			2741	7078	LE45156			AIR TUBE BROKEN.  REMOVED AND REPLACED.						1	G	7	2 	3U	3	U		H13EU   	E5NE				 
1999020500004	19990205	00004	NE  	1999	2	5	99ZZZX458        	3	19990115	G	6111	A32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05								HL27		PROPELLER S/N HL27 WAS RETURNED FOR OVERHAUL.  AFTER DISASSEMBLY, INSPECTION REVEALED 1 BROKEN A-3204-1 PRELOAD SET SCRE	W.  THE SCREW WAS BROKEN INTO TWO PIECES WITH THE B-3368 LOCKNUT STILL ATTACHED TO THE SCREW.  DAMAGE TO THE C-6066-1 PR	ELOAD PLATE WAS WITHIN OVERHAUL LIMITS.  THE PRELOAD PLATE SET SCREW WAS SENT TO HARTZELL ENGINEERING FOR EVALUATION AND	 REPLACED WITH NEW.			2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999121800243	19991218	00243	EU  	1999	12	18	99ZZZX4580       	1	19990702	G	3340	30050423	LIGHT           			BOLKMS	117   	BK117A4     	5626017	EU  										STROBE	FAILED          	B			TI1R	K				NONE                    				L	W		NO TEST                   	INADEQUATE Q C            		IN	INSP/MAINT     	1			SW	05	171MU				127609	7138				LIGHT FLASHED 7 TIMES THEN QUIT.  OUT OF BOX FAILURE.  REMOVED AND REPLACED.						1	G	7	2 	3U				H13EU   					 
1999121800244	19991218	00244		1999	12	18	99ZZZX4581       	4	19990925	G	3422	060001500	GYRO            		KG102A      	BELL  	222   	222U        	1182140	SW  										COCKPIT	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	222HX	10   			29975	47533				GYRO TRIPS CIRCUIT BREAKER.  MEASURED 4-5+ AMP DRAM ON 28 VDC POWER TO UNIT.  HAPPENS AFTER UNIT SPOOLS.  REMOVED AND RE	PLACED.					1	G	7	2 	3U				H9SW    					 
1999121800246	19991218	00246	NE  	1999	12	18	99ZZZX4583       	2	19990903	G	7310	430123604	MAINFOLD        			BOLKMS	117   	BK117B1     	5626012	EU  	LYC   	LTS101	LTS101750B1 	41560	NE  					ENGINE FUEL	MALFUNCTIONED   	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	117VU	1310 			1YG02316	7211				DELAYED STARTS AND HOT STARTS.  REMOVED AND REPLACED.						1	G	7	2 	3U	3	U		H13EU   	E5NE10				 
1999121800247	19991218	00247		1999	12	18	99ZZZX4584       	4	19990827	G	3457	066040312121	GPS             			BOLKMS	BK117 	BK117C1     	5626025	EU  										COCKPIT	FAILED          	B			TI1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	317MC				80155	7505				UNIT DROPS OFF-LINE.  WILL NOT PICK UP SIGNALS.  REMOVED AND REPLACED.						1	G	7	2 	3U			NC	H13EU   					 
1999121800248	19991218	00248	SW  	1999	12	18	99ZZZX4585       	1	19991019	G	5302	407023800118S	SUPPORT         		407030801101	BELL  	407   	407         		SW  										TAIL BOOM	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	527AL				53212	53211				DURING DAILY INSPECTION.  CRACK IN RADIUS OF ANGLE DUE TO POOR QUALITY CONTROL MEASURES AND STRESS ON PART WHEN INSTALLE	D.					1	G	7	1 	3U			O	H2SW    					 
1999121800249	19991218	00249	SW  	1999	12	18	99ZZZX4586       	1	19991029	G	5320	407030734103	PANEL           			BELL  	407   	407         		SW  										FUSELAGE	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437AL	2999 				53141				DURING TAILROTOR DRIVESHAFT REPLACEMENT.  OIL COOLER BLOWER DECK IS CRACKED AND THE OIL COOLER TRANSITION DUCT IS CRACKE	D.					1	G	7	1 	3U			O	H2SW    					 
1999121800250	19991218	00250	SW  	1999	12	18	99ZZZX4587       	1	19991026	G	5311	206032305127206	FRAME           			BELL  	407   	407         		SW  										FUSELAGE	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	477AL	3381 				53203				ROUTINE INSPECTION.  FRAME AND ANGLE CRACKED BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999121800251	19991218	00251	GL  	1999	12	18	99ZZZX4588       	2	19991027	G	7250	23061922	ROTOR           		6898735     	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3912Q		784  		ER47582	3271	CAE834438			UPON VISUAL INSPECTION OF THE POWER TURBINE SECTION WHEN REMOVED FOR 10W POWER REPAIR.  DISASSEMBLED P.T. ROTOR AND FOUN	D CRACKED DIAPHRAGM THROUGH NR 4 NOZZLE INNER BAND.  POSSIBLE CAUSE IS DUE TO NOZZLE UNABLE TO HANDLE STRESS FROM HEAT. 	 NOTE:  THIS DIAPHRAGM HAS BEEN UPGRADED PER ALLISION BOOK FAX 97-AMC-051 TO PREVENT THIS PROBLEM, BUT IT CONTINUES TO O	CCUR.  CONDITION OF PART IS REPAIRABLE.			1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999121800252	19991218	00252	SW  	1999	12	18	99ZZZX4589       	1	19991021	G	6322	206061432121	HOUSING         		407040303105	BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427AL	1422 			A263	53107				DURING DAILY INSPECTION, FOUND CRACKED BLOWER HOUSING.						1	G	7	1 	3U			O	H2SW    					 
1999020500005	19990205	00005	NE  	1999	2	5	99ZZZX459        	3	19990112	G	6111	A32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05								HL259		PROPELLER S/N HL259 WAS RETURNED FOR A LOOSE BLADE.  AFTER DISASSEMBLY, INSPECTION REVEALED 1 BROKEN A-3204-1 PRELOAD SE	T SCREW.  THE SCREW WAS BROKEN INTO TWO PIECES WITH THE B-3368 LOCKNUT STILL ATTACHED TO THE INBOARD SECTION OF THE BROK	EN A-3204-1 SCREW.  THE SCREW WAS REMOVED, SENT TO HARTZELL ENGINEERING FOR EVALUATION AND REPLACED WITH NEW.				2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999121800254	19991218	00254	SW  	1999	12	18	99ZZZX4591       	1	19991011	G	6322	206061432121	HOUSING         		407040303105	BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	477AL	1982 			AFS1027	53203				DURING DAILY INPSECTION, FOUND CRACKED BLOWER HOUSING.						1	G	7	1 	3U			O	H2SW    					 
1999121800255	19991218	00255	SW  	1999	12	18	99ZZZX4592       	1	19991006	G	6322	206061432121	HOUSING         		407040303105	BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	547AL	268  			A375	53240				DURING DAILY INSPECTION, FOUND CRACKED BLOWER HOUSING.						1	G	7	1 	3U			O	H2SW    					 
1999121800256	19991218	00256	SW  	1999	12	18	99ZZZX4593       	1	19990929	G	6510	206061432121	HOUSING         		407040303105	BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427AL				AFS1204	53107				DURING DAILY INSPECTION, FOUND CRACKED BLOWER HOUSING.						1	G	7	1 	3U			O	H2SW    					 
1999121800257	19991218	00257	SW  	1999	12	18	99ZZZX4594       	1	19991107	G	6322	206061432121	HOUSING         		407040303105	BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427AL	23   			A489	53107				DURING DAILY INSPECTION, FOUND CRACKED BLOWER HOUSING.						1	G	7	1 	3U			O	H2SW    					 
1999121800258	19991218	00258	SW  	1999	12	18	99ZZZX4595       	1	19991028	G	6322	206061432121	HOUSING         		407040303105	BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	477AL	106  			A469	53203				DURING DAILY INSPECTION, FOUND CRACKED BLOWER HOUSING.						1	G	7	1 	3U			O	H2SW    					 
1999121800259	19991218	00259	SW  	1999	12	18	99ZZZX4596       	1	19991103	G	6322	206061432121	HOUSING         		407040303105	BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427AL	351  			A272	53107				DURING DAILY INSPECTION, FOUND CRACKED BLOWER HOUSING.						1	G	7	1 	3U			O	H2SW    					 
1999121800261	19991218	00261		1999	12	18	99ZZZX4598       	4	19990928	G	3416	5934P3	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	FAILED          	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	350AZ	291  			402060	3127				INDICATOR OUT OF SPEC AT HIGHER ALTITUDES.  REMOVED AND REPLACED.						1	G	7	1 	3U				H9EU    					 
1999020500006	19990205	00006	NE  	1999	2	5	99ZZZX460        	3	19990112	G	6111	A32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		155  						HL17		PROPELLER, S/N HL17, WAS RETURNED FOR A LOOSE BLADE.  AFTER DISASSEMBLY, INSPECTION REVEALED 1 BROKEN A-3204-1 PRELOAD S	ET SCREW.  THE SCREW WAS BROKEN INTO TWO PIECES WITH THE B-3368 LOCKNUT STILL ATTACHED TO THE INBOARD SECTION OF THE BRO	KEN A-3204-1 SCREW.  THE SCREW WAS REMOVED, SENT TO HARTZELL FOR EVALUATION AND ALL SCREWS WERE REPLACED WITH NEW.  THE 	C-6066-1 PRELOAD PLATE THREAD WAS DAMAGED, BUT WITHIN ACCEPTABLE LIMITS AND THE PLATE WAS REPAIRED AND RETURNED TO SERVI	CE.		2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999121800264	19991218	00264	SW  	1999	12	18	99ZZZX4601       	1	19991004	G	2820	70009H015C152	LINE            			BELL  	206   	206L1       	1182107	SW  										FUEL SYSTEM	CORRODED        	B	P		ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	206SL					45245				DURING REMOVAL OF COMPONENTS FOR AIRCRAFT MAJOR AIRFRAME INSPECTION.  SEVERE CORROSION OF FITTING CAUSED BY MOISTURE TRA	PPED IN THE FIRE SLEEVE PROTECTION.  PART WAS SCRAPPED.					1	G	7	1 	3U				H2SW    					 
1999121800680	19991218	00680	NE  	1999	12	18	99ZZZX4602       	2	19990930	G	7310	697753	LINE            			BOEING	747   	747122      	1384872	NM  	PWA   	JT9   	JT9D7AH     	52054	NE  					FUEL SYSTEM	CRACKED         	B			QEMY	E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			K	B	J	FLUID LOSS                	SMOKE/FUMES/ODORS/SPARKS  	WARNING INDICATION        	NR	NOT REPORTED   	1			EA	35	854FT					19754	662560			ENGINE EXPERIENCED WHAT APPEARED TO BE A STALL FOLLOWED BY A FIRE WARNING.  ENGINE WAS SHUT DOWN AND AN AIR TURN-BACK AC	COMPLISHED.  CORE COWL DAMAGE WAS OBSERVED IMMEDIATELY AFTER LANDING. SUBSEQUENT INVESTIATION IDENTIFIED A CRACKED FUEL 	HYDRAULIC LINE.  THE DEFECT CONSIDERED THE LIKELY CAUSE OF EXCESS FUEL SPILLAGE AND IGNITION SOURCE WITHIN NACELLE ENVIR	ONMENT.  MODERATE FIRE DAMAGE WAS OBSERVED IN IMMEDIATE VACINITY OF FAILED TUBE.			2	L	7	4 	4F	4	F		A20WE   	E20EA				 
1999121800681	19991218	00681	EA  	1999	12	18	99ZZZX4603       	2	19991122	G	8550		LINE            			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					CRANKCASE	CRACKED         	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			GL	11	4964G	3222 	1400 		L712376	17273511	L712376			INVESTIGATED OIL LEAK.  FOUND CRANKCASE TO BE CRACKED AT LEFT FRONT OF CASE.  CRACK STARTS AT LOWER THROUGH STUD HOLE, R	UNS BACK HORIZONTALLY .50 INCH THEN VERTICAL 2.50 INCHES.  AIRCRAFT WAS INVOLVED IN A PROPELLER STRIKE 1,330 HOURS AGO. 	 SUSPECT THIS MAY HAVE LED TO THE CRACK.				1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999121800682	19991218	00682	SO  	1999	12	18	99ZZZX4604       	2	19991027	G	7314	6462121	FUEL PUMP       		646181      						CONT  	O520  	IO520*      	17032	SO  					ENGINE	LEAKING         	B			O3OR	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03					E229726BR					THE FUEL PUMP 646212-1 USUALLY USED ON TCM ENGINES IO520.  THIS FUEL PUMP IS ONE OF SEVERAL FUEL PUMPS FOUND TO LEAK PAS	T THE SEAL PN 646181.  ALSO, NEW PRODUCTION OF THIS SEAL IS FOUND TO BE SMALLER THAN THE OLDER VERSION WHICH CAUSED IT N	OT TO BE SEATED FIRMLY IN THE BODY.									3	O			E5CE				 
1999121800683	19991218	00683	CE  	1999	12	18	99ZZZX4605       	1	19991206	G	7810	085071123	EXHAUST PIPE    			CESSNA	401   	401A        	207590D	CE  										LT ENGINE	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	17	4057Q					401A0109				LEFT EXHAUST TAIL PIPE WAS FOUND CRACKED AND A PIECE OF THE PIPE APPROXIMATELY 2 INCHES BY 2.50 INCHES WAS MISSING.  IT 	APPEARED THE CRACKING WAS MOST LIKELY  CAUSED BY VIBRATION.  EXHAUST GAS LEAKING FROM THIS TAIL PIPE CAN CAUSE DAMAGE TO	 THE WING SPAR.				1	L	7	2 	3O				A7CE    					 
1999121800685	19991218	00685	SO  	1999	12	18	99ZZZX4607       	2	19991128	G	8530	653816A5	VALVE SEAT      			CESSNA	175   	175B        	2072506	CE  	CONT  	O300  	GO300D      	17022	SO  					CYLINDER	SEPARATED       	D				A				UNSCHED LANDING         				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			NM	11	175VC	112  				17556798	161760D			DURING FLIGHT, PILOT/OWNER HAD A LOSS OF POWER AND ENGINE RAN ROUGH.  PILOT RETURNED TO AIRPORT WITH ENGINE PRODUCING RE	DUCED POWER.  UPON INSPECTION MAINTENANCE FOUND THE INTAKE VALVE SEAT HAD COME LOOSE FROM CYLINDER.  THE ENGINE HAD RECE	NTLY HAD A TOP OVERHAUL 112 HOURS EARLIER WITH NEW CONTINENTAL CYLINDERS.				1	H	7	1 	3O	3	O		3A17    	E298				 
1999121800689	19991218	00689	CE  	1999	12	18	99ZZZX4609       	1	19991107	G	3230	51420025	DRAG BRACE      			CESSNA	402   	402C        	207590R	CE  										NLG	FAILED          	C				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NE	01	83PB					402C0350				NOSE GEAR DRAG BRACE, P/N 5142002-5, (NEW, HEAVY DUTY STYLE), FAILED ON GEAR EXTENSION APROXIMATELY ONE INCH AFT OF THE 	NOSE GEAR ACTUATOR ROD END ATTACH LUG.  AIRCRAFT LANDED WITH MINOR DAMAGE TO THE NOSE AREA OF THE AIRCRAFT.					1	L	7	2 	3O				A7CE    					 
1999020500007	19990205	00007	NE  	1999	2	5	99ZZZX461        	3	19990112	G	6111	A32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		2026 						HL58		PROPELLER, S/N HL58, WAS RETURNED FOR SERVICE, BULLETINS 5 AND 14.  AFTER DISASSEMBLY, INSPECTION REVEALED 1 BROKEN A320	4-1 PRELOAD SET SCREW.  THE B-3368 LOCKNUT WAS STILL ATTACHED TO THE INBOARD SECTION OF THE A-3204-1 SCREW.  THE SCREW W	AS REMOVED, SENT TO HARTZELL ENGINEERING FOR EVALUATION AND REPLACED WITH NEW.				2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999121800690	19991218	00690	CE  	1999	12	18	99ZZZX4610       	1	19991025	G	3233		ACTUATOR        			BEECH 	1900  	1900D       	1154162	CE  										MLG	FAILED          	C				O				OTHER                   				J			WARNING INDICATION        			LD	LANDING        	1			SO	23	2FOR	3541 								POWER PACK SCREWS BROKE OFF IN-FLIGHT.   PILOT COULD NOT LOCK NOSE GEAR.  PILOT THEN PROCEEDED TO EXTEND MANUALLY, BUT N	OSE GEAR DID NOT LOCK.  PROCEEDED TO MAKE A VERY SOFT LANDING AND AIRCRAFT HAD BOTH PROPS CUT OFF.  NOSE WHEELWELL DAMAG	ED, AND ENGINE REMOVED AND SENT TO P&W, CANADA.  POWER PACK REMOVED AND SENT TO RAYTHEON.  THEY STATED SCREWS WERE OVERT	ORQUED.			2	L	7	2 	4T			RT	A24CE   					 
1999121800691	19991218	00691	CE  	1999	12	18	99ZZZX4611       	1	19991112	G	3233		ACTUATOR        			BEECH 	1900  	1900D       	1154162	CE  										MLG	FAILED          	C				O				OTHER                   				J			WARNING INDICATION        			LD	LANDING        	1			SO	23	2FOR	6140 								PILOT IN APPROACH LANDING NOTICED NOSE GEAR WAS NOT LOCKED.  TALKED TO THE TOWER AND THEY CONFIRMED THAT, PILOT TRIED TO	 EXTEND BY EMERGENCY AND AGAIN COULD NOT LOCK NOSE GEAR.  AIRCRAFT LANDED HARD AND NOSE GEAR LOCKED UP IN VERY LAST MOME	NT AFTER PILOT PUT MAIN WHEEL ON GROUND.				2	L	7	2 	4T			RT	A24CE   					 
1999121800692	19991218	00692	CE  	1999	12	18	99ZZZX4612       	1	19991112	G	2497		WIRE            			LEAR  	35    	35A         	5170602	CE  										ELECTRICAL	CHAFED          	B			EKGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	242MT	4371 				621				RIGHT 'ROLEX' PANEL AFT OF CIRCUIT BREAKERS HOT, MELTED, AND PILOT CHECKLIST LYING NEXT TO PANEL IS MELTED ALSO.  DISASS	EMBLED RT CIRCUIT BREAKER PANEL.  FOUND AND REMOVED 2 BUTT SPLICES ON NR 20 GAUGE WIRE FOR 40-AMP ESS BUSS.  SOLDERED NR	 10 GAUGE WIRE AND GROUND RUN SYSTEM.  NO DEFECTS NOTED.  RE-ASSEMBLED IAW LEARJET MM.				2	L	7	2 	4F			 	A10CE   					 
1999121800693	19991218	00693		1999	12	18	99ZZZX4613       	1	19991105	G	6410	117317411	BLADE           																	TAIL ROTOR	DAMAGED         	B			TI1R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	05					211					RETURNED WITH DAMAGED BLADE, SN 212.  REMOVED AND REPLACED.																			 
1999121800694	19991218	00694		1999	12	18	99ZZZX4614       	1	19991105	G	6410	117317411	BLADE           																	TAIL ROTOR	DAMAGED         	B			TI1R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	05					212					REMOVING BLADE FROM BOX, FOUND IMPACT DENT IN BLADE.  REMOVED AND REPLACED.																			 
1999121800695	19991218	00695		1999	12	18	99ZZZX4615       	1	19991201	G	7111	9638002117	ACTUATOR        																	COWL FLAP	FAILED          	G				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	15	830Q		78   		2637					BEGINNING 9-20-99 AT 646.5 HOBBS, COWL FLAP ACTUATOR WAS REPLACED.  A PART WAS ORDERED THROUGH BEECHCRAFT.  THE NEXT FAI	LURE OCCURRED AT 9-30-99 AT 672.4 HOBBS, AND, THEREAFTER, 10-19-99 AT 704.7 HOBBS, 11-4-99 AT 763.0 HOBBS, AND 11-30-99 	AT 840.8 HOBBS.  AT EACH FAILURE, THE COMPONENT WAS REPLACED WITH A NEW OR OVERHAULED PART WITH A BEECHCRAFT PART NUMBER	.  ALL FAILURES OCCURRED UNDER NORMAL OPERATING CIRCUMSTANCES AND SEEM TO HAVE A LIFE LIMITED TIME OF AN AVERAGE 48.5 HO	URS.															 
1999121800696	19991218	00696	EU  	1999	12	18	99ZZZX4616       	1	19991129	G	2913	AP09V0303	HYDRAULIC PUMP  	ABEX        		AMD   	FALC10	FALCON10    	2730101	EU  										LT ENGINE	FAILED          	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			WP	05	711FJ		88   		AH49579A	149				THE SERIAL NUMBERED PUMP WAS INSTALLED ON THIS ARICRAFT AS A REPLACEMENT OF AN OVERHAULED PUMP BY THIS VENDOR (THE ZEE C	O) WHICH FAILED AFTER 157 HOURS OF OPERATION. THIS PUMP, SN AH-49579A, WAS IN OPERATION ONLY 87.9 HOURS BEFORE IT HAD A 	FAILURE WHICH CAUSED ITS REPLACEMENT.  HYDRAULIC FLUID WAS NOTICED ON THE BOTTOM OF THE COWLING AND AFTER INVESTIGATING,	 FOUND ONE OF THE HEX CAP SCREW HEADS HAD SHEARED OFF.  THE CAP HEAD DANGLED FROM THE PUMP BY THE SAFETY WIRE.			2	L	7	2 	4F				A33EU   					 
1999121800697	19991218	00697		1999	12	18	99ZZZX4617       	4	19991129	G	3421		TUBE            			BEECH 	35    	V35A        	1151544	CE  										COCKPIT GYRO	CHAFED          	D		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	23	7048N					D8636				LOST FLIGHT INSTRUMENTS SHORTLY AFTER TAKEOFF.  FOUND THE GYRO INSTRUMENTS WOULD TUMBLE WHEN THE GEAR WAS RETRACTED AND 	INSTRUMENT AIR PRESSURE DROP TO NEAR ZERO.  AIR PRESSURE AND INSTRUMENT OPERATION RETURNED TO NORMAL WHEN GEAR WAS EXTEN	DED. INSPECTION FOUND THE PLASTIC TUBING PROTRUDED INTO THE WHEELWELL FAR ENOUGH FOR THE NOSE WHEEL TO CONTACT AND OBSTR	UCT IT WHEN THE GEAR WAS RETRACTED. EVIDENCE OF THE SAME CONDITION WAS NOTED ON ANOTHER AIRCRAFT MODEL V35B, S/N D9102, 	N-4042A.		1	L	7	1 	3O				3A15    					 
1999121800698	19991218	00698	CE  	1999	12	18	99ZZZX4618       	1	19991123	G	5730	052309510	SKIN            			CESSNA	172   	172S        	2072439	CE  										RT WING	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP					172S8035				DURING FIRST PHASE 3 INSPECTION, FOUND RT UPPER WING TRAILING EDGE SKIN ASSY CRACKED.  THE THIRD RIVET FROM INBOARD TRAI	LING EDGE HAD A ONE INCH CRACK EMANATING FROM THE RIVET HEAD.  REPLACED TRAILING EDGE SKIN AND RE-PAINTED.					1	H	7	1 	3O			NT	3A12    					 
1999121800699	19991218	00699	CE  	1999	12	18	99ZZZX4619       	1	19991123	G	5753	052390138	RIVET           			CESSNA	172   	172S        	2072439	CE  										TE FLAP	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP					1728035				DURING FIRST PHASE 3 INSPECTION WITH TOTAL AIRFRAME TIME OF 482.8 HOURS, FOUND RT FLAP TRAILING EDGE RIVETS HAD CRACKS A	ROUND 2 RIVETS.  THE CRACKS WERE AROUND THE 13TH AND 16TH RIVETS FROM THE INBOARD END.  ONE CRACK .50 INCH IN LENGTH, TH	E OTHER .25 INCH IN LENGTH. REPLACED FLAP UNDER WARRANTY.				1	H	7	1 	3O			NT	3A12    					 
1999020500008	19990205	00008	NE  	1999	2	5	99ZZZX462        	3	19990112	G	6111	A32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05								HL231		PROPELLER, S/N HL231, WAS RETURNED FOR A LOOSE BLADE.  AFTER DISASSEMBLY, INSPECTION REVEALED ONE BROKEN A-3204-1 PRELOA	D SET SCREW.  THE SCREW WAS BROKEN INTO TWO PIECES WITH THE B-3368 LOCKNUT STILL ATTACHED TO THE INBOARD SECTION OF THE 	BROKEN A-3204-1 SCREW.  THE SCREW WAS REMOVED, SENT TO HARTZELL ENGINEERING FOR EVALUATION AND REPLACED WITH NEW.  THE C	-6066-1 PRELOAD PLATE THREAD WAS DAMAGED, BUT WITHIN ACCEPTABLE LIMITS AND THE PLATE WAS REPAIRED AND RETURNED TO SERVIC	E.		2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999121800700	19991218	00700		1999	12	18	99ZZZX4620       	4	19991123	G	3421	S33261	INDICATOR       	SIGMATEK    		CESSNA	172   	172S        	2072439	CE  										COCKPIT	FAILED          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	03	494SP	483  			T66684L	172S8035				ATTITUDE INDICATOR TUMBLED FOR ABOUT 45 MINUTES ON A CROSS-COUNTRY FLIGHT BEFORE RE-ERECTING.  VACUUM SYSTEM TESTS SATIS	FACTORY, NO OTHER DEFECTS NOTED.  REPLACED GYRO, FURTHER OPERATION SATISFACTORY.					1	H	7	1 	3O			NT	3A12    					 
1999121800701	19991218	00701	CE  	1999	12	18	99ZZZX4621       	1	19991123	G	7722	TE4099802	THERMOCOUPLE    			CESSNA	172   	172S        	2072439	CE  										ENGINE	INOPERATIVE     	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	03	494SP					172S8035				EGT THERMOCOUPLE INOPERATIVE.  WIRES ARE SEPARATED FROM PROBE.  TOTAL AIRFRAME TIME 482.8 HOURS AND SUBMITTER STATED THI	S IS THE SECOND EGT THERMOCOUPLE REPLACED ON THIS AIRCRAFT.  REPLACED EGT THERMOCOUPLE, OPERATIONAL CHECKED SATISFACTORY	.				1	H	7	1 	3O			NT	3A12    					 
1999121800702	19991218	00702	CE  	1999	12	18	99ZZZX4622       	1	19990916	G	5711		SPAR            			BEECH 	18    	H18         	1151012	CE  										WING	CRACKED         	D	L			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	954	8759 				BA670				INTERNAL CORROSION AND CRACKS ON MAIN WING SPAR.  INDICATIONS WERE FOUND ON RADIOGRAPHIC VIEWS.  REFERENCE AD 75-27-09 R	2 COPY OF INSPECTION.					1	L	7	2 	3R				A765    					 
1999121800703	19991218	00703	SO  	1999	12	18	99ZZZX4623       	1	19991124	G	5720		PLANK           			GULSTM	G1159 	G1159B      	3953535	SO  										WING	CORRODED        	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	05	928GF	9364 				119				DURING NDT OF WING CLOTHESPIN FITTINGS, FOUND CORROSION ON TOP OF UPPER AFT WING PLANK.  CORROSION MAY BE DUE TO HARSH A	REA THAT IT IS SUBJECTED TO.					2	L	7	2 	4F			RT	A12EA   					 
1999121800704	19991218	00704	EA  	1999	12	18	99ZZZX4624       	2	19991013	G	8530	76220	STUD            			PIPER 	PA28  	PA28RT201   	7102818	SO  	LYC   	O360  	IO360C1C    	41514	EA  					CYLINDER	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	01	8265S	7312 				28R8118001	L218265IA			NR 2 CYLINDER HAD TWO BROKEN STUDS PREVIOUS TO THIS INCIDENT.  SUBMITTER STATED SHOULD HAVE REMOVED THROUGH-STUDS ALSO A	ND HAD MAGNAFLUXED AND CHECKED BEFORE RE-INSTALLING CYLINDER AT THAT TIME.					1	L	7	1 	3O	3	O		2A13    	1E10				 
1999122300001	19991223	00001	EU  	1999	12	23	99ZZZX4625       	1	19990907	G	2821	312263701	FILTER          			UROCOP	EC135 	EC135P1     	8680990	EU  										ENGINE	MALFUNCTIONED   	B			TI1R	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	05	911SV	234  			AM0121	0070				FILTER WILL NOT RESET.  REMOVED AND REPLACED.						1	G	7	2 	3U			O	H88EU   					 
1999020500009	19990205	00009	NE  	1999	2	5	99ZZZX463        	3	19990112	G	6111	A32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		1657 						HL233		PROPELLER, S/N HL233, WAS RETURNED FOR VIBRATION.  AFTER DISASSEMBLY, INSPECTION REVEALED ONE BROKEN A-3204-1 PRELOAD SE	T SCREW.  THE SCREW WAS BROKEN INTO TWO PIECES WITH THE B-3368 LOCKNUT STILL ATTACHED TO THE INBOARD SECTION OF THE BROK	EN A-3204-1 SCREW.  THE SCREW WAS REMOVED, SENT TO HARTZELL ENGINEERING FOR EVALUATION AND REPLACED WITH NEW.  THE C-606	6-1 PRELOAD PLATE THREAD WAS DAMAGED, BUT WITHIN ACCEPTABLE LIMITS AND THE PLATE WAS REPAIRED AND RETURNED TO SERVICE.			2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999123100042	19991231	00042	EU  	1999	12	31	99ZZZX4632       	1	19990629	G	6200	L621M1010225	ABSORBER        			UROCOP	EC135 	EC135P1     	8680990	EU  										FUSELAGE	SEPARATED       	B			TI1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	05	911SV	183  				0070				VIBRATION ABSORBER CAME LOOSE IN-FLIGHT.						1	G	7	2 	3U			O	H88EU   					 
1999123100043	19991231	00043	CE  	1999	12	31	99ZZZX4633       	1	19991213	G	2822	5100003	PUMP            			CESSNA	172   	172R        	2072401	CE  										FUEL SYSTEM	FAILED          	B			BF8R	C				ABORTED TAKEOFF         				O			OTHER                     			TO	TAKEOFF        	1			WP	07	403ER	344  			1438	17280245				ON TAKEOFF ROLL, HEARD ELECTRIC FUEL PUMP SURGING.  ABORTED TAKEOFF.  SUMPED STRAINER TWICE AND FOUND BRASS FLAKES BOTH 	TIMES.  LEFT THE BRASS FLAKES IN THE STRAINER FOR MAINTENANCE TO VERIFY.					1	H	7	1 	3O			NT	3A12    					 
1999123100044	19991231	00044	EA  	1999	12	31	99ZZZX4634       	2	19991213	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B			BF8R	O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			AP	APPROACH       	1			WP	07	416ER	1892 				17280281	L2732651A			WHILE IN CLOSED TRAFFIC 7R AFTER COMPLETING TURN TO CROSSWIND, APPROXIMATELY 600 FEET AGL, THE ENGINE SPUTTERED AND PART	IALLY LOST POWER.  THERE WAS A 300 RPM DROP FOR ABOUT 3 SECONDS.  AFTER 3 SECONDS, POWER RETURNED TO NORMAL.  NO EMERGEN	CY WAS DECLARED, AND LANDING WAS AS PLANNED AND UNEVENTFUL.				1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999123100045	19991231	00045		1999	12	31	99ZZZX4635       	4	19991215	G	3424	1394T100	INDICATOR       	ELECTRICGYRO																COCKPIT	FAILED          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	99					78210					PILOT REPORTED THE TURN COORDINATOR WAS NOT OPERATING.  HOWEVER, THE INDICATOR FLAG SHOWED THE INSTRUMENT WAS OPERATING.	  THE PILOT PULLED THE CIRCUIT BREAKER FOR THE INSTRUMENT AND THE FLAG SHOWED THE INSTRUMENT WAS OFF.  WHEN THE CIRCUIT 	BREAKER WAS RESET, THE FLAG WOULD RETRACT INDICATING THE INSTRUMENT WAS OPERATING WHEN, IN FACT, IT WAS NOT.  THIS CONDI	TION COULD LEAD TO LOSS OF CONTROL OF THE AIRCRAFT IN A PARTIAL PANEL IFR OR NIGHT SITUATION.  THE INSTRUMENT WAS REMOVE	D AND SENT FOR OVERHAUL.															 
1999123100046	19991231	00046	EA  	1999	12	31	99ZZZX4636       	2	19991213	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B			BF8R	O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			WP	07	449ER	1306 				17280610	L2773851A			THE PILOT REPORTED A BRIEF POWER LOSS.  THE ENGINE AND RELATED SYSTEMS WERE INSPECTED.  THE FLOW DIVIDER WAS DISASSEMBLE	D, CLEANED, AND RE-ASSEMBLED.  A POST-MAINTENANCE GROUND RUN INDICATED NORMAL OPERATION.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999123100047	19991231	00047	EA  	1999	12	31	99ZZZX4637       	2	19991213	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B			BF8R	O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			WP	07	477ER	936  				17280622	L2803951A			THE PILOT REPORTED A BRIEF POWER LOSS.  THOROUGHLY INSPECTED ENGINE AND COMPONENTS.  CLEANED AND INSPECTED SPARK PLUGS, 	FLOW DIVIDER, INSPECTED FUEL STRAINER AND SERVO SCREEN, CLEANED AND INSPECTED FUEL NOZZLES.  A POST-MAINTENANCE GROUND R	UN INDICATED NORMAL OPERATION.				1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999123100048	19991231	00048	CE  	1999	12	31	99ZZZX4638       	1	19991213	G	2822		PUMP            			CESSNA	172   	172R        	2072401	CE  										FUEL BOOST	FAILED          	B			BF8R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	07	424ER	97   				17280640				THE PILOT REPORTED ZERO FUEL PRESSURE WHEN THE BOOST PUMP WAS TURNED ON.  INVESTIGATION REVEALED IT HAD FAILED IN THE PU	MP SECTION.  THE METAL PARTICLES HAD MIGRATED THROUGHOUT THE FUEL SYSTEM REQUIRING THE INSPECTION, CLEANING, AND REPLACE	MENT OF COMPONENTS AND HOSES.				1	H	7	1 	3O			NT	3A12    					 
1999123100049	19991231	00049	EA  	1999	12	31	99ZZZX4639       	2	19991124	G	7414	I0382807	CONDENSER       			PIPER 	PA44  	PA44180     	7104402	SO  	LYC   	O360  	LO360E1A6   	41514	EA  					MAGNETO	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	2197K	30   				447995206	L30077T			ENGINE WOULD NOT PRODUCE A MAGNETO DROP DURING RUN-UP.  FOUND CONDENSER OPEN.  REPLACED WITH NEW.  OPS CHECK OK.  SUBMIT	TER STATED  COULD CAUSE INJURY TO GROUND PERSONNEL THINKING MAGNETOS WERE GROUNDED.  DATE CODE ON CONDENSER 9914.					1	L	7	2 	3O	3	O		A19S0   	E286				 
1999020500010	19990205	00010	NE  	1999	2	5	99ZZZX464        	3	19990112	G	6111	A32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05								HL189		PROPELLER, S/N HL189, WAS RETURNED FOR VIBRATION.  AFTER DISASSEMBLY, INSPECTION REVEALED ONE BROKEN A-3204-1 PRELOAD SE	T SCREW.  THE SCREW WAS BROKEN INTO TWO PIECES WITH THE B-3368 LOCKNUT STILL ATTACHED TO THE INBOARD SECTION OF THE BROK	EN A-3204-1 SCREW.  THE SCREW WAQS REMOVED, SENT TO HARTZELL ENGINEERING FOR EVALUATION AND REPLACED WITH NEW.  THE C-60	66-1 PRELOAD PLATE THREAD WAS DAMAGED, BUT WITHIN ACCEPTABLE LIMITS AND THE PLATE WAS REPAIRED AND RETURNED TO SERVICE.			2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999123100050	19991231	00050	EA  	1999	12	31	99ZZZX4640       	2	19991129	G	8500		ENGINE          			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FORWARD	MALFUNCTIONED   	B			BF8R	O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			WP	07	410ER	1887 				17280257	L2722651A			THE PILOT REPORTED A MOMENTARY POWER LOSS.  A COMPLETE INSPECTION OF THE ENGINE AND ENGINE SYSTEMS FOUND NO ABNORMALTIES	.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999123100051	19991231	00051		1999	12	31	99ZZZX4641       	1	19991213	G	2721	03112	SWITCH          	STEC        																COCKPIT	CRACKED         	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	99										CONCERNED ABOUT THE QUALITY OF TRIM SWITCH.  THIS IS THE THIRD SWITCH TO HAVE BEEN INSTALLED IN SAME AIRCRAFT.																			 
1999123100053	19991231	00053	GL  	1999	12	31	99ZZZX4643       	1	19991020	G	3230	AN8224D	FITTING         			AMTR  	GLASAR	GLASAIRSHII 	05620TB	GL  										MLG	SHEARED         	H				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			GL	03	86D	1091 				577				ON LANDING, AIRCRAFT'S NOSE GEAR COLLAPSED, PROPELLER STRUCK RUNWAY THEN MAIN LANDING GEAR COLLAPSED.  INSPECTION OF LEF	T MAIN LANDING GEAR FOUND AN822-4D FITTING SHEARED AT HYDRAULIC ACTUATING CYLINDER.  IT APPEARED THE SIDE BRACE ARM RUBB	ED AND PRELOADED THE DOWN PRESSURE LINE CAUSING THE FITTING TO BREAK IN A SHEAR ACROSS THE THREADS.  THIS AREA IS DIFFIC	ULT TO INSPECT WITH THE MAIN GEAR STRUT FAIRING INSTALLED.  SUBMITTER RECOMMENDED THAT AT CONDITION INSPECT, REMOVE FAIR	ING AND INSPECT FOR POTENTIAL PRELOAD IN THIS AREA.		1	L	7	1 	3O			RT	EXPA    					 
1999123100054	19991231	00054	NE  	1999	12	31	99ZZZX4644       	2	19990912	G	7240		HOUSING         		213114905   						LYC   	ALF502	ALF502R5    	41580	NE  					COMBUST SECTION	FRACTURED       	B	P		TX7Y	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	35					992497200044		LF05867A			DURING GROUND (TEST CELL) TEST, ENGINE S/N LF05867A, A LOUD BANG WAS HEARD AND SPARKS WERE OBSERVED.  THE ENGINE WAS THR	OTTLED BACK TO IDLE AND SHUT DOWN IAW MM (286-1) PROCEDURES.  INSP OF ENG REVEALED THE CUSTOMER AIR BLEED MANIFOLD HAD A	 SKIN FRACTURE AT 5 O'CLOCK POSITION.  THE RESULTING HOLE WAS APPROX 2 INCHES IN DIA.  FRACTURE DID NOT START AT ANY EDG	ES OF WELD SEAMS.  NO OTHER DAMAGE FOUND AT STRIP-DOWN.  ENG HAD BEEN  RUNNING FOR 45 MINS WHEN INCIDENT OCCURRED.  ALL 	PARAMETERS NORMAL, NO HOT STARTS EXPERIENCED.  AIR BLEED MANIFOLD IS PART OF COMBUSTOR HOUSING (PRESS VESSEL) THAT DIREC	TS COMPRESSOR OUTLET AIR TO THE ACFT SERVICES.						4	F			E6NE				 
1999123100055	19991231	00055	GL  	1999	12	31	99ZZZX4645       	2	19990810	G	7321	23065104	FCU             			BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	FAILED          	D				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	99	187AA				319211	3969				DURING AN UNSCHEDULED REPLACEMENT OF THE FUEL CONTROL, INSTALLED A TSO ZERO FUEL CONTROL, SN 319211.  GROUND RAN ACFT, C	OMPLETED LEAK CHECK AND ATTEMPTED TO SHUTDOWN.  THE ENGINE WOULD NOT TURN OFF.  SEVERAL OTHER  ATTEMPTS MADE TO SHUTDOWN	 WITH NO RESULTS.  THE FUEL VALVE WAS SUBSEQUENTLY TURNED OFF AND THE ENGINE SHUT OFF.  FUEL CONTROL RIGGING CHECK C/W. 	 NO DEFECTS FOUND.  REPLACED DEFECTIVE FUEL CONTROL, ENGINE FUNCTIONAL CHECK OK.  DEFECTIVE FUEL CONTROL, SN 319211 WAS 	RECENTLY OVERHAULED ON 8-9-99.		1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999123100056	19991231	00056		1999	12	31	99ZZZX4646       	1	19991109	G	2761	654494710	ACTUATOR HOUSING		65448517    															SPOILER	CRACKED         	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		45036	32336		4383	737*				HOUSING IS CRACKED ON SIDE OPPOSITE OF PORTS.  OVERSTRESSED, FATIGUE, AND/OR POSSIBLE FLAW IN HOUSING DESIGN.																			 
1999123100057	19991231	00057	NM  	1999	12	31	99ZZZX4647       	1	19991109	G	2910	30001764	HOUSING         		30001300009A	BOEING	747   	747*        		NM  										HYDRAULIC SYSTEM	CRACKED         	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					P353					HOUSING HAS VISIBLE LEAKAGE AT BASE OF FILTER BOSS JUST BELOW THE PRESSURE PORT (P1 OR 4) DUE TO CRACKING.  STRESS CRACK	ING/DESIGN FLAW AT MANUFACTURING.  C/W CMM 27-10-01, TEMPORARY REV NR 27-07 UNTIL EXISTING LOWER PISTON HOUSING ASSY IS 	REPLACED WITH NEW 41007178-102.				2	L	7	4 	4F			RT	A20WE   					 
1999123100058	19991231	00058	NM  	1999	12	31	99ZZZX4648       	1	19991118	G	3240	B2701	VALVE           		B270014     	BOEING	727   	727         	UTILSYS	NM  										BRAKE	CRACKED         	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					2887					BODY IS CRACKED IN THE PRESSURE AND BRAKE PORTS.  FATIGUE, OVERSTRESSED.						2	L	7	3 	4J			RT	A3WE    					 
1999123100059	19991231	00059	NM  	1999	12	31	99ZZZX4649       	1	19991112	G	5510	69778551	SPRING          		65C347512   	BOEING	737   	737*        		NM  										HORIZONTAL STAB	CRACKED         	B			IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01		18876			00417					SPRINGS, PN 69-77855-1, ARE BROKEN IN THE AUXILIARY BRAKE SYSTEM.  IMPROPER HEAT-TREATING, AUSTENITE, FATIGUE, AND INCRE	ASED SPRING COIL STRESSES.					2	L	7	2 	4F			RT	A16WE   					 
1999020500011	19990205	00011	NE  	1999	2	5	99ZZZX465        	3	19990114	G	6111	A32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		2408 						HL247		PROPELLER, S/N HL247, WAS RETURNED FOR LOOSE BLADE.  AFTER DISASSEMBLY, INSPECTION REVEALED 1 LOOSE A-3204-1 PRELOAD SET	 SCREW.  THE SCREW WAS BACKED OUT APPROXIMATELY .50 INCH WITH THE B-3368 LOCKNUT STILL ATTACHED TO THE SCREW.  ALSO, 2 B	ROKEN A-3204-1 SCREWS.  THE SCREWS WERE BROKEN INTO TWO PIECES WITH THE B-3368 LOCKNUTS STILL ATTACHED TO THE INBOARD SE	CTIONS OF THE SCREWS.  ALL PRELOAD PLATE COMPONENTS WERE REMOVED, SENT TO HARTZELL ENGINEERING FOR EVALUATION AND REPLAC	ED WITH NEW.		2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999123100060	19991231	00060	NM  	1999	12	31	99ZZZX4650       	1	19991115	G	3240	511531	HOUSING         	PNEUDRAULICS	5059        	BOEING	737   	737*        		NM  										SHUTTLE VALVE	DAMAGED         	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					3325					HOUSING HAS HOLES IN TWO OF THE ATTACHMENT BOLT HOLES ADJACENT TO THE PLUG THREADS.  WEAK AREA OF HOUSING, FATIGUE.						2	L	7	2 	4F			RT	A16WE   					 
1999123100061	19991231	00061	NM  	1999	12	31	99ZZZX4651       	1	19991115	G	3240	511531	HOUSING         	PNEUDRAULICS	5059        	BOEING	737   	737*        		NM  										SHUTTLE VALVE	DAMAGED         	B	S		IU6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01					3177					HOUSING HAS HOLES IN ONE OF THE ATTACHMENT BOLT HOLES ADJACENT TO THE PLUG THREADS. WEAK AREA OF HOUSING						2	L	7	2 	4F			RT	A16WE   					 
1999123100062	19991231	00062	CE  	1999	12	31	99ZZZX4652       	1	19991208	G	2822	5100003	PUMP            			CESSNA	172   	172R        	2072401	CE  										FUEL BOOST	FAILED          	B			BF8R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	07	9559D	499  			0695	17280488				THE ELECTRIC FUEL PUMP FAILED AND CAUSED THE CIRCUIT PROTECTION DEVICE TO TRIP.  SUBMITTER STATED THIS IS A COMON PROBLE	M ON THIS FLEET OF 172R AIRCRAFT.					1	H	7	1 	3O			NT	3A12    					 
1999123100063	19991231	00063	SO  	1999	12	31	99ZZZX4653       	2	19991124	G	8520	643627	CRANKSHAFT      			PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360KB   	17025	SO  					LT ENGINE	CRACKED         	B			W6NR	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			GL	25	8375N	864  				348133076	268155R			TRANSIT ACFT LANDED EN ROUTE WITH LT ENGINE SHUT DOWN DUE IN-FLIGHT OIL LEAK.  CLEANED ENG AND DID A SHORT RUN AND FOUND	 OIL COMING FROM PROP SHAFT AREA.  REMOVED PROP AND CHECKED O-RING AND IT CHECKED OK.  UPON FURTHER INVEST, APPEARED TO 	BE A CRACK BEHIND PROP FLANGE OF CRANKSHAFT.  A SMALL CHIP WAS FOUND INSIDE CRANKSHAFT WITH POSSIBLE CRACK.  DYE CHECK O	N OUTSIDE INDICATED CRACK APPROX ONE-FOURTH OF THE WAY AROUND.  PAINT CLEANED OFF AND SECOND DYE CHK INDICATED CRACK.  E	NG 27.7 HRS OUT OF REPAIR FOR PROP STRIKE AND CRANKSHAFT INSPECTED AT THAT TIME PER LOG ENTRY.  ENG O/H 4-2-93, 864.2 HR	S.	1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999123100065	19991231	00065	CE  	1999	12	31	99ZZZX4655       	1	19991208	G	2822	5100003	PUMP            			CESSNA	172   	172R        	2072401	CE  										FUEL BOOST	FAILED          	B			BF8R	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			WP	07	421ER	1320 			0879	17280638				THE ELECTRIC FUEL PUMP FAILED AND CAUSED THE CIRCUIT PROTECTION DEVICE TO TRIP.  SUBMITTER STATED THIS A COMMON PROBLEM 	ON THIS FLEET OF 172R AIRCRAFT.					1	H	7	1 	3O			NT	3A12    					 
1999123100066	19991231	00066	CE  	1999	12	31	99ZZZX4656       	1	19991208	G	2822	510003	PUMP            			CESSNA	172   	172R        	2072401	CE  										FUEL BOOST	FAILED          	B			BF8R	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			WP	07	407ER	89   			0959	17280234				THE ELECTRIC FUEL PUMP FAILED AND CAUSED THE CIRCUIT PROTECTION DEVICE TO TRIP.  SUBMITTER STATED THIS IS A COMMON PROBL	EM ON THIS FLEET OF 172R AIRCRAFT.					1	H	7	1 	3O			NT	3A12    					 
1999123100067	19991231	00067	CE  	1999	12	31	99ZZZX4657       	1	19991208	G	2822	5100003	PUMP            			CESSNA	172   	172R        	2072401	CE  	LYC   	IO360 	IO360L2A    		EA  					FUEL BOOST	FAILED          	B			BF8R	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			WP	07	405ER	120  			1049	17280285				THE ELECTRIC FUEL PUMP FAILED AND CAUSED THE CIRCUIT PROTECTION DEVICE TO TRIP.  SUBMITTER STATED THIS IS A COMMON PROBL	EM ON THIS FLEET OF 172R AIRCRAFT.					1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999123100068	19991231	00068	NE  	1999	12	31	99ZZZX4658       	2	19991209	G	7230	808145	RETAINING PLATE 								PWA   	JT8   	JT8D15A     	52051	NE  					COMPRESSOR	NOT INSTALLED   	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	99							P700576			DURING DISASSEMBLY OF ENGINE FOR SALVAGE OF USEABLE PARTS, THE MECHANICS NOTED THE 1ST STAGE COMPRESSOR BLADE RETAINING 	PLATE WAS NOT INSTALLED.  ENGINEERING REVIEW AND FURTHER RESEARCH FAILED TO CONFIRM THIS ENGINE WAS NOT OPERATED WITHOUT	 THIS PART INSTALLED.  NOTIFICATION WAS MADE TO THE CURRENT OWNER OF THIS ENGINE; THE PRATT & WHITNEY SPARES MATERIAL LO	GISTICS (SML) ORGANIZATION, FOR FURTHER INVESTIGATION.								4	F			E2EA				 
1999123100069	19991231	00069	CE  	1999	12	31	99ZZZX4659       	1	19991211	G	2710		CONTROL CABLE   			CESSNA	310   	310         	2074202	CE  										AILERON	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99										DURING ROUTINE 100-HOUR ANNUAL, NOTED AILERON CABLE TENSION WAS SLACK ENOUGH THAT THE CABLES WERE RUBBING ON THE STRINGE	R WHERE THEY PASSED THROUGH (BELOW THE FLOOR UNDER THE COCKPIT).  THE TENSION WAS SO LOW AS NOT TO READ ON THE TENSIONME	TER.  THE CABLES WERE TIGHTENED IAW THE MFG DATA.				1	L	7	2 	3O			RT	3A10    					 
1999020500012	19990205	00012	NE  	1999	2	5	99ZZZX466        	3	19990112	G	6111	S32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		2062 						HL57		PROPELLER, S/N HL57, WAS RETURNED FOR SERVICE, BULLETINS 5 AND 14.  AFTER DISASSEMBLY, INSPECTION REVEALED 1 BROKEN A-32	04-1 PRELOAD SET SCREW.  THE B-3368 LOCKNUT WAS STILL ATTACHED TO THE INBOARD SECTION OF THE A-3204-1 SCREW.  THE SCREW 	WAS REMOVED, SENT TO HARTZELL ENGINEERING FOR EVALUATION AND REPLACED WITH NEW.				2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999123100070	19991231	00070	CE  	1999	12	31	99ZZZX4660       	1	19991211	G	2710		CONTROL CABLE   			CESSNA	320   	320         	2074502	CE  										AILERON	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99										DURING ROUTINE 100-HOUR ANNUAL, NOTED AILERON CABLE TENSION WAS SLACK ENOUGH THAT THE CABLES WERE RUBBING ON THE STRINGE	R WHERE THEY PASSED THROUGH (BELOW THE FLOOR UNDER THE COCKPIT).  THE TENSION WAS SO LOW AS NOT TO READ ON THE TENSIONME	TER.  THE CABLES WERE TIGHTENED IAW THE MFG DATA.				1	L	7	2 	3O			 	3A25    					 
1999123100071	19991231	00071	SO  	1999	12	31	99ZZZX4661       	1	19991209	G	2432	4076	BATTERY         	SAFT        		GULSTM	G1159 	G1159       	3953505	SO  										E/E BAY	WRONG PART      	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	99										SAFT MODEL 4076 BATTERIES WERE FOUND INSTALLED IN SEVERAL G-11/G-III AIRCRAFT.  AFTER REVIEW OF THE AIRCRAFT MANUFACTURE	R'S DOCUMENTS AND TALKING DIRECTLY WITH THE MANUFACTURER, NOTHING COULD SUBSTANTIATE THIS PARTICULAR BATTERY BEING INSTA	LLED IN THIS MODEL AIRCRAFT.  THE CORRECT BATTERY FOR A G-II OR ANON-VSCF (D.C.) G-III IS THE MARATHON MODEL NR MA-5 OR 	CA-5 19 CELL BATTERY.  THE CORRECT BATTERY FOR THE VSCF (A.C.) G-III IS THE SAFT 4076-11 20 CELL BATTERY.			2	L	7	2 	4F			RT	A12EA   					 
1999123100072	19991231	00072	CE  	1999	12	31	99ZZZX4662       	1	19990301	G	2432	G25	BATTERY         	GILLBATT    		CESSNA	172   	172         	2072402	CE  										E/E BAY	FAILED          	H				O				OTHER                   				H	G	J	ELECT. POWER LOSS-50 PC   	MULTIPLE FAILURE          	WARNING INDICATION        	NR	NOT REPORTED   	1			SW	99	9117B				G01815685	36617				BATTERY INSTALLED MARCH, 1999.   IN NOVEMBER, 1999, BATTERY DEVELOPED AN INTERNAL SHORT WHICH CAUSED AN OVERLOAD IN THE 	AIRCRAFT ELECTRICAL SYSTEM.  SHORT CAUSED DESTRUCTION OF THE AIRCRAFT VOLTAGE REGULATOR, AND BLEW THE GENERATOR FUSE CAU	SING LOSS OF ELECTRICAL POWER IN-FLIGHT AFFECTING ALL COMMUNICATIONS AND NAVIGATION SYSTEMS.  AIRCRAFT LANDED SAFELY.  L	OCAL MECHANIC REPORTED THIS IS THE THIRD GILL MODEL G-25 BATTERY HE HAS SEEN GO BAD THIS YEAR WITH AROUND 6 TO 9 MONTHS 	TIME IN SERVICE. TOTAL TIME ON PART AT TIME OF FAILURE:  69 HOURS, AND EIGHT MONTHS TIME IN SERVICE.		1	H	7	1 	3O			NT	3A12    					 
1999123100074	19991231	00074	NE  	1999	12	31	99ZZZX4664       	1	19991006	G	6320	SB1060102	BEARING         		643520400065	SKRSKY	S64   	S64E        	8142604	NE  										GEARBOX	FAILED          	B		A	JYDR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			NM	09	194AC	792  			EAC1727	64017				DUPLEX BEARING, PN SB1060-102, SN EAC 1727, TT OF 792.0 HRS, FAILED IN MGB, PN 6435-20400-065, SN A6-037, LEAVING LARGE 	FRAGMENTS OF FERROUS METAL IN SUMP AND SUMP SCREEN.  FURTHER INSP INDICATED BOTH INNER-BEARING RACES OF SB1060-102 DUPLE	X BEARING INSTALLED ON RT INTERMEDIATE BEVEL GEAR SHAFT FAILED PREMATURELY DUE TO EXCESSIVE SPALLING.  LOWER BEARING AS 	INSTALLED ON THE INTERMEDIATE BEVEL GEAR SHAFT SHOWED MORE SPALLING THAN INNER-BEARING RACE INSTALLED IN THE UPPER POSIT	ION.  MAIN GEARBOX PN 6435-20400-065, SN A6-037, INSTALLED FOR LAST 792.0 FLIGHT HRS, WHOSE PRIMARY MISSION HAS BEEN LOG	GING.  SUBMITTER STATED THIS IS 3RD MGB THE SB1060-102 DUPLEX BEARING WAS DETERMINED TO BE PRIMARY CAUSE OF FAILURE SINC	2	G	7	2 	4U				H4EA    					 
1999123100315	19991231	00315	SO  	1999	12	31	99ZZZX4666       	1	19991108	G	7120		MOUNT           			PIPER 	PA25  	PA25235     	7102504	SO  										LT ENGINE	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	9649P	4756 				257556008				UPPER LEFT ATTACH POINT .25 INCH AFT OF WASHER IN BACK OF MOUNT RUBBER.  NO PART OF BREAK WAS CLOSER THEN .25 INCH OF AN	Y WELD.  BREAK WAS IN PROCESS FOR SOME TIME.					1	L	7	1 	3O				2A10    					 
1999123100316	19991231	00316	NE  	1999	12	31	99ZZZX4667       	3	19991102	G	6111		SHIELD          													HARTZL	HCE4A	HCE4A3I     	NE  	PROP BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01					D5133			HJ183A		EROSION SHIELD DEBOND, OUT OF LIMITS, NR 4 BLADE.  REMOVED AND REPLACED EROSION SHIELD IAW PROCESS SPECIFICATION PROCEDU	RE 001 AS APROVED BY FAA ADMINISTRATOR.															5	C	P10NE	 
1999123100317	19991231	00317	NE  	1999	12	31	99ZZZX4668       	3	19991102	G	6111		SHIELD          													HARTZL	HCE4A	HCE4A3I     	NE  	PROP BLADE	CRACKED         	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			3798 		D5133			HJ536		CRACKED EROSION SHIELD BLADE NR 1.  REMOVED AND REPLACED EROSION SHIELD ON BLADE NR 1.  TOUCHED UP PAINT AND STATIC BALA	NCED PROPELLER IAW MFG CMM.															5	C	P10NE	 
1999123100318	19991231	00318	NE  	1999	12	31	99ZZZX4669       	3	19991124	G	6111		SHIELD          													HARTZL	HCE4A	HCE4A3I     	NE  	PROP BLADE	DEBONDED        	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01					D5133			HJ941		EROSION SHIELD DEBOND BLADE NR 2.  REPLACED EROSION SHIELD BLADE NR 2, S/N 791MA.  RE-ASSEMBLED PROPELLER, SET BLADE ANG	LE, STATIC BALANCED PROPELLER IAW MFG CMM.															5	C	P10NE	 
1999020500013	19990205	00013	NE  	1999	2	5	99ZZZX467        	3	19990112	G	6111	A32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05								HL113		PROPELLER, S/N HL113, WAS RETURNED FOR BROKEN PRELOAD SET SCREW.  AFTER DISASSEMBLY, INSPECTION REVEALED 1 BROKEN A-3204	-1 PRELOAD SET SCREW.  THE B-3368 LOCKNUT WAS STILL ATTACHED TO THE INBOARD SECTION OF THE A-3204-1 SCREW.  THE SCREW AN	D SPRING WERE REMOVED, SENT TO HARTZELL ENGINEERING FOR EVALUATION AND REPLACED WITH NEW.  THE C-6066-1 PRELOAD PLATE TH	READ WAS DAMAGED, BUT WITHIN ACCEPTABLE LIMITS AND THE PLATE WAS REPAIRED AND RETURNED TO SERVICE.			2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999123100319	19991231	00319	NE  	1999	12	31	99ZZZX4670       	3	19991203	G	6111		SHIELD          													HARTZL	HCE4A	HCE4A3I     	NE  	PROP BLADE	CRACKED         	B			GLBR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	01			1446 		D5133			HJ1023		EROSION SHIELD CRACKED ON NR 3 BLADE, S/N 1776.  REPLACED EROSION SHIELD BLADE NR 3, S/N 1776, TOUCHED UP PAINT, STATIC 	BALANCED PROPELLER IAW MFG CMM.  REPLACED WORN SLIP RING WITH REPLATED, REPLACED BETA RING WITH NEW.															5	C	P10NE	 
1999123100320	19991231	00320		1999	12	31	99ZZZX4671       	1	19991109	G	3246	2605509	WHEEL           	BENDIX      	260356111   															MLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19										FOUND CRACK ON BOLT HOLE IN OUTBOARD WHEEL HALF, POSSIBLY DUE TO METAL FATIGUE.																			 
1999123100321	19991231	00321	SO  	1999	12	31	99ZZZX4672       	2	19991210	G	8520	649895	CRANKSHAFT      			BEECH 	58    	58          	1152740	CE  	CONT  	O520  	IO520C      	17032	SO  					ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03	6AC				I159922N	TH267	561925			100 HOURS AFTER INSTALLATION OF A NEW TCM CRANKSHAFT AT OVERHAUL, THE ENGINE EXPERIENCED A CATASTROPHIC FAILURE.  DURING	 TEAR-DOWN, ONE COUNTERWEIGHT ROLLER, ONE RETAINING PLATE, AND ONE RETAINING RING WERE FOUND UNDAMAGED AMONG THE DEBRIS 	IN THE OIL SUMP.  THE MARK ON THE ADJACENT CONNECTING ROD SHOWED THE IMPRINT OF THE ROLLER.  COUNTERWEIGHTS WERE INSTALL	ED AT THE FACTORY AND CAME AS PART OF THE NEW ASSY.			1	L	7	2 	3O	3	O		3A16    	E5CE				 
1999123100322	19991231	00322	CE  	1999	12	31	99ZZZX4673       	1	19991208	G	2910	631700350	TUBE            			CESSNA	525   	525         	2076601	CE  										HYDRAULIC SYSTEM	FAILED          	G				O	K			OTHER                   	NONE                    			J			WARNING INDICATION        			NR	NOT REPORTED   	1			EA	21	49CJ	2413 				5250049				INVESTIGATED 'OCCURRENCE' AND RECEIVED REPORT FROM MAINTENANCE PERSONNEL THAT A  MAIN SYSTEM HYDRAULIC FAILURE OCCURRED 	IN-FLIGHT.  LANDING GEAR EXTENDED VIA EMERGENCY SYSTEM.  AIRCRAFT LANDED WITHOUT INCIDENT WITH NO SPEED BRAKES, THRUST R	EVERSERS (ATTENTUATORS) AND ZERO DEGREE FLAPS.  MAINTENANCE FOUND HYDRAULIC TUBE BETWEEN THE HIGH PRESSURE FILTERS AND B	YPASS VALVE CRACKED IN THE 30 DEGREE BEND RADIUS, OUTBOARD OF J-BOX.  TUBE WAS FOUND TO BE PROPERLY SECURED WITH NO APPA	RENT ABNORMAL STRESS POINTS NOTED.  POSSIBLE MATERIAL DEFECT.		1	L	7	2 	4F			RT	A1WI    					 
1999123100323	19991231	00323	EA  	1999	12	31	99ZZZX4674       	2	19991203	G	7414	10382681	CONDENSER       		D6LN3000    	PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					MAGNETO	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	21	300VF				CODE9804	317852050				REMOVED CONDENSER, P/N 10-382681, WITH DATE CODE 9804, AND REPLACED WITH CODE 9920.  SUBMMITTER STATED NUMEROUS FAILURES	 OF THIS CONDENSER HAVE HAPPENED LATELY (12 MONTHS).					1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999123100325	19991231	00325	NE  	1999	12	31	99ZZZX4676       	2	19991209	G	7230	772568QQ	BOLT            								PWA   	JT8   	JT8D7B      	52053	NE  					COMPRESSOR	FAILED          	B			WG4R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SO	19							657514			PMA BOLT, P/N 772568QQ, REPLACEMENT FOR OEM BOLT, P/N 772568, FAILED AFTER 780.0 HOURS AND 1,169 CYCLES IN SERVICE.  BOL	T FRACTURED CAUSING HEAD TO BE INGESTED INTO THE N-2 COMPRESSOR DRIVE TURBINE WHERE EXTENSIVE DAMAGE WAS INFLICTED.  BOL	T WAS FROM AFFECTED BATCHES AS DESCRIBED IN FLIGHT STANDARDS INFORMATION BULLETIN FOR AIRWORTHINESS NUMBER FSAW 99-07.									4	F			E2EA				 
1999123100326	19991231	00326	SW  	1999	12	31	99ZZZX4677       	1	19991228	G	2822	1C274	BOOST PUMP      			BELL  	206   	206B3       	1181506	SW  										FUEL SYSTEM	FAILED          	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09	198H		59   		61002	3647				HORIZON HELICOPTERS HAD NOTICED FUEL CONTAMINATION AFTER A BOOST PUMP FAILURE ON 4 OCCASIONS.  THE FILTER IS FULL OF BLA	CK CARBON.  SUBMITTER BELIEVES THE BOOST PUMP INTERNAL BREAKDOWN IS THE SOURCE OF CONTAMINATION AND HAS SAMPLE PUMP AND 	FILTER AT FACILITY FROM THIS AIRCRAFT.				1	G	7	1 	3U				H2SW    					 
1999123100328	19991231	00328	CE  	1999	12	31	99ZZZX4679       	1	19991207	G	2821	45AS480141	FILTER ASSY     			MTSBSI	MU300 	MU300       	5780602	CE  										FUEL SYSTEM	MISINSTALLED    	B		A	FGQR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	01	10NM					A016SA				DURING A NORMAL INSPECTION, BOTH FUEL STRAINERS WERE FOUND INSTALLED BACKWARDS.  WITH FUEL FLOW IN THE WRONG DIRECTION, 	THE BYPASS ANNUNCIATOR WOULD BE INOPERATIVE.  THIS WAS THE FIRST MAJOR INSPECTION OF THIS AIRCRAFT BY THIS FACILITY.  TH	E PROBLEM WAS DETECTED BY THE CHIEF INSPECTOR.  THE STRAINS WERE INSTALLED PREVIOUSLY BY PERSONS UNKNOWN.				2	H	7	2 	4F			RT	A14SW   					 
1999020500014	19990205	00014	NE  	1999	2	5	99ZZZX468        	3	19990115	G	6111	A32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05								HL255		PROPELLER, S/N HL255, WAS RETURNED FOR SB 5 AND SB 14 COMPLIANCE.  AFTER DISASSEMBLY, INSPECTION REVEALED 1 BROKEN A-320	4-1 PRELOAD SET SCREW.  THE SCREW WAS BROKEN INTO TWO PIECES WITH THE B-3368 LOCKNUT STILL ATTACHED TO THE SCREW.  DAMAG	E TO THE C-6066-1 PRELOAD PLATE THREADS WAS BEYOND MANUAL LIMITS.  THE PRELOAD PLATE AND SET SCREW WERE RETIRED FROM SER	VICE.			2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999123100329	19991231	00329	SO  	1999	12	31	99ZZZX4680       	2	19991207	G	8530	654960A1	CYLINDER        			CESSNA	182   	182P        	2075816	CE  	CONT  	O470  	O470U       	17026	SO  					NR 3	WORN            	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			GL	23	953CC	472  				18264109	813458R			DURING A ROUTINE COMPRESSION CHECK, THE NR 3 CYLINDER WAS FOUND LEAKING EXCESSIVELY PAST THE INTAKE VALVE.  THE EXHAUST 	VALVE AND PISTON RINGS WERE REMOVED.  CYLINDER WAS FOUND TO HAVE A DEFORMED INTAKE VALVE FACE, A WORN OUT EXHAUST VALVE,	 AND GUIDE AND NO CHOKE LEFT IN THE CYLINDER.				1	H	7	1 	3O	3	O	NT	TA13    	E273				 
1999123100330	19991231	00330	CE  	1999	12	31	99ZZZX4681       	1	19991118	G	3260		SWITCH          			CESSNA	310   	310R        	2074245	CE  										NLG	OUT OF ADJUST   	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	07	6122C					310R1290				FSD - NOSE GEAR NOT SHOWING DOWN AND LOCKED.  LANDED, NO PROBLEM.  MAINTENANCE JACKED AIRCRAFT, ADJUSTED DOWNLOCK SWITCH	.  OPS CHECKED OK.					1	L	7	2 	3O				3A10    					 
1999123100333	19991231	00333	SO  	1999	12	31	99ZZZX4684       	2	19991129	G	8530		ROD             			CESSNA	120   	120         	2071402	CE  	CONT  	C85   	C8512F      	17008	SO  					NR 4 CYLINDER	FAILED          	D				O				OTHER                   				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		NR	NOT REPORTED   	1			EA	13	76470		120  			10902	24500612			PILOT REPORTED LOSS OF OIL PRESSURE. THIS WAS FOLLOWED BY ABNORMAL ENGINE SOUNDS.  UPON INSPECTION, THE ENGINE TURNED FR	EELY, THE CABLE WAS FOUND CRACKED ABOVE THE NR 4 CYLINDER.  CRACK APPEARS TO HAVE BEEN CAUSED BY A BROKEN CONNECTING ROD	.				1	H	7	1 	3O	3	O		A768    	E233				 
1999123100334	19991231	00334	CE  	1999	12	31	99ZZZX4685       	1	19991228	G	3230	MS203921C53	PIN             			BEECH 	76    	76          	1153005	CE  										MLG	FAILED          	B			IC1R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	23	6627X					ME215				PIN HOLDING MLG SHOCK ABSORBER TO LOWER MLG TRAILING LINK SEPARATED DUE TO FAILURE OF PART IN BOX 6 WHICH HELD MISSING P	ART IN PLACE RESULTING IN PARTIAL FOLD-UP OF RIGHT MLG WHICH SUBSTANTIALLY DAMAGED AIRCRAFT.  SUBMITTER RECOMMENDED INSP	ECTION OF ALL LANDING GEAR CLEVIS LOCK PINS FOR WEAR AND CONDITION BY WEAR ON ALL MOVING PARTS, HOUSINGS, AND BEARINGS. 	 REPLACED SUBJECT PIN AT 200-HOUR INTERVALS.			1	L	7	2 	3O				A29CE   					 
1999123100336	19991231	00336	SW  	1999	12	31	99ZZZX4687       	1	19991119	G	6510	E5731861	BLOWER ASSY     			BELL  	407   	407         		SW  										TAIL ROTOR	INOPERATIVE     	B			FKFR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03	2RW	205  				53319				MOTOR IN BLOWER ASSY IS OPERATIVE, HOWEVER, THE FAN CAME DISENGAGED FROM SHAFT.  THE FAN BUSHING WAS COMPLETELY WORN OUT	.  APPARENTLY, THE FAN BUSHING TO BLOWER MOTOR PIN IS POOR FIT.					1	G	7	1 	3U			O	H2SW    					 
1999123100337	19991231	00337	EU  	1999	12	31	99ZZZX4688       	1	19991115	G	3230	803682	DETECTOR        			AMD   	FALC90	FALCON900EX 	2730009	EU  										MLG	FAILED          	B			JU2R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	23	327K	459  				37				LANDING GEAR FAILED TO COME DOWN ON NORMAL EXTENSION.  USED EMERGENCY EXTENSION FOR GEAR DOWN, FOUND RIGHT MAIN GEAR DOO	R DETECTOR FAILED 28V TEST.  REMOVED AND REPLACED LEFT AND RIGHT MAIN GEAR DOOR DETECTOR.  RIGHT SIDE CHANGED AS PRECAUT	IONARY.  PERFORMED TEST FLIGHT, ALL SYSTEM OPS CHECKED NORMAL.				2	L	7	3 	4F			RT	A46EU   					 
1999123100338	19991231	00338		1999	12	31	99ZZZX4689       	1	19990922	G	3211		BRACKET         			AMTR  		ACROSPORTI  												RT MLG	BROKEN          	G	S			O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	15	118DM	433  				71180				ON LANDING, THE RIGHT MLG FORWARD ATTACH POINT BROKE.  GEAR FOLDED UNDER THE AIRCRAFT.									0 										 
1999020500015	19990205	00015	NE  	1999	2	5	99ZZZX469        	2	19990114	G	7311	RK25198A	OIL COOLER      		RK35783A    	FOKKER	F27   	F27MK400    	4990626	EU  	RROYCE	DART  	DART5357R   	54509	NE  					NR 1 ENGINE	FAILED          	D				A				UNSCHED LANDING         				K	J		FLUID LOSS                	WARNING INDICATION        		CL	CLIMB          	1			SO	05			1370 		NAYR433799		14803			SHORTLY AFTER TAKEOFF, FLIGHT CREW NOTICED THE NR 1 ENGINE OIL PRESSURE DROPPING.  AS CREW WAS RETURNING TO DEPARTURE AI	RPORT, NR 1 ENG LOW OIL PRESS LIGHT ILLUMINATED.  CREW SHUT DOWN NR 1 ENG AND MADE UNEVENTFUL SINGLE ENG LANDING; 1/2 HO	UR ELAPSED BETWEEN TAKEOFF AND PARKING.  POST-FLIGHT INSP REVEALED LARGE AMTS OF OIL ON LT NACELLE AND FUSELAGE WITH OIL	 DRAINING FROM ENG COWLING DRAINS.  AFTER REMOVING ENG COWLING AND WASHING OFF ENG OIL, ENG SERVICED WITH 8 QUARTS OF EN	G OIL AND MOTORED TO DETERMINE THE SOURCE OF OIL LEAK.  OIL WAS DRAINING FROM THE OIL COOLER AIR EXIT DUCT DRAIN HOLES. 	 THE OIL COOLER SUFFERED A RUPTURE OF ITS OIL TUBE MATRIX.	2	H	7	2 	4T	4	T		A817    	E297				 
1999123100339	19991231	00339	GL  	1999	12	31	99ZZZX4690       	3	19990929	G	6111		BLADE           			PIPER 	PA28  	PA28181     	7102807	SO  						MCAULY	1A170	1A170B*     	GL  	PROPELLER	FAILED          	H				A				UNSCHED LANDING         				D			INFLIGHT SEPARATION       			CL	CLIMB          	1			AL	03	30541	1326 				287990095		0A011		TWO MINUTES AFTER TAKEOFF, NR 2 BLADE SEPARATED 6 INCHES FROM TIP CAUSING SEVERE VIBRATION PUTTING THE AIRCRAFT ALMOST O	UT OF CONTROL. TOTAL TIME ON PROPELLER, 1,216.2 HOURS.  SUBMITTER RECOMMENDED PROPELLER OVERHAUL AT 1,000 HOURS.					1	L	7	1 	3O				2A13    		5	N	P857	 
1999123100340	19991231	00340		1999	12	31	99ZZZX4691       	1	19991201	G	7932	6320622BF	DIP STICK       								CONT  	O550  	IO550D      	17042	SO  					ENGINE OIL	MISMANUFACTURED 	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CE	07							284345R			THE LOCKING GROOVE IN DIP STICK IS IN WRONG LOCATION PREVENTING LOCKING RING ON TUBE FROM LOCKING DIP STICK IN TUBE PROP	ERLY.  DIP STICK MIGHT BLOW OUT CREATING OIL LEAK.										3	O			E3SO				 
1999123100341	19991231	00341	CE  	1999	12	31	99ZZZX4692       	1	19991101	G	7714	625886	GEAR            			CESSNA	182   	182Q        	2072732	CE  										TACHOMETER	FAILED          	D				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			WP	23	97084	65   				18266972				AIRCRAFT TACHOMETER FAILED IN CRUISE FLIGHT.  AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT.  TEAR-DOWN INDICATED TACH DRIV	E SHAFT BEVEL GEAR FAILED AT OIL PUMP INTERFACE DUE TO OVERHEAT CONDITION.  SEVERE GAULING OF SHAFT WAS NOTED.  REPLACEM	ENT OIL PUMP COVER HAD OIL INLET HOLE FORTY THOUSANDTHS BIGGER THAN ORIGINAL.				1	H	7	1 	3O			NT	3A13    					 
1999123100343	19991231	00343	SO  	1999	12	31	99ZZZX4693       	2	19991201	G	8530	639615	ROCKER ARM      			CESSNA	172   	172         	2072402	CE  	CONT  	O300  	O300A       	17022	SO  					NR 6 CYLINDER	FAILED          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	01	7452A	3750 	1550 			29552	14298DSA			NR 6 CYLINDER EXHAUST ROCKER ARM FAILED ON TAKEOFF, INBOARD SECTION CRACKED AT PUSHROD END OIL FEED HOLE AND APPROXIMATE	LY 180 DEGREES FROM THAT HOLE.  PART IS MAGNETIZED.					1	H	7	1 	3O	3	O	NT	3A12    	E253				 
1999123100344	19991231	00344	CE  	1999	12	31	99ZZZX4694       	1	19991020	G	2823	S15339	CONTROL CABLE   		S19032      	CESSNA	172   	172S        	2072439	CE  										FUEL SHUT-OFF	BROKEN          	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	686SP	263  				172S8097				DURING PRE-FLIGHT, PILOT PULLED THE FUEL SHUT-OFF CABLE OUT TO THE OFF POSITION AND THE CABLE CAME OUT OF ITS HOUSING. U	PON INSPECTION, THE CABLE WAS FOUND BROKEN AT THE FUEL SHUT-OFF VALVE LEVER.  THE CABLE WAS CLAMPED TIGHT AGAINST THE LE	VER AND WAS NOT ABLE TO MOVE FREELY WHEN THE LEVER WAS MOVED.  SUBMITTER STATED IT APPEARED TO HAVE BEEN BENT BACK AND F	ORTH UNTIL IT BROKE.			1	H	7	1 	3O			NT	3A12    					 
1999123100345	19991231	00345	CE  	1999	12	31	99ZZZX4695       	1	19991220	G	5523	MS35206251	SCREW           			CESSNA	310   	310R        	2074245	CE  										ELEVATOR	CORRODED        	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	09	5338C	15674				310R1544				SCREWS (P/N'S MS35206-251 AND MS35206-333) SECURING ELEVATOR TRIM TAB HORN, SEVERELY CORRODED AND RUSTED AWAY TO A THICK	NESS NO LARGER THAN A PENCIL LEAD.  THE SPANNER BLOCK THEY PASS THROUGH WAS CRACKED AND IN TWO PIECES WHEN REMOVED.					1	L	7	2 	3O				3A10    					 
1999123100346	19991231	00346	CE  	1999	12	31	99ZZZX4696       	1	19991220	G	5523	MS35206333	SCREW           			CESSNA	310   	310R        	2074245	CE  										ELEVATOR	CORRODED        	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	09	5338C	15674				310R1544				SCREWS (P/N'S MS35206-251 AND MS35206-333) SECURING ELEVATOR TRIM TAB HORN, SEVERELY CORRODED AND RUSTED AWAY TO A THICK	NESS NO LARGER THAN A PENCIL LEAD.  THE SPANNER BLOCK THEY PASS THROUGH WAS CRACKED AND IN TWO PIECES WHEN REMOVED.					1	L	7	2 	3O				3A10    					 
1999123100347	19991231	00347	NE  	1999	12	31	99ZZZX4697       	1	19991212	G	2910	SS48C2C163000	LINE            			SKRSKY	S76   	S76A        	8143006	NE  										HYDRAULIC SYSTEM	FAILED          	H				O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		NR	NOT REPORTED   	1			CE	09	5445J					760178				DURING FLIGHT, NR 2 HYDRAULIC SYSTEM PRESSURE FELL TO ZERO PSI AND WARNING LIGHT ILLUMINATED.  FLIGHT RETURNED TO AIRPOR	T AND LANDING GEAR WAS EXTENDED WITH EMERGENCY SYSTEM.  INSPECTION REVEALED NR 2 HDRAULIC SYSTEM PRESSURE LINE FROM HYDR	AULIC PUMP HAD FAILED ALLOWING ALL HYDRAULIC FLUID FROM NR 2 SYSTEM TO LEAK OUT.  STEEL BRAID COVERING HOSE WAS ABRADED 	WHERE LEAK ORIGINATED.			1	G	7	2 	3U				H1NE    					 
1999123100348	19991231	00348	CE  	1999	12	31	99ZZZX4698       	1	19991122	G	2720	03101965	SPRING          			CESSNA	172   	172R        	2072401	CE  										RUDDER	BROKEN          	B		A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	03	381ES	1509 				17280081				FOUND LEFT RUDDER RETURN SPRING BROKEN AT RUDDER PEDDLE ATTACH POINT.  SUBMITTER STATED THIS IS SECOND SPRING FOUND BROK	EN ON FLEET OF 4 AIRCRAFT.					1	H	7	1 	3O			NT	3A12    					 
1999123100349	19991231	00349	SO  	1999	12	31	99ZZZX4699       	2	19991213	G	7414	S6RN1225	MAGNETO         	BENDIX      		CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  					LEFT	FAILED          	D				O				OTHER                   				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			NE	05	995RA	8    			H059916F	U20604252	579261			PILOT REPORTED MINOR ENGINE ROUGHNESS IN-FLIGHT AT HIGH ALTITUDES.  IN-FLIGHT MAGNETO CHECK SHOWED MAGNETO ON LEFT SIDE 	TO BE COMPLETELY DEAD.  POINTS AND ROTOR AND CONDENSER ARE OK.					1	H	7	1 	3O	3	O		A4CE    	E5CE				 
1999020500016	19990205	00016	NE  	1999	2	5	99ZZZX470        	3	19990112	G	6111	A32041	SCREW           			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		767  						HL134		PROPELLER, S/N HL134, WAS RETURNED FOR LOOSE BLADE.  AFTER DISASSEMBLY, INSPECTION REVEALED ONE BROKEN A-3204-1 PRELOAD 	SET SCREW.  THE SCREW WAS BROKEN INTO TWO PIECES WITH THE B-3368 LOCKNUT STILL ATTACHED TO THE INBOARD SECTION OF THE BR	OKEN A-3204-1 SCREW.  ALL SIX B-3368 LOCKNUTS, SIX A-3204-1 SET SCREWS, SIX C-6066 PRELOAD PLATES, SIX A-6406 CAPS, SIX 	A-6404 SPRINGS, AND SIX A-6405 PLUGS WERE REMOVED, SENT TO HARTZELL ENGINEERING FOR EVALUATION AND REPLACED WITH NEW.			2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999123100351	19991231	00351	SW  	1999	12	31	99ZZZX4701       	1	19991025	G	6220	500N7201	CABLES          			HUGHES	500N  	500N        	3027374	SW  										MAIN ROTOR	FRACTURED       	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	23	904PD	4    				LN032				DURING POST-CRASH EXAMINATION OF THE ANTI-TORQUE CONTROL SYSTEM, FRACTURES WERE FOUND OF THE PUSH/PULL TYPE THRUSTER CON	TROL CABLES P/N 500N7201-5 AND -37.  THE FORWARD CABLE FRACTURED AT THE SWIVEL BALL JOINT ALLOWING THE HOUSING TO SEPARA	TE BY 2.95 INCHES.  RIGHT PEDAL INPUT CAUSED BOWING OF THE INTERNAL CABLE/WIRE AND NO THRUSTER DIRECTION CHANGE.  SB AND	 AD TO BE ISSUED.			1	G	7	1 	3U			NC	H3WE    					 
1999123100352	19991231	00352	NM  	1999	12	31	99ZZZX4702       	1	19991110	G	7330	92024553	HOSE            			PIPER 	PA60  	PA60600     	7106001	NM  										FUEL INDICATOR	LEAKING         	H				O				OTHER                   				K	B		FLUID LOSS                	SMOKE/FUMES/ODORS/SPARKS  		CL	CLIMB          	1			GL	07	6896B					600919816126				CMH - FUEL SMELL IN CABIN AFTER TAKEOFF. FOUND HOLE IN FUEL HOSE GOING TO 3-IN-1 GAUGE COPILOT'S  INSTRUMENT PANEL.  REM	OVED AND REPLACED BOTH FUEL PRESSURE HOSES.  OPS CHECKED GOOD.					1	M	7	2 	3O			RT	A17WE   					 
1999123100354	19991231	00354	NE  	1999	12	31	99ZZZX4704       	2	19991025	G	7320	BACC10GU107	CLAMP           			BOEING	767   	76733AER    	1385230	NM  	PWA   	4060  	PW4060      	52119	NE  					FADEC	CHAFED          	B			HN6R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	637TW					25403				INSPECTED NR 1 AND NR 2 ENGINE PYLONS FOR FADEC WIRING CHAFE THROUGH AT CLAMPS.  FOUND CONDITION ON NR 1 ENGINE AND NOT 	NR 2 ENGINE PYLON.  FADEC WIRING CHAFED THROUGH THE SHIELDING TO THE CORE WIRES AT TWO CLAMP LOCATIONS.  PER THE LETTER,	 DAMAGE TO THE WIRES APPEARED TO BE THE RESULT OF ABRASION BETWEEN THE WIRE BUNDLES AND THE SOFT DUCTILE CLAMP MATERIAL 	HAD ERODED AWAY TO EXPOSE ITS METAL ENDOSKELETON.			2	L	7	2 	4F	4	F	RT	A1NM    	E24NE				 
1999123100355	19991231	00355	NM  	1999	12	31	99ZZZX4705       	1	19991216	G	3242	2445902	CARRIER         	BFGOODRICH  	21565       	DHAV  	DHC8  	DHC8*       		NM  										NR 2 BRAKE	FAILED          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					0063					BRAKE ASSEMBLY, P/N 2-1575, FAILED PREMATURELY.  NR 2 CARRIER AND LINING ASSY BROKEN IN HALF.  SUBMITTER STATED THIS IS 	A CONTINUAL DISCREPANCY.  OEM PARTS INSTALLED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 2-1565.					2	H	7	2 	4T			RT	A13NM   					 
1999123100356	19991231	00356	NE  	1999	12	31	99ZZZX4706       	2	19991207	G	7230	2A0001	BEARING         			AIRBUS	320   	A320232     	3930326	EU  	IAE   	V2527 	V2527A5     		NE  					ENGINE	SPALLED         	B			RA1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05		2214 			PGGUAK0425		V10103			ENGINE REMOVED DUE TO M50 MATERIAL ON THE MAG CHIP DETECTORS.  DISASSEMBLY OF THE ENGINE REVEALED THE NR 4 BEARING EXHIB	ITED SPALLING DAMAGE ON THE OUTER RACE. THE BEARING WAS SUBMITTED TO THE LAB FOR ANALYSIS.  THE INVESTIGATION IS STILL I	N PROGRESS AT THIS AGENCY.				2	L	7	2 	4F	4	F	RT	A28NM   	E40NE				 
1999123100357	19991231	00357	NE  	1999	12	31	99ZZZX4707       	2	19991207	G	7230	2A0001	BEARING         			AIRBUS	320   	A320232     	3930326	EU  	IAE   	V2500 	V2500A1     		NE  					ENGINE	SPALLED         	B			RA1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05		881  			PGGUAK0495		V0262			ENGINE WAS REMOVED DUE TO M50 MATERIAL ON THE MAG CHIP DETECTORS.  DISASSEMBLY OF THE ENGINE REVEALED THE NR 4 BEARING E	XHIBITED SPALLING DAMAGE ON THE OUTER RACE.  THE BEARING WAS SUBMITTED TO THE LAB FOR ANALYSIS.  THE INVESTIGATION IS ST	ILL IN PROGRESS AT THIS AGENCY.				2	L	7	2 	4F	4	F	RT	A28NM   	E311NE				 
1999020500032	19990205	00032	CE  	1999	2	5	99ZZZX486        	1	19990122	G	3242	30143	BRAKE           	CLEVELAND   		CESSNA	441   	441         	2076020	CE  										MLG	MISMANUFACTURED 	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	99	441EL					4410245				WHEN LEFT AND RIGHT LANDING GEAR ARE RETRACTED, THE BRAKE ASSY, PN 30-143, MAKES HOLES IN THE UPPER WING SKIN HONEYCOMB,	 PN 572231-1.  AT THE SAME TIME, THE BRAKE PISTONS ARE PUSHED INTO THE HOUSING ALLOWING ENOUGH SPACE FOR THE BRAKE PADS,	 PN 066-07300, TO FALL OUT IN-FLIGHT.  THESE BRAKES ARE INSTALLED ON THE CESSNA 441 UNDER STC NR SA644GL.				1	L	7	2 	3T			RT	A28CE   					 
1999020500034	19990205	00034	EA  	1999	2	5	99ZZZX488        	2	19990114	G	7200		ENGINE          			PIPER 	PA42  	PA42        	7104202	SO  	PWA   	PT6   	PT6A41      	52043	EA  					LEFT	FAILED          	H				B	A			EMER. DESCENT           	UNSCHED LANDING         			T	X		ENGINE CASE PENETRATION   	ENGINE FLAMEOUT           		CR	CRUISE         	1			CE	01	5PA	4563 				428001051	PCE85213			CATASTROPHIC FAILURE OF LEFT ENGINE.  AIRCRAFT WAS EN ROUTE TO DESTINATION WHEN AN IN-FLIGHT FAILURE OF LEFT ENGINE OCCU	RRED.  DESTRUCTION AND SEPARATION OF TURBINE BLADES AFT OF HOT SECTION OCCURRED.  PIECES OF BLADES WENT THROUGH AND DEST	ROYED BOTH EXHAUST STACKS.  THE POWER SECTION OF THE ENGINE LOCKED UP.  TWO OF THREE Q-TIPS SEPARATED FROM PROPELLER WIT	H THE 3RD TIP BEGINNING TO STRAIGHTEN, BUT HAD NOT YET SEPARATED.  ENGINE AND PROPELLER WERE REMOVED.			1	L	7	2 	4T	4	T		A23SO   	E4EA				 
1999020500088	19990205	00088	CE  	1999	2	5	99ZZZX492        	1	19990113	G	2842	S33311	TRANSMITTER     			CESSNA	172   	172R        	2072401	CE  										RT WING FUEL	MALFUNCTIONED   	B		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	500ER	270  				17280653				RIGHT FUEL GAUGE NEEDLE READS ERRATICALLY.  SHOWS A ZERO TO FULL INDICATION.  INSPECTED THE FUEL SYSTEM AND FOUND THE RI	GHT FUEL SENDER, P/N S-3331-1, BAD.  DE-FUELED THE RIGHT FUEL TANK AND REPLACED THE FUEL SENDER.					1	H	7	1 	3O			NT	3A12    					 
1999020500089	19990205	00089	CE  	1999	2	5	99ZZZX493        	1	19990113	G	2842	S33311	TRANSMITTER     			CESSNA	172   	172R        	2072401	CE  										LT WING FUEL	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	436ER	279  				17280659				RIGHT FUEL GAUGE NEEDLE READS ERRATICALLY.  SHOWS A ZERO TO FULL INDICATION.  INSPECTED THE FUEL SYSTEM AND FOUND THE RI	GHT FUEL SENDER, P/N S-3331-1, BAD.  DE-FUELED THE RIGHT FUEL TANK AND REPLACED THE FUEL SENDER.					1	H	7	1 	3O			NT	3A12    					 
1999020500091	19990205	00091	CE  	1999	2	5	99ZZZX495        	1	19990112	G	5312	121241510	BULKHEAD        		12124158    	CESSNA	210   	P210N       	2073454	CE  										BS 194	CRACKED         	B			S8AR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	05	4801P	1920 				P2100013				BULKHEAD ASSEMBLY AT STA 194.80 CRACKED/BROKEN LOWER RIGHT CORNER, THE AUTOPILOT KFC 200 PITCH SERVO AFT MOUNT, BOLTS 2 	INCHES INBOARD OF CRACK.					1	H	7	1 	3O				3A21    					 
1999020500092	19990205	00092	CE  	1999	2	5	99ZZZX496        	1	19990103	G	2842	S33311	TRANSMITTER     			CESSNA	172   	172R        	2072401	CE  										RT WING FUEL	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	460ER	279  				17280668				DURING INSPECTION OF THE ALTERNATOR SYSTEM, FOUND LEFT AND RIGHT FUEL GAUGE NEEDLES WERE FLUCTUATING FROM FULL TO ZERO. 	 INSPECTED THE FUEL INDICATING SYSTEM AND FOUND THE RIGHT FUEL SENDER, P/N S-3331-1, BAD.  DE-FUELED THE RIGHT FUEL TANK	 AND REPLACED THE FUEL SENDER.				1	H	7	1 	3O			NT	3A12    					 
1999020500093	19990205	00093	CE  	1999	2	5	99ZZZX497        	1	19990113	G	2842	S33311	TRANSMITTER     			CESSNA	172   	172R        	2072401	CE  										LT WING FUEL	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	460ER	279  				17280668				DURING AN INSPECTION OF THE ALTERNATOR SYSTEM, FOUND THE LEFT AND RIGHT FUEL GAUGE NEEDLES WERE FLUCTUATING FROM FULL TO	 ZERO.  INSPECTED THE FUEL INDICATING SYSTEM AND FOUND THE LEFT SENDER, P/N S-3331-2, BAD.  DE-FUELED THE LEFT FUEL TANK	 AND REPLACED THE FUEL SENDER.  REPLACEMENT OF THE FUEL SENDER CORRECTED THE PROBLEM FOR A SHORT TIME WITH THE QUANTITY 	INDICATOR.			1	H	7	1 	3O			NT	3A12    					 
1999020500094	19990205	00094	CE  	1999	2	5	99ZZZX498        	1	19990113	G	2842	S33311	TRANSMITTER     			CESSNA	172   	172R        	2072401	CE  										RT WING FUEL	MALFUNCTIONED   	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	432ER	314  				17280652				RIGHT FUEL GAUGE NEEDLE READS ERRATICALLY.  SHOWS ZERO TO FULL INDICATION.  INSPECTED THE FUEL SYSTEM AND FOUND THE RIGH	T FUEL SENDER, P/N S-3331-1, BAD.  DE-FUELED THE RIGHT FUEL TANK AND REPLACED THE FUEL SENDER.					1	H	7	1 	3O			NT	3A12    					 
1999020500095	19990205	00095	SO  	1999	2	5	99ZZZX499        	1	19990114	G	3233	452729	ROD END         		3579705     	PIPER 	PA28  	PA28R201T   	7102813	SO  										NLG	BROKEN          	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	13	38793	2205 				28R7703278				PILOT NOTICED NOSE GEAR EXTENDED IN-FLIGHT AND COULD NOT GET IT TO COME UP.  INSPECTION REVEALED THAT NOSE GEAR ACTUATOR	 ROD END BEARING HAD PULLED APART ALLOWING NOSE GEAR TO FALL.  NEW PART WAS INSTALLED AND GEAR RIGGING CHECK PERFORMED.					1	L	7	1 	3O				2A13    					 
1999020500105	19990205	00105	SW  	1999	2	5	99ZZZX509        	1	19990113	G	7922	53E19600	VALVE           			MOONEY	M20   	M20J        	5870219	SW  										TEMP BYPASS	FAILED          	D				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			EA	17	1084B	1010 			66755	243266				DURING FLIGHT, OBSERVED HIGH OIL TEMPERATURE OF 230 DEGREES FAHRENHEIT, OAT MINUS 10 DEGREES CELCIUS.  CHT NORMAL, OIL P	RESSURE NORMAL.  AFTER FLIGHT, OIL LEVEL 6-1/2 QUARTS, NORMAL.  OIL COOLER APPEARED CLEAN, BUT COLD.  REMOVED THERMOSTAT	IC BYPASS VALVE.  CHECKED WITH HOT WATER TEST, NOTICED NO MOVEMENT OF VALVE.  INSTALLED NEW THERMOSTATIC BYPASS VALVE, S	UPERIOR, P/N SL 53E19600, S/N 106U.  FLIGHT TEST SHOWED OIL TEMPERATURE OF 170 DEGREES FAHRENHEIT, OAT MINUS NINE DEGREE	S CELCIUS.  ALL CONDITIONS NORMAL.  S/N 66755 INSTALLED 12-1-95 AT 703.6 HOURS TTSN PER SB 518C.  S/N 10611 INSTALLED 1-	4-99 AT 1,713.0 HOURS TTSN.	1	L	7	1 	3O				2A3     					 
1999020500106	19990205	00106	SO  	1999	2	5	99ZZZX510        	2	19990107	G	8550	6521713	DIPSTICK        			CESSNA	310   	T310R       	2074246	CE  	CONT  	O520  	TSIO520B    	17040	SO  					LT ENGINE	BROKEN          	B			RE4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03	711ED					310R0246	500120B			DIPSTICK BECAME SEPARATED FROM CAP ALLOWING THE DIPSTICK AND SPRING TO DROP INTO DIPSTICK TUBE.  THERE ARE FOUR TUBES BU	ILT INTO THE CAP AND 3 OF THE 4 WERE BROKEN.  THE NEW PART NUMBERED DIPSTICK IS  MANUFACTURED TO ALLEVIATE THIS FROM HAP	PENING AGAIN BY NOT HAVING THESE SMALL TABS HOLDING THE DIPSTICK TO THE CAP.				1	L	7	2 	3O	3	O		3A10    	E8CE				 
1999020500107	19990205	00107	EA  	1999	2	5	99ZZZX511        	2	19990112	G	8500		ENGINE          			PIPER 	PA60  	PA60600     	7106001	NM  	LYC   	O540  	IO540K1J5   	41532	EA  					LEFT	FAILED          	G				O				OTHER                   				Y			ENGINE STOPPAGE           			NR	NOT REPORTED   	1			EA	01	8073J					600556180				LEFT ENGINE SHUT DOWN IN-FLIGHT.  ICE FOUND IN INDUCTION AIR FILTER, ALTERNATE AIR, AND FUEL SERVO.  INSPECTION OF RIGHT	 ENGINE FOUND SAME CONDITION.  AIRCRAFT OPERATING IN SNOW CONDITIONS.  SUBMITTER RECOMMENDED INSPECTION OF INDUCTION SYS	TEM AFTER FLIGHT IN KNOWN ICING CONDITIONS, RE-DESIGN OF SYSTEM, OR CHANGES IN P.O.H.				1	M	7	2 	3O	3	O	RT	A17WE   	1E4				 
1999020500496	19990205	00496	NM  	1999	2	5	99ZZZX519        	1	19990120	G	5530	35250501	TAIL STRUT      			CHRIS 	HUSKY 	A1          	221020X	NM  										THREADS	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	15	23HG	243  				1269				STAINLESS STEEL STRUT ASSEMBLY BROKEN AT THREADS LOWER TERMINAL, TIE ROD.						1	H	7	1 	3O			NC	A22NM   					 
1999020500497	19990205	00497	GL  	1999	2	5	99ZZZX520        	1	19990111	G	2751	2027501500	BRACKET         			DIAMON	DA20  	DA20C1      	2990001	GL  										TE FLAP	BENT            	B				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			GL	21	222ND	27   				C0030				PILOTS REPORT FLAP OPERATION AS SLOW AND JERKY WITH NO POSITION INDICATION.  UPON INVESTIGATION, FOUND THE FLAP POSITION	 SWITCH ASSEMBLY BENT DUE TO BINDING ON THE ACTUATOR ROD OF THE SLIDE BUSHING.  IMPROPER LUBRICATION AT THE FACTORY MAY 	HAVE CONTRIBUTED TO THIS.  ASSEMBLY WAS REPLACED, ROD AND BUSHING LUBED.  SYSTEM FUNCTIONED NORMALLY.				1	L	7	1 	3O			NT	TA4CH   					 
1999020500498	19990205	00498	CE  	1999	2	5	99ZZZX521        	1	19990120	G	3222		NOSE GEAR       			CESSNA	310   	310C        	2074210	CE  										NLG	LOW             	G				O				OTHER                   				O			OTHER                     			AP	APPROACH       	1			SO	14	218S	6838 				35963				NOSE GEAR DID NOT EXTEND ON FINAL APPROACH.  NOSE STRUT PRESSURE WAS INSUFFICIENT TO EXTEND STRUT.  NOSE WHEEL FENDER HU	NG UP ON RIGHT NOSE GEAR DOOR HINGE PREVENTING GEAR EXTENSION.  SUBMITTER RECOMMENDS INCREASED AWARENESS OF STRUT HEIGHT	 DURING PREFLIGHT WALK-AROUND.				1	L	7	2 	3O				3A10    					 
1999020500503	19990205	00503		1999	2	5	99ZZZX526        	2	19990122	G	7414	ES103571644	COIL            																	MAGNETO	CRACKED         	B			KC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03					2987					COIL IS AFTERMARKET COIL.  COIL POTTING COMPOUND HAS CRACKS NEAR HIGH TENSION OUTPUT TAB.  HIGH TENSION VOLTAGE LEAKING 	FROM CRACKS TO GROUND.  SUBMITTER STATED THIS COULD EVENTUALLY RESULT IN A DEAD MAG.																		 
1999020500505	19990205	00505		1999	2	5	99ZZZX528        	4	19990106	G	6122	8210393	GOVERNOR        																	PROPELLER	WORN            	B			OL3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	27			2963 		2491486					UNIT CAME IN FOR REPAIR DUE TO TORQUE FLUX AT BENCH TEST WHILE TESTING UNIT FEATHERING OPERATION.  NOTICED SIGNIFICANT V	IBRATION WITH A MARKED INCREASE IN THE INTERNAL LEAKAGE AS SPEED LEVER WAS MOVED TOWARDS FEATHER STOP.  AT TEAR DOWN INS	PECTION, FOUND EXCESSIVE WEAR AT TIP OF IDLER GEAR STUD AND BASE.  BASE PLATE WEAR IS AT POINT OF IDLER GEAR STUD INSERT	ION INTO BASE.  IDLER GEAR POCKET SHOWS SIGNS OF EXCESSIVE GEAR RUB.  SUBMITTER SUSPECTED IDLER STUD MOVING BACK AND FOR	TH WITH DIFFERENT PRESSURE LOADS AND FLOW.															 
1999020500506	19990205	00506	EA  	1999	2	5	99ZZZX529        	2	19990115	G	8530	SL134441	PIN             	SUPAIRPART  							LYC   	O320  	O320H2AD    	41508	EA  					PISTON	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	01										EXCESSIVE PIN WEAR IN WALL OF CYLINDER IN 1,541 HOURS TOTAL TIME.  ALL FOUR CYLINDERS WERE NEW STEEL CYLINDERS.  ENGINE 	IS O320-H2AD.  ENGINE PULLED  BECAUSE OF CRACKED CASE.										3	O			E274				 
1999020500507	19990205	00507		1999	2	5	99ZZZX530        	2	19990113	G	7414	ES103825881	COIL            	BENDIX      	D6LN2031    															MAGNETO	CRACKED         	B			KC2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03		500  			495					THIS MAGNETO WAS OVERHAULED AND ISSUED S/N 5080123.  MAG WAS REMOVED FOR A ROUTINE 500-HOUR INSPECTION.  THE RIGHT COIL 	WITH A DATE CODE OF 4-95 WAS FOUND WITH A CRACK EXTENDING THE LENGTH OF THE COIL BY THE HIGH TENSION OUTPUT TAB.																		 
1999020500508	19990205	00508	CE  	1999	2	5	99ZZZX531        	1	19990106	G	2721	17132691	RUDDER WHEEL    			CESSNA	182   	182S        	2072701	CE  										COCKPIT	MALFUNCTIONED   	B	P		AMYR	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CE	05	182S	149  				18280193				OWNER SQUAWKED AIRCRAFT WAS NOT PRODUCING ENOUGH RT RUDDER TRIM TO CENTER THE TURN COORDINATOR BALL.  THIS CONDITION WAS	 CORRECTED TWICE TO NO AVAIL BY POPPING THE INDICATOR PIN BACK INTO ITS GROOVE.  THE CONDITION WOULD RECUR DURING NEXT F	LIGHT.  AFTER FURTHER INVESTIGATION, DISCOVERED RUDDER TRIM WHEEL HAD EXCESSIVE UP AND DOWN PLAY.  AS A RESULT, THE SPRO	CKET ON THE TRIM WHEEL THAT DRIVES THE AFT TRIM SPROCKET WOULD TEND TO SKIP CAUSING THE INDICATOR TO PREMATURELY REACH I	TS STOP.  THIS WOULD NOT ALLOW A FULL DEFLECTION OF THE RUDDER AND INABILITY TO 'CENTER THE BALL'.  TO CORRECT THE PROBL	EM, THIN WASHER WAS REMOVED FROM THE BOTTOM OF THE WHEEL SHAFT AND REPLACED WITH A THICK ONE ELIMINATING EXCESSIVE PLAY.	1	H	7	1 	3O			NT	3A13    					 
1999020500510	19990205	00510	SO  	1999	2	5	99ZZZX533        	1	19990112	G	5513	1565829A1	BALANCE WEIGHT  			PIPER 	PA23  	PA23250     	7102308	SO  										STABILATOR	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	23	27CY	5332 				277654118				DURING 100-HOUR INSPECTION OF BALANCE WEIGHTS AND ARMS PER AD 78-02-03, FOUND BOTH ARMS CRACKED.  REPLACED BOTH WITH SER	VICEABLE PARTS.  CAUSE UNKNOWN, POSSIBLE THAT ICE ACCUMULATION ON STABLIZER CAUSED SLIGHT FLUTTER.					1	L	7	2 	3O				1A10    					 
1999020500515	19990205	00515	SO  	1999	2	5	99ZZZX538        	2	19990106	G	7414	1051678	SLINGER         		106006061   	CESSNA	402   	402C        	207590R	CE  	CONT  	O520  	TSIO520VB   	17040	SO  					MAGNETO	MISSING         	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	01	3292M	285  			DO19816ER	402C0304	290293R			DURING PHASE INSPECTION, DIQSCOVERED L.E. LEFT MAGNETO HAD OIL INTERNALLY.   DISSAMBLED MAGNETO IAW OM.  FOUND OIL SLING	ER WAS NOT INSTALLED.					1	L	7	2 	3O	3	O		A7CE    	E8CE				 
1999020500516	19990205	00516	SO  	1999	2	5	99ZZZX539        	1	19990101	G	3340	587827	SWITCH          			PIPER 	PA32  	PA32300     	7103212	SO  										LANDING LIGHT	FAILED          	B			BXSR	O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			EA	09	304MM					3240588				PILOT REPORTED SMOKE IN THE COCKPIT WHEN THE LANDING LIGHT WAS SWITCHED ON.  TROUBLESHOT AND FOUND THE SWITCH DEFECTIVE.						1	L	7	1 	3O				A3SO    					 
1999020500521	19990205	00521	EA  	1999	2	5	99ZZZX544        	1	19990111	G	2931	600591341	SWITCH          			CNDAIR	CL600 	CL6002B16   	1900305	EA  										HYD PRESSURE	FAILED          	D				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			EA	13	270RA	226  			2572	5337				'GROUND SPOILER' CAUTION MESSAGE ON WITH FLAP SELECTION (I.E., FLAPS DOWN INBOARD PUMP OPERATING).  NEW SWITCH CLEARED M	ESSAGE.  SUBMITTER STATED THIS IS THIRD FAILURE IN 700 HOURS.  MANUFACTURER NOTIFIED.					2	L	7	2 	4F			RT	A21EA   					 
1999020500522	19990205	00522	NM  	1999	2	5	99ZZZX545        	1	19990119	G	5320		CHANNEL         			DOUG  	MD11  	MD11        	3023602	NM  										BS 1701-1802	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	273WA					48519				CENTER CARGO COMPARTMENT, FS 1701 - FS 1802, BL 30 - BL 36, RT CHANNEL ASSY, BROKEN.  REMOVED AND REPLACED CHANNEL IAW M	D 11 SRM'S 51-31-01, 51-21-02, 51-41-01, 50-90-02.					2	L	7	3 	4F			RT	A22WE   					 
1999020500525	19990205	00525		1999	2	5	99ZZZX548        	4	19990112	G	3420	7000466951	INDICATOR       			CESSNA	500   	550         	2076604	CE  										COCKPIT	MALFUNCTIONED   	B			RC0R	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	17	26494				83112074	5500605				DURING SLOW RATE OF TURNS, THE ATTITUDE FLAG APPEARS AND ADI SPHERE STUCK.  ADI STUCK SEVERAL TIMES ON BOTH LEFT AND RIG	HT BANKS AND ATTITUDE FLAG COMES IN VIEW.					1	L	7	2 	4F				A22CE   					 
1999020500531	19990205	00531	WP  	1999	2	5	99ZZZX554        	1	19990113	G	3246	152059	WHEEL           	BENDIX      	1542511     	DOUG  	DC8   	DC861F      	3021953	WP  										MLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					H4045					VISUALLY DETECTED LEAKING AREA BETWEEEN TIE BOLTS.  CONFIRMED CRACK TUBE WALL ROTOR DRIVE KEY HOLE.  NO CRACKS PERMITTED	 THIS AREA.  BENDIX OHM 32-40-05 REV 15 DATE 10-15-96.  CHECK SECTION PARA 2B.					2	L	7	4 	4F				4A25    					 
1999020500532	19990205	00532	WP  	1999	2	5	99ZZZX555        	1	19990113	G	3246	152059	WHEEL           	BENDIX      	1542511     	DOUG  	DC8   	DC861F      	3021953	WP  										MLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					B6195					VISUALLY DETECTED LEAKING AREA BETWEEEN TIE BOLTS.  CONFIRMED CRACK TUBE WALL ROTOR DRIVE KEY HOLE.  NO CRACKS PERMITTED	 THIS AREA.  BENDIX OHM 32-40-05 REV 15 DATE 10-15-96.  CHECK SECTION PARA 2B.					2	L	7	4 	4F				4A25    					 
1999021900015	19990219	00015	CE  	1999	2	19	99ZZZX575        	1	19990118	G	5511	12326216	SPAR            			CESSNA	210   	T210M       	2073451	CE  										HORIZ STABILIZER	CRACKED         	B			DPOR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	7067Z	7462 				21062572				DURING AN ANNUAL INSPECTION A CRACK APPROXIMATELY 1 INCH LONG WAS DETECTED ON THE LEFT HORIZONTAL STABILIZER AFT SPAR LO	WER RADIUS.					1	H	7	1 	3O				3A21    					 
1999021900018	19990219	00018	CE  	1999	2	19	99ZZZX578        	1	19990125	G	2730	0510105309	CONTROL CABLE   			CESSNA	172   	172M        	2072418	CE  										ELEVATOR	FRAYED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	01	12944	8102 				17262390				DURING A 100-HOUR INSPECTION, FOUND THE UP ELEVATOR CABLE FRAYED AFTER REMOVING THE PULLEY FOR REPLACEMENT.						1	H	7	1 	3O			NT	3A12    					 
1999021900021	19990219	00021	GL  	1999	2	19	99ZZZX581        	1	19990101	G	8011	654046	STARTER         			DIAMON	DA20  	DA20C1      	2990001	GL  										ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	113CL	90   			J069713AA	C0013				REMOVED STARTER FOR REPLACEMENT.  FOUND GEAR ON STARTER AND DRIVE GEAR ON ENGINE DESTROYED.  STARTER DRIVE SHAFT SHEARED	.  STARTER GEAR SPLINED TO ENGAGE AND TURN ONE DIRECTION WITH CENTRIFUGAL FORCE ONCE ENGINE HAS STARTED.  TO DISENGAGE, 	ENGINE HAS A TENDENCY TO KICK BACK SEVERAL ROTATIONS ON COLD START ATTEMPTS.  STARTER GEAR NOT DESIGNED TO GO BACKWARDS 	RESULTING IN STRIPPED GEARS AND SHEARED SHAFT.  ENGINE IS BEING REPLACED FOR METAL CONTAMINATION.   SUBMITTER STATED DIA	MOND AIRCRAFT AND TCM HAVE BEEN MADE AWARE OF THIS PROBLEM.		1	L	7	1 	3O			NT	TA4CH   					 
1999021900022	19990219	00022	CE  	1999	2	19	99ZZZX582        	1	19990115	G	5321	04102381	FLOORBOARD      			CESSNA	150   	152         	2071835	CE  										BS 27-56	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	13	66934					15281670				DURING ANNUAL INSPECTION, FOUND THE FLOOR PAN CRACKED AT THE END OF THE COPILOT'S INBOARD SEAT TRACK.  THIS IS THE FORTH	 PLANE OUT OF SIX 152'S THAT HAVE HAD TO BE REPAIRED.  THE SEAT TRACK IS WEARING INTO THE RADIUS OF THE BEND OF THE FLOO	R PAN.  THERE IS NO SUPPORT UNDER THE FLOORBOARD.  THIS HAS BEEN AN ONGOING PROBLEM AND NEEDS TO BE LOOKED AT.  THE CRAC	K CANNOT BE SEEN UNTIL IT RETRACTS OUT FROM UNDER THE SEAT RAIL.			1	H	7	1 	3O			NT	3A19    					 
1999021900023	19990219	00023	SO  	1999	2	19	99ZZZX583        	2	19990115	G	8530		ROD             			CESSNA	421   	421C        	2076016	CE  	CONT  	O520  	GTSIO520N   	17032	SO  					CYLINDER	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	01	637DT	4060 	4    			421C0508	R610420			ENGINE STARTED EXTREME VIBRATION CLIMBING THROUGH 13,000 FEET.  OIL LEAK OBSERVED COMING FROM LOUVERS.  ENGINE WAS SHUT 	DOWN AND PROPELLER FEATHERED.  INSPECTION REVEALED 2 HOLES IN CASE HALVES ABOVE NR 1 AND NR 2 CYLINDERS.  NR 1 CYLINDER 	ROD BROKEN.  SEVERAL INTERNAL PIECES LAYING IN BAFFELING.  RT MAGNETO DESTROYED DUE TO FOREIGN OBJECT IMPACT.				1	L	7	2 	3O	3	O		A7CE    	E7CE				 
1999021900034	19990219	00034	CE  	1999	2	19	99ZZZX594        	1	19990101	G	7120	121343316	SUPPORT         			CESSNA	206   	U206F       	2073333	CE  										ENGINE MOUNT	CRACKED         	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	27	1003V	6700 				U20602388				DURING A ROUTINE INSPECTION, THE RIGHT REAR SUPPORT (CESSNA P/N 1213433-16) WAS FOUND CRACKED AT THE AFT RADIUS.  THE CR	ACK WAS APPROXIMATELY .25 INCH LONG AND WAS VISABLE BECAUSE CORROSION OF THE EXPOSED STEEL.  CLOSER INSPECTION SHOWED AL	L 4 MOUNTS TO BE CRACKED TO A LESSER DEGREE.  THERE DOES APPEAR TO BE SOME UN-DOCUMENTED DAMAGE TO THE NOSE AREA WHICH H	AD BEEN REPAIRED.			1	H	7	1 	3O				A4CE    					 
1999021900245	19990219	00245	NM  	1999	2	19	99ZZZX610        	1	19990101	G	5751	652176648	SKIN            			BOEING	727   	7272B7      	138407L	NM  										AILERON	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	923PG					22163				DURING A C-CHECK, CORROSION WAS NOTED ON LOWER SKIN RT OUTBOARD AILERON.						2	L	7	3 	4F				A3WE    					 
1999021900247	19990219	00247	CE  	1999	2	19	99ZZZX612        	1	19990104	G	5280	11581006012	HINGE           			BEECH 	99    	B99         	1154004	CE  										MLG DOOR	WORN            	B	S		TIMR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	07	99TH					11155				INSPECTION OF GEAR DOOR HINGE REVEALED FORE AND AFT MOVEMENT BETWEEN HINGE HALVES.  THIS ACTION RESULTED IN EXCESS TRAVE	L OF DOOR IN THE GEAR DOWN POSITION.  REPLACED HINGE AND 2 COUPLE LINKAGE COMPONENTS.  POSSIBLE CAUSE OF HINGE DISCREPAN	CY DETERMINED TO BE CAUSED BY A COMBINATION OF NORMAL AGING AND VIBRATION ASSOCIATED WITH THE NORMAL OPERATION OF THE AI	RPLANE.			1	L	7	2 	3T				A14CE   					 
1999021900259	19990219	00259	SO  	1999	2	19	99ZZZX624        	1	19990119	G	2434	ALY6421	SHAFT           	PRESTOLITE  		PIPER 	PA32  	PA32R301    	7103218	SO  										ALTERNATOR	MISINSTALLED    	B			IBIR	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			EA	27	9264A				A135388	32R8613003				ALTERNATOR SHAFT NOT FULLY INSTALLED INTO ARMATURE/ALTERNATOR BODY.  KEYWAYS NOT MATCHING UP.  SHAFT TOO LONG.  UNIT WAS	 OVERHAULED BY AERO ELECTRIC INC.  NV2ROYSL.					1	L	7	1 	3O				A3SO    					 
1999021900263	19990219	00263	SO  	1999	2	19	99ZZZX628        	1	19990119	G	3230	4204200	ARM             			PIPER 	PA31  	PA31350     	7103110	SO  										MLG	CRACKED         	B	S		ES4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	01	9FW	10691				317405468				ARM FOUND CRACKED DURING 100-HOUR INSPECTION.  ARM, P/N 42042-00.						1	L	7	2 	3O				A20SO   					 
1999021900264	19990219	00264	SO  	1999	2	19	99ZZZX629        	1	19990114	G	5347		SEAT TRACK      			PIPER 	PA24  	PA24250     	7102404	SO  										BS 87	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	8052P					243298				SPECIAL ATTENTION FOR HARD TO SEE PROBLEM OF CRACKING SEAT TRACK FORMER BULKHEAD STA 87.  GENERALLY, ONLY THIS ONE SHOWS	 DISTRESS, SOMETIMES ONLY PILOT'S SIDE.  PART NUMBERS ON FICHE PA24 PARTS MANUAL:  20601-08 LT; DASH 07 RT.  23656-02 LT	 - DASH 03 RT.				1	L	7	1 	3O				1A15    					 
1999021900279	19990219	00279	CE  	1999	2	19	99ZZZX644        	1	19990104	G	2140	671U769	FUEL PUMP       		8259HL2     	CESSNA	402   	402C        	207590R	CE  										HEATER	LEAKING         	D				O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		CL	CLIMB          	1			NE	01	2651G	525  			769	402C0101				AFTER TAKEOFF, CREW TURNED ON AIRCRAFT HEATER, CABIN FILLED WITH FUEL ODOR.  CREW TURNED OFF HEATER, VENTED CABIN AND RE	TURNED TO BASE.  MAINTENANCE FOUND HEATER FUEL PUMP PARTING HALVES LOOSE.  RE-TORQUED HARDWARE AND RE-INSTALLED PUMP HOU	SING COVER.  RETURNED AIRCRAFT TO SERVICE.				1	L	7	2 	3O				A7CE    					 
1999021900280	19990219	00280	SO  	1999	2	19	99ZZZX645        	1	19990101	G	2510	7955510	FRAME           			PIPER 	PA28  	PA28R201    	7102816	SO  										SEAT BACK	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	3463Q	6821 				28R7737055				AS PILOTS ENTER AIRCRAFT, THEY LEAN ON SEAT BACKS TO MANEUVER INTO THE SEAT AND CRACK SEAT BACK FRAMES WHICH, IN TURN, W	ILL BEND SEAT BACK CONTROL ROD, AND CAUSE SEAT BACK TO RECLINE.					1	L	7	1 	3O				2A13    					 
1999021900281	19990219	00281	SO  	1999	2	19	99ZZZX646        	1	19990101	G	2520		SEAT            			PIPER 	PA28  	PA28180     	7102808	SO  										CABIN	WRONG PART      	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	44195	3300 				287405228				WRONG BACK SEATS ARE INSTALLED IN AIRCRAFT.  LATCHES FOR BACK SEAT ARE TYPE THAT YOU PULL UPON SEAT, AND IT COMES OUT. S	EATS THAT WERE INSTALLED IN AIRCRAFT WERE OF TYPE SCREW DRIVER TURNS LATCH AND SEATS COME OUT.  SEATS WOULD HAVE COME OU	T WITHOUT ANY FORCE APPLIED.				1	L	7	1 	3O				2A13    					 
1999021900282	19990219	00282	SO  	1999	2	19	99ZZZX647        	1	19990101	G	2720	63451	BRACKET         			PIPER 	PA28  	PA28180     	7102808	SO  										COCKPIT	BENT            	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	44195	3300 				287405228				ON ANNUAL INSPECTION, FOUND RUDDER PEDAL SUPPORT BRACKET BENT AND CRACK AT ATTACH POINT.  SUBMITTER STATED SECOND AIRCRA	FT FOUND THIS WAY.					1	L	7	1 	3O				2A13    					 
1999021900283	19990219	00283	CE  	1999	2	19	99ZZZX648        	1	19990101	G	5412	05530313	FIREWALL        			CESSNA	172   	172R        	2072401	CE  						MCAULY	IC235	IC235LFA7570	EA  	COWL MOUNT	WRINKLED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	409ES		262  			17280231		RD060		FOUND FIREWALL SEVERELY WRINKLED, NOSE ATTACH STRUCTURE RIVETS SHEARED.  TWO INCH CRACK IN FIREWALL BELOW BATTERY BOX AT	 COWL MOUNT.  SUBMITTER STATED A POSSIBLE CAUSE AS HARD LANDING.  THICKER FIREWALL COULD PREVENT RECURRENCE.					1	H	7	1 	3O			NT	3A12    		5	N	P12EA	 
1999021900285	19990219	00285	CE  	1999	2	19	99ZZZX650        	1	19990101	G	3230	24130023	FITTING         			CESSNA	172   	172RG       	2072438	CE  										NLG	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	01	4669V					172RG0359				NOSE GEAR ACTUATOR ASSY ATTACHING BOLT TO FITTINGS/CASTING FROZEN CAUSING CASTING TO CRACK.  INSPECT ACTUATOR FOR FREE M	OVEMENT, REMOVE BOLTS, CLEAN AND GREASE BOTH ENDS OF ACTUATOR.					1	H	7	1 	3O				3A17    					 
1999021900539	19990219	00539	SO  	1999	2	19	99ZZZX652        	2	19990101	G	8520	352059	GASKET          			BEECH 	35    	G35         	1151516	CE  	CONT  	E225  	E2258       	17015	SO  					CRANKCASE	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	4254D	20   				D4471	39944C			THE GASKETS THAT SEAL THE INTAKE MANIFOLD (WHICH HAS ENGINE OIL CIRCULATING THROUGH IT) HAVE BRASS EYELETS FORMED INTO T	HE PAPER GASKET AROUND THE BOLT HOLES.  USING STANDARD TORQUE OF 175 INCH/POUND FOR THE .3125 INCH - 18 EACH BOLTS RESUL	TED IN THE GASKET LEAKING.  RE-TORQUING RESULTED IN THE PAPER GASKET SPLITTING AND LEAKING MORE.  MADE PAPER GASKETS WIT	HOUT EYELETS AND RESOLVED THE PROBLEM.  SUBMITTER RECOMMENDS DISCONTINUING USE OF THE GASKETS WITH EYELETS IN THE APPLIC	ATION.		1	L	7	1 	3O	3	O		A777    	E267				 
1999021900540	19990219	00540	SO  	1999	2	19	99ZZZX653        	2	19990101	G	8520	352060	GASKET          			BEECH 	35    	G35         	1151516	CE  	CONT  	E225  	E2258       	17015	SO  					CRANKCASE	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	4254D	20   				D4471	39944C			THE GASKETS THAT SEAL THE INTAKE MANIFOLD (WHICH HAS ENGINE OIL CIRCULATING THROUGH IT) HAVE BRASS EYELETS FORMED INTO T	HE PAPER GASKET AROUND THE BOLT HOLES.  USING STANDARD TORQUE OF 175 INCH/POUND FOR THE .3125 INCH - 18 EACH BOLTS RESUL	TED IN THE GASKET LEAKING.  RE-TORQUING RESULTED IN THE PAPER GASKET SPLITTING AND LEAKING MORE.  MADE PAPER GASKETS WIT	HOUT EYELETS AND RESOLVED THE PROBLEM.  SUBMITTER RECOMMENDS DISCONTINUING USE OF THE GASKETS WITH EYELETS IN THE APPLIC	ATION.		1	L	7	1 	3O	3	O		A777    	E267				 
1999021900546	19990219	00546	SO  	1999	2	19	99ZZZX659        	1	19990115	G	3242	1331096	BRAKE           	BFGOODRICH  	21585       	EMB   	120   	EMB120      	3260201	SO  										MLG	FAILED          	B			XC4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					1417					BRAKE ASSY, P/N 2-1585, FAILED PREMATURELY.  NR 1 STATOR BROKEN IN HALF CAUSING DAMAGE BEYOND SERVICEABLE LIMITS TO TORQ	UE TUBE KEY SLOT AREA.  THIS IS A CONTINUAL DISCREPANCY.  BRAKE ASSY SHOULD LAST 2,500 CYCLES.  NOTE:  OEM PARTS INSTALL	ED IN BRAKE ASSY AND THE MOST RECENT BRAKE CONFIGURATION, P/N 2-1585.				2	L	7	2 	4T			RT	A31SO   					 
1999021900557	19990219	00557	EU  	1999	2	19	99ZZZX670        	1	19990119	G	3260	430M1	GEAR HORN       			ISRAEL	1125  	ASTRASPX    	4500205	EU  										COCKPIT	INOPERATIVE     	D				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			EA	13	275RA	323  			17245	098				GEAR HORN WOULD NOT WORK WHEN TESTED.  FOUND NOT TO WORK AT ALL.  REPLACED WITH NEW.  PROBLEM SOLVED.						2	L	7	2 	4F			RT	A16NM   					 
1999021900558	19990219	00558		1999	2	19	99ZZZX671        	4	19990119	G	2350	6027664	MICROPHONE      			ISRAEL	1125  	ASTRASPX    	4500205	EU  										COCKPIT	INTERMITTENT    	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	275RA	334  	245  		18830	098				WHEN BUTTON IS PRESSED, CAN ONLY TRANSMIT SOME OF THE TIME.  REPLACEMENT OF UNIT FIXED PROBLEM.  SENT FOR OVERHAUL.						2	L	7	2 	4F			RT	A16NM   					 
1999021900559	19990219	00559		1999	2	19	99ZZZX672        	4	19990119	G	2212	73131	COMPENSATOR     			ISRAEL	1125  	ASTRASPX    	4500205	EU  										AILERON	LEAKING         	D				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EA	13	273RA	187  			0085	097				THIS UNIT FAILED PRESSURE TEST DURING AN INSPECTION.  THIS IS A KNOWN PROBLEM.  UNIT MUST HOLD APPROXIMATELY 40 PSI FOR 	3 HOURS AND CAN ONLY LEAK DOWN 5 PSI DURING THIS TIME.  THIS UNIT WENT TO ZERO PSI IN 1.5 HOURS.					2	L	7	2 	4F			RT	A16NM   					 
1999021900560	19990219	00560	EU  	1999	2	19	99ZZZX673        	1	19990119	G	7830	717571	VALVE           			ISRAEL	1125  	ASTRASPX    	4500205	EU  										RT THRUST REVERS	INOPERATIVE     	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	273RA		101  		0053	097				RIGHT 'T/R UNSAFE' ILLUMINATED AND WOULD NOT GO OUT.  THRUST REVERSER WAS CLOSED AND LOCKED NORMALLY.  SUBMITTER STATED 	THIS IS A KNOWN PROBLEM AND SUPPOSEDLY HAS BEEN FIXED WITH A MODIFICATION TO A DASH 3.  DASH 3 WAS INSTALLED.  PROBLEM G	ONE.				2	L	7	2 	4F			RT	A16NM   					 
1999021900561	19990219	00561		1999	2	19	99ZZZX674        	4	19990119	G	2210	501119705	GYRO            			ISRAEL	1125  	ASTRASPX    	4500205	EU  										COCKPIT	MALFUNCTIONED   	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	273RA	150  			6301	097				THIS UNIT WILL NOT STABILIZE AFTER IT IS UNCAGED.  AFTER 10 MINUTES, IT ROLLS TO THE RIGHT.  SENT OUT FOR REPAIR AND INS	TALLED SERVICEABLE UNIT.  FIXED PROBLEM.					2	L	7	2 	4F			RT	A16NM   					 
1999021900562	19990219	00562	WP  	1999	2	19	99ZZZX675        	1	19990122	G	3246	152059	WHEEL           	BENDIX      		DOUG  	DC8   	DC861F      	3021953	WP  										MLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					B4920					NDT SPECS MIL-I-6870 DETECTED CRACK IN TUBEWALL WEB AREA DRIVE KEY HOLE.  NO CRACKS PERMITTED THIS AREA.  BENDIX OHM 32-	40-05 REV 15 DATED 10-15-96.  CHECK SECTION PARA 2B.					2	L	7	4 	4F				4A25    					 
1999022600079	19990226	00079	CE  	1999	2	26	99ZZZX696        	1	19990121	G	7120	539518	MOUNT           			BEECH 	95    	95B55       	1152729	CE  										ENGINE	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	21	7873L		636  			TC1018				635.9 HOBBS.  WHILE CHANGING CABLES ON THE LEFT ENGINE, MAINTENANCE NOTICED THE AFT INBOARD MOUNT LEG WAS BROKEN.  FURTH	ER INSPECTION REVEALED THE FORWARD INBOARD LEG ALSO BROKEN.  A COMPLETE INSPECTION OF THE ENGINE AND PROPELLER SHOWED NO	 OTHER DAMAGE.  MINOR SCUFF MARKS ON ONE PROPELLER BLADE WITH SAME BLADE TRACKING SLIGHTLY AFT OF OTHER 2 BLADES.  CAUSE	 IS UNKNOWN.  NO PILOT REPORTS OF PROPELLER STRIKE.			1	L	7	2 	3O			RT	3A16    					 
1999022600090	19990226	00090	CE  	1999	2	26	99ZZZX707        	1	19990101	G	3233		BOLT            			CESSNA	182   	R182        	2072734	CE  										NLG ACTUATOR	CORRODED        	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	01	268ER					R18201643				NOSE GEAR ACTUATOR ASSY BOLTS FROZEN ON EACH END.  GEAR END/FUSELAGE END.  REMOVED CLEANED, LUBED, AND REASSEMBLED.  INS	PECTED FOR FREE MOVEMENT.					1	H	7	1 	3O			RT	3A13    					 
1999022600107	19990226	00107		1999	2	26	99ZZZX724        	4	19990116	G	2565	D17464509	ASPIRATOR       	AIRCRUISERS 	2403005011  															SLIDE	CONTAMINATED    	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19					19672					RECEIVING INSPECTION FOUND ONE EACH ASPIRATOR WAS COVERED WITH PIECES OF WHITE ADHESIVE TAPE.  THIS TAPE COVERING THE AS	PIRATOR WILL PREVENT THE AMBIENT AIR FROM BEING INJESTED THROUGH THE OPENING OF THE ASPIRATOR (RT) CAUSING THE SLIDE/RAF	T TO HAVE A LOW INFLATION PRESSURE DURING A DEPLOYMENT OF THE SLIDE/RAFT.  UNIT LAST OVERHAULED 10/98 LABELED ON UNIT.																	 
1999030500025	19990305	00025	WP  	1999	3	5	99ZZZX744        	1	19990101	G	6710	369A7304	BRACKET         			HUGHES	369   	369D        	4470706	WP  										ROTOR CONTROL	CRACKED         	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	8694F	9306 				380275D				CRACK IN BEARING CAP NOTED DURING 300 HOUR INSPECTION.  THIS IS THE INBOARD SUPPORT (OF TWO) FOR THE MAIN ROTOR COLLECTI	VE TORQUE TUBE.  CAP IS A MACHINED MATE TO SUPPORT BRACKET REQUIRING REPLACEMENT OF ENTIRE SUPPORT BRACKET AS WELL AS BU	NGEE BRACKET.  FACTORY REPLACEMENT IS A HEAVY DUTY SUPPORT, CAP, AND BUNGEE BRACKET.				1	G	7	1 	3U				H3WE    					 
1999030500037	19990305	00037	EA  	1999	3	5	99ZZZX756        	2	19990112	G	8520	LW17060	CRANKSHAFT      			ROBSIN	R22   	R22         	7640102	WP  	LYC   	O320  	O320B2C     	41508	EA  					ENGINE	MISMANUFACTURED 	B		A	YECR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09		2063 			V16741		L1491739A			AT OVERHAUL, CRANKSHAFT GEAR COUNTERBORE WAS INSPECTED PER FAA AD 91-14-22.  NEW GEAR, P/N 13S19646, COULD NOT BE INSTAL	LED IN CRANKSHAFT DUE TO OUT-OF-TOLERANCE CONDITION OF DOWEL HOLE RADIAL POSITION IN CRANKSHAFT.  CRANKSHAFT WAS REPAIRE	D BY RELOCATING DOWEL HOLE .0035 INCH CLOSER TO CRANKSHAFT AXIS AND INSTALLING OVERSIZE DOWEL.  THIS IS THE EIGHTH EXAMP	LE OF THIS CONDITION NOTED BY THIS REPAIR STATION.			1	G	7	1 	3O	3	O		H10WE   	E274				 
1999030500038	19990305	00038	SW  	1999	3	5	99ZZZX757        	1	19990120	G	3212	206373901103	VALVE           			BELL  	407   	407         		SW  										FLOAT	LEAKING         	B			GS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	8694V	99   			191	53173				VALVE REPLACED WITH NEW DUE TO LEAK.						1	G	7	1 	3U			O	H2SW    					 
1999030500039	19990305	00039	SW  	1999	3	5	99ZZZX758        	1	19990107	G	6321	204076036005	BRAKE           			BELL  	412   	412EP       	1182205	SW  										MAIN ROTOR	LEAKING         	B			GS1R	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	03	4445V	11   			HR222	36211				BRAKE MASTER CYLINDER REPLACED WITH NEW DUE TO LEAK.						1	G	7	2 	4U				H4SW    					 
1999030500041	19990305	00041	SW  	1999	3	5	99ZZZX760        	1	19990125	G	3212		VALVE HOUSING   	AIRCRUISERS 	206050248117	BELL  	206   	206L1       	1182107	SW  										FLOAT	CRACKED         	B				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			NE	05	87TV	932  			0724	45572				FLOAT BAG FAILED 180-DAY LEAK TEST.  BAG WOULD NOT FULLY INFLATE.  PLASTIC HOUSING (BOSS) THAT RELIEF VALVE THREADS INTO	 CRACKED APPROXIMATELY 180 DEGREES AROUND HOUSING.  BAG MAY HAVE BEEN STEPPED ON OR EXTREME COLD TEMPS OR BOTH.					1	G	7	1 	3U				H2SW    					 
1999030500046	19990305	00046	GL  	1999	3	5	99ZZZX765        	3	19990120	G	6111		BLADE           			CESSNA	188   	188CESSNA   	2073002	CE  						MCAULY	2A34C	D2A34C98    	GL  	PROPELLER	CRACKED         	B			PI4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	07								750348		CRACK IN THIRD BLADE THREADS OF NR 1 HUB SOCKET.  DETECTED WITH EDDY CURRENT.  CAUSE UNKNOWN.						1	L	7	1 	3O				A9CE    		5	C	P3EA	 
1999030500047	19990305	00047	GL  	1999	3	5	99ZZZX766        	3	19990120	G	6111		BLADE           			CESSNA	188   	188CESSNA   	2073002	CE  						MCAULY	2A34C	B2A34C205   	GL  	PROPELLER	CRACKED         	B			PI4R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	07								850969		CRACK APPROXIMATELY THREE INCHES LONG INSIDE BOTTOM OF HUB (ABOVE STUDS).  DETECTED BY EDDY CURRENT DURING OVERHAUL.  CA	USE KNOWN.					1	L	7	1 	3O				A9CE    		5	C	P3EA	 
1999030500448	19990305	00448	CE  	1999	3	5	99ZZZX786        	1	19990202	G	3510	1015602041595	TUBE            			BEECH 	B300  	B300        	1159232	CE  										OXYGEN SYSTEM	DAMAGED         	B	P		JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	1084W	327  				FL144				REMOVED TUBE ASSEMBLY TO FACILITATE OTHER MAINTENANCE.  FOUND DOUBLE FLARE TOO LARGE FOR B-NUT TO SLIDE OVER FLARE.  B-N	UT WOULD THREAD ON FLARE AND TIGHTEN LEADING INSTALLER TO BELIEVE FLARE WAS TIGHT AGAINST FITTING WHEN IT WAS NOT.  THIS	 PART WAS INSTALLED AT THE MANUFACTURER WHEN THE AIRCRAFT WAS BUILT.				2	L	7	2 	4T			RT	A24CE   					 
1999030500449	19990305	00449	EU  	1999	3	5	99ZZZX787        	1	19990113	G	3411		LINE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										CABIN	CHAFED          	B	P	A	JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	800VC	4978 				NA0415				NR 2 AIR DATA P2 LINE HAS BEEN SLIGHTLY CHAFED BY THE ELEVATOR CONTROL CABLE.  IT APPEARS THE ELEVATOR CONTROL CABLE TUR	NBUCKLE SLAPS PITOT LINE FROM TIME TO TIME.  LINE IS NOT DAMAGED TO WARRANT REPLACEMENT.  LINE NEEDS TO BE MOVED TO INCR	EASE CLEARANCE.  THIS AREA IS NOT AN EASY AREA TO INSPECT DUE TO EQUIPMENT INSTALLED IN THIS AREA.				2	L	7	2 	4F			RT	A3EU    					 
1999030500451	19990305	00451	CE  	1999	3	5	99ZZZX789        	1	19990120	G	5320		WEB             			LEAR  	35    	35LEAR      	5170600	CE  										BS 160	CHAFED          	B	P		JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	31WS	8639 				O27				CHAFING DAMAGE TO LEFT AFT AREA OF NOSE WHEELWELL.  TUNNEL AT FRAME 5, FS 160.77 CAUSED BY STRUT BOLT INSTALLED IN WRONG	 DIRECTION.					2	L	7	2 	4F				A10CE   					 
1999030500452	19990305	00452	CE  	1999	3	5	99ZZZX790        	1	19990120	G	3250	99140807	STEERING UNIT   		406891      	CESSNA	650   	650         	2076802	CE  										NLG	MALFUNCTIONED   	B	P		JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	85DA	1246 				6500073				AIRCRAFT HAD A PROBLEM WITH NOSE WHEEL SHIMMY AFTER A NOSE TIRE CHANGE.  THE TIRE WAS REPLACED WITH A NEW NOSE TIRE.  AF	TER THIS, COUPLE OF INSTANCES WHERE THE LANDING GEAR WOULD NOT RETRACT.  UNABLE TO DUPLICATE LANDING GEAR NOT RETRACTING	 PROBLEM ALTHOUGH SUSPECTED THE NOSE STRUT CENTERING SWITCH WAS NOT GOING TO THE CENTER POSITION.  REMOVED THE STRUT TO 	INVESTIGATE WHEN STRUT WAS NOT CENTERING.  FOUND LOWER BEARING IN THE POWER STEERING HOUSING FOR THE PISTON AND PINION A	SSY, P/N 40689-1, FAILED.  LANDINGS, 1,089.		2	L	7	2 	4F				A9NM    					 
1999030500453	19990305	00453	EU  	1999	3	5	99ZZZX791        	1	19990128	G	3411	257SF20735	LINE            			BRAERO	DH125 	BAE125800A  	1500285	EU  										CABIN	CHAFED          	B	P		JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	596SW	2604 				258096				NR 2 AIR DATA P2 LINE HAS BEEN CHAFED BY THE ELEVATOR CONTROL CABLE.  IT APPEARS THE ELEVATOR CONTROL CABLE TURNBUCKLE S	LAPS PITOT LINE FROM TIME TO TIME.  LINE NEEDS TO BE MOVED TO INCREASE CLEARANCE.  THIS AREA IS NOT AN EASY AREA TO INSP	ECT DUE TO EQUIPMENT INSTALLED IN THIS AREA.				2	L	7	2 	4F			RT	A3EU    					 
1999030500454	19990305	00454		1999	3	5	99ZZZX792        	1	19990122	G	5320	5P32891	BEAM            																	FUSELAGE	CRACKED         	B	S		XQ2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	01										SIX PARTS DETECTED DURING MAGNETIC PARTICLE INSPECTION.  FATIGUE CRACKS.  REJECTED/RETURNED TO CUSTOMER.																			 
1999030500461	19990305	00461	CE  	1999	3	5	99ZZZX798        	1	19990114	G	2612	61423473275	FIRE DETECTOR   			BEECH 	200   	200BEECH    	1152920	CE  										ENGINE	FAILED          	B			RC0R	O				OTHER                   				N			FALSE WARNING             			TO	TAKEOFF        	1			SW	17	6507B	156  			2085	BB498				SIX EACH NEW FIRE DETECTORS INSTALLED IN JUNE '98 AT 8,233.9 HOURS.  FAILED NOVEMBER '98 AT 8,389.4 HOURS.  FAILED DEC '	98 AT 8,394.4 HOURS.  BOTH DETECTORS CAUSED IDENTICAL PROBLEMS.  'FIRE LIGHT FLICKER ON TAKEOFF'.  WHEN TROUBLESHOOTING 	WIRING, LIGHT WOULD FLICKER WHEN MOVING WIRING HARNESS ENTERING DETECTORS.  BELIEVE POSSIBLE BREAKDOWN IN SEALANT USED T	O ISOLATE CONNECTORS INTERNALLY.			1	L	7	2 	4T				A24CE   					 
1999030500462	19990305	00462	CE  	1999	3	5	99ZZZX799        	1	19990114	G	2612	61423473275	FIRE DETECTOR   			BEECH 	200   	200BEECH    	1152920	CE  										ENGINE	FAILED          	B			RC0R	O				OTHER                   				N			FALSE WARNING             			TO	TAKEOFF        	1			SW	17	6507B	156  			2084	BB498				SIX EACH NEW FIRE DETECTORS INSTALLED IN JUNE '98 AT 8,233.9 HOURS.  FAILED NOVEMBER '98 AT 8,389.4 HOURS.  FAILED DEC '	98 AT 8,394.4 HOURS.  BOTH DETECTORS CAUSED IDENTICAL PROBLEMS.  'FIRE LIGHT FLICKER ON TAKEOFF'.  WHEN TROUBLESHOOTING 	WIRING, LIGHT WOULD FLICKER WHEN MOVING WIRING HARNESS ENTERING DETECTORS.  BELIEVE POSSIBLE BREAKDOWN IN SEALANT USED T	O ISOLATE CONNECTORS INTERNALLY.			1	L	7	2 	4T				A24CE   					 
1999030500464	19990305	00464	EU  	1999	3	5	99ZZZX801        	1	19990201	G	2435	230651210	TERMINAL BLOCK  	LUCAS       	23079009    	BAG   	JETSTM	JETSTM3101  	1500215	EU  										START/GENERATOR	DAMAGED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	23	904FH				6431	613				STARTER/GENERATOR TERMINAL BLOCK WAS SEVERELY BURNED AND DAMAGED FROM SEVERE ARCING TO THE POINT OF BURNING PAINT ON LOW	ER COWLING.  TERMINAL BLOCK FELL APART WHEN TOUCHED.  POSSIBLE CAUSE:  ARCING FROM POWER TERMINAL TO BLOCK MOUNTING BOLT	S INTERNALLY WITHIN THE BLOCK.				2	L	7	2 	4T			RT	A21EU   					 
1999030500465	19990305	00465	WP  	1999	3	5	99ZZZX802        	2	19990126	G	7200		ENGINE          			RKWELL	NA265 	NA26565     	7630107	CE  	GARRTT	TFE731	TFE7313R    	01518	WP  					RIGHT	MALFUNCTIONED   	B			HAXR	E				ENGINE SHUTDOWN         				O			OTHER                     			NR	NOT REPORTED   	1			SW	11	91BZ					46519	P83141			ENGINE SHUT DOWN AT ALTITUDE BY PILOT.  METAL PARTICLES FOUND IN TAIL PIPE DURING ENGINE REMOVAL.  ENGINE FAN AND FAN TU	RBINE TURNED FREELY WITH NO NOISE.  ENGINE OIL TANK SERVICED ABOVE SITE GAUGE.  AIRFRAME TIME:  6,917.7 HOURS.  CYCLES: 	6,514.  RIGHT ENGINE TIME:  6,544.6 HOURS; CYCLES:  5,335.				2	L	7	2 	4J	4	F		A2WE    	E6WE				 
1999030500467	19990305	00467	CE  	1999	3	5	99ZZZX804        	1	19990121	G	3246	L610549	BEARING         	DUNLOP      	AHA1814     	RAYTHN	DH125 	HAWKER800XP 		CE  										NR 1 WHEEL	FAILED          	D				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			TX	TAXI/GRND HDL  	1			GL	17	880SP	985  			TW137	258298				PILOT NOTED ON GROUND, TAXI AIRCRAFT SEEMED TO PULL TO THE LEFT.  AT POST-FLIGHT, NOTED THE LEFT MAIN OUTBOARD WHEEL ASS	Y WAS SMOKING AND WAS VERY HOT TO THE TOUCH.  THE AIRCRAFT WAS ALSO HARD TO REPOSITION.  ON DISASSEMBLY OF THE LEFT OUTB	OARD WHEEL, DISCOVERED THE INNER WHEEL BEARING WAS DESTROYED.  ITEMS ALSO FOUND UNSERVICEABLE DUE TO THE BEARING FAILURE	; WHEEL ASSY, HEAT PACK, AXLE ASSY, AND MAXARET.			2	L	7	2 	4F			RT	A3EU    					 
1999030500468	19990305	00468	NE  	1999	3	5	99ZZZX805        	2	19990122	G	7200		ENGINE          			DOUG  	DC10  	DC1010      	3022110	WP  	GE    	CF6   	CF66D1A     	30020	NE  					NR 3	MALFUNCTIONED   	H				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			EU	01	572SC	56228				46977	451330			DELIVERY FLIGHT, POST-HEAVY MAINTENANCE, A POST-TROUBLE FREE 4 HOUR TEST FLIGHT, NR 3 ENGINE CONSUMPTION 3 QUARTS/HOUR A	T 95 PERCENT N1.  OIL WAS EXITING ENGINE AT CENTRAL JET PIPE BREATHER.  ENGINE WAS REMOVED AND SENT FOR INVESTIGATION. E	NGINE CYCLES:  18,228.				2	L	7	3 	4F	4	F		A22WE   	E23EA				 
1999030500471	19990305	00471	CE  	1999	3	5	99ZZZX808        	1	19990128	G	5610	10138402522	WINDSHIELD      			BEECH 	300   	300BEECH    	1152930	CE  										COCKPIT	CRACKED         	D				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			CE	03	100BG	2200 			95212H2645	FL6				AT FL 350, AFTER 3 HOURS OF CRUISE, THE COPILOT'S WINDSHIELD INNER PANE SHATTERED.  WINDSHIELD HEAT WAS 'ON' AND NO CABI	N PRESSURE CHANGES WERE MADE PRIOR TO FAILURE.					2	L	7	2 	4T				A24CE   					 
1999030500472	19990305	00472		1999	3	5	99ZZZX809        	4	19990201	G	3416	EA801A	ENCODER         			CESSNA	425   	425         	2076018	CE  										COCKPIT	MALFUNCTIONED   	B			FC6R	D				RETURN TO BLOCK         				O			OTHER                     			NR	NOT REPORTED   	1			NM	11	926FS				2313	4250093				ERRORS AFTER 2 HOUR FLIGHT AT 13,000 FEET.  REMOVED AND REPLACED WITH OVERHAULED UNIT.						1	L	7	2 	3T			RT	A7CE    					 
1999030500473	19990305	00473	CE  	1999	3	5	99ZZZX810        	1	19990208	G	7110	10191011339	SKIN            			BEECH 	300   	300BEECH    	1152930	CE  										COWL	DEBONDED        	D	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	09	1WV	3606 			0081	FA62				UPON PERFORMING POST-FLIGHT INSPECTION, FOUND LEFT OUTBOARD COWL DOOR DEBONDED FROM LOWER FORWARD CORNER UP 9.5 INCHES A	FT 4.25 INCHES, LOWER FORWARD SCREW WAS MISSING.  PILOT STATED SCREW WAS IN PLACE WHEN PRE-FLIGHT WAS PERFORMED.  OUTER 	SKIN BENT OUT.  TORN FROM LOWER FORWARD LATCH MOUNTING RIVET UP APPROXIMATELY .5 INCH, DOWN APPROXIMATELY .825 INCH.  CA	USE OF DEBOND UNKNOWN.			2	L	7	2 	4T				A24CE   					 
1999030500474	19990305	00474	SW  	1999	3	5	99ZZZX811        	1	19990112	G	2450		TRANSFORMER     	GE          	8KE1AE      	LKHEED	SP2   	SP2H        	5269601	SW  										COCKPIT	DAMAGED         	H				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			NM	05	4235N				3255121	144681				DURING A ROUTINE VFR TRAINING FLIGHT, THE CREW NOTICED A STRONG ODOR OF AN ELECTRICAL BURN.  THE AIRCRAFT ELECTRICAL SYS	TEM WAS TURNED OFF AND A LANDING MADE WITHOUT INCIDENT.  FAILURE OF THE G2 COMPASS AMPLIFIER WAS FOUND TO BE THE SOURCE.	  THE TRANSFORMER CONTAINED WITHIN HARD THERMAL DAMAGE INDICATED.  NO DAMAGE TO AIRCRAFT STRUCTURE.				2	M	7	4 	4R			RT	A15SW   					 
1999030500475	19990305	00475	CE  	1999	3	5	99ZZZX812        	1	19990127	G	2710		SUPPORT         			CESSNA	172   	172R        	2072401	CE  										COCKPIT	BINDING         	B		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	255HP	410  				17280308				CONTROL YOKE STICKING ON FLAREOUT AT LANDING.  FOUND LEFT GUIDE SUPPORT WAS PUSHED UP TO GIVE CLEARANCE FOR ROLLER ON CO	NTROL YOKE ASSY THAT WAS BINDING WHEN IT CAME OUT OF GUIDE ASSY.  ALSO, FOUND RIGHT GUIDE ASSY HAS BEEN SPREAD APART TO 	GIVE CLEARANCE FOR FORWARD AND AFT OPERATION.  REPLACED BOTH GUIDE ASSY, WAS UNABLE TO MOVE CONTROL YOKE.  REPLACED CONT	ROL YOKE.  OPS CHECKS NORMAL.  THE CONTROL YOKES ARE WELDED WRONG AND CESSNA SHOULD HAVE NOT RELEASED THIS AIRCRAFT UNTI	L GUIDES AND YOKE WERE REPLACED.  THIS COULD HAVE BEEN A FATAL ACCIDENT.		1	H	7	1 	3O			NT	3A12    					 
1999030500476	19990305	00476	SO  	1999	3	5	99ZZZX813        	1	19990113	G	3320	BCI0047019	LIGHT           	BRUCE       		GULSTM	G1159 	GIV         	3980115	SO  										GALLEY	INOPERATIVE     	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05	315GA	892  				1315				LAMP WAS INOPERATIVE.  AFTER GAINING ACCESS TO LAMP, FOUND THE BRUCE LIGHT BULB 'FLUORESCENT' WAS PUSHED OUT OF ITS SOCK	ET DUE TO THE MELTING OF THE PLASTIC RETAINING CAP.  THE P/N OF THE LAMP IS BR9800-009 DATED '96'.  THIS IS A GULFSTREAM	 FLEET PROBLEM PER CUSTOMER BULLETIN NR 98.  THESE LIGHTS SHOULD NOT BE INSTALLED IN AIRCRAFT.				2	L	7	2 	4F			RT	A12EA   					 
1999030500478	19990305	00478	CE  	1999	3	5	99ZZZX815        	1	19990121	G	7830	650161	SWITCH          	ROHR        	2250007511  	BEECH 	MU300 	400A        	1155402	CE  										LT THRST REVERSE	FAILED          	B			BUER	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	23	9PW	1642 				RK007				LEFT THRUST REVERSER WOULD NOT STOW AFTER LANDING, LEFT THRUST REVERSER CIRCUIT BREAKER WILL NOT RESET (OCCURRED ON LAND	ING).  REPAIRED BROKEN WIRE.					2	H	7	2 	4F			RT	A16SW   					 
1999030500479	19990305	00479	NM  	1999	3	5	99ZZZX816        	1	19990115	G	5320		THRESHOLD       			BOEING	727   	727259      	138408J	NM  										CABIN	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON L-1 DOOR THRESHOLD.						2	L	7	3 	4F				A3WE    					 
1999030500480	19990305	00480	NM  	1999	3	5	99ZZZX817        	1	19990115	G	5347		SEAT TRACK      			BOEING	727   	727259      	138408J	NM  										BS 480	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK STA 480 LBL 24.75.						2	L	7	3 	4F				A3WE    					 
1999030500481	19990305	00481	NM  	1999	3	5	99ZZZX818        	1	19990115	G	5320	65602082	FITTING         			BOEING	727   	727259      	138408J	NM  										BS 1183	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED UNDER TENSION TIE STA 1183, STR 29R.						2	L	7	3 	4F				A3WE    					 
1999030500482	19990305	00482	NM  	1999	3	5	99ZZZX819        	1	19990115	G	5320		STIFFENER       			BOEING	727   	727259      	138408J	NM  										BS 1183	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON VERTICAL STIFFENER ON 1183 BULKHEAD (BL ZERO).						2	L	7	3 	4F				A3WE    					 
1999030500483	19990305	00483	NM  	1999	3	5	99ZZZX820        	1	19990115	G	5347		SEAT TRACK      			BOEING	727   	727259      	138408J	NM  										BS 990-1030	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON SEAT TRACK OUTBOARD, STA 990 - STA 1030.						2	L	7	3 	4F				A3WE    					 
1999030500484	19990305	00484	NM  	1999	3	5	99ZZZX821        	1	19990115	G	5320		WEB             			BOEING	727   	727259      	138408J	NM  										BS 950-970	CORRODED        	B			KT3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	203AV					22474				DURING A C-CHECK, CORROSION WAS NOTED ON WEB AT STA 950F - STA 970, STR 29R.						2	L	7	3 	4F				A3WE    					 
1999030500486	19990305	00486	CE  	1999	3	5	99ZZZX823        	1	19990203	G	3610		DUCT            		45A635141   	MTSBSI	MU300 	MU300       	5780602	CE  										TAIL COMPARTMENT	CRACKED         	B			QMZR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	05	400GK					A019SA				AN INVESTIGATION WAS CONDUCTED TO DETERMINE THE CAUSE OF A VERY SUBSTANTIAL BLEED AIR LEAK IN THE TAIL COMPARTMENT.  THE	 LEAK WAS TRACED TO A DRILLED HOLE IN THE OUTER WALL OF THE 45A63514-1 VENTURI. THE VENTURI WAS REMOVED AND INSPECTED IN	TERNALLY.  THE INNER DUCT WAS CRACKED AT THE BASE OF THE CIRCUMFERENTIAL WELD ALL THE WAY AROUND THE TUBE.  THIS ALLOWED	 BLEED AIR TO LEAK INTO THE SPACE BETWEEN THE INNER AND OUTER TUBES AND EXIT THROUGH THE DRILLED HOLE.  THE DASH ONE HAS	 BEEN REPLACED BY A DASH ELEVEN ON WHICH THE OUTER TUBE IS ELIMINATED.		2	H	7	2 	4F			RT	A14SW   					 
1999031800003	19990318	00003	WP  	1999	3	18	99ZZZX824        	2	19990126	G	7230	30724021	BLADE           		30716529    	RKWELL	NA265 	NA26565     	7630107	CE  	GARRTT	TFE731	TFE7313R    	01518	WP  					COMPRESSOR	SEPARATED       	B	P		IY2R	E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			J			WARNING INDICATION        			CR	CRUISE         	1			SW	15	91BZ	6545 			8121122660	46519	P83141			DURING CRUISE AT FL 350, RT ENG HAD A RAPID RISE IN ITT AND VIBRATION LEVEL.  CREW SHUT DOWN ENG.  ENG REMOVED TO DETERM	INE CAUSE OF FAILURE ANDTO REPAIR.  DISASSY REVEALED ON LOW PRESS, 4TH STAGE COMP BLADE, P/N 3072402-1, 'MISSING' FROM C	OMP ROTOR.  BLADE DEBRIS CAUSED EXTENSIVE DOWN STREAM DAMAGE.  BLADE RELEASE CAUSED BY CRACKING OF THE BLADE DOVETAIL, W	HICH IS RESULT OF AN UPSTREAM EXCITATION FROM 4 DIFFUSER STRUTS AFT OF LP COMP, 4TH STAGE STATOR ASSY.  CRACK ALLOWED BL	ADE TO EXIT DISC DOVETAIL.  ALLIED SIGNAL ISSUED SB TFE731-72-3483, WHICH INCORP NEW 4TH STAGE STATOR, P/N 3074555-8.  N	EW STATOR HAS ONE ADDITIONAL VANE (83 TO 84) AND EXIT ANGLE CHANGE IN 54 LOCATIONS COINCIDENT WITH 4 DOWNSTREAM STRUTS.	2	L	7	2 	4J	4	F		A2WE    	E6WE				 
1999030500487	19990305	00487	EA  	1999	3	5	99ZZZX825        	1	19990127	G	3610		BLEED AIR LINE  			CNDAIR	CL600 	CL6002B16   	1900305	EA  										NR 2 ENGINE	SEPARATED       	B				A				UNSCHED LANDING         				J			WARNING INDICATION        			NR	NOT REPORTED   	1			GL	09	449ML					5022				14TH STAGE BLEED AIR LINE CAME LOOSE ON NR 2 ENGINE.  THIS HAPPENED IN-FLIGHT.  PILOT POWERED BAD ENGINE AND LANDED UNEV	ENTULLY IN BTL.  BLEED AIR DAMAGED COWL AND WIRE HARNESS.  PARTS REPLACED AS NECESSARY.  AIRCRAFT TEST FLOWN.   CAUSE UN	KNOWN.  ACFT:  6,039 HOURS.				2	L	7	2 	4F			RT	A21EA   					 
1999030500488	19990305	00488	EA  	1999	3	5	99ZZZX826        	1	19990106	G	7110	22850142602	COWL            			CNDAIR	CL600 	CL6002B19   		EA  										RT ENGINE	CHAFED          	B			SH5R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03	5100X	4725 				7008				RIGHT ENGINE, UPPER CORE COWL IS CHAFING ON OIL TANK LEVEL INDICATOR DUE TO IMPROPER POSITION OF LEVEL INDICATOR.  CHAFE	 DAMAGE WAS  CORRECTED BY BLENDING IAW RJ SRM CSP A-008.  LANDINGS:  6,453.					2	L	7	2 	4F			RT	A21EA   					 
1999030500489	19990305	00489	EU  	1999	3	5	99ZZZX827        	1	19990125	G	2520		PAN             		3410        	AIRBUS	320   	A320232     	3930326	EU  										CABIN	CRACKED         	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	409UA					462				DURING FIRST HEAVY MAINT VISIT (HMV-1), ALL COACH SEATS IN PAX CABIN WERE FOUND WITH CRACKED SEAT PANS AT FWD ATTACH HOL	ES FOR SEAT PAN.  THESE ARE RECARO 720 SERIES SEATS INSTALLED IN A320232.  SEAT MFG DESIGNATES THE SEAT PAN AS PRIMARY S	TRUCTURE FOR SEAT.  SEAT PANS ARE BEING REPLACED WITH NEW SEAT PANS WITH SAME DESIGN.  THESE SEAT PANS WILL CRACK IN SAM	E PLACES DURING THEIR SERVICE LIFE.  SUBMITTER STATED AD SHOULD BE ISSUED TO INSPECT THESE SEAT PANS FOR CRACKS EACH 90 	DAYS, AND FOR REMOVAL FROM SERVICE OF ANY SEAT PANS THAT ARE CRACKED.  THERE ARE 132 OF THESE SEAT PANS ON ACFT.  THIS I	S 8TH CONSECUTIVE A320232 THAT HAS EXHIBITED A 100 PERCENT FAILURE RATE OF THESE SEAT PANS THAT EQUALS 1,056 FAILURES.	2	L	7	2 	4F			RT	A28NM   					 
1999031200403	19990312	00403	GL  	1999	3	12	99ZZZX856        	1	19990128	G	6320	28131709R	GEARBOX         			ENSTRM	F28   	F28F        	3300412	GL  										MAIN ROTOR	MAKING METAL    	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	17	52PD	1901 	701  		5733494T	807				2.5 HOURS AFTER OIL CHANGE, M/R GEARBOX HAD CHIP LIGHT.  LARGE FLAKES, BLACK OIL, SMELLED BURNT.  OIL LEVEL CORRECT.  OI	L SAMPLE TAKEN.					1	G	7	1 	3O				H1CE    					 
1999031200404	19990312	00404	NE  	1999	3	12	99ZZZX857        	2	19990127	G	7230	738181	BEARING         								PWA   	JT8   	JT8D219     	52053	NE  					ENGINE	FAILED          	B			RA1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	05			6295 		7116		P716761			ENGINE REMOVED FROM SERVICE DUE TO A GROUND OPERATIONAL FIRE.  DISASSEMBLY OF THE ENGINE REVEALED AN INTERNAL OIL FIRE A	ND NR 6 BEARING FAILURE.  FAILURE INVESTIGATION IS IN PROGRESS AT GE ENGINE SERVICES - DALLAS.										4	F			E9NE				 
1999031200405	19990312	00405	WP  	1999	3	12	99ZZZX858        	2	19990126	G	7230	31013751	BEARING         			SWRNGN	SA226 	SA226TC     	8780404	SW  	GARRTT	TPE33 	TPE3313U303G	01514	WP  					COMPRESSOR	FAILED          	B			K2TR	O				OTHER                   				O			OTHER                     			AP	APPROACH       	1			SW	11	509SS	650  				TC206	P03297			AIRCRAFT WAS ON APPROACH WHEN LOSS OF POWER WAS NOTED.  UPON LANDING, ENGINE QUIT (LOCKED UP).  MALFUNCTION - COMPRESSOR	 BEARING FAILURE CAUSING COMPLETE ENGINE DESTRUCTION.  NOTE:  S.O.A.P. SAMPLE TAKEN APPROXIMATELY 30 HOURS EARLIER WAS N	ORMAL.  SUBMITTER RECOMMENDED REDUCED LIFE LIMITATION FROM 3600 HRS TO 1000 HRS OR LESS.  MANDATORY COMPLIANCE OF SB 72-	1074.  INSTALLATION OF P/N 3101405-1 OR SB 72-0634 INSTALLING P/N 3103708-1.			2	L	7	2 	4T	4	T	RT	A8SW    	E4WE				 
1999031200407	19990312	00407	EU  	1999	3	12	99ZZZX860        	1	19990202	G	2520	3410	SEAT            			AIRBUS	320   	A320232     	3930326	EU  										CABIN	CRACKED         	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	408UA					457				DURING FIRST HMV-1 FOR THIS ACFT, ALL COACH SEATS IN PAX CABIN WERE FND CRACKED AT FWD ATTACHMENT HOLES OF THE SEAT PAN.	  THESE ARE RECARO 720 SERIES SEATS INSTALLED.  SEAT MFG DESIGNATES SEAT PAN AS PRIMARY STRUCTURE IN ITS COMPT MM.  SEAT	 PANS BEING REPLACED WITH NEW SEAT PANS THAT ARE OF SAME DESIGN.  THESE SEAT PANS WILL FAIL (CRACK) IN SAME PLACES DURIN	G THEIR SERV LIFE.  SUBMITTER STATED AD SHOULD BE ISSUED TO INSPECT THESE SEAT PANS FOR CRACKS EACH 90 DAYS AND FOR REMO	VAL FROM SERVICE OF SEAT PANS THAT ARE CRACKED.  THERE ARE 132 OF THESE SEAT PANS ON ACFT.  THIS IS 9TH CONSECUTIVE A320	232 THAT HAS EXHIBITED A 100 PERCENT FAILURE RATE OF THESE SEAT PANS.  THAT IS 1,188 DEFECTIVE SEAT PANS IN 6 MONTHS.	2	L	7	2 	4F			RT	A28NM   					 
1999031200408	19990312	00408	SO  	1999	3	12	99ZZZX861        	1	19990119	G	5410	12003852D01	FRAME           			EMB   	120   	EMB120RT    		SO  										RT/LT	CRACKED         	B			WVER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	09	243AS					120072				DURING ROUTINE MAINTENANCE CHECKS, A CRACK WAS FOUND ON BOTH ENGINE NACELLES' FRAME 1.  THE CRACK IS LOCATED ON THE LOWE	R SIDE OF THE STIFFENING WEB BETWEEN THE TOP OUTBOARD MOUNTING BOLT HOLE AND THE OUTBOARD EDGE OF THE FRAME.  RECOMMEND 	REPLACING BOTH FRAMES, AND CONTINUE MONITORING IAW EXISTING MAINTENANCE CHECKS.				2	L	7	2 	4T			RT	A31SO   					 
1999031200409	19990312	00409	SO  	1999	3	12	99ZZZX862        	1	19990119	G	5400	12030995	ANGLE           			EMB   	120   	EMB120RT    		SO  										LT/RT NACELLE	BROKEN          	B			WVER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	09	243AS					120072				DURING C-CHECK INSPECTION, THE FRAME 2 ANGLE WAS FOUND BROKEN ON BOTH LEFT AND RIGHT NACELLES.  REPLACED THE ANGLE AND W	ILL CONTINUE MONITORING IAW EXISTING C-CHECK INSPECTIONS.					2	L	7	2 	4T			RT	A31SO   					 
1999031200410	19990312	00410	SO  	1999	3	12	99ZZZX863        	1	19990119	G	5320	12019522001	BRACKET         			EMB   	120   	EMB120RT    		SO  										BS 14280/14615	BROKEN          	B			WVER	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	09	243AS					120072				FS X14280.0 AND FS X14615.0 FUSELAGE FRAMES ATTACH TO CARGO DOOR OPENING UPPER FRAME WITH SUPPORT BRACKETS P/N 120-19522	-D01.  BRACKETS UPSTANDING FLANGES SEPARATED COMPLETELY AT BOTH FRAME STATIONS.  POSSIBLE CAUSE IS FRETTING CORROSION. C	ARGO BAY LINER AND INSULATION MUST BE REMOVED TO ALLOW INSPECTION IN THIS AREA.				2	L	7	2 	4T			RT	A31SO   					 
1999031200411	19990312	00411	WP  	1999	3	12	99ZZZX864        	2	19990112	G	7250	30727121	BLADE           			LEAR  	35    	35LEAR      	5170600	CE  	GARRTT	TFE731	TFE73122B   	01518	WP  					TURBINE	FAILED          	B		A	IY2R	A	E			UNSCHED LANDING         	ENGINE SHUTDOWN         			J			WARNING INDICATION        			CR	CRUISE         	1			SW	15	190GC	3281 				35014	P74146			DURING CRUISE, ENG EXPERIENCED VIBRATION AND RAPID RISE IN ITT.  CREW SHUT DOWN ENGINE.  ENG TEAR-DOWN REVEALED STRESS R	UPTURE OF HIGH PRESS TURBINE BLADE, P/N 3072712-1.  BLADE HRS 3,280.8.  SUBMITTER STATED APROX 35 CATASTROPHIC FAILURES 	HAVE OCCURRED IN 1998.  ALLIED SIGNAL HAS ISSUED TFE731 SPECIAL PROGRAM NUMBER FIVE TO ENSURE ALL MAINT ACTION OCCURS AT	 THEIR CONTROLLED MAINT FACILITIES.  SUBMITTER RECOMMENDS FAA ENG ISSUE AD TO LIMIT OPERATING HRS TO 1,500 HRS FOR ALL T	FE731-2-1C (FALCON 10/100) AND 2,800 HRS FOR ALL TFE731-2-2B POWERPLANTS WHICH POWERS LEAR 30 SERIES ACFT.  REF:  W.O. N	R GR2-317.	2	L	7	2 	4F	4	F		A10CE   	E6WE				 
1999031200412	19990312	00412	NE  	1999	3	12	99ZZZX865        	3	19990112	G	6111	A32041	SET SCREW       			DORNER	DO32  	DO328100    	2996000	NM  						HARTZL	HDE6C	HDE6C3B     	NE  	PROPELLER BLADE	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	05		1330 						HL234		PROPELLER S/N HL234 WAS RETURNED FOR FAILURE TO DYNAMIC BALANCE.  AFTER DISASSEMBLY, INSPECTION REVEALED 1 BROKEN A-3204	-1 PRELOAD SET SCREW.  THE B-3368 LOCKNUT WAS STILL ATTACHED TO THE INBOARD SECTION OF THE A-3204-1 SCREW.  THE SCREW WA	S REMOVED, SENT TO HARTZELL ENGINEERING FOR EVAULUATION AND REPLACED WITH NEW.  THE C-6066-1 PRELOAD PLATE THREAD WAS DA	MAGED, BUT WITHIN ACCEPTABLE LIMITS AND THE PLATE WAS REPAIRED AND RETURNED TO SERVICE.			2	H	7	2 	4T			RT	A45NM   		6	C	P34NE	 
1999031200419	19990312	00419	CE  	1999	3	12	99ZZZX872        	1	19990116	G	3233	58202085	ACTUATOR        	POINTER     		BEECH 	200   	200BEECH    	1152920	CE  										MLG	MISOVERHAULED   	B				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SO	11	503WJ				22779	BB503				INSTALLED OVERHAULED ACTUATOR AND DURING RIGGING OF GEAR HEARD POPPING NOISE. STARTED LOOKING FOR NOISE AND FOUND CLEVIS	 BINDS IN NUT.					1	L	7	2 	4T				A24CE   					 
1999031200420	19990312	00420	NE  	1999	3	12	99ZZZX873        	2	19990122	G	7421	CPW3039828	IGNITER         			CESSNA	500   	550         	2076604	CE  	PWA   	JT15  	JT15D4      	52112	NE  					ENGINE	DAMAGED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	37201	132  			9753859	5500655	PCE71540			IGNITERS WERE REMOVED FOR INSPECTION AND CENTER ELECTRODE APPEARED TO BE MISSING ON ONE OF THE IGNITERS.  FURTHER INVEST	IGATION SHOWED THAT WHEN LEAD WAS REMOVED FROM IGNITER, THE CENTER ELECTRODE WAS LOOSE INSIDE THE IGNITER AND PULLED PAR	TIALLY OUT CAUSING THE FIRING END TO RECEDE INTO THE IGNITER SHELL GIVING THE APPEARANCE THAT IT WAS MISSING.  THERE WAS	 ALSO WHITE POWDER INSIDE THE END WHERE THE LEAD CONNECTS.  THE LEAD WAS NOT FUSED TO THE ELECTRODE AS SEEN IN THE PAST,	 IT LOOKS LIKE THE CERAMIC WAS NOT BONDED TO THE ELECTRODE AND THE LEAD WAS HOLDING EVERYTHING IN PLACE.		1	L	7	2 	4F	4	F		A22CE   	E1NE				 
1999031200421	19990312	00421	NE  	1999	3	12	99ZZZX874        	3	19990120	G	6111	57D0495	FORK            			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	PITCH CHANGE	CRACKED         	B			EY2R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	03		2221 			3082			HJ153A		FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS.  TWO CRACKS.						2	L	7	2 	4T			RT	A24CE   		5	C	P10NE	 
1999031200425	19990312	00425	WP  	1999	3	12	99ZZZX876        	2	19990201	G	7261	30722311	HOUSING         			BRAERO	DH125 	BAE125800A  	1500285	EU  	GARRTT	TFE731	TFE7315R    	01518	WP  					OIL FILTER	CRACKED         	B	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99	861CE	6949 								HAIR LINE CRACK FOUND IN RADIUS OF OIL FILTER HOUSING.						2	L	7	2 	4F	4	F	RT	A3EU    	E6WE				 
1999031200426	19990312	00426	EA  	1999	3	12	99ZZZX877        	1	19990107	G	2432	237BC1011	BATTERY CHARGER 			CNDAIR	CL600 	CL6002B16   	1900305	EA  										APU BAY	DAMAGED         	C	L			O				OTHER                   				B	J		SMOKE/FUMES/ODORS/SPARKS  	WARNING INDICATION        		CR	CRUISE         	1			WP	27	14R	859  			204	5319				ACFT EN ROUTE, HAD AN 'APU BATT CHGR FAIL' STATUS MESSAGE.  CREW SELECTED ELEC SYNOPTIC PAGE AND BATTERY WAS NOT CHARGIN	G.  THROUGHOUT FLT, MESSAGE CAME AND WENT AT LEAST 5 TIMES.  AFTER SEVERAL OCCURRENCES, CB TRIPPED.  CREW DID NOT RESET.	  ONCE ON GROUND, CREW ATTEMPTED TO RESET CB AND IT TRIPPED IMMEDIATELY.  MX INVEST FOUND HARNESS TO THE APU BATT CHARGE	R MELTED AND FUSED.  AREA AROUND BATT CHARGER OF APROX 10 SQUARE INCHES WAS BLACKENED FROM HEAT.  MX INVEST FOR ANY CHAF	ING ON ADJ STRUCT AND NONE FOUND.  BATT CHARGER INSP, SEVERAL CONN PINS ON J11PA MELTED.  APU BATT CHARGER REPLACED.  HA	RNESS BETWEEN CHARGER AND BATT REPLACED.  ALL WIRING INSPECTED AND REPAIRED.  P/N ON, 237BC101-1, S/N 558.	2	L	7	2 	4F			RT	A21EA   					 
1999031200427	19990312	00427	EU  	1999	3	12	99ZZZX878        	1	19990205	G	3340	G99301FFS	BEACON          			HWKSLY	DH125 	DH1251A     	4230106	EU  										FUSELAGE	SHORTED         	B				O				OTHER                   				O	K		OTHER                     	FLUID LOSS                		NR	NOT REPORTED   	1			SW	15	10D					25029				PILOT REPORTED THAT STROBE CIRCUIT BREAKER TRIPPED.  UPON INVESTIGATION, THE LOWER STROBE FOUND TO BE BURNED UP.  SIGNS 	OF FUEL WERE FOUND IN THE AREA.  SURMISE THAT HIGH VOLTAGES FOUND IN STROBE, IGNITED THE FUEL TRAPPED IN THE STROBE.  TH	E FUEL LEAK WAS REPAIRED BEFORE NEW STROBE WAS INSTALLED.  SUBMITTER STATED EVEN IF A FUEL LEAK IS WITHIN MAINTENANCE MA	NUAL ALLOWANCES, IT MUST BE ASCERTAINED THAT THERE IS NO DANGER FOR FUEL IGNITION AT THE LOWEST POINT WHERE FUEL CAN COL	LECT.		2	L	7	2 	4J				A3EU    					 
1999031200431	19990312	00431	CE  	1999	3	12	99ZZZX882        	1	19990201	G	3411		PITOT           			RAYTHN	DH125 	HAWKER800XP 		CE  										PITOT/STATIC SYS	CORRODED        	B	P		JGVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	09	1910H	844  				258318				DURING COMPLETION OF RAYTHEON RIL MODIFICATION PITOT/STATIC DRAIN VALVES, RESERVOIR S8 WAS FOUND WITH CORROSION ON THE I	NSIDE OF THE RESERVOIR BODY.  RESERVOIR BODY WAS REPLACED.  THIS AIRCRAFT IS LESS THAN 2 YEARS OLD.					2	L	7	2 	4F			RT	A3EU    					 
1999031200432	19990312	00432	CE  	1999	3	12	99ZZZX883        	1	19990105	G	2840	10038006151	FUEL PROBE      			BEECH 	200   	B200        	1152922	CE  										FUEL SYSTEMS	MALFUNCTIONED   	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	401HC				4514	BB1294				FUEL PROBE MALFUNCTIONED.						1	L	7	2 	4T				A24CE   					 
1999031200433	19990312	00433	CE  	1999	3	12	99ZZZX884        	1	19990105	G	2823	1013890253	VALVE           			BEECH 	200   	B200        	1152922	CE  										FUEL SOV	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	401HC				1229	BB1294				FUEL SHUT-OFF VALVE FAILED.						1	L	7	2 	4T				A24CE   					 
1999031200434	19990312	00434	CE  	1999	3	12	99ZZZX885        	1	19990105	G	2840	10038006119	FUEL PROBE      			BEECH 	200   	B200        	1152922	CE  										FUEL SYSTEM	MALFUNCTIONED   	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	401HC				2364	BB1294				FUEL PROBE MALFUNCTIONED						1	L	7	2 	4T				A24CE   					 
1999031200669	19990312	00669	SW  	1999	3	12	99ZZZX895        	1	19990128	G	7160	206064819006	DOOR            		206064819159	BELL  	407   	407         		SW  										COWL	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467AL	1913 				53190				ROUTINE INSPECTION.  EXCESSIVE CORROSION (INTERGRANULAR).						1	G	7	1 	3U			O	H2SW    					 
1999031200670	19990312	00670	SW  	1999	3	12	99ZZZX896        	1	19990126	G	6420	406312100101	BEARING         		407012101107	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427AL	1284 			A257	53107				TAIL ROTOR ASSEMBLY WAS REMOVED FOR WORN BEARINGS.  FOUND THE TWO INBOARD BEARINGS BADLY WORN. THE OUTER RACE LINERS DEB	ONDED.  THREE T/R HUBS HAVE BEEN FOUND IN THIS CONDITION.  BEARING KEPT FOR POSSIBLE EVALUATION.  RECOMMEND:  REMOVE T/R	 BLADES AND INSPECT INBOARD BEARINGS EVERY 800 HOURS.  REPLACED TWO EACH BEARINGS.				1	G	7	1 	3U			O	H2SW    					 
1999031200671	19990312	00671	SW  	1999	3	12	99ZZZX897        	1	19990128	G	7160	206064819005	DOOR            		206064819159	BELL  	407   	407         		SW  										COWL	CORRODED        	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467AL	2203 				53190				ROUTINE INSPECTION, FOUND INTERGRANULAR CORROSION.						1	G	7	1 	3U			O	H2SW    					 
1999031200672	19990312	00672	SW  	1999	3	12	99ZZZX898        	1	19990126	G	6710	206001564001	SERVO WEB       			BELL  	206   	206L1       	1182107	SW  										SUPPORT EARS	DAMAGED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1084Y				RH0396	45433				DURING REFURBISHING, FOUND DAMAGE IN SERVO MOUNTING EARS CAUSED BY ROD END CONTACTING SUPPORT.						1	G	7	1 	3U				H2SW    					 
1999031200673	19990312	00673	SW  	1999	3	12	99ZZZX899        	1	19990128	G	5302	407023800118	SUPPORT         		407030801101	BELL  	407   	407         		SW  										TAILBOOM	CRACKED         	B			ALGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	497AL	84   				53172				DAILY INSPECTION, FOUND APPROXIMATELY .8750 INCH CRACK IN RADIUS.  OEM PART DOES NOT FIT PROPERLY CAUSING UNDO STRESS.						1	G	7	1 	3U			O	H2SW    					 
1999031200683	19990312	00683	SW  	1999	3	12	99ZZZX908        	1	19990308	G	5302		SKIN            			BELL  	407   	407         	1182206	SW  										TAILBOOM	CRACKED         	B	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	547AL					53240				AFTER FINAL FLIGHT OF THE DAY DURING POST-FLIGHT INSPECTION, A CRACK IN THE TAILBOOM, PN 407-030-801-101, SN 53239, TT: 	 1,621.3 HOURS, WAS FOUND.  THE CRACK INITITATED FROM THE FORWARD EDGE OF THE HORIZONTAL STABILIZER MOUNT AREA.  THE TAI	LBOOM IS CURRENTLY HELD AT THE AIR LOGISTICS, LLC FACILITY IN NEW IBERIA, LA.				1	G	7	1 	3U			O	H2SW    					 
1999031901096	19990319	01096	SO  	1999	3	19	99ZZZX913        	2	19990124	G	8520	A40083	MASTER ROD      			BOEING	75    	A75N1       	1380134	CE  	CONT  	R670  	W67016      	17016	SO  					ENGINE	CRACKED         	G	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	4935N		200  			752087	13773			MASTER ROD, PN A40083, BROKE AT BASE OF ROD POSSIBLY TO DUE METAL FATIGUE.  METAL APPEARS TO HAVE BEEN CRACKED FOR SOME 	TIME PRIOR TO FAILURE EVIDENCED BY GRAY AREA AT SEPARATION AND LARGE AREA OF NON-DUCTILE METAL SEPARATION.  MASTER ROD I	NSTALLED 219 HRS TSO.  ROD HAD BEEN MAGNAFLUXED AS REQUIRED BY OHM.  ENG HAD BEEN ON AN OIL SAMPLING PROGRAM AND SHOWED 	NO EVIDENCE OF AN ALERT REQUIRED.			1	Q	7	1 	3R	3	R		A743    	E162				 
1999031901100	19990319	01100	CE  	1999	3	19	99ZZZX917        	1	19990216	G	3250	25430121	BELLCRANK       		2543001200  	CESSNA	303   	T303        	2073820	CE  										NLG STEERING	CRACKED         	H	P	A		O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			EU	01	LVVEL	2281 				00258				THE PILOT REPORTED AIRCRAFT DID NOT TURN LEFT ON GROUND.  AIRCRAFT RETURNED TO SERVICE STATION FOR INSPECTION.  INSPECTI	ON REVEALED CRACK ON STEERING BELLCRANK, LEFT ARM OF BELLCRANK SEPARATE OF ASSY.					1	L	7	2 	3O				A34CE   					 
1999031901101	19990319	01101	SO  	1999	3	19	99ZZZX918        	2	19990205	G	8530	654651A8STL	CYLINDER        								CONT  	O520  	IO520D      	17032	SO  					ENGINE	MISMANUFACTURED 	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	07										AT INSTALLATION HOLE WHERE FUEL INJECTOR MOUNTS WAS FOUND TO NOT HAVE ANY THREADS.  POSSIBLE CAUSE IS LACK OF QUALITY CO	NTROL IN THE MACHINING PROCESS AT THE FACTORY.										3	O			E5CE				 
1999031901102	19990319	01102		1999	3	19	99ZZZX919        	1	19990201	G	2500	440785	SEAT BELT       	AMERICANSFTY																COCKPIT	MALFUNCTIONED   	H	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99										INSPECTED AIRCRAFT FOR AD 98-25-10 AND FOUND NOT APPLICABLE BY NOT BEING INSTALLED.  FURTHER INSPECTION SHOWED 8 OF 84 S	EAT BELTS INSPECTED HAD BUCKLES WITH WEAK LATCH SPRINGS.  LATCHES IN BUCKLES WITH WEAK SPRINGS DID NOT FULLY ENGAGE WITH	 THE BASE.  THE SEAT BELTS SEEMED TO LOCK FIRMLY, BUT THEY WERE NOT LOAD TESTED.  SEAT BELT WAS SENT TO BUCKLE FOR EVALU	ATION.  RECOMMEND BUCKLES WITH WEAK SPRINGS BE REPAIRED OR REPLACED.																 
1999031901103	19990319	01103	NE  	1999	3	19	99ZZZX920        	2	19990211	G	7250	2A0851	SEAL            								IAE   	V2500 	V2500A1     		NE  					NR 4 BEARING	CRACKED         	B			WNFR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03					V0201					TURBINE SEAL CRACKED.											4	F			E311NE				 
1999031901104	19990319	01104	NE  	1999	3	19	99ZZZX921        	3	19990129	G	6111	57D0495	FORK            			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	PITCH CHANGE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	99		8219 	4517 		2239NR			HJ287		FORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS.  FOUR EACH CRACKS.						2	L	7	2 	4T			RT	A24CE   		5	C	P10NE	 
1999031901105	19990319	01105	SO  	1999	3	19	99ZZZX922        	2	19990208	G	8520	643626A103	PIN             								CONT  	O520  	TSIO520H    	17040	SO  					ENGINE	MISMANUFACTURED 	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NE	03					H119702N		19871571H			NEW VAR TYPE CRANK WAS RECEIVED TO REPLACE A NON-VAR TYPE.  COUNTERWEIGHTS WERE AS INSTALLED BY TCM.  COUNTERWEIGHTS WER	E REMOVED TO CHECK PIN SIZES AND PART NUMBERS TO MAKE SURE TCM INSTALLED THE CORRECT ONES AND IN THE PROPER LOCATIONS. S	UBMITTER FOUND THE TWO 4TH ORDER PINS P/N 643626-A103 WERE .0005 INCH UNDERSIZE ON THE DIAMETER PER TCM SB 89-24.									3	O			E8CE				 
1999031901106	19990319	01106	EU  	1999	3	19	99ZZZX923        	1	19990121	G	3230	A23802102	SWITCH          			AMD   	FALC20	FALCON      	2720302	EU  										LT MLG WW	BROKEN          	B				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			GL	09	100AS					274				SWITCH DID NOT INDICATE A DOWN AND LOCKED POSITION DURING GEAR EXTENSION.  REPLACED SWITCH WITH NEW, OPS CHECKED OK.						2	L	7	2 	4F				A7EU    					 
1999031901107	19990319	01107	CE  	1999	3	19	99ZZZX924        	1	19990113	G	2612	872224	HARNESS         			MTSBSI	MU2   	MU2B35      	5780411	CE  	GARRTT	TPE331	TPE3316252M 	01514	NE  					ENGINE	DAMAGED         	D				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			SW	15	113SD					600	P20199			FOUND FIRE DETECT CABLE GROUNDED DUE TO CONDITION OF CABLE, CHANGE CABLE BEFORE REACHING SAME CONDITON.  THE RIGHT ENGIN	E'S, P-20199, FIRE LIGHT CAME ON IN-FLIGHT.  THE ENGINE WAS SHUT DOWN AND THE PLANE WAS RETURNED TO DFW.  THERE WAS NO I	NDICATION OF FIRE AND PROBLEM WAS NOT DUPLICATED ON GROUND.				1	H	7	2 	3T			RT	A10SW   	E2WE				 
1999031901108	19990319	01108	SW  	1999	3	19	99ZZZX925        	1	19990201	G	3610		MUFFLER         			GULSTM	114   	114B        	O145001	SW  										EXHAUST	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	114PW					14542				MUFFLER/HEAT EXCHANGER END FLANGE SEPARATED FROM THE MUFFLER HOUSING CAUSING LARGE AMOUNTS OF EXHAUST TO ENTER THE CABIN	.  PART TT:  1,711.4 HOURS.  MUFFLER MIGHT HAVE BEEN REPAIRED BY WELDING ON THE OUTSIDE OF BOTH THE FLANGES.  SUBMITTER 	SUGGESTED NEW STYLE MUFFLER OR REPETATIVE INSPECTIONS.				1	L	7	1 	3O			RT	A12SO   					 
1999031901109	19990319	01109	SO  	1999	3	19	99ZZZX926        	1	19990128	G	2434	ALU8421R5	ALTERNATOR      			PIPER 	PA46  	PA46350P    		SO  										ENGINE	CRACKED         	B			LF1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	126SR	258  				4622036				PILOT NOTED LEFT ALTERNATOR BELT TENSION LOOSE AND FOUND ALTERNATOR BROKEN AT MOUNT EAR.  INSPECTED INSTALLATION AND FOU	ND LYCOMING SI 1451 HAD BEEN C/W.  HOWEVER, WEAR WAS FOUND AT FREON COMPRESSOR WHERE LINK BETWEEN ALTERNATOR AND COMPRES	SOR ATTACHES.  THIS INSTALLATION SEEMS VERY PRONE TO WEAR EVEN THOUGH HARDWARE IS SEVERELY TIGHTENED.  SUBMITTER STATED 	SIMILAR PROBLEMS USED TO OCCUR ON RT SIDE UNTIL LYC SB 511 WAS ISSUED.  UNTIL SYSTEM IS RE-DESIGNED, RECOMMEND CHECKING 	TORQUE OF HARDWARE AT EACH OIL CHANGE.		1	L	7	1 	3O			RT	A25SO   					 
1999031901110	19990319	01110	SO  	1999	3	19	99ZZZX927        	1	19990111	G	5720	4301600	SUPPORT         			PIPER 	PA31  	PA31350     	7103110	SO  										WING	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	132MF					317752072				DURING A VISUAL INSPECTION OF THE WING, A CRACK WAS NOTED IN THE UPPER PORTION OF THE INBOARD WING BETWEEN THE FUSELAGE 	AND THE NACELLE (WS 49.0).  FURTHER INVESTIGATION SHOWED THE TWO SUPPORT ANGLES THAT HOLD THE LANDING GEAR BUMPER ASSY (	P/N 43016-00 AND P/N 43016-01) WERE CRACKED IN THE RADIUS OF THE SUPPORTING CHANNEL.				1	L	7	2 	3O				A20SO   					 
1999031901111	19990319	01111	SO  	1999	3	19	99ZZZX928        	1	19990111	G	5720	4301601	SUPPORT         			PIPER 	PA31  	PA31350     	7103110	SO  										WING	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	132MF					317752072				DURING A VISUAL INSPECTION OF THE WING, A CRACK WAS NOTED IN THE UPPER PORTION OF THE INBOARD WING BETWEEN THE FUSELAGE 	AND THE NACELLE (WS 49.0).  FURTHER INVESTIGATION SHOWED THE TWO SUPPORT ANGLES THAT HOLD THE LANDING GEAR BUMPER ASSY (	P/N 43016-00 AND P/N 43016-01) WERE CRACKED IN THE RADIUS OF THE SUPPORTING CHANNEL.				1	L	7	2 	3O				A20SO   					 
1999031901112	19990319	01112	GL  	1999	3	19	99ZZZX929        	3	19990106	G	6110		VALVE           			PIPER 	PA31  	PA31350     	7103110	SO  						HARTZL	HCE3Y	HCE3YR2A    	GL  	PROPELLER	LOOSE           	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	132MF					317752072		DJ11004A		ACFT RETURNED FROM A CHARTER WITH THE COMPLAINT OF A ROUGH RUNNING ENGINE.  UPON ARRIVAL, PROPELLER DOME REMOVED AND THE	 PRESSURE WAS CHECKED.  THE PRESSURE IN THE DOME WAS 20 POUNDS. THE PRESSURE SHOULD HAVE BEEN 38 POUNDS.  AIR WAS ADDED 	TO MEET THE PROPER PRESSURE, AND THE AIRCRAFT WAS TEST FLOWN.  THE FLIGHT WAS GOOD.  UPON RETURN OF AIRCRAFT, PRESSURE W	AS CHECKED, AND WAS FOUND TO BE FIVE POUNDS LOW.  THE SHRADER VALVE WAS REMOVED AND REINSTALLED TO INSURE THAT IT WAS PR	OPERLY SEATED, AND PRESSURE WAS RECHARGED IN THE DOME.  THE AIRCRAFT WAS THEN TEST FLOWN AGAIN AND NO DISCREPANCIES NOTE	D.	1	L	7	2 	3O				A20SO   		5	C	P33EA	 
1999031901113	19990319	01113	GL  	1999	3	19	99ZZZX930        	3	19990108	G	6114	A2404	STOP            			PIPER 	PA31  	PA31350     	7103110	SO  						HARTZL	HCE3Y	HCE3YR2A    	GL  	PROPELLER	STRIPPED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	17	132MF		757  			317752072		DJ11004A		REMOVED PROPELLER SPINNER.  NOTED THAT THREADS WERE STIRPPED.  REMOVED AND REPLACED STOP.						1	L	7	2 	3O				A20SO   		5	C	P33EA	 
1999031901114	19990319	01114	SO  	1999	3	19	99ZZZX931        	2	19990126	G	7310		LINE            			BEECH 	45    	A45         	1152006	CE  	CONT  	O550  	IO550B      		SO  					FUEL PRESSURE	LOOSE           	H				A				UNSCHED LANDING         				Y	K		ENGINE STOPPAGE           	FLUID LOSS                		NR	NOT REPORTED   	1			GL	19	134VW					534100	281763R			AFTER AN OFF-FIELD LANDING AS THE RESULT OF A COMPLETE POWER FAILURE, FOUND FUEL PRESS LINE FROM FUEL  MANIFOLD VALVE TO	 COCKPIT LOOSE AT A BULKHEAD FITTING ON THE REAR ENG BAFFLE.  SUBMITTER STATED MAIN CAUSE OF POWER FAILURE WAS DUE TO LO	OSE FUEL PRESS LINE, AND THE FITTING IN THE FUEL MANIFOLD VALVE WAS A NORMAL BRASS MS20822-4 FITTING.  CORRECT FITTING I	S A CONTINENTAL P/N 631658A1.  THE DIFFERENCE IS THE CONT FITTING HAS A SMALL ORIFICE IN IT PRIMARILY TO REDUCE FUEL PRE	SS INDICATOR FLUCTUATIONS.  HOWEVER, IF THIS FITTING WOULD HAVE BEEN INSTALLED, IT WOULD HAVE REDUCED AMOUNT OF FUEL LEA	KING AND MOST LIKELY WOULD NOT HAVE CAUSED THE ENGINE TO QUIT.	1	L	7	1 	3O	3	O		5A3     	E3SO				 
1999031901116	19990319	01116	EA  	1999	3	19	99ZZZX933        	2	19990130	G	7314	LW15473	FUEL PUMP       			PIPER 	PA28  	PA28R201    	7102816	SO  	LYC   	O360  	IO360C1C6   	41514	EA  					ENGINE	FAILED          	B			OG5R	O				OTHER                   				Y			ENGINE STOPPAGE           			NR	NOT REPORTED   	1			GL	21	175ND	11   				2837029	RL2033051A			ENGINE STOPPED.  IN-FLIGHT INSPECTION FOUND ENGINE DRIVEN FUEL PUMP ACTUATING ARM HAD BROKEN AT PIVOT POINT.  BROKEN PIE	CE WAS RETRIEVED FROM SUMP.  NO OTHER CONTAMINATION FOUND.  PUMP WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.  PUMP HA	D BEEN IN PARTS ROOM FOR 4 YEARS PRIOR TO INSTALLATION.				1	L	7	1 	3O	3	O		2A13    	1E10				 
1999031901117	19990319	01117	CE  	1999	3	19	99ZZZX934        	1	19990203	G	5310	50130461	DOUBLER         			CESSNA	414   	414         	2075908	CE  										NLG WHEELWELL	CRACKED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	19	18EG	3669 				4140394				DOUBLER ASSY, P/N 5013046-1, DEVELOPED COMPOUND CRACKS UNDER NORMAL LANDING LOADS. NOSE WHEELWELL SKIN ALSO EXPERIENCED 	CRACKS DUE TO DOUBLER FAILURE.  SUBMITTER SUGGESTED CAUSE OF CRACKS MAY BE ATTRIBUTED TO CROSS WIND AND HARD LANDINGS OR	 OVERBAGGAGE LOADING.				1	L	7	2 	3O			RT	A7CE    					 
1999031901118	19990319	01118	CE  	1999	3	19	99ZZZX935        	1	19990217	G	5744	35115247	FLAP TRACK      			BEECH 	33    	F33A        	1151425	CE  										LT WING	WORN            	B			AKGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	05	1809L	1995 				CE639				FOUND BOTH LT AND RT INBOARD FLAP TRACK WORN BY FLAP ROLLERS INTO SIDE OF TRACK.  CANNOT BE PROPERLY DETECTED WITH FLAP 	INSTALLED.   FOURTH PAIR OF TRACKS IN LAST 5 INSPECTIONS (3 MONTHS) 2 PAIR WERE REPAIRABLE, THE OTHERS WERE REPLACED.  T	HE 5TH HAD LESS THAN 1,000 HOURS TT.				1	L	7	1 	3O				3A15    					 
1999031901119	19990319	01119	CE  	1999	3	19	99ZZZX936        	1	19990217	G	5744	3511524710	FLAP TRACK      			BEECH 	33    	F33A        	1151425	CE  										RT WING	WORN            	B			AKGR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CE	05	1809L	1995 				CE639				FOUND BOTH LT AND RT INBOARD FLAP TRACK WORN BY FLAP ROLLERS INTO SIDE OF TRACK.  CANNOT BE PROPERLY DETECTED WITH FLAP 	INSTALLED.   FOURTH PAIR OF TRACKS IN LAST 5 INSPECTIONS (3 MONTHS) 2 PAIR WERE REPAIRABLE, THE OTHERS WERE REPLACED.  T	HE 5TH HAD LESS THAN 1,000 HOURS TT.				1	L	7	1 	3O				3A15    					 
1999031900728	19990319	00728	EA  	1999	3	19	99ZZZX938        	2	19990120	G	8500		ENGINE          			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					ENGINE BAY	MAKING METAL    	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	07	123GJ		314  			17270706	L681076T			WHILE C/W AD 80-04-0322 DURING AN ANNUAL INSPECTION, LARGE AMOUNTS OF METAL FLAKES WERE FOUND IN THE OIL FILTER.  THE FI	LTER WAS SENT TO LYCOMING FOR ANALYSIS.  AT LYCOMING'S RECOMMENDATION, ENGINE WAS REMOVED FROM SERVICE.  METAL WAS DETER	MINED TO BE ALUMINUM AND AND BEARING MATERIAL.  SUBMITTER STATED VERY IMPORTANT THAT ALL OIL FILTERS BY INSPECTED AT EAC	H OIL CHANGE.			1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999031900729	19990319	00729	GL  	1999	3	19	99ZZZX939        	3	19990212	G	6111	AN417A	BOLT            			MTSBSI	MU2   	MU2B35      	5780411	CE  						HARTZL	HCB3T	HCB3TN5     	GL  	PROPELLER	DAMAGED         	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	25	155AS		590  			589		BV2142		DURING 150-HOUR INSPECTION ON BOTH PROPELLERS, THE PROPELLER STOP LOCK BOLTS ON ALL PROP BLADES WERE FOUND CHAFING ON TH	E BLADE STOP PLATES.  REMOVED ALL 6 BOLTS, PN AN4-417A, ON THE STOP LOCKS.  INSTALLED ALL NEW BOLTS, PN AN4-16A, AND NEW	 NUTS, P/N B3808.  RT PROP S/N BV2187.				1	H	7	2 	3T			RT	A10SW   		6	C	P15EA	 
1999031900730	19990319	00730	SO  	1999	3	19	99ZZZX940        	2	19990128	G	8530		CYLINDER        			PIPER 	PA28  	PA28140     	7102802	SO  	CONT  	O520  	TSIO520J    	17040	SO  					NR 3	DAMAGED         	B			JZRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	1852T		1198 			287225001	208320J			HEAD SEPARATION AT BARREL THREADS.  CRACK PRODUCED STARTING AT HEAD AND BARREL ATTACHING THREADS DUE TO AGING CYLINDER.						1	L	7	1 	3O	3	O		2A13    	E8CE				 
1999031900733	19990319	00733	CE  	1999	3	19	99ZZZX943        	1	19990119	G	2810	04003111	DRAIN LINE      			CESSNA	150   	150C        	2071808	CE  										FUEL SYSTEM	CONTAMINATED    	G				C				ABORTED TAKEOFF         				R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			GL	13	1956Z	4604 				15059756				AIRCRAFT LOST POWER ON TAKEOFF.  WATER IN THE FUEL VALVE DRAIN LINE HAD FROZEN AND EXPANDED INTO THE FUEL SUPPLY LINE WI	TH THE RESULTANT RESTRICTED FUEL FLOW TO THE ENGINE.  SUBMITTER SUGGESTED THIS LINE, CESSNA PN 0400311-1, AND SIMILAR LI	NES ON OTHER CESSNA SINGLE ENGINE AIRCRAFT SHOULD BE EQUIPPED WITH QUICK DRAINS IN ORDER FOR THE PILOT TO DRAIN COLLECTE	D WATER OR IN THE CASE OF FROZEN WATER, ALERT HIM TO A PROBLEM.			1	H	7	1 	3O				3A19    					 
1999031900739	19990319	00739	CE  	1999	3	19	99ZZZX949        	1	19990201	G	2810	1200406Y76	LINE            			CESSNA	206   	U206G       	2073356	CE  										FUEL SYSTEM	CHAFED          	H		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	01	206JK	3574 				U20606367				100 HOUR INSPECTION FOUND RT AILERON CABLE RUBBED THROUGH FORWARD FUEL LINE INSIDE CABIN (UPPER RT SIDE WHERE FUEL LINE 	ENTERS CABIN BY WINDSHIELD.)  INSTALLED NEW PART, ADJUSTED AWAY FROM CABLE WHEN CONNECTED TO TANK.					1	H	7	1 	3O				A4CE    					 
1999031900740	19990319	00740	SO  	1999	3	19	99ZZZX950        	1	19990106	G	5710	AN176	BOLT            			PIPER 	PA28  	PA28R201    	7102816	SO  										WING	CORRODED        	D		A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	2073M	3273 				28R7837065				MAIN WING SPAR BOLTS REMOVED IN ORDER TO REMOVE WING FOR REPAIRS.  FOUND BOLTS BADLY CORRODED.  BOLTS HAVE TO BE REMOVED	 TO SEE CORROSION.  SUBMITTER STATED THIS IS THE THIRD AIRCRAFT IN SIX MONTHS THAT HAS BEEN FOUND IN THIS SHOP.					1	L	7	1 	3O				2A13    					 
1999031900741	19990319	00741	CE  	1999	3	19	99ZZZX951        	1	19990211	G	3242	1640806	ROTOR           	PARKERHANFIN	3028        	CESSNA	195   	195B        	2073112	CE  										BRAKE	CRACKED         	B	S			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	15	2156C	320  				16141				MAG-PARTICLE INSPECTION SHOWS A RADIAL CRACK ACROSS 3/4 WIDTH OF FLANGE AND 1/2 WAY THROUGH THE THICKNESS.						1	H	7	1 	3R				A790    					 
1999031900742	19990319	00742	CE  	1999	3	19	99ZZZX952        	1	19990208	G	7810		EXHAUST PIPE    			BEECH 	36    	A36         	1151604	CE  										ENGINE	SEPARATED       	B		A		A				UNSCHED LANDING         				D	B		INFLIGHT SEPARATION       	SMOKE/FUMES/ODORS/SPARKS  		NR	NOT REPORTED   	1			SW	99	2024Q	545  				E1339				EXHAUST PIPE DEPARTED ACFT, PRESUMABLY IN-FLIGHT.  PILOT NOTED SMOKE IN COCKPIT; NO INAPPROPRIATE GAUGE CHANGES.  PILOT 	DIRECTED ACFT TO CLOSEST AIRPORT, SHUT ENG DOWN, SHORT FINAL.  SUCCESSFUL LANDING.  INSP REVEALED EXCESS HEAT DIRECTED I	NTO ENG COMPT AFT OF TURBOCHARGER.  BRAKE LINES AND HOSES DESTROYED.  HOLE BURNED IN LT SIDE OF ENG PEDESTAL MOUNT.  EXH	 ATTACH CLAMP SPLIT.  EXT SIDE SKIN PAINT SCORCHED.  SPECIAL NOTE:  EVENT ORIG NOTED AT APPROX 3,000 FEET AGL WITH AIRPO	RT APPROX 5-8 MILES AWAY.  PILOT'S RESPONSE TOWARD CLOSEST AIRPORT PROMPTED LANDING SEQUENCE, I.E., LANDING GEAR DOWN. A	CTION POSSIBLY AVOIDED NOSE TIRE FIRE.  SUBMITTER SUGGESTED PILOT INSP DURING PRE-FLIGHT AND AT ANNUAL.  STC SA5223NM.	1	L	7	1 	3O				3A15    					 
1999031900743	19990319	00743	CE  	1999	3	19	99ZZZX953        	1	19990218	G	5520		BRACKET         			CESSNA	206   	U206G       	2073356	CE  										ELEVATOR	CORRODED        	B			WWKR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	22306	6825 				U20606570				ANNUAL INSPECTION OF AIRCRAFT USED EXTENSIVELY IN SALT WATER/FLOAT OPERATION, REVEALED BOTH OTBD ELEVATOR ATTACH BRACKET	S CORRODED AND LIGHT DAMAGE TO STABILIZER REAR SPARS.					1	H	7	1 	3O				A4CE    					 
1999031900745	19990319	00745	SO  	1999	3	19	99ZZZX955        	1	19990114	G	5751	1710013	RIB             			PIPER 	PA23  	PA23250     	7102308	SO  										AILERON	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	23	2556Z	9952 				278054048				DURING 100-HOUR INSPECTION, FOUND CRACK INBOARD AILERON RIB.						1	L	7	2 	3O				1A10    					 
1999031900746	19990319	00746	SO  	1999	3	19	99ZZZX956        	2	19990203	G	8530	631996	RETAINER        			PIPER 	PA28  	PA28R201T   	7102813	SO  	CONT  	O360  	TSIO360FB   	17025	SO  					ROCKER SHAFT	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	25	2610M	205  				28R7803137	299622R			UPON COMPLETION OF CSB 98-1A, FOUND THAT NR 2 CYLINDER EXHAUST ROCKER SHAFT RETAINER WAS CRACKED.  SUBMITTER SUGGESTED A	 POSSIBLE CAUSE IS OVERTORQUING OF ROCKER SHAFT RETAINER NUT OR MANUFACTURER DEFECT.					1	L	7	1 	3O	3	O		2A13    	E9CE				 
1999031900748	19990319	00748	CE  	1999	3	19	99ZZZX958        	1	19990203	G	3242	416242	LINE            			BBAVIA	8     	8KCAB       	2110612	CE  										BRAKE	SEPARATED       	H				O				OTHER                   				K			FLUID LOSS                			AB	AEROBATIC      	1			GL	25	295AC					75695				DURING AEROBATIC MANEUVERING, THE RT BRAKE FLUID LINE CAME LOOSE FROM THE PLASTIC T-FITTING ON THE BRAKE FLUID RESERVOIR	.  SUFFICIENT FLUID REMAINED IN THE BRAKE CYLINDER TO PROVIDE NORMAL BRAKING DURING LANDING.  THE BRAKE SYSTEM (AS DELIV	ERED) USES PLASTIC TUBES WITHOUT CLAMPS AT EITHER THE RESERVOIR T-FITTING OR BRAKE CYLINDER BARB FITTINGS.  THE AIRCRAFT	 WAS PLACED IN SERVICE ON 9-19-95, AND HAD ACCUMULATED 325 HRS TT PRIOR TO THE INCIDENT ON 1-26-99.  NO SERVICE PRIOR TO	 THIS INCIDENT HAS BEEN PERFORMED ON THIS SUBSYSTEM.		1	H	7	1 	3O				A21CE   					 
1999031900751	19990319	00751	CE  	1999	3	19	99ZZZX961        	1	19990204	G	3213	0541153	BOLT            			CESSNA	172   	172E        	2072412	CE  										MLG	BROKEN          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	31303	5377 				17250609				DURING ANNUAL INSPECTION DISCOVERD RT MAIN GEAR LEG LOOSE AND REAR NUT MISSING FROM U-BOLT AT GEAR ATTACH.  REMOVED U-BO	LT AND REPLACED WITH NEW BOLT, NUTS, AND WASHERS.  APPEARED TO HAVE BROKEN JUST BEHIND NUT AS IF OVERTORQUED.  RUST COVE	RED BREAK AREA.  BOLT HOLES AND OTHER BOLT IN GOOD CONDITION.  INSTALLED NEW HARDWARE AND TORQUED.  PROBLEM SOLVED.  SUB	MITTER RECOMMENDED WHILE INSPECTING WHEELS AND GEAR, THAT AIRCRAFT (LIGHT) BE SUPPORTED/LIFTED BY OTHER MEANS THAN GEAR 	LEG, I.E., FLOOR JACK WITH WOOD CUSHION ALONG RIVET LINES OF GEARBOX.  THIS ALLOWS MOVEMENT OF GEAR LEG TO BE DETECTED E	ARLIER.	1	H	7	1 	3O			NT	3A12    					 
1999031900753	19990319	00753	EA  	1999	3	19	99ZZZX963        	2	19990203	G	8530		STUD            			MOONEY	M20   	M20E        	5870212	SW  	LYC   	O360  	IO360C1C    	41514	EA  					NR 3 CYLINDER	BROKEN          	D				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			CE	09	333WS	2670 	1111 			323	L603751A			PILOT REPORTED LOSS IN ENGINE POWER WHILE AIRCRAFT IN CRUISE POWER SETTING.  INSPECTION REVEALED BROKEN CYLINDER HOLD-DO	WN STUDS, CYLINDER NR 3.  SUBMITTER SUGGESTED UNDER OR OVERTORQUE POSSIBLY A CONTRIBUTING FACTOR IN HOLD-DOWN STUDS FAIL	URE.				1	L	7	1 	3O	3	O		2A3     	1E10				 
1999031900755	19990319	00755	CE  	1999	3	19	99ZZZX965        	1	19990201	G	3242	070009998	BRAKE LINE      			CESSNA	182   	R182        	2072734	CE  										FUSELAGE	CHAFED          	D				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			EA	21	369CP					R18201613				ELEVATOR CABLE CUT HOLE IN BRAKE LINE.  THIS LINE IS LOCATED UNDER PANEL JUST FORWARD OF PILOT.  CABLE DOES NOT TOUCH LI	NE, BY ABOUT .25 INCH, ONLY WHEN PULLING BACK ON ELEVATOR WILL THE CABLE TOUCH THE LINE AND THEN ONLY SLIGHTLY.  CABLE T	ENSION WAS CORRECT.  SUBMITTER SUSPECTED LINE WAS PUSHED DOWN WHEN FACTORY AIR CONDITIONING WAS INSTALLED.				1	H	7	1 	3O			RT	3A13    					 
1999031900756	19990319	00756	CE  	1999	3	19	99ZZZX966        	1	19990127	G	3411	S11332	CONNECTOR       			CESSNA	172   	172R        	2072401	CE  										PITOT TUBE	MISINSTALLED    	B	P			K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	375ES	196  				17280057				PERFORMED STATIC LEAK CHECK PER SB 97-32-02R1, ALT STATIC VALVE REPLACEMENT.  STATIC CHECK FAILED DUE TO CROSS-THREADED 	CONNECTOR INTO PITOT TUBE ITEM 41 AND CROSS-THREADED B-NUT ITEM 42 OF IPC (34-11-00-01).  REPLACED BOTH CONNECTORS.  OPS	 CHECKS NORMAL.  SUBMITTER RECOMMENDATION TO PREVENT RECURRENCE; HAVE IT INSTALLED CORRECTLY AT CESSNA AIRCRAFT.				1	H	7	1 	3O			NT	3A12    					 
1999031900757	19990319	00757	CE  	1999	3	19	99ZZZX967        	1	19990218	G	8120	08511219	BEAM            			CESSNA	414   	414         	2075908	CE  										TURBOCHARGER	CORRODED        	G	P	A		K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	01	381JR	4400 				4140484				DURING REMOVAL OF THE LT ENGINE TURBO TO F.O.M., THE TURBO ATTACH BRACKET SEPARATED FROM THE OUTBOARD ENGINE BEAM, PN 08	51121-9.  THIS AREA IS VERY DIFFICULT TO INSPECT.  SUBMITTER SUSPECTED GALVANIC CORROSION FROM DISSIMILAR METAL CONTACT.	  REMOVED AND REPLACED BEAM, TREATED WITH ALODINE, RE-INSTALLED MOUNTING BRACKET.  INSPECTED RIGHT INSTALLATION.  NO DEF	ECTS NOTED.			1	L	7	2 	3O			RT	A7CE    					 
1999031900758	19990319	00758	CE  	1999	3	19	99ZZZX968        	1	19990127	G	3411	S11301	NUT             			CESSNA	172   	172R        	2072401	CE  										PITOT TUBE	MISINSTALLED    	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	07	375ES	196  				17280057				PERFORMED STATIC LEAK CHECK PER SB 97-32-02R1, ALT STATIC VALVE REPLACEMENT.  STATIC CHECK FAILED DUE TO CROSS-THREADED 	CONNECTOR INTO PITOT TUBE ITEM 41 AND CROSS-THREADED B-NUT ITEM 42 OF IPC (34-11-00-01).  REPLACED BOTH CONNECTORS.  OPS	 CHECKS NORMAL.  SUBMITTER RECOMMENDATION TO PREVENT RECURRENCE; HAVE IT INSTALLED CORRECTLY AT CESSNA AIRCRAFT.				1	H	7	1 	3O			NT	3A12    					 
1999031900971	19990319	00971	SO  	1999	3	19	99ZZZX970        	1	19990122	G	3232	455961	ROD             			PIPER 	PA42  	PA42        	7104202	SO  										MLG DOOR	BROKEN          	E				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	11	395DR	4907 				428001065				LEFT MAIN GEAR DOOR ACTUATOR ROD END BROKE OFF 1.50 INCHES FROM END OF ROD END.						1	L	7	2 	4T				A23SO   					 
1999031900973	19990319	00973	CE  	1999	3	19	99ZZZX972        	1	19990205	G	3230	5201K	BEARING         	FAFNIR      	958100175   	BEECH 	95    	95B55       	1152729	CE  										MLG	FAILED          	D	P			O				OTHER                   				J			WARNING INDICATION        			AP	APPROACH       	1			GL	23	4450W					TC1673				LANDING GEAR RETRACTED NORMALLY AFTER TAKEOFF.  ON RETURN, LANDING GEAR FAILED TO EXTEND.  PILOT TRIED TO LOWER GEAR USI	NG THE EMERGENCY PROCEDURES OUTLINED IN PILOT HANDBOOK, EXTENSION HANDLE WOULD NOT ENGAGE THE ACTUATOR WORM GEAR SHAFT. 	 THE 5201K BEARING HAD FAILED AND THE BALL BEARINGS WERE LOOSE AND BROKEN JAMMING THE WORM GEAR SHAFT.  THE 5201K BEARIN	G IS ALSO A THRUST BEARING AND WHEN IT FAILED IT ALLOWED THE WORM DRIVE GEAR AND SHAFT TO MOVE AWAY FROM THE EMERG HANDL	E ENGAGING SHAFT.  WHEN GEAR SELECTOR WAS PLACED IN THE DOWN POSITION, THE MOTOR AND WORM GEAR SHAFT MOVED A LITTLE AND 	THEN JAMMED.  HOBBS:  3,572.	1	L	7	2 	3O			RT	3A16    					 
1999031900977	19990319	00977	SO  	1999	3	19	99ZZZX976        	2	19990203	G	7414	10357586	GEAR DIST       	BENDIX      	S6RSC25P    	PIPER 	PA46  	PA46310P    	7104605	SO  	CONT  	O520  	TSIO520BE   	17040	SO  					ENGINE	FAILED          	D				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			EA	03	4380D				L018915D	468508045				PILOT REPORTED LOSS OF POWER AND A ROUGH RUNNING ENGINE.  AFTER COMPLETING MAGNETO CHECK, A DEAD LT MAGNETO WAS DISCOVER	ED.  THE MAGNETO WAS DISASSEMBLED AND THE DISTRIBUTOR GEAR WAS DISASSEMBLED AND THE DISTRIBUTOR GEAR WAS FOUND TO HAVE 1	5 TEETH THAT WERE LIBERATED FROM IT WHICH RENDERED THE OUTPUT OF THE MAGNETO USELESS.  SUBMITTER STATED DISTRIBUTOR GEAR	S SHOULD BE DISCARDED AT ROUTINE OVERHAUL DUE TO HEAT CRYSTALIZATION AND EMBRITTLEMENT.			1	L	7	1 	3O	3	O	RT	A25SO   	E8CE				 
1999031900981	19990319	00981	CE  	1999	3	19	99ZZZX980        	1	19990126	G	2842	S33312	FUEL SENDER     			CESSNA	172   	172R        	2072401	CE  										LT FUEL TANK	FAILED          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	15	416ER	87   				17280281				DURING A POST-INSPECTION ENGINE RUN-UP, THE LEFT FUEL GAUGE NEEDLE WAS READING ERRATIC (FULL TO ZERO).    INSPECTION OF 	THE FUEL INDICATION SYSTEM FOUND THE LEFT FUEL TANK SENDER BAD.					1	H	7	1 	3O			NT	3A12    					 
1999031900983	19990319	00983	EA  	1999	3	19	99ZZZX982        	2	19990128	G	8530	LW12966	CYLINDER        			PIPER 	PA31  	PA31310     	7103103	SO  	LYC   	O540  	TIO540A2C   	41532	EA  					LT ENGINE	DAMAGED         	B			JZRR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	4081F		1233 			318112036	L765961A			EXHAUST VALVE SEAT LOOSENED FROM CYLINDER HEAD CAUSING EXHAUST VALVE TO MISALIGN, AND DAMAGE CYLINDER HEAD.  SUBMITTER S	TATED LOOSE INTERFERENCE FIT BETWEEN VALVE SEAT AND CYLINDER HEAD, AND HIGH CHT DUE TO PROBLEM IN TURBO SYSTEM MAY HAVE 	CAUSED PROBLEM TO DEVELOP.				1	L	7	1 	3O	3	O	RT	A20SO   	E14EA				 
1999031900984	19990319	00984	SO  	1999	3	19	99ZZZX983        	1	19990208	G	3250	3519200	HORN ASSY       			PIPER 	PA28  	PA28161     	7102803	SO  										NLG	CRACKED         	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	07	43438	3004 				288416052				CRACKED ALONG WELD WHERE NOSE GEAR MOUNTING PLATE ATTACHES TO ANGLES.  SUBMITTER STATED WELD IS UNDERCUT WITH INSUFFICIE	NT MATERIAL.					1	L	7	1 	3O				2A13    					 
1999031900985	19990319	00985	SO  	1999	3	19	99ZZZX984        	2	19990119	G	7322	25765404F	FUEL SERVO      			PIPER 	PA34  	PA34220T    	7103420	SO  	CONT  	O360  	TSIO360KB   	17025	SO  					FUEL SYSTEM	MISMANUFACTURED 	H		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	28	4123C				70164908	3449042				NEW FUEL SERVO INSTALLED ON AIRCRAFT.  FUEL LEAK AT FUEL INLET.  REMOVED ADAPTER FROM UNIT, O-RING PACKING, PN 951789, W	AS MISSING.  SUBMITTER STATED THIS WAS A NEW SERVO AND ALL FITTINGS INSTALLED WERE TORQUED.					1	L	7	2 	3O	3	O		A7SO    	E9CE				 
1999031900987	19990319	00987	EA  	1999	3	19	99ZZZX986        	2	19990128	G	8530	LW11775	PISTON PIN      			CESSNA	172   	172S        	2072439	CE  	LYC   	IO360 	IO360L2A    		EA  					NR 2 CYLINDER	WORN            	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	494SP					172S8035	L2790951A			NEW CESSNA WITH 24.1 HOURS, DRAINED OIL AND REPLACED OIL FILTER.  WHEN FILTER WAS CUT OPEN AND INSPECTED FOUND EXCESSIVE	 AMOUNT OF ALUMINUM IN FILTER.  NOTIFIED CESSNA AND LYCOMING.  THEY REQUIRED A PIECE OF FILTER TO ANALYZE.  AFTER ANALYS	IS, LYCOMING ADVISED TO REPLACE LW-11775 PISTON PIN PLUGS WITH OLD STYLE 60828.  WHEN PISTON PIN PLUGS WERE REMOVED, THE	Y SHOWED EXCESSIVE END WEAR.			1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999031900988	19990319	00988	EA  	1999	3	19	99ZZZX987        	2	19990128	G	8530	LW11775	PISTON PIN      			CESSNA	172   	172S        	2072439	CE  	LYC   	IO360 	IO360L2A    		EA  					NR 3 CYLINDER	WORN            	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	494SP					172S8035	L2790951A			NEW CESSNA WITH 24.1 HOURS, DRAINED OIL AND REPLACED OIL FILTER.  WHEN FILTER WAS CUT OPEN AND INSPECTED FOUND EXCESSIVE	 AMOUNT OF ALUMINUM IN FILTER.  NOTIFIED CESSNA AND LYCOMING.  THEY REQUIRED A PIECE OF FILTER TO ANALYZE.  AFTER ANALYS	IS, LYCOMING ADVISED TO REPLACE LW-11775 PISTON PIN PLUGS WITH OLD STYLE 60828.  WHEN PISTON PIN PLUGS WERE REMOVED, THE	Y SHOWED EXCESSIVE END WEAR.			1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999031900989	19990319	00989	EA  	1999	3	19	99ZZZX988        	2	19990128	G	8530	LW11775	PISTON PIN      			CESSNA	172   	172S        	2072439	CE  	LYC   	IO360 	IO360L2A    		EA  					NR 1 CYLINDER	WORN            	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	494SP					172S8035	L2790951A			NEW CESSNA WITH 24.1 HOURS, DRAINED OIL AND REPLACED OIL FILTER.  WHEN FILTER WAS CUT OPEN AND INSPECTED FOUND EXCESSIVE	 AMOUNT OF ALUMINUM IN FILTER.  NOTIFIED CESSNA AND LYCOMING.  THEY REQUIRED A PIECE OF FILTER TO ANALYZE.  AFTER ANALYS	IS, LYCOMING ADVISED TO REPLACE LW-11775 PISTON PIN PLUGS WITH OLD STYLE 60828.  WHEN PISTON PIN PLUGS WERE REMOVED, THE	Y SHOWED EXCESSIVE END WEAR.			1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999031900990	19990319	00990	EA  	1999	3	19	99ZZZX989        	2	19990128	G	8530	LW11775	PISTON PIN      			CESSNA	172   	172S        	2072439	CE  	LYC   	IO360 	IO360L2A    		EA  					NR 4 CYLINDER	WORN            	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	494SP					172S8035	L2790951A			NEW CESSNA WITH 24.1 HOURS, DRAINED OIL AND REPLACED OIL FILTER.  WHEN FILTER WAS CUT OPEN AND INSPECTED FOUND EXCESSIVE	 AMOUNT OF ALUMINUM IN FILTER.  NOTIFIED CESSNA AND LYCOMING.  THEY REQUIRED A PIECE OF FILTER TO ANALYZE.  AFTER ANALYS	IS, LYCOMING ADVISED TO REPLACE LW-11775 PISTON PIN PLUGS WITH OLD STYLE 60828.  WHEN PISTON PIN PLUGS WERE REMOVED, THE	Y SHOWED EXCESSIVE END WEAR.			1	H	7	1 	3O	3	O	NT	3A12    	1E10				 
1999031900991	19990319	00991	CE  	1999	3	19	99ZZZX990        	1	19990218	G	2500	05142158	FITTING         		051421223   	CESSNA	172   	172S        	2072439	CE  										SEAT BACK	MISMANUFACTURED 	D		A		K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	494SP	39   				172S8035				NEW CESSNA WITH 39.4 HOURS.  PILOT'S SEAT BACK WOULD NOT SWING FORWARD FOR ACCESS TO REAR SEAT.  LOOSENED RECLINE CYLIND	ER BOLT IN L-SEAL BACK FITTING SO SEAT BACK WOULD SWING FORWARD.  WITH THIS BOLT LOOSE AS REQUIRED, FOUND SEAT BACK IN F	ULL UPRIGHT POSITION WAS RECLINED APPROXIMATELY 4 INCHES.  FURTHER INVESTIGATION FOUND L-SEAT BACK ATTACH FITTING, PN 05	14215-8, WAS BENT 2 INCHES AFT.  CESSNA CONFIRMED IMPROPER HEAT TREATING OF FITTING.			1	H	7	1 	3O			NT	3A12    					 
1999031900992	19990319	00992	CE  	1999	3	19	99ZZZX991        	1	19990108	G	7714		TACHOMETER      			CESSNA	172   	172S        	2072439	CE  										COCKPIT	MISMANUFACTURED 	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	494SP					172S8035				ACCEPTANCE INSPECTION OF NEW CESSNA WITH 8.0 HOURS SINCE MANUFACTURE REVEALED THE TACHOMETER WAS IN ERROR.  A CALIBRATED	 TACHOMETER TESTER INDICATED THE AIRCRAFT TACHOMETER WAS 25 RPM'S LOW AT TAKEOFF AND 75 RPM'S LOW AT IDLE.  A REPLACEMEN	T TACHOMETER IS BEING INSTALLED.				1	H	7	1 	3O			NT	3A12    					 
1999031900993	19990319	00993	CE  	1999	3	19	99ZZZX992        	1	19990108	G	2434		BELT            			CESSNA	172   	172S        	2072439	CE  										ALTERNATOR	LOOSE           	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP					172S8035				ACCEPTANCE INSPECTION OF  NEW CESSNA WITH 8.0 HOURS SINCE MANUFACTURE REVEALED THE ALTERNATOR BELT TENSION WAS LOOSE.  A	DJUSTED TENSION WITHIN LIMITS, 11 TO 13 FEET/POUNDS.					1	H	7	1 	3O			NT	3A12    					 
1999031900994	19990319	00994	CE  	1999	3	19	99ZZZX993        	1	19990108	G	7110		COWL            			CESSNA	172   	172S        	2072439	CE  										FUSELAGE	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	494SP					172S8035				ACCEPTANCE INSPECTION OF NEW CESSNA WITH 8.0 HOURS SINCE MANUFACTURE REVEALED THE LOWER ENGINE COWLING WAS CHAFING THE F	USELAGE AT THE 3 AND 10 O'CLOCK POSITIONS.  RE-SHIMMED THE 3 AND 10 O'CLOCK COWL SHOCK MOUNTS BY ADDING SPACERS ELIMINAT	ED CHAFING.				1	H	7	1 	3O			NT	3A12    					 
1999031900995	19990319	00995	CE  	1999	3	19	99ZZZX994        	1	19990108	G	3411		LINE            			CESSNA	172   	172S        	2072439	CE  										STATIC SYSTEM	MISINSTALLED    	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	494SP					172S8035				ACCEPTANCE INSPECTION ON NEW CESSNA WITH 8.0 HOURS SINCE MANUFACTUE REVEALED WITH FULL AFT ELEVATOR, THE YOKE HIT THE AL	TERNATE STATIC SOURCE VALVE T-FITTING RESTRICTING ELEVATOR TRAVEL.  RE-ROUTED ALTERNATE STATIC SOURCE LINES AND T-FITTIN	G.				1	H	7	1 	3O			NT	3A12    					 
1999031900996	19990319	00996	CE  	1999	3	19	99ZZZX995        	1	19990108	G	2720		CONTROL CABLE   			CESSNA	172   	172S        	2072439	CE  										RUDDER	OUT OF ADJ      	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	494SP					172S8035				ACCEPTANCE INSPECTION ON NEW CESSNA WITH 8.0 HOURS SINCE MANUFACTURE REVEALED THE RUDDER WAS NOT CENTERED WITH THE NOSE 	WHEEL CENTERED.  ADJUSTED CABLE TENSION TO ALIGN RUDDER AND RUDDER PEDALS.					1	H	7	1 	3O			NT	3A12    					 
1999031900997	19990319	00997	CE  	1999	3	19	99ZZZX996        	1	19990108	G	2701		CONTROL CABLE   			CESSNA	172   	172S        	2072439	CE  										YOKE	OUT OF ADJ      	D				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			NM	03	494SP					172S8035				ACCEPTANCE INSPECTION ON NEW CESSNA WITH 8.0 HOURS SINCE MANUFACTURE REVEALED THE PILOTS AND COPILOTS YOKES WERE NOT ALI	GNED IN NEUTRAL.  ADJUSTED CABLE TO ALIGN YOKES THAN CHECKED CARRY-THROUGH CABLE TENSION AND FOUND IT ADJUSTED TO 58 POU	NDS.  ADJUSTED CABLE TENSION TO 40 PLUS OR MINUS 10 POUNDS AND CHECKED STOPS.  NO FURTHER DEFECTS NOTED.				1	H	7	1 	3O			NT	3A12    					 
1999031900998	19990319	00998	CE  	1999	3	19	99ZZZX997        	1	19990108	G	2840		LIGHT           			CESSNA	172   	172S        	2072439	CE  										COCKPIT	BROKEN          	B				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP					172S8035				ACCEPTANCE INSPECTION OF NEW CESSNA WITH 8.0 HOURS SINCE MANUFACTURE REVEALED THE FUEL SELECTOR LIGHT WAS INOPERATIVE. T	HE LIGHT SOCKET BASE WAS BROKEN.  REPLACED SOCKET AND OPERATIONAL CHECKED SATISFACTORY.					1	H	7	1 	3O			NT	3A12    					 
1999031900999	19990319	00999	CE  	1999	3	19	99ZZZX998        	1	19990108	G	2731		TAB             			CESSNA	172   	172S        	2072439	CE  										ELEVATOR TRIM	OUT OF ADJUST   	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	494SP					172S8035				ACCEPTANCE INSPECTION ON NEW CESSNA WITH 8.0 HOURS SINCE MANUFACTURE REVEALED ELEVATOR TRIM TAB OUT OF ADJUSTMENT.  NEUT	RAL POSITION WAS UP .25 INCH AND THE UP/DOWN LIMITS WERE 25 DEGREES/27 DEGREES.  THE TRIM TAB WAS ADJUSTED TO NEUTRAL AN	D THE UP/DOWN STOPS ADJUSTED TO 22 DEGREES/19 DEGREES.				1	H	7	1 	3O			NT	3A12    					 
1999031901000	19990319	01000	EA  	1999	3	19	99ZZZX999        	2	19990108	G	7414	M3081	BREAKER         	SLICK       	4251        	CESSNA	172   	172M        	2072418	CE  	LYC   	O320  	O320E2D     	41508	EA  					MAGNETO	FAILED          	D				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	03	1370U				95110109	17267041				500-HOUR MAGNETO INSPECTION ACCOMPLISHED ON RIGHT AND LEFT MAGNETOS, 4200 SERIES.  NEW BREAKER ASSY'S INSTALLED P/N M-30	81, MANUFACTURE DATE 9-20-98.  MAGNETOS INTERNALLY TIMED AND RE-ASSEMBLED.  INSTALLED MAGNETO ON ENGINE AND L-TIMING LIG	HT WOULD NOT GO OUT WITH POINT OPENING AND CLOSING.  REMOVED MAGNETO, DISASSEMBLED, REPLACED BREAKER ASSY WITH OTHER NEW	 SET.  INTERNALLY TIMED, RE-ASSEMBLED, AND RE-INSTALLED ON ENGINE WITH NO FURTHER PROBLEMS.  OPERATIONAL CHECKED SATISFA	CTORY.		1	H	7	1 	3O	3	O	NT	3A12    	E274				 
1999061800146	19990618	00146	NM  	1999	6	18	A3L2990401       	1	19990330	G	3246	2602540	BOLT            			BOEING	737   	737*        		NM  										MLG WHEEL	BROKEN          	B			A3L2	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	09										THREE FAILED MAIN WHEEL TIE BOLTS.  (X)						2	L	7	2 	4F			RT	A16WE   					 
1999082000989	19990820	00989	WP  	1999	8	20	AALA991084       	1	19990719	G	5313		LONGERON        			DOUG  	DC9   	DC982       	3022082	WP  										BS 1418	CRACKED         	A			AALA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	587AA					53250				TUL - REF:  F58 NR 3047920, L2R CRACKED, AFT END, STA 1418.  INSTALLED DOUBLER AND FASTENERS PER AARD 53-30-00-2.  TST: 	 38,873.21 HOURS.  CYCLES:  12,091.  (X)					2	L	7	2 	4F				A6WE    					 
2001012900063	20010129	00063	NE  	2001	1	29	AC2A0000003      	1	19990925	G	6210	7615009100051A	BLADE           			SKRSKY	S76   	S76         	8143010	NE  										MAIN ROTOR	CRACKED         	A			AC2A	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5402T	11951	334  			760140				CRACKED SPAR AT ROOT END.  REPLACED MAIN ROTOR BLADE.  (X)						1	G	7	2 	3U			 	H1NE    					 
2001012900068	20010129	00068	EU  	2001	1	29	AC2A0000004      	1	19990925	G	7600	23057869	GOVERNOR        			BOLKMS	105   	BO105S      	5626006	EU  										ENGINE	SURGES          	A			AC2A	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SW	03	50588	8471 	1167 			S780				TORQUE SURGING. REMOVED GOVERNOR AND FOUND MISSING EPOXY.  SNAP RING AND WASHERS FOUND INSIDE DRIVE CAVITY.  REPLACED GO	VERNOR WITH SERVICEABLE UNIT.  (X)					1	G	7	2 	3U			 	H3EU    					 
2001012900055	20010129	00055	SW  	2001	1	29	AC2A0000006      	1	19990916	G	3340	900601	GEAR            			BELL  	430   	430         	1182150	SW  										SEARCH LIGHT	SHIFTED         	A			AC2A	O				OTHER                   				L			NO TEST                   			NR	NOT REPORTED   	1			SW	03	430CH					49037				SEARCH LIGHT FAILS TO EXTEND FULLY (GEAR ON MOTOR SHIFTED CAUSING BIND AGAINST CASE).  (X)						1	G	7	2 	3U			RT	H9SW    					 
2001012900036	20010129	00036		2001	1	29	AC2A0000007      	4	19990919	G	3425	430375002105	DISPLAY         			BELL  	407   	407         	       	SW  										EFIS	INTERMITTENT    	A			AC2A	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03		1198 	1    							EFIS DISPLAY WILL NOT COME UP UNTIL 20-25 MINUTES OF FLIGHT.  (PROBLEM INTERMITTENT).  (X)						1	G	7	1 	3U			O	H2SW    					 
2001012900054	20010129	00054	SW  	2001	1	29	AC2A0000008      	1	19990905	G	6400	21006819	BUSHING         			BELL  	430   	430         	1182150	SW  										T/R GUARD	FROZEN          	A			AC2A	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	1194 				49037				LOWER AFT MOUNT FOR TAIL ROTOR GUARD LOOSE (BUSHING FROZEN ON BOLT CAUSING WEAR AD PLAY).  (X)						1	G	7	2 	3U			RT	H9SW    					 
2001013000039	20010130	00039	NE  	2001	1	30	AC2A0000009      	1	19991025	G	6210	7615009100041A	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	DELAMINATED     	A			AC2A	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	72649	11715				760292				SKIN DELAMINATED ON TOP FROM STA 32 EXTENDING OUT TO STA 105, 6 INCHES BACK FROM LEADING EDGE ABOUT 5 INCHES.  (X)						1	G	7	2 	3U			 	H1NE    					 
2001012900069	20010129	00069	GL  	2001	1	29	AC2A0000010      	2	19991106	G	7321	1564T1005	SERVO           			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C*       	 	GL  					FUEL CONTROL	INOPERATIVE     	A			AC2A	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	50588		446  			S780				SERVO MOTOR WILL NOT OPERATE.  REPLACED ACTUATOR.  (X)						1	G	7	2 	3U	3	U	 	H3EU    	E4CE				 
2001012900038	20010129	00038	SW  	2001	1	29	AC2A0000011      	1	19991211	G	7810	206064300005	EXHAUST PIPE    			BELL  	206   	206L3       	1182108	SW  										ENGINE	CRACKED         	A			AC2A	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	17592	468  				51535				EXHAUST ASSEMBLY CRACKED.  REPLACED.  (X)						1	G	7	1 	3U			 	H2SW    					 
2001020600087	20010206	00087	EU  	2001	2	6	AC2A0000012      	1	19991004	G	5320	10545408	STRUCTURE       			BOLKMS	105   	BO105S      	5626006	EU  										SIDE WALL	CRACKED         	B			AC2A	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2900	9768 				S776				LEFT SIDE WALL PART IS CRACKED.  REPLACED PART.  (X)						1	G	7	2 	3U			 	H3EU    					 
2001020500083	20010205	00083	NE  	2001	2	5	AC2A0000013      	1	19991230	G	2435	18301	BRUSHES         			SKRSKY	S76   	S76A        	8143006	NE  										STARTER GEN	WORN            	B			AC2A	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	72649	804  				760292				PART IS PITTED,  BRUSHES REPLACED.  (X)						1	G	7	2 	3U			 	H1NE    					 
2001012900051	20010129	00051	SW  	2001	1	29	AC2A0000028      	1	19991121	G	6420	430010433101	BEARING         			BELL  	430   	430         	1182150	SW  										ROD END	WORN            	A			AC2A	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	1433 				49037				BEARING WORN BEYOND LIMITS.  REPLACED ROD END.  (X)						1	G	7	2 	3U			RT	H9SW    					 
2001012900060	20010129	00060	SW  	2001	1	29	AC2A0000032      	1	19990831	G	6510	378551	DISC PACK       			BELL  	430   	430         	1182150	SW  										TAIL ROTOR	MISMANUFACTURED 	A			AC2A	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	430CH					49037				NEW PART WHEN TORQUEING THE BOLTS ON THE THOMAS COUPLING, THE DISC WOULD SPREAD.  REPLACED.  (X)						1	G	7	2 	3U			RT	H9SW    					 
2001012900059	20010129	00059	SW  	2001	1	29	AC2A0000033      	1	19990904	G	6510	363001	DISC PACK       			BELL  	430   	430         	1182150	SW  										TAIL ROTOR SHAFT	CORRODED        	A			AC2A	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	430CH	1154 				49037				THE THOMAS COUPLING WAS CORRODED AND PITTED BEYOND LIMITS.   REPLACED.  (X)						1	G	7	2 	3U			RT	H9SW    					 
2001020100062	20010201	00062	SW  	2001	2	1	AC2A0000073      	1	19990422	G	7810	206064300005	EXHAUST PIPE    			BELL  	206   	206L3       	1182108	SW  										ENGINE	CRACKED         	A			AC2A	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31079	7203 				51526				EXHAUST ASSEMBLY IS CRACKED.  REPLACED PART.  (X)						1	G	7	1 	3U			 	H2SW    					 
2001020100064	20010201	00064	SW  	2001	2	1	AC2A0000075      	1	19990430	G	7810	206064300005	EXHAUST PIPE    			BELL  	206   	206L3       	1182108	SW  										ENGINE	CRACKED         	A			AC2A	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7159J	372  				51408				EXHAUST ASSY CRACKED.  REPLACED PART.  (X)						1	G	7	1 	3U			 	H2SW    					 
2001020100065	20010201	00065	SW  	2001	2	1	AC2A0000076      	1	19990718	G	7810	206064300005	EXHAUST PIPE    			BELL  	206   	206L3       	1182108	SW  										ENGINE	CRACKED         	A			AC2A	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7159H	270  				51397				EXHAUST ASSY CRACKED.  REPLACED PART.  (X)						1	G	7	1 	3U			 	H2SW    					 
2000021900504	20000219	00504	SW  	2000	2	19	AU000110033      	1	19991222	G	2435	230321823	STATOR          	LUCAS       	23032018    	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					STARTER/GEN	MISOVERHAULED   	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA				96   		12597		CAE822683			(AU) STARTER/GENERATOR SENT TO OVERHAUL AFTER ONLY 96 HOURS.  STATOR COWLING OUTLET SCREEN FOUND TO BE CLOGGED WITH SOME	 FOREIGN INSULATION WHICH HAD OCCURRED DURING THE PREVIOUS REWIND.  STATOR IS NOW QUARANTINED UNTIL FURTHER INVESTIGATIO	N IS COMPLETED AS TO WHY PROPER CHECKS WERE NOT CARRIED OUT PREVIOUSLY THAT WOULD HAVE PRVENTED THIS FROM HAPPENING.  SE	NT TO AARPE ON 8 FEB 00 FOR INVESTIAGATION.			1	G	7	1 	3U	3	U		H2SW    	E4CE				 
2000021900523	20000219	00523	CE  	2000	2	19	AU000128043      	1	19991218	G	7160	628122	ARM             	CONT        	O200A       	CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A102	1A102OCM    	GL  	CARB HEAT	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						253620A		253620A	K18371		(AU) CARBURETOR HEAT BOX ACTUATOR ARM HAD BROKEN OFF AT RIVETS THAT SECURE SPRING STEEL STRIP TO ARM.						1	H	7	1 	3O	3	O		3A19    	E252	5	N	P918	 
1999021200083	19990212	00083	CE  	1999	2	12	AU990001         	1	19990104	G	2410	MS20365720C	NUT             			CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  					ALTERNATOR	MISSING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			457  		280140		280140R			(AUS) DURING PERIODIC ENGINE INSPECTION, IT WAS DISCOVERED THAT THE BOLT (PN AN7-46A) SECURING THE ALTERNATOR TO THE ALT	ERNATOR MOUNT (PN 643935) WAS LOOSE AND HAD ELONGATED THE MOUNTING HOLES IN THE MOUNT AND ALTERNATOR.  FURTHER INVESTIGA	TION REVEALED THAT THE NUT WAS MISSING.				1	H	7	1 	3O	3	O		A4CE    	E5CE				 
1999021200084	19990212	00084	EU  	1999	2	12	AU990002         	1	19990103	G	2720	540691	CONTROL CABLE   			PARTEN	P68   	P68B        	6780104	EU  										RUDDER	FAILED          	W				O				OTHER                   				F			FLT CONT AFFECTED         			LD	LANDING        	1			AU	S 										(AUS) PILOT REPORTED RUDDER CABLE SLIPPAGE.  INVESTIGATION FOUND THAT THE RT RUDDER (FORWARD) CABLE HAD FAILED AT THE FO	RWARD MOST PULLEY.  THE LT CABLE WAS THEN INSPECTED AND WAS FOUND WITH BROKEN STRANDS.  2,394.					1	H	7	2 	3O			 	A31EU   					 
1999021200085	19990212	00085	CE  	1999	2	12	AU990003         	1	19990106	G	2710	0510105364	CONTROL CABLE   			CESSNA	172   	172R        	2072401	CE  										AILERON	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AILERON CABLES SHOWED EXCESSIVE WEAR OVER PHENOLIC BLOCK FORWARD OF FLAP BAY - ESPECIALLY THE LEFT SIDE.						1	H	7	1 	3O			NT	3A12    					 
1999021200086	19990212	00086	CE  	1999	2	12	AU990004         	1	19990106	G	2710	0510105365	CONTROL CABLE   			CESSNA	172   	172R        	2072401	CE  										AILERON	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AILERON CABLES SHOWED EXCESSIVE WEAR OVER PHENOLIC BLOCK FORWARD OF FLAP BAY - ESPECIALLY THE LEFT SIDE.						1	H	7	1 	3O			NT	3A12    					 
1999021200087	19990212	00087	CE  	1999	2	12	AU990005         	1	19990104	G	5712		RIB             			CESSNA	310   	310R        	2074245	CE  										WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) SMALL CRACKS WERE FOUND IN LEFT WHEELWELL RIB MODIFICATION PLATES.  ON CLOSER INSPECTION, BOTH INBOARD AND OUTBOAR	D PLATES WERE FOUND TO HAVE MORE SERIOUS CRACKS.  THE OUTBOARD PLATE HAD ALMOST COMPLETELY LOST STRENGTH.  THE INBOARD P	LATE HAD TWO MINOR CRACKS AT THE HOLE RADII.  FOUND IAW AD/CESSNA/310/56 AMDT 1.  PART TC:  9,130.				1	L	7	2 	3O				3A10    					 
1999021200088	19990212	00088	CE  	1999	2	12	AU990006         	1	19990104	G	3222	MS166241231	SNAP RING       			CESSNA	441   	441         	2076020	CE  										NLG	MISINSTALLED    	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE OLEO ASSEMBLY UPPER RETAINING CIRCLIP NOT INSTALLED CORRECTLY ALLOWING THE OLEO TO MOVE OUT OF THE TRUNNION A	SSEMBLY AND LOCK IN A FULLY EXTENDED POSITION.					1	L	7	2 	3T			RT	A28CE   					 
1999021200089	19990212	00089		1999	2	12	AU990007         	4	19990108	G	2220	SNO3372019121	DETECTOR        			STBROS	SD3   	SD360       	8100606	EU  										STALL WARNING	JAMMED          	W				O				OTHER                   				N			FALSE WARNING             			TO	TAKEOFF        	1			AU	S 										(AUS) DURING THE TAKEOFF ROLL, STICK SHAKER ACTIVATION OCCURRED.  INVESTIGATION FOUND THE LEFT STALL VANE HAD STUCK IN T	HE UP POSITION.					2	H	7	2 	4T				A41EU   					 
1999021200090	19990212	00090		1999	2	12	AU990008         	4	19990101	G	2220	2TP127	SWITCH          			STBROS	SD3   	SD360       	8100606	EU  										STALL WARNING	INTERMITTENT    	W				O				OTHER                   				N			FALSE WARNING             			CL	CLIMB          	1			AU	S 										(AUS) SHORTLY AFTER TAKEOFF, STALL WARNING AND STICK SHAKER ACTIVATED.  PROBLEM BECAME INTERMITTENT WHEN CREW CYCLED APP	ROPRIATE CBS.  COULDN'T BE REPRODUCED ON GROUND - TEST SWITCH SUSPECTED AND REPLACED.					2	H	7	2 	4T				A41EU   					 
1999021200091	19990212	00091	NM  	1999	2	12	AU990009         	1	19990109	G	2437	108400238	WARNING SYSTEM  	AMETEK      	5224871     	DHAV  	DHC8  	DHC8102     	2809003	NM  										COCKPIT	ACTIVATED       	W				A				UNSCHED LANDING         				N			FALSE WARNING             			CL	CLIMB          	1			AU	S 					108400238					(AUS) ON INITIAL CLIMB, BOTH MAIN AND AUXILIARY BATTERY WARNING LIGHTS ILLUMINATED ON THE CENTRAL WARNING PANEL.						2	H	7	2 	4T			RT	A13NM   					 
1999021200092	19990212	00092	EA  	1999	2	12	AU990010         	2	19990107	G	7420		IGNITION HARNESS	BENDIX      	S4LN21      	PIPER 	PA30  	PA30        	7103002	SO  	LYC   	O320  	IO320B1A    	41508	EA  					MAGNETO	INCORRECT PART  	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							L254155AL253			(AUS) MAGNETO HARNESS DISTRIBUTOR BACK PLATES (BOTH) FOUND TO BE OVERSIZE PREVENTING CORRECT FITMENT AND SEATING.						1	L	7	2 	3O	3	O		A1EA    	1E12				 
1999021200093	19990212	00093	SO  	1999	2	12	AU990011         	1	19990105	G	7712		CONNECTOR       			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  					ENGINE	CONTAMINATED    	W				A				UNSCHED LANDING         				N			FALSE WARNING             			TO	TAKEOFF        	1			AU	S 										(AUS) DURING TAKEOFF, THE AUTOFEATHER WARNING CAME ON.  GROUND INVESTIGATION FOUND THE TORQUE SIGNAL CONDITION UNIT (PN 	30005-0000-26) PLUG TO CONNECTORS CONTAMINATED.					2	L	7	2 	4T	4	T	RT	A31SO   	E20NE				 
1999021200094	19990212	00094	EU  	1999	2	12	AU990012         	1	19990113	G	5720		SPLICE          			AVIONS	R2160 	R2160       	0960101	EU  	LYC   	O320  	O320D2A     	41508	EA  	SNSNCH	74D	74DM        	EA  	WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							L1163239A	A117877		(AUS) LEFT WING AFT LOWER SPLICE PLATE CRACKED APPROXIMATELY 2 MM (0.079 INCH) IN LENGTH.  ALSO, THE FORWARD RIGHT ANGLE	 DOUBLER WAS CRACKED IN THE LOWER BEND RADIUS FOR APPROXIMATELY 25 MM (0.984 INCH).  FOUND IAW AD/ROBIN/8A2.  PART TC: 5	,707.				1	L	7	1 	3O	3	O	RT	A48EU   	E274	5	N	P88614	 
1999021200095	19990212	00095	SO  	1999	2	12	AU990013         	1	19990110	G	3234	12038594001	MODULE          			EMB   	120   	EMB120      	3260201	SO  										MLG	MALFUNCTIONED   	W				A				UNSCHED LANDING         				O			OTHER                     			CL	CLIMB          	1			AU	S 			698  							(AUS) AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT WHEN SELECTED.  INVESTIGATION FOUND THE LANDING GEAR CONTROL MOD	ULE MALFUNCTIONING.  PART TC:  15,199.					2	L	7	2 	4T			RT	A31SO   					 
1999021200096	19990212	00096	EU  	1999	2	12	AU990014         	1	19990105	G	5713		STRINGER        			FOKKER	F27   	F27MK50     		EU  										RT & LT WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) CRACKS FOUND AT RIB LOCATIONS ON STRINGER NRS 5 AND 6 (UPPER AND LOWER) ON BOTH LT AND RT WINGS.  FOUND IAW SBF50-	57-019.    PART TC:  21,456.					2	H	7	2 	4T			RT	A817    					 
1999021200097	19990212	00097	EU  	1999	2	12	AU990015         	1	19990107	G	5313		STRINGER        			FOKKER	F27   	F27MK50     		EU  										BS 11675	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE LT SIDE STRINGER NR 1143 BETWEEN FRAME NR 11675 AND STA 14926 FOUND WITH ADVANCED EXFOLIATION CORROSION E	FFECTING APPROXIMATELY 70 PERCENT OF ITS LENGTH.  ALSO, THE SAME STRINGER ON THE RIGHT SIDE OF THE FUSELAGE HAD THE SAME	 TYPE OF CORROSION FOR 100 MM (3.937 INCHES) EACH SIDE OF FRAME NRS 12975, 10725 AND 10275.  CORROSION WAS FOUND DURING 	A SCHEDULED 12 YEARLY INSPECTION.  PART TC:  21,456.			2	H	7	2 	4T			RT	A817    					 
1999021200098	19990212	00098	CE  	1999	2	12	AU990016         	1	19990106	G	3221	5842000211	TRUNNION        			CESSNA	441   	441         	2076020	CE  										NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR LT AND RT TRUNNION LOWER RADII CRACKED:   LEFT,  APPROXIMATELY 10 MM (0.394 INCH).  RIGHT,  APPR	OXIMATELY 8 MM (0.315 INCH).  FOUND DURING NDI INSPECTION.  PART TC:  13,966.					1	L	7	2 	3T			RT	A28CE   					 
1999031200041	19990312	00041	EU  	1999	3	12	AU990017         	1	19990113	G	5741	951354000	BOLT            			AVIONS	R2160 	R2160       	0960101	EU  	LYC   	O320  	O320D2A     	41508	EA  	SNSNCH	74D	74DM        	EA  	WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							L1163239A	A117877		(AUS) WHEN WING SPAR BOLTS WERE MAGNAFLUXED, (NOT A REQUIREMENT OF THIS AD), ALL 12 BOLTS WERE FOUND CRACKED UNDER HEAD.	  FOUND DURING COMPLIANCE WITH AD/ROBIN/8A2.   PART TC:  5,707.					1	L	7	1 	3O	3	O	RT	A48EU   	E274	5	N	P88614	 
1999031200042	19990312	00042	NM  	1999	3	12	AU990018         	1	19990109	G	2810	MS295262	CAP             			BOEING	737   	737376      		NM  										FUEL CELL	MISSING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUEL CAP WAS MISSING AND FUEL PANEL OPEN.  FOUND FOLLOWING AIRCRAFT ARRIVAL.						2	L	7	2 	4F			RT	A16WE   					 
1999031200043	19990312	00043	SO  	1999	3	12	AU990019         	1	19990113	G	5711		SPAR            			AYRES 	S2    	S2RT15NORMAL	0970105	SO  	PWA   	PT6   	PT6A15AG    	52043	NE  	HARTZL	HCB3T	HCB3TN3     	GL  	WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							PCE14051			(AUS) WING FRONT SPAR SPLICE RIGHT OUTBOARD HOLE HAS A SMALL CRACK AT THE INBOARD LOWER CORNER OF THE SPAR SECTION RUNNI	NG UP THE BOLT HOLE.  CRACK LENGTH APPROXIMATELY 3.175 MM (0.125 INCH).  FOUND DURING NDT INSPECTION IAW AD/ACSNOW/24 AM	DT1.				1	L	7	1 	3T	4	T		A3SW    	E4EA	6	C	P15EA	 
1999031200044	19990312	00044	SW  	1999	3	12	AU990020         	1	19990112	G	2720	27U2051041A	TORQUE TUBE     			SWRNGN	SA226 	SA226TC     	8780404	SW  	GARRTT	TPE331	TPE33110UA  	01514	WP  	HARTZL	HCB3T	HCB3TN5     	GL  	RUDDER	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) DURING RUDDER REMOVAL, IT WAS FOUND THAT THE PRESSURIZATION SEAL CARRIER HAD WORN INTO THE RUDDER TORQUE TUBE.  SU	SPECTED CAUSE ATTRIBUTED TO THE BELLCRANK BEARING HAVING EXCESSIVE SIDE PLAY.					2	L	7	2 	4T	4	T	RT	A8SW    	E4WE	6	C	P15EA	 
1999031200045	19990312	00045		1999	3	12	AU990021         	4	19990113	G	2562	016262	BATTERY         	ACK         	E01         	CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	ELT	UNAPPROVED PART 	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 					016262					(AUS) ELT FAULTY.  INVESTIGATION FOUND THAT INCORRECT BATTERIES HAD BEEN FITTED.						1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22EA	 
1999031200046	19990312	00046	CE  	1999	3	12	AU990022         	1	19990112	G	3213		LUG             		514110313   	CESSNA	402   	402C        	207590R	CE  	CONT  	O520  	TSIO520VB   	17040	SO  	MCAULY	3AF32C	3AF32C87    	GL  	LT MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WHILE CHARGING THE LEFT LANDING GEAR STRUT, IT WAS NOTICED THAT THE RETRACT LUG ON THE STRUT P/N 5141103-13 EXHIBI	TED SIGNS OF CRACKING.  A DYE PENETRANT CHECK CONFIRMED THE DEFECT.   PART TC:  32.					1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22EA	 
1999031200047	19990312	00047	EU  	1999	3	12	AU990023         	1	19990112	G	3213	A103JS	NUT             			BNORM 	BN2   	BN2A8       	1520209	EU  	LYC   	O540  	O540E4C5    	41532	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	LT MLG	SHEARED         	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) LEFT MAIN LANDING GEAR TORQUE LINK NUT (P/N A103JS) SHEARED OFF THE BOLT (P/N A10217J) STRIPPING THE SPLIT PIN IN 	THE SAME ACTION.  RUNWAY SURFACE WAS REPORTED ROUGH.   PART TC:  61.					1	H	7	2 	3O	3	O		A17EU   	E295	5	C	P920	 
1999031200048	19990312	00048	SW  	1999	3	12	AU990024         	1	19990113	G	3260	1543011SN1	SWITCH          			SWRNGN	SA226 	SA226TC     	8780404	SW  	GARRTT	TPE331	TPE3313UW   	01514	WP  	HARTZL	HCB3T	HCB3TN5     	GL  	NLG	LEAKING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					0625					(AUS) NOSE LANDING GEAR PRESSURE SWITCH LEAKING OIL FROM WELDED SEAM.						2	L	7	2 	4T	4	T	RT	A8SW    	E4WE	6	C	P15EA	 
1999031200049	19990312	00049	EU  	1999	3	12	AU990025         	1	19990116	G	3244	22X675X10	TIRE            	DUNLOP      	AHA1837     	JETAIR	JETSTM	JETSTM4101  	1500501	EU  	GARRTT	TPE331	TPE33114GR  	01514	NE  					MLG	FAILED          	W				C				ABORTED TAKEOFF         				O			OTHER                     			TO	TAKEOFF        	1			AU	S 			23   		TF032					(AUS) DURING TAKEOFF, NR 1 MAIN LANDING GEAR TIRE TREAD SEPARATED.  TIRE WAS A RETREADED PRODUCT.						2	L	7	2 	4T	4	T	RT	A41NM   	E18NE				 
1999031200050	19990312	00050	EU  	1999	3	12	AU990026         	1	19990120	G	7810	1379048H401	TAILPIPE        			BAG   	JETSTM	JETSTM3201  	1500217	EU  	GARRTT	TPE331	TPE33112UHR 		WP  	ROTOL	R333	R333482F12  	GL  	RT ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							P66277			(AUS) ROGHT ENGINE TAIL PIPE ASSEMBLY AFT END HAD EXCESSIVE ORBITAL MOVEMENT. THE PIPE WAS REMOVED AND IT WAS DISCOVERED	 THAT THE PIPE HAD CRACKED THE AFT END WAS SEPARATING FROM THE FORWARD FLANGED END FOR 99.5 PERCENT OF ITS CIRCUMFERENCE	.  THE CAUSE WAS FOUND TO BE THE FORWARD AND AFT LOCATING AND RETENTION BOLTS COMING ADRIFT DUE TO EXCESSIVE FATIGUE AND	 WEAR.  AIRCRAFT WAS IMPORTED FROM THE USA.			2	L	7	2 	4T	4	T	RT	A56EU   	E4WE	6	C	P61GL	 
1999031200051	19990312	00051	EU  	1999	3	12	AU990027         	1	19990121	G	5720	68140133	ANGLE           	PARTEN      	P68B        	PARTEN	P68   	P68B        		EU  	LYC   	O360  	IO360A1B6   	41514	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					124					(AUS) FORWARD WING SPAR RIGHT AFT SPAR CAP ANGLE FOUND TO BE CRACKED IN THE AREA OUTBOARD OF THE RIGHT WING ATTACHMENT. 	 FOUND DURING INSPECTION IAW AD/P68/45 (SB/65).   PART TC:  6,062.					1	H	7	2 	3O	3	O		A31EU   	1E10	5	C	P920	 
1999031200052	19990312	00052	CE  	1999	3	12	AU990028         	1	19990114	G	3213	12411172	STRUT           			CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	RT MLG	CRACKED         	W				C				ABORTED TAKEOFF         				O			OTHER                     			TO	TAKEOFF        	1			AU	S 			10205				240743H	931708		(AUS) DURING TAKEOFF ROLL, THE RIGHT WING WAS NOTICED TO DROP.  INSPECTION OF THE LANDING GEAR LEG REVEALED IT HAD CRACK	ED COMPLETELY OFF APPROXIMATELY 25.4 MM (1.0 INCH) OUTBOARD OF THE MAIN GEAR SADDLE.  AIRCRAFT REGULARLY OPERATES FROM B	EACH AIRSTRIPS.  PART TC:  10,205.				1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
1999031200053	19990312	00053		1999	3	12	AU990029         	1	19990116	G	7722	0301037070	HARNESS         								TMECA 	ARRIEL	ARRIEL1A    	60030	NE  					NR 2 ENGINE	MALFUNCTIONED   	W				O				OTHER                   				N			FALSE WARNING             			CR	CRUISE         	1			AU	S 			221  		154		154			(AUS) NR 2 ENGINE T4 PYROMETRIC HARNESS FAULTY.  NR 2 ENGINE T4 GAUGE GAVE ERRONEOUS READINGS.   PART TC:  221.											3	U			E19EU				 
1999031200054	19990312	00054	CE  	1999	3	12	AU990030         	1	19990119	G	5720	042640012	ANGLE           			CESSNA	150   	152         	2071835	CE  						MCAULY	1A103	1A103TCM    	GL  	LT WING	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT WING ROOT LEADING ATTACHMENT ANGLE CORRODED.  FOUND DURING INVESTIGATION OF A FUEL TANK PROBLEM.   PART TC: 8	,168.					1	H	7	1 	3O			NT	3A19    		5	N	P50GL	 
1999031200055	19990312	00055	NM  	1999	3	12	AU990031         	1	19990108	G	5714		WEB             			BOEING	727   	727277      	138408S	NM  	PWA   	JT8   	JT8D15      	52051	NE  					WING BOX	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WING CENTER SECTION REAR SPAR WEB CRACKED IN THE AREA BETWEEN RBL 12 AND RBL 13.  THE CRACK WAS LOCATED JUST BELOW	 THE TANGENT POINT OF THE MACHINED LAND RADIUS OF THE WEB.  CRACK LENGTH 19.05 MM (0.750 INCH).  FOUND DURING NDT INSPEC	TION IAW AD/B727/152.				2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
1999031200056	19990312	00056	CE  	1999	3	12	AU990032         	1	19990119	G	3230	358250944	PLUNGER         			BEECH 	58    	58          	1152740	CE  	CONT  	O550  	IO550C      		SO  	MCAULY	3AF32C	3AF32C512   	GL  	NLG	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR AFT FORWARD RETRACTION ROD PLUNGER AFT ATTACHMENT LUG BROKEN.  ONE OF THE TWO LUGS WAS BROKEN IN	 HALF.   PART TC:  8,180.					1	L	7	2 	3O	3	O		3A16    	E3SO	5	C	P22EA	 
1999031200057	19990312	00057	EU  	1999	3	12	AU990033         	1	19990118	G	5751	NB24D287	BALANCE WEIGHT  		NB244302    	BNORM 	BN2   	BN2B26      	1520350	EU  	LYC   	O540  	O540E4C5    	41532	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	AILERON	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT AILERON MASS BALANCE ARM SNAPPED OFF ADJACENT TO ITS CLAMP DURING MEDIUM WIND BUFFETING.  INSPECTION OF THE 	ARM REVEALED CORROSION AROUND 70 PERCENT OF THE CIRCUMFERENCE.  THE LEFT ARM ASSEMBLY WAS THEN INSPECTED AND FOUND TO BE	 CORRODED ON THE REAR OF THE ARM IN AN AREA LOCATED TOWARDS THE FLUTED AILERON SECTION.				1	H	7	2 	3O	3	O	RT	A17EU   	E295	5	C	P920	 
1999031200058	19990312	00058	CE  	1999	3	12	AU990034         	1	19990121	G	2910	510011172	PIPE            			CESSNA	402   	402C        	207590R	CE  	CONT  	O520  	TSIO520VB   	17040	SO  	MCAULY	3AF32C	3AF32C87    	GL  	HYDRAULIC SYS	CRACKED         	W				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			LD	LANDING        	1			AU	S 										(AUS) DURING LANDING, THE PILOT NOTED A STRONG HYDRAULIC OIL SMELL.  INVESTIGATION FOUND THE HYDRAULIC PRESSURE LINE LOC	ATED IN THE AREA BEHIND THE RIGHT ENGINE FIREWALL WAS TWISTED AND SPLIT.  THE ELBOW FITTING P/N AN837-6 WAS LOOSE IN THE	 FIREWALL AND TIGHTENING THE NUT HAD NO EFFECT.  THE FITTING WAS REMOVED AND IT WAS DISCOVERED THAT THE WASHER P/N AN960	-1016 HAD NOT BEEN PROPERLY LOCATED ON THE FITTING.  PART TC:  10,009.			1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22EA	 
1999031200059	19990312	00059	NM  	1999	3	12	AU990036         	1	19990112	G	5410		WEB             			BOEING	767   	767204      		NM  	GE    	CF6   	CF680A      	30025	NE  					LT NACELLE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT ENGINE PYLON TOP WEB CRACKED AT THE REAR OUTBOARD CORNER OF ONE WEB CUT-OUT.  CRACK LENGTH 9.53 MM (0.375 INC	H).  FOUND DURING EDDY CURRENT INSPECTION.					2	L	7	2 	4F	4	F	RT	A1NM    	E13NE				 
1999031200060	19990312	00060	NM  	1999	3	12	AU990037         	1	19990113	G	5754		WEDGE           			BOEING	767   	767204      		NM  	GE    	CF6   	CF680A      	30025	NE  					SLAT	DISBONDED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES FOUND WITH DISBONDED AREAS ON A TOTAL OF SEVEN SLATS.  FOUND DURING VISUAL 	AND ULTRASONIC INSPECTIONS IAW BOEING ALERT SB 767-57A0039.					2	L	7	2 	4F	4	F	RT	A1NM    	E13NE				 
1999031200061	19990312	00061	SO  	1999	3	12	AU990038         	2	19990116	G	7310	630658	LINE            			CESSNA	172   	R172K       	2072431	CE  	CONT  	O360  	IO360HB     	17025	SO  	MCAULY	2A34C	2A34C203    	GL  	FUEL SYSTEM	FRACTURED       	W				O				OTHER                   				E			VIBRATION/BUFFET          			CR	CRUISE         	1			AU	S 					265125R		265125R			(AUS) NR 2 CYLINDER INJECTOR LINE FRACTURED AT THE FERRULE ON THE DISTRIBUTOR END.						1	H	7	1 	3O	3	O		3A17    	E1CE	5	C	P3EA	 
1999031200062	19990312	00062	NM  	1999	3	12	AU990039         	1	19990107	G	5311		FRAME           			BOEING	737   	737377      		NM  										FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT AND RIGHT FORWARD PRESSURE BULKHEAD SIDE CHORDS CRACKED.  TWO CRACKS WERE ALSO FOUND IN THE BULKHEAD WEB AND 	ONE IN THE VERTICAL CHORD LOCATED AT LBL 5.7.					2	L	7	2 	4F			RT	A16WE   					 
1999031200063	19990312	00063		1999	3	12	AU990040         	4	19990119	G	2312	1720	TRANSCEIVER     			AIRBUS	320   	A320212     		EU  										VHF COMM	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					1720					(AUS) VHF COM 1 TRANSCEIVER FAULTY.  TRANSCEIVER CAUSES CONTINUOUS TRANSMISSION ON BRISBANE FREQUENCY VHF 121.70 MHZ.  E	XTENSIVE WORKSHOP TESTING COULD FIND NO FAULTS.  PART TC:  13,323.					2	L	7	2 	4F			RT	A28NM   					 
1999031200064	19990312	00064	SO  	1999	3	12	AU990041         	1	19990121	G	7810	LW16696	EXHAUST PIPE    			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	ENGINE	FAULTY          	W				O				OTHER                   				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		DE	DESCENT        	1			AU	S 			1241 				L278368A			(AUS) DURING DESCENT, THE RT ENGINE MAP DROPPED.  INVESTIGATION REVEALED EXHAUST SLIP JOINTS HAD EXPANDED OPEN ENOUGH FO	R A GAP TO APPEAR BETWEEN THE PIPE ENDS.  FURTHER INVESTIGATION FOUND THAT THE FEMALE SECTION OF PIPE EXPANDED TO A LARG	E DIAMETER THAN MALE PIPE, BUT WHEN COLD, THE EXHAUST PIPE FITTED CORRECTLY.				1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
1999031200065	19990312	00065	NM  	1999	3	12	AU990042         	1	19990120	G	5210	MS166241037	CIRCLIP         			BOEING	737   	737376      		NM  										PASSENGER DOOR	MISSING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) UNABLE TO OPEN L1 DOOR.  INVESTIGATION FOUND THE UPPER GUIDE ARM ATTACHMENT PIN HAD MIGRATED UP RESTRICTING MOVEME	NT OF THE DOOR DUE TO THE ATTACHMENT PIN CIRCLIP SEPARATING.					2	L	7	2 	4F			RT	A16WE   					 
1999031200066	19990312	00066	NM  	1999	3	12	AU990043         	1	19990116	G	5230	85230448001	BELLCRANK       			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					CARGO DOOR	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					013					(AUS) CARGO DOOR WOULD NOT LOCK AFTER LOADING AIRCRAFT.  ROTATION OF THE BAGGAGE DOOR HANDLE HAD NO EFFECT ON DOOR LOCKI	NG.  INVESTIGATION FOUND THAT BELLCRANK FAILURE HAD OCCURRED BETWEEN THE HANDLE AND DOOR LOCKING MECHANISM AT THE BEARIN	G RETAINER.  PART TC:  13,252.				2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999031200067	19990312	00067		1999	3	12	AU990044         	4	19990113	G	6122	C20908	DRIVE DISC      	MCAULY      	DEFS290D753 	CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	PROP GOVERNOR	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1696 		790858					(AUS) PROPELLER GOVERNOR FLYWEIGHT DRIVE DISC BROKE IN TWO.						1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22EA	 
1999031200068	19990312	00068	WP  	1999	3	12	AU990045         	2	19990125	G	8520		CRANKCASE       			DHAV  	DHC1  	DHC1SER22   	2801714	GL  	DHAVXX	GIPSY 	GIPSYMAJOR1 	20004	WP  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							11263			(AUS) DURING COFA INSPECTION, THE ENGINE CRANKCASE WAS FOUND TO BE CRACKED ON THE RT SIDE.  CRACK LENGTH 150 MM (5.91 IN	CH).  ON ENGINE STRIP DOWN THE FOLLOWING ADDITIONAL DEFECTS WERE FOUND:  1.  THREE OF THE FOUR CONNECTING RODS HAD IMPAC	T DAMAGE SCRATCHES AND NICKS SOME OF WHICH HAD BEEN REWORKED WITH A FILE OR  SANDPAPER.  DENTS ON THE ROD WERE UP TO 2 M	M (0.079 INCH) DEEP.  2.  CRANKSHAFT MAIN BEARING JOURNALS WORN.  3.  CENTER AND REAR MAIN BEARINGS SHOWED EXTREME WEAR.			1	L	7	1 	3O	3	I		EXPA1L71	A8EU				 
1999031200069	19990312	00069	EU  	1999	3	12	AU990046         	1	19990106	G	5343		FITTING         		HC537L000200	BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR RETRACTION JACK ATTACHMENT BOSS CRACKED IN THE FOLLOWING THREE PLACES:  1.  ONE 10 MM (0.394 INC	H) AND ONE 12 MM (0.47 INCH) CRACK IN THE BORE EXTENDING FOR 20 MM (0.78 7INCH) ACROSS THE FACE OF THE BOSS.  2.  ONE CR	ACK ACROSS THE ENTIRE BOSS FACE EXTENDING 9 MM (0.354 INCH) DOWN OUTSIDE OF THE BOSS FACE AND FOR 20 MM (0.787 INCH) IN 	THE BORE FOUND DURING INSPECTION IAW AD/BAE146/071.   PART TC:  40,744.			2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999031200070	19990312	00070		1999	3	12	AU990047         	1	19990116	G	7810	7210D1902	EXHAUST PIPE    								CONT  	O240  	IO240A      		SO  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NR 2 AND NR 3 CYLINDER EXHAUST PIPE TO CYLINDER MOUNTING FLANGES CRACKED AROUND THE CIRCUMFERENCE OF THE WELD.  CR	ACK LENGTH APPROXIMATELY 50.8 MM (2.0 INCH).  MUFFLER CANS ALSO CRACKED IN THREE PLACES AT WELDS SECURING THE SHROUD SUP	PORT BRACKETS.  FOUND DURING INSPECTION IAW AD/X-TS/1.   PART TC:  486.									3	O			E7SO				 
1999031200071	19990312	00071		1999	3	12	AU990049         	1	19990125	G	7810	7210D1902	EXHAUST PIPE    								CONT  	O240  	IO240A      		SO  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NR 2 CYLINDER EXHAUST PIPE TO CYLINDER MOUNTING FLANGE CRACKED APPROXIMATELY 50.8 MM (2 INCHES) AROUND CIRCUMFEREN	CE OF WELD.  FOUND DURING INSPECTION IAW AD/X-TS/1.  PART TC:  195.										3	O			E7SO				 
1999031200072	19990312	00072	EU  	1999	3	12	AU990050         	1	19990117	G	5240		BUSHING         			AIRBUS	320   	A320212     		EU  										SERVICE DOOR	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS)  RIGHT FORWARD SERVICE DOOR LOWER CONNECTION LINK BUSHING MIGRATED.						2	L	7	2 	4F			RT	A28NM   					 
1999031200073	19990312	00073	EU  	1999	3	12	AU990051         	1	19990113	G	5610	97290H8026	WINDSHIELD      			AIRBUS	320   	A320212     		EU  										COCKPIT	CRACKED         	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			AU	S 					97290H8026					(AUS) FIRST OFFICER'S RIGHT NR 1 WINDOW CENTER GLASS PANE SHATTERED.  PART TC:  1,703.						2	L	7	2 	4F			RT	A28NM   					 
1999031200074	19990312	00074	NM  	1999	3	12	AU990052         	1	19990126	G	2130		REGULATOR       			BOEING	737   	737476      		NM  										CABIN PRESSURE	FAULTY          	W				O				OTHER                   				O			OTHER                     			DE	DESCENT        	1			AU	S 										(AUS) CABIN PRESSURIZATION SYSTEM FAULTY.  LEFT SYSTEM HIGH STAGE REGULATOR P/N 107484-5 AND RIGHT SYTEM HIGH STAGE VALV	E P/N 3214446-4 AND BLEED AIR REGULATOR P/N 107492-2 CHANGED.					2	L	7	2 	4F			RT	A16WE   					 
1999031200075	19990312	00075	CE  	1999	3	12	AU990053         	1	19990128	G	7120	07516001	MOUNT           			CESSNA	182   	182Q        	2072732	CE  	CONT  	O470  	O470*       	17026	SO  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ENGINE MOUNT CRACKED AS INDICATED IN AD/CESSNA180/4 AMDT1.  PART TC:  1,880.						1	H	7	1 	3O	3	O	NT	3A13    	E273				 
1999031200076	19990312	00076	SW  	1999	3	12	AU990054         	1	19990113	G	5311		FRAME           	MOONEY      		MOONEY	M20   	M20J        	5870219	SW  	LYC   	O360  	IO360A1B6   	41514	EA  	MCAULY	2D34C	B2D34C214   	GL  	FUSELAGE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE TUBULAR FRAMES CORRODED EXTERNALLY.  FOUND DURING INSPECTION IAW SB M20-208B.   PART TC:  2,208.						1	L	7	1 	3O	3	O		2A3     	1E10	5	C	P7EA	 
1999031200077	19990312	00077	SO  	1999	3	12	AU990055         	2	19990127	G	8520	630046	PLUG            								CONT  	O520  	IO520D      	17032	SO  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NEW CYLINDER KITS CONTAINED CRACKED PISTON PIN END PLUGS.  KITS WERE SUPPLIED AS A NEW ITEM.											3	O			E5CE				 
1999031200078	19990312	00078	CE  	1999	3	12	AU990056         	1	19990108	G	5311	12110041	FRAME           			CESSNA	206   	TU206G      	2073357	CE  	CONT  	O520  	TSIO520M    	17040	SO  	MCAULY	D3A34	D3A34C402   	GL  	FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					06787					(AUS) LEFT FRONT DOOR POST FRAME CRACKED THROUGH.  DOUBLER ALSO CRACKED.  AIRCRAFT OPERATES AS A FLOAT PLANE.						1	H	7	1 	3O	3	O		A4CE    	E8CE	5	C	P47GL	 
1999031200079	19990312	00079	EU  	1999	3	12	AU990057         	1	19990119	G	5741	951354000	BOLT            			AVIONS	R2160 	R2160       	0960101	EU  	LYC   	O320  	O320D2A     	41508	EA  	SNSNCH	74D	74DM        	EA  	SPAR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							L1163339A	A57396		(AUS) WING SPAR BOLTS CRACKED UNDER THE BOLT HEAD.   PART TC:  3,547.						1	L	7	1 	3O	3	O	RT	A48EU   	E274	5	N	P88614	 
1999031200080	19990312	00080	EU  	1999	3	12	AU990058         	1	19990108	G	5343	HC537L0002004	FITTING         			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BOSS CONTAINED TWO CRACKS IN THE FOLLOWING AREAS:  1.  CRACK LOCA	TED IN THE BORE ONLY - CRACK LENGTH 7 MM (0.275 INCH).  2.  ONE CRACK LOCATED BOTH INSIDE THE BORE AND ACROSS THE FACE W	ITH THE BORE CRACK LENGTH 3 MM (0.118 INCH) AND THE FACE CRACK 13 MM (0.511 INCH).  FOUND DURING EDDY CURRENT INSPECTION	 IAW AD/BAE146/071.   PART TC:  32,291.			2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999031200081	19990312	00081	EU  	1999	3	12	AU990059         	1	19990113	G	5343	HC537L0002004	FITTING         			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR ACTUATOR ATTACHMENT BOSS CRACKED.  CRACK RAN FROM THE EDGE OF THE BORE TO A POINT APPROXIMATELY 	1 MM (0.0393 INCH) FROM THE EDGE OF THE BOSS AT THE 6 O'CLOCK POSITION.  FOUND DURING EDDY CURRENT INSPECTION IAW AD/BAE	146/071. PART TC:  25,335.				2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999031200082	19990312	00082	EU  	1999	3	12	AU990060         	1	19990113	G	5343	HC537L0002004	FITTING         			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR ACTUATOR ATTACHMENT BOSS FACE CRACKED.  CRACK RAN FROM THE BORE TO A POINT 6 MM (0.236 INCH FROM	 THE OUTER EDGE OF THE BOSS AT THE 3 O'CLOCK POSITION.  FOUND DURING EDDY CURRENT INSPECTION IAW AD/BAE146/071.   PART T	C:  27,739.				2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999031200083	19990312	00083	EU  	1999	3	12	AU990062         	1	19990129	G	2782		ACTUATOR        			AIRBUS	320   	A320212     		EU  										LE FLAP	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT NR 2 LEADING EDGE SLAT OUTBOARD ACTUATOR FAULTY.						2	L	7	2 	4F			RT	A28NM   					 
1999031200084	19990312	00084	NE  	1999	3	12	AU990063         	2	19990118	G	7311	AEY00243	HEAT EXCHANGER  								GE    	CF6   	CF680A      	30025	NE  					LT ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			26858		AEY00243		580179			(AUS) LEFT ENGINE FUEL/OIL HEAT EXCHANGER HEADER RADIUS CONTAINED TWO CRACKS.  FOUND DURING ULTRASONIC INSPECTION IAW GE	6-79-00-2C AND GE SERVICE BULLETIN SB79-023.   PART TC:  26,858.										4	F			E13NE				 
1999031200085	19990312	00085	NE  	1999	3	12	AU990064         	2	19990124	G	7200		ENGINE          								GE    	CF6   	CF680A      	30025	NE  					LEFT	MAKING METAL    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							580176			(AUS) LEFT ENGINE CHIP DETECTOR CONTAMINATED WITH M50 BEARING MATERIAL.											4	F			E13NE				 
1999031200086	19990312	00086	NM  	1999	3	12	AU990065         	1	19990112	G	5311		FRAME           			BOEING	737   	737377      		NM  										BS 847	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE FRAME LOCATED IN THE AFT CARGO COMPARTMENT AT STN 847 BETWEEN STRINGERS S25R AND S26R CONTAINED SEVERE CO	RROSION.					2	L	7	2 	4F			RT	A16WE   					 
1999031200087	19990312	00087	NM  	1999	3	12	AU990066         	1	19990117	G	5280	655051435	BRACKET         			BOEING	737   	737377      		NM  										NLG DOOR	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT NOSE LANDING GEAR DOOR AFT HINGE BRACKET BROKEN INTO TWO PIECES.   PART TC:  34,874.						2	L	7	2 	4F			RT	A16WE   					 
1999031200088	19990312	00088	EU  	1999	3	12	AU990067         	1	19990107	G	5210		BUSHING         			AIRBUS	320   	A320212     		EU  										PASSENGER DOOR	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) PASSENGER/SERVICE DOOR LATCH LINK BUSHINGS MIGRATED ON THE FOLLOWING DOORS:  1.  LT AFT DOOR - TWO FLANGED BUSHING	S.  2. RIGHT AFT DOOR - ONE LOWER FLANGED BUSHING FOUND DURING INSPECTION IAW ER A32-52-10-7D.					2	L	7	2 	4F			RT	A28NM   					 
1999031200089	19990312	00089	NE  	1999	3	12	AU990068         	2	19990131	G	7230		BLADE           								LYC   	ALF502	ALF502R5    	41580	NE  					NR 2 ENGINE	DAMAGED         	W				O				OTHER                   				E	C		VIBRATION/BUFFET          	F.O.D.                    		TO	TAKEOFF        	1			AU	S 										(AUS) NR 2 ENGINE FAN BLADES AND ADJACENT BLADE MID-SPAN SUPPORTS DAMAGE DUE TO BIRDSTRIKE.											4	F			E6NE				 
1999031200090	19990312	00090		1999	3	12	AU990072         	4	19990125	G	2562		SWITCH          	ACK         	E0101       	BEECH 	33    	F33A        	1151425	CE  	CONT  	O520  	IO520B      	17032	SO  	MCAULY	3A32C	3A32C76     	GL  	ELT	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELT INERTIA SWITCH FAULTY.						1	L	7	1 	3O	3	O		3A15    	E5CE	5	C	P21EA	 
1999031200091	19990312	00091	SO  	1999	3	12	AU990073         	1	19990121	G	2460	W31X2M1G40	SWITCH          			PIPER 	PA31  	PA31350     	7103110	SO  						HARTZL	HCE3Y	HCE3YR2     	GL  	DC SYSTEM	FAILED          	W				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			CR	CRUISE         	1			AU	S 										(AUS) SWITCH OVERHEATED.  SWITCH IS LOCATED IN THE LEFT INSTRUMENT PANEL.  PART TC:  11,700.						1	L	7	2 	3O				A20SO   		5	C	P33EA	 
1999031200092	19990312	00092	NM  	1999	3	12	AU990074         	1	19990124	G	2450		HARNESS         			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					AC SYSTEM	WORN            	W				O				OTHER                   				N			FALSE WARNING             			CL	CLIMB          	1			AU	S 										(AUS) WIRING HARNESS LOCATED IN THE LEFT CABIN UNDERFLOOR TROUGH CHAFED.  HARNESS HAD SUFFERED PREVIOUS MECHANICAL DAMAG	E.   PART TC:  21,573.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999031200093	19990312	00093	EU  	1999	3	12	AU990075         	1	19990128	G	5343	HC537L0002004	FITTING         			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BOSS CRACKED IN THE FOLLOWING THREE AREAS:  1.  CRACK LOCATED AT 	APPROXIMATELY THE 4 O'CLOCK POSITION - CRACK LENGTH IN BORE 12.7 MM (0.5 INCH) ACROSS THE BOSS FACE TO WITHIN 4.826 MM (	0.19 INCH).   2.  CRACK LOCATED AT APPROXIMATELY THE 3 O'CLOCK POSITION - CRACK LENGTH IN BORE 12.7 MM (0.5 INCH) AND AC	ROSS THE BORE FACE.  3.  CRACK LOCATED AT APPROXIMATELY THE 9 O'CLOCK POSITION - CRACK LENGTH IN BORE 6.35 MM (0.25 INCH	) AND ACROSS THE BOSS FACE FOR 6.35 MM (0.25 INCH).  FOUND DURING EDDY CURRENT INSPECTION IAW AD/BAE146/071.   PART TC: 	 40,979.	2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999031200094	19990312	00094	EU  	1999	3	12	AU990076         	1	19990101	G	5280	HC321B0040000	BRACKET         			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					LT MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT MAIN LANDING GEAR DOOR REAR HINGE BRACKET CRACKED.  FOUND DURING INSPECTION IAW ER BA6-32-10-30.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999031200095	19990312	00095	WP  	1999	3	12	AU990077         	2	19990204	G	7314	P63089	PUMP            	GARRTT      							GARRTT	TPE331	TPE33110UA  	01514	WP  	ROTOL	R333	R333482F12  	GL  	NR 2 ENGINE	FAILED          	W				E				ENGINE SHUTDOWN         				E			VIBRATION/BUFFET          			CL	CLIMB          	1			AU	S 					P63089		P63089			(AUS) NR 2 ENGINE GEARBOX FUEL PUMP DRIVE FAILED.											4	T			E4WE	6	C	P61GL	 
1999031200096	19990312	00096	SO  	1999	3	12	AU990078         	1	19990201	G	3260	12041126001	SENSOR          			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  	HAMSTD	14RF	14RF9       	NE  	MLG	FAULTY          	W				C				ABORTED TAKEOFF         				N			FALSE WARNING             			TO	TAKEOFF        	1			AU	S 										(AUS) LANDING GEAR UPLOCK PROXIMITY SENSOR FAULTY.  DOWNLOCK PROXIMITY SENSOR TARGET OUT OF ADJUSTMENT.   PART TC:  24,9	49.					2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	C	P11NE	 
1999031200097	19990312	00097		1999	3	12	AU990079         	4	19990202	G	2562	C589110117	BATTERY         		C5895110117 	CESSNA	182   	182Q        	2072732	CE  										ELT	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					2662					(AUS) ELT BATTERIES LEAKING.  BATTERY CASE CORRODED.  BATTERIES WERE TWELVE MONTHS OUT OF DATE.						1	H	7	1 	3O			NT	3A13    					 
1999031200098	19990312	00098	CE  	1999	3	12	AU990080         	1	19990202	G	2510	110705001	SEAT BELT       			CESSNA	182   	182Q        	2072732	CE  										COCKPIT	FRAYED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) SEAT BELT FRAYED.						1	H	7	1 	3O			NT	3A13    					 
1999031200099	19990312	00099	EU  	1999	3	12	AU990081         	1	19990121	G	5551	TB1034020001	SUPPORT         			SOCATA	TB10  	TB10TOBAGO  	8680696	EU  	LYC   	O360  	O360A1A     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	HORIZ STAB	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) HORIZONTAL STABILIZER LEFT HINGE SUPPORT BRACKET CONTAINED EXFOLIATION CORROSION.  FURTHER INVESTIGATION FOUND THA	T THE HORIZONTAL STABILIZER P/N TB1034020100 CONTAINED MINOR EXFOLIATION CORROSION.   PART TC:  4,880.					1	L	7	1 	3O	3	O	NT	A51EU   	E286	5	C	P920	 
1999031200100	19990312	00100	WP  	1999	3	12	AU990082         	1	19990202	G	5711	H34737	SPAR            			DHAVXX	DH82  	DH82AROBRTSN	2801002	WP  	DHAVXX	GIPSY 	GIPSYMAJOR1 	20004	WP  					WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			549  							(AUS) LEFT UPPER MAIN PLANE FRONT SPAR P/N H34737 AND REAR SPAR P/N H34356 CONTAINED HORIZONTAL CRACKING AND SPLITS FROM	 THE ROOTS TO THE TIPS.  FOUND DURING INSPECTION IAW AD/DH82/11 AMDT1 (BRITISH AEROSPACE T.N.S. CT(MOTH) NR 32 ISSUE 2).	   PART TC:  2,549.				1	Q	7	1 	3I	3	I		A8EU    	A8EU				 
1999031200101	19990312	00101	NM  	1999	3	12	AU990083         	1	19990117	G	2150	78279012	ACM             	HAMSTD      	78279012    	DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					CABIN COOLING	SEIZED          	W				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			AU	S 			6206 		84631					(AUS) AIR CYCLE MACHINE BINDING.  TURBINE WHEEL EVENTUALLY SEIZED.  PART TC:  17,225.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999031200102	19990312	00102	NM  	1999	3	12	AU990085         	1	19990125	G	5610	141T480014	WINDSHIELD      			BOEING	767   	767338      		NM  	GE    	CF6   	CF680C      		GL  					COCKPIT	FAILED          	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			AU	S 					TX2482					(AUS) NR 1 RT WINDOW OUTER PANE SHATTERED.  SEVERE DISCOLORIZATION WAS EVIDENT ALONG THE BOTTOM OF THE WINDOW PANE.						2	L	7	2 	4F	4	F	RT	A1NM    	E23EA				 
1999031200103	19990312	00103	CE  	1999	3	12	AU990086         	1	19990128	G	3411		STATIC SYSTEM   			CESSNA	206   	U206B       	2073322	CE  	CONT  	O520  	IO520A      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	PITOT SYS	CONTAMINATED    	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) STATIC SYSTEM CONTAMINATED WITH WATER.  AIRCRAFT HAD BEEN PARKED IN THE OPEN DURING A RAIN STORM.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
1999031200104	19990312	00104	CE  	1999	3	12	AU990087         	1	19990202	G	7603	12503172	BRACKET         			CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	POWER LEVER	BROKEN          	W				O				OTHER                   				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CL	CLIMB          	1			AU	S 							810207R			(AUS) ENGINE THROTTLE/MIXTURE CONTROL CABLE SUPPORT BRACKET BROKEN.  BRACKET IS MOUNTED ON THE INDUCTION MANIFOLD.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P22EA	 
1999031200105	19990312	00105	CE  	1999	3	12	AU990088         	1	19990128	G	5711		SPAR            			BEECH 	58    	58          	1152740	CE  	CONT  	O550  	IO550C      		SO  	MCAULY	3AF32C	3AF32C512   	GL  	WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FORWARD WING SPAR CARRY THOUGH STRUCTURE CRACKED ON THE RT SIDE IN BOTH THE FORWARD AND AFT AREAS AS DESCRIBED IN 	BEECHCRAFT SERVICE BULLETIN NR 2269 REV 1 (NOT APPLICABLE TO THIS AIRCRAFT).   PART TC:  81,801.					1	L	7	2 	3O	3	O		3A16    	E3SO	5	C	P22EA	 
1999031200106	19990312	00106	NM  	1999	3	12	AU990089         	1	19990112	G	5311		FRAME           			BOEING	737   	737377      		NM  										FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE FRAME INNER CHORD LOCATED AT LHS BS 639 CONTAINED A CRACK EMANATING FROM THE FASTENER.  FOUND DURING EDDY	 CURRENT INSPECTION IAW ER B73-53-10-41A.					2	L	7	2 	4F			RT	A16WE   					 
1999031200107	19990312	00107	SO  	1999	3	12	AU990090         	2	19990127	G	8530	648049	PISTON          			CESSNA	337   	337G        	2075730	CE  	CONT  	O360  	IO360G      	17025	SO  	MCAULY	2AF34C	D2AF34C306  	GL  	ENGINE	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					244583R		244583R			(AUS) NR 6 CYLINDER PISTON DAMAGED DUE TO DETONATION.  METAL CONTAMINATION OF THE ENGINE.  ENGINE FACTORY REMANUFACTURED	 457.1 HOURS PREVIOUSLY.   PART TC:  457.					1	H	7	2 	3O	3	O		A6CE    	E1CE	5	C	P5EA	 
1999031200108	19990312	00108	SW  	1999	3	12	AU990091         	1	19990204	G	7160	BA620	FILTER          			MOONEY	M20   	M20J        	5870219	SW  	LYC   	O360  	IO360A1B6   	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	AIR INTAKE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							L2300451A			(AUS) ENGINE AIR FILTER ASSEMBLY SCREEN BREAKING UP AROUND THE ATTACHMENT RIVETS.  FILTER GASKET ALSO BROKEN WITH SMALL 	PARTS OF THE GASKET MISSING.					1	L	7	1 	3O	3	O		2A3     	1E10	5	C	P920	 
1999031200109	19990312	00109	EU  	1999	3	12	AU990092         	1	19990128	G	3234	713025501	VALVE           	ITT         	713025      	ISRAEL	1124  	1124        	4500102	EU  										MLG	FAILED          	W				O				OTHER                   				N			FALSE WARNING             			TX	TAXI/GRND HDL  	1			AU	S 					K75201					(AUS) LANDING GEAR SELECTOR VALVE BYPASSING INTERNALLY.  LEFT LANDING GEAR COLLAPSED ALLOWING THE AIRCRAFT TO SETTLE ONT	O THE LT TIP TANK.					2	M	7	2 	4F				A2SW    					 
1999031200110	19990312	00110	CE  	1999	3	12	AU990093         	1	19990205	G	2612		WARNING SYSTEM  			BEECH 	200   	B200C       	1152924	CE  	PWA   	PT6   	PT6A41      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	FIRE DETECTION	CONTAMINATED    	W				O				OTHER                   				N			FALSE WARNING             			TO	TAKEOFF        	1			AU	S 										(AUS) FIRE WARNING SYSTEM CONTAMINATED WITH MOISTURE CAUSING FALSE FIRE WARNING.						1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15EA	 
1999031200111	19990312	00111	EU  	1999	3	12	AU990094         	1	19990204	G	2612	51533172	FIRE LOOP       			SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT75A2      	30030	NE  	ROTOL	R354	R3544123F13 	NE  	RT ENGINE	WORN            	W				O				OTHER                   				N			FALSE WARNING             			CL	CLIMB          	1			AU	S 										(AUS) RT ENGINE BLEED AIR FIRE WIRE CHAFED.   PART TC:  19,652.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE6	6	C	P61GL	 
1999031200112	19990312	00112	SW  	1999	3	12	AU990095         	1	19990210	G	3241	60064911	VALVE           			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UAR 	01514	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	BRAKE	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					94070012					(AUS) ANTI-SKID BRAKE CONTROL VALVE SUSPECT FAULTY.   PART TC:  2,825.						2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999031200113	19990312	00113	SO  	1999	3	12	AU990097         	2	19990205	G	8530	652956	VALVE           			BEECH 	33    	35B33       	1151406	CE  	CONT  	O470  	IO470K      	17026	SO  	MCAULY	2A36C	2A36C23     	GL  	EXHAUST	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					092981R		092981R			(AUS) NR 6 CYLINDER EXHAUST VALVE STEM BREAKING UP.  STEM COULD BE MARKED EASILY INDICATING SOFT MATERIAL.  VALVE STEM W	AS FOUND TO BE WORN BY 0.1778 MM (0.007 INCH) IN THE VALVE GUIDE CONTACT AREA.  THE ENGINE HAD BEEN FACTORY REMANUFACTUR	ED 284 HOURS PREVIOUSLY.  FOUND DURING INSPECTION WITH CONTINENTAL CRITICAL SERVICE BULLETIN 98.1 (CSB 98.1).   PART TC:	  284.			1	L	7	1 	3O	3	O		3A15    	3E1	5	C	P880	 
1999031200114	19990312	00114	SO  	1999	3	12	AU990098         	2	19990120	G	8520	619512	CRANKSHAFT      		C85         	UNIVAR	415   	415D        	0420306	NM  	CONT  	C85   	C8512F      	17008	SO  	MCAULY	1B90	1B90CM      	GL  	ENGINE	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			285  		619512		619512			(AUS) CRANKSHAFT AND TIMING GEARS DAMAGED.  ENGINE HAD BEEN OVERHAULED IN THE USA APPROXIMATELY 285 HOURS PREVIOUSLY.						1	L	7	1 	3O	3	O		A787    	E233	5	N	P842	 
1999031200115	19990312	00115	EU  	1999	3	12	AU990099         	1	19990203	G	7921	8540252	OIL COOLER      			STBROS	SD3   	SD360       	8100606	EU  	PWA   	PT6   	PT6A65R     	52043	EA  	HARTZL	HCB5M	HCB5MP3     	GL  	RT ENGINE	FAULTY          	W				O				OTHER                   				E	K		VIBRATION/BUFFET          	FLUID LOSS                		CL	CLIMB          	1			AU	S 					81KC252					(AUS) RT ENGINE OIL COOLER FAULTY.						2	H	7	2 	4T	4	T		A41EU   	E4EA	6	C	P44GL	 
1999031200116	19990312	00116	EU  	1999	3	12	AU990100         	1	19990201	G	7712	7239060502	CTOT PANEL      			SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT75A2      	30030	NE  	ROTOL	R354	R3544123F13 	NE  	COCKPIT	INOP            	W				O				OTHER                   				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		TO	TAKEOFF        	1			AU	S 										(AUS) CONSTANT TORQUE ON TAKEOFF (CTOT) PANEL SUSPECT FAULTY.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE6	6	C	P61GL	 
1999031200117	19990312	00117	EA  	1999	3	12	AU990101         	2	19990127	G	7314	78528	HOUSING         			PIPER 	PA28  	PA28161     	7102803	SO  	LYC   	O320  	O320D3G     	41508	EA  	SNSNCH	74D	74DM        	EA  	OIL PUMP	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1700 		L893339A		L893339A			(AUS) ENGINE OIL PUMP HOUSING BROKEN.  METAL CONTAMINATION OF ENGINE OIL SYSTEM.						1	L	7	1 	3O	3	O		2A13    	E274	5	N	P88614	 
1999031200118	19990312	00118	NM  	1999	3	12	AU990102         	1	19990208	G	7722	CA15000	CONNECTOR       			BOEING	737   	737377      		NM  	CFMINT	CFM56 	CFM563BFR   	13802	EU  					EGT INDICATOR	FAULTY          	W				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			AU	S 										(AUS) NR 2 ENGINE EGT HARNESS CONNECTOR D1208 SUSPECT FAULTY.  LOWER EGT HARNESS P/N TC174-00 AND ELECTRICAL INTERFACE C	OUPLING P/N CA150-00 ALSO REPLACED.					2	L	7	2 	4F	4	F	RT	A16WE   	E21EU				 
1999031200119	19990312	00119	EU  	1999	3	12	AU990103         	1	19990210	G	2497		WIRE            			AIRBUS	320   	A320212     	       	EU  										AC SYSTEM	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELECTRICAL DISTRIBUTION SYSTEM WIRES (48OFF) LOCATED IN AN AREA AT THE BACK OF THE FORWARD CARGO LOCKER WALL PANEL	S 131AW, 131BW, AND 132BW WERE FOUND TO BE CHAFED.  SOME OF THE AFFECTED WIRES (9OFF) WERE PART OF THE FLY-BY-WIRE CONTR	OL SYSTEM INCLUDING:  1.  FROM 90VC-A WIRES NR 2792-0910, N 2792-0911, NR 2792-0936, AND NR 2792-09382.  FROM 88VC-A WIR	ES NR 2792-1137, NR 2792-1159, AND NR 2792-7243 3.  FROM 80VC-A WIRES NR 2794-0403, AND NR 2794-0391.			2	L	7	2 	4F			RT	A28NM   					 
1999031200120	19990312	00120	NM  	1999	3	12	AU990104         	1	19990126	G	2761	A44700009	ACTUATOR        			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					AILERON	MALFUNCTIONED   	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) RT INBOARD ROLL SPOILER ACTUATOR FAULTY.  SPOILER PANEL WOULD NOT FULLY RETRACT.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999031200121	19990312	00121		1999	3	12	AU990105         	4	19990208	G	3420	7001182906	ADI             			BAG   	JETSTM	JETSTM3107  	1500215	EU  						ROTOL	R333	R333482F12  	GL  	INSTRUMENT PANEL	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					89111086					(AUS) NR 2 ATTITUDE DIRECTION INDICATOR (ADI) SUSPECT FAULTY.  WATER FOUND IN THE AREA OF NR 2 VERTICAL GYRO (VG).						2	L	7	2 	4T			RT	BA15CAA 		6	C	P61GL	 
1999031200122	19990312	00122	EA  	1999	3	12	AU990106         	2	19990208	G	7414	IO357584	GEAR            			ROBSIN	R22   	R22BETA     		NM  	LYC   	O320  	O320B2C     	41508	EA  					MAGNETO	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1084 		L068804E		LH926027A			(AUS) MAGNETO NYLON DISTRIBUTOR GEAR HAD TWO BROKEN TEETH.						1	G	7	1 	3O	3	O		H10WE   	E274				 
1999031200123	19990312	00123	WP  	1999	3	12	AU990107         	2	19990201	G	7200	P70164	ENGINE          	GARRTT      		FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UHR 		WP  	MCAULY	4HFR34	4HFR34C652  	NE  	LEFT	MALFUNCTIONED   	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					P70164		P70164			(AUS) LT ENGINE LOST POWER AND DID NOT RESPOND TO THE LT POWER LEVER.  EXTENSIVE INSPECTION AND GROUND RUN FOLLOWED BY A	 TEST FLIGHT COULD FIND NO FAULTS.  ENGINE HAS OPERATED SATISFACTORILY SINCE.  DEFECT NOT CONFIRMED.					2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999031200124	19990312	00124	EU  	1999	3	12	AU990108         	1	19990208	G	7722		CONNECTOR       			BAG   	JETSTM	JETSTM3201  	1500217	EU  	GARRTT	TPE331	TPE33112UHR 		WP  	MCAULY	4HFR34	4HFR34C653  	NE  	EGT INDICATOR	CONTAMINATED    	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 							P66329			(AUS) LT ENGINE EGT SYSTEM CONNECTION CONTAMINATED WITH MOISTURE.						2	L	7	2 	4T	4	T	RT	A56EU   	E4WE	6	C	3PNE	 
1999031200125	19990312	00125	NM  	1999	3	12	AU990109         	1	19990207	G	5311	85320058	FRAME           			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					BS 354	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					67					(AUS) FUSELAGE FRAME LOCATED AT STN 354.25 CRACKED FROM THE OUTSIDE EDGE TO THE LIGHTENING HOLE IN THE AREA BETWEEN STRI	NGER 21S AND STRINGER 22S (RT).   PART TC:  24,813.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999031200126	19990312	00126	CE  	1999	3	12	AU990110         	1	19990128	G	2410	627276	BRACKET         		627068      	BEECH 	55    	95A55       	1152704	CE  	CONT  	O470  	IO470L      	17026	SO  	HARTZL	HCC2Y	BHCC2YF2    	GL  	GENERATOR	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) GENERATOR MOUNT BRACKET BROKEN AT BOTH ENDS.  GENERATOR UPPER STAY ALSO BROKEN.  LOWER STAY WORE THROUGH THE BRASS	 ELBOW ON THE FUEL PUMP.					1	L	7	2 	3O	3	O		3A16    	3E1	5	C	P920	 
1999031200127	19990312	00127	SO  	1999	3	12	AU990111         	1	19990208	G	5330		SKIN            			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  					BS 3293-3956	LIGHTNING STRIKE	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) AIRCRAFT SUFFERED A LIGHTNING STRIKE.  POST-LIGHTNING STRIKE INSPECTION CARRIED OUT IAW EMB120 MAINTENANCE MANUAL 	CHAPTER 5.50.1 AND PRATT AND WHITNEY MAINTENANCE MANUAL 5.50.00.   FOUND DAMAGE TO THE FOLLOWING AREAS:  1.  NR 2 VHF CO	MMUNICATION ANTENNA.  2.  NR 1 RADIO ALTIMETER TRANSCEIVER.  3.  RT ELEVATOR OUTBOARD HINGE BEARING WELDED.  4.  SCREW F	ASTENERS AT THE APU BLEED DUCT FAIRING, REAR FUSELAGE  FAIRING, APU EXHAUST TAIL CONE CONTAINED HEAT BURN MARKS.   5.  F	USELAGE SKIN AT FS 16223, FS 15791.8, FS 5873.5, FS 5118.0,  FS 4825.5, FS 4214.0, FS 3956.5 AND FS 3293.0 CONTAINED HEA	T BURN MARKS.  6.  NLG MAGNETISED.	2	L	7	2 	4T	4	T	RT	A31SO   	E20NE				 
1999031200128	19990312	00128	CE  	1999	3	12	AU990112         	1	19990109	G	3233	96380022	MOTOR           			BEECH 	55    	E55         	1152732	CE  	CONT  	O520  	IO520C      	17032	SO  	HARTZL	HCC2Y	HCC2YF2     	GL  	MLG ACTUATOR	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 			142  		4072					(AUS) LANDING GEAR MOTOR OUTPUT DRIVE GEAR TEETH STRIPPED AND IDLER SPUR GEAR DAMAGED.  SUSPECT DAMAGED DURING AIRCRAFT 	INCIDENT ON THE THIRD OF SEPTEMBER 1998 AT APPROXIMATELY 5000 HOURS.					1	L	7	2 	3O	3	O		3A16    	E5CE	5	C	P920	 
1999031200129	19990312	00129	WP  	1999	3	12	AU990113         	1	19990202	G	5711	H34356	SPAR            			DHAVXX	DH82  	DH82AROBRTSN	2801002	WP  	DHAVXX	GIPSY 	GIPSYMAJOR1 	20004	WP  					LT WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			549  							(AUS) LT UPPER MAIN PLANE FRONT SPAR (P/N H34737) AND REAR SPAR (P/N  H34356) CRACKED AND SPLIT HORIZONTALLY FROM WING R	OOTS TO WING TIPS.  FOUND DURING INSPECTION IAW AD/DH82/11 AMDT1 (BRITISH AEROSPACE T.N.S. CT(MOTH) NR 32 ISSUE 2).   PA	RT TC:  2,549.				1	Q	7	1 	3I	3	I		A8EU    	A8EU				 
1999031200130	19990312	00130	NE  	1999	3	12	AU990114         	3	19990213	G	6110	660710398	BOLT            			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R375	R3754123F21 	NE  	PROPELLER	SHEARED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			6762 							(AUS) PROPELLER MOUNT BOLT HEAD SHEARED DURING PROPELLER REMOVAL.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P17NE	 
1999031200131	19990312	00131	GL  	1999	3	12	AU990115         	3	19990211	G	6111	1A103TCM6958	BLADE           	MCAULY      	1A103TCM6958	CESSNA	150   	152         	2071835	CE  						MCAULY	1A103	1A103TCM    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 								RH004		(AUS) PROPELLER BLADE FACE CONTAINED EXFOLIATION CORROSION LOCATED APPROXIMATELY 50 MM (1.96 INCHES) FROM THE LEADING ED	GE.   PART TC:  198.					1	H	7	1 	3O			NT	3A19    		5	N	P50GL	 
1999031200132	19990312	00132	SO  	1999	3	12	AU990116         	1	19990119	G	2810	454335MAIN	FUEL CELL       			PIPER 	PA30  	PA30        	7103002	SO  	LYC   	O320  	IO320B1A    	41508	EA  	HARTZL	HCE2Y	HCE2YR2     	GL  	RT WING	DAMAGED         	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					301346		LHL475255A			(AUS) RT MAIN FUEL TANK BURNED AT AFT OUTBOARD TOP CORNER.  OUTBOARD FUEL TANK BADLY HEAT AFFECTED IN THE AREA OF THE OU	TLET NIPPLE.  SUSPECT FUEL LEAKING FROM THE TANK CAUSED AN ELECTRICAL FIRE.   PART TC:  547.					1	L	7	2 	3O	3	O		A1EA    	1E12	5	C	P9EA	 
1999031200133	19990312	00133	SO  	1999	3	12	AU990117         	1	19990119	G	2810	454333AUX	FUEL CELL       			PIPER 	PA30  	PA30        	7103002	SO  	LYC   	O320  	IO320B1A    	41508	EA  	HARTZL	HCE2Y	HCE2YR2     	GL  	RT WING	DAMAGED         	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					301346		RHL130555A			(AUS) RT OUTBOARD FUEL TANK DAMAGED BY ELECTRICAL/FUEL FIRE IN THE AREA OF THE OUTLET NIPPLE. SEE MDR AU990116 FOR ADDIT	IONAL INFORMATION.   PART TC:  547.					1	L	7	2 	3O	3	O		A1EA    	1E12	5	C	P9EA	 
1999031200134	19990312	00134	NM  	1999	3	12	AU990118         	1	19990112	G	5313		STRINGER        			BOEING	737   	737377      		NM  										BS 727	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE STRINGER WEB 18A LOCATED AT BS 727 CRACKED ON BOTH LT AND RT SIDES RUNNING AFT FROM FASTENERS.  FOUND DUR	ING EDDY CURRENT INSPECTION IAW ER B73-53-10-40A.					2	L	7	2 	4F			RT	A16WE   					 
1999031200135	19990312	00135	NM  	1999	3	12	AU990119         	1	19990122	G	2720	69372921	BUSHING         			BOEING	737   	737376      		NM  										RUDDER	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RUDDER POWER CONTROL UNIT FORWARD ATTACHMENT BOLT NYLON BUSHING DISPLACED AND MAIN LOCKNUT UNDERTORQUED ALLOWING T	HE BOLT TO SIT PROUD.					2	L	7	2 	4F			RT	A16WE   					 
1999031200136	19990312	00136	NM  	1999	3	12	AU990120         	1	19990122	G	2910	65C268103024	LINE            			BOEING	737   	737376      		NM  										HYDRAULIC SYS	CHAFED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RT MAIN LANDING GEAR HYDRAULIC PIPE WALL THICKNESS WORN DUE TO RUBBING AGAINST THE RT MAIN LANDING GEAR TELEFLEX C	ABLE P/N 10-61337-8.					2	L	7	2 	4F			RT	A16WE   					 
1999031200137	19990312	00137	NM  	1999	3	12	AU990121         	1	19990131	G	2120	BACC10BN550LM	CLAMP           			BOEING	737   	737376      		NM  										AIR DIST	BROKEN          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) LT AIR CONDITIONING SYSTEM SUPPLY DUCT CLAMP LOCATED AT THE AIR CONDITIONING DISTRIBUTION BAY PRESSURE BULKHEAD BR	OKEN ALLOWING LEAKING PAST THE DUCT/FUSELAGE SEAL.   PART TC:  28,002.					2	L	7	2 	4F			RT	A16WE   					 
1999031200138	19990312	00138		1999	3	12	AU990122         	4	19990208	G	3421	7000622901	GYRO            			BAG   	JETSTM	JETSTM3107  	1500215	EU  						ROTOL	R333	R333482F12  	GL  	ATTITUDE	MALFUNCTIONED   	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					87045847					(AUS) NR 2 VERTICAL GYRO FAULTY.						2	L	7	2 	4T			RT	BA15CAA 		6	C	P61GL	 
1999031200139	19990312	00139	SO  	1999	3	12	AU990123         	1	19990210	G	2823	755837	O RING          	SCOTT       		PIPER 	PA34  	PA34200T    	7103406	SO  						HARTZL	HCC2Y	BHCC2YF2    	GL  	FUEL SELECTOR	DETERIORATED    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					11840					(AUS) LT SIDE FUEL SELECTOR VALVE `O' RING SEAL MELTED (DISINTEGRATED).  SUSPECT DUE TO INCOMPATIBILTY WITH THE FUEL. PA	RT TC:  6,427.					1	L	7	2 	3O				A7SO    		5	C	P920	 
1999031200140	19990312	00140	CE  	1999	3	12	AU990124         	1	19990123	G	2730	0205	MOUNT           		404         	CESSNA	404   	404CESSNA   	2075901	CE  						MCAULY	3FF32	3FF32C501   	GL  	ELEVATOR	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			22455		0205					(AUS) ELEVATOR CONTROL BELLCRANK MOUNT RIVETS LOOSE.   PART TC:  22,455.						1	L	7	2 	3O				A25CE   		5	C	P45GL	 
1999031200141	19990312	00141	NE  	1999	3	12	AU990125         	2	19990211	G	7250	M5957406	BOLT            			AIRTRC	AT500 	AT502B      	0390307	SW  	PWA   	PT6   	PT6A34AG    	52053	NE  	HARTZL	HCB3T	HCB3TN3     	GL  	TURBINE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					PCEPH0010		PCEPH0010	BUA19374		(AUS) POWER TURBINE CONTAINMENT RING ATTACHMENT BOLT FAILED.  THE BOLT WAS FOUND IN THE COMBUSTION LINER WITH THE LOCK W	IRE ATTACHED.  PART TC:  1,203.					1	L	7	1 	3T	4	T	NC	A17SW   	E4EA	6	C	P15EA	 
1999031200142	19990312	00142	SW  	1999	3	12	AU990126         	1	19990214	G	2731	27	ACTUATOR        			FRCHLD	SA227 	SA227DC     	3377521	SW  						MCAULY	4HFR34	4HFR34C652  	NE  	ELEVATOR	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) ELEVATOR PITCH TRIM ACTUATOR RATCHETING.						2	L	7	2 	4T			RT	A18SW   		6	C	3PNE	 
1999031200143	19990312	00143	CE  	1999	3	12	AU990127         	1	19990215	G	2460	ATC30	FUSE            	LAMAR       	MCO12       	CESSNA	172   	172R        	2072401	CE  										DC SYSTEM	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					80115105					(AUS) FUSE DAMAGED.  FUSE SEVERED THROUGH LEG NOT THROUGH THE FUSEABLE LINK.   PART TC:  978.						1	H	7	1 	3O			NT	3A12    					 
1999031200144	19990312	00144	CE  	1999	3	12	AU990128         	1	19990128	G	3213	51411011	STRUT           			CESSNA	402   	402C        	207590R	CE  	CONT  	O520  	TSIO520VB   	17040	SO  	MCAULY	3AF32C	3AF32C505   	GL  	MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			9597 							(AUS) MAIN LANDING GEAR STRUTS CRACKED.  EXCESSIVE PLAY IN TORQUE LINKS AND WHEEL MISALIGNMENT WAS ALSO FOUND.   PART TC	:  9,597.					1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22EA	 
1999031200145	19990312	00145	EU  	1999	3	12	AU990129         	1	19990101	G	3260	AIR130900	HARNESS         			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R375	R3754123F21 	NE  	NLG	DIRTY           	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) NOSE LANDING GEAR DOWNLOCK WIRING HARNESS SUSPECT FAULTY.  NLG DOWNLOCK MICROSWITCH PLUNGER CONTAMINATED AND STIFF	 TO OPERATE.					2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P17NE	 
1999031200146	19990312	00146	CE  	1999	3	12	AU990130         	1	19990218	G	5522	TH470	SKIN            			BEECH 	58    	58          	1152740	CE  	CONT  	O520  	IO520C      	17032	SO  	MCAULY	3AF34C	3AF34C502   	GL  	LT ELEVATOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					TH470					(AUS) LT ELEVATOR TOP SKIN AND RT ELEVATOR TOP AND BOTTOM SKINS CORRODED.						1	L	7	2 	3O	3	O		3A16    	E5CE	5	C	P22EA	 
1999031200147	19990312	00147	NE  	1999	3	12	AU990132         	2	19990214	G	7240		COMBUSTOR       								CFMINT	CFM56 	CFM565A1    		NE  					LT ENGINE	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LT ENGINE HIGH PRESSURE TURBINE BLADE CONTAINED IMPACT DAMAGE AND MISSING MATERIAL.  ONE FUEL NOZZLE FOUND CHAFED 	(FRETTING WEAR ON THE NOZZLE STEM).  LARGE AMOUNTS OF MATERIAL MISSING FROM THECOMBUSTOR OUTER COWL.										4	F			E29NE				 
1999031200148	19990312	00148	EU  	1999	3	12	AU990133         	1	19990216	G	5343	HC5370002004	FITTING         			BAG   	BAE146	BAE146300A  	1500267	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR RETRACTION JACK ATTACHMENT BOSS CONTAINED TWO CRACKS IN THE BORE IN THE FOLLOWING LOCATIONS:  1.	  ONE CRACK AT THE 4 O'CLOCK POSITION - CRACK LENGTH 8 MM  (0.314 INCH) ACROSS THE FACE EXTENDING 6 MM (0.236 INCH) INTO	 THE  BORE.   2.  ONE CRACK AT THE 5 O'CLOCK POSITION - CRACK LENGTH 13 MM (0.511 INCH) ACROSS THE FACE EXTENDING 6 MM (	0.236 INCH) INTO THE BORE FOUND DURING INSPECTION IAW ER BA6-53-10-16.  NOTE:  NEITHER CRACK EXTENDS BEYOND THE JACK ATT	ACHMENT PIN FLANGE POSITION.		2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999031200149	19990312	00149	EU  	1999	3	12	AU990134         	1	19990203	G	5610	50079	WINDSHIELD      			AIRBUS	320   	A320212     		EU  										COCKPIT	CRACKED         	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					50079					(AUS) LT WINDSHIELD SHATTERED FOLLOWING APPROXIMATELY THIRTY SECONDS OF ELECTRICAL ARCING.  SUSPECT ARCING CAUSED BY WAT	ER INGRESS.  INVESTIGATION FOUND THAT THE OUTER PANE CRACKING HAD ORIGINATED FROM SEVERAL BURN SPOTS IN THE BUSS BAR ARE	A ALONG THE LOWER EDGE AND UPPER INBOARD CORNER OF THE WINDOW.   PART TC:  30,310.				2	L	7	2 	4F			RT	A28NM   					 
1999031200150	19990312	00150	NM  	1999	3	12	AU990135         	1	19990203	G	2740	BACB10CF14PP	BEARING         			BOEING	737   	737377      		NM  										HORIZ STAB	FAILED          	W				O				OTHER                   				F			FLT CONT AFFECTED         			CR	CRUISE         	1			AU	S 										(AUS) RT TRIM WHEEL OUTBOARD SHAFT SUPPORT BEARING COLLAPSED.  ALL BEARING BALLS MISSING. PART TC:  34,858.						2	L	7	2 	4F			RT	A16WE   					 
1999031200151	19990312	00151	EU  	1999	3	12	AU990136         	1	19990209	G	3040	2312M782	CONVERTER       			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R375	R3754123F21 	NE  	WINDSHIELD	FAILED          	W				C				ABORTED TAKEOFF         				O			OTHER                     			TO	TAKEOFF        	1			AU	S 					00618					(AUS) LT WINDSCREEN WIPER CONVERTER FAULTY.  SUSPECT WORN GEAR.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P17NE	 
1999031200152	19990312	00152	SW  	1999	3	12	AU990137         	1	19990212	G	5510	2743062013	FITTING         			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UAR 	01514	WP  					HORIZONTAL STAB	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) HORIZONTAL STABILIZER ACTUATOR ATTACHMENT LUG CRACKED.						2	L	7	2 	4T	4	T	RT	A18SW   	E4WE				 
1999031200153	19990312	00153	EA  	1999	3	12	AU990138         	2	19990212	G	8530	LW12596	BOLT            								LYC   	O540  	IO540K1A5   	41532	EA  					ENGINE	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 					RL253548A		RL253548A			(AUS) CONNECTING ROD BOLTS INCORRECT PART.  BOLTS P/N LW12596 (12OFF) WERE ORDERED.  WHEN THE ORIGINAL LYCOMING PACKAGIN	G WAS OPENED THE BOLTS APPEARED TO BE TORQUE TYPE BOLTS INSTEAD OF THE CORRECT STRETCH TYPE BOLTS.										3	O			1E4				 
1999031200154	19990312	00154		1999	3	12	AU990139         	4	19990203	G	6113		BACKPLATE       			CESSNA	310   	310K        	2074228	CE  	CONT  	O470  	IO470U      	17026	SO  	MCAULY	2AF34C	D2AF34C81   	GL  	RT PROPELLER	CRACKED         	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) RT PROPELLER SPINNER BACKING PLATE FAILED.  BACKING PLATE HAD CRACKED AROUND THE CIRCUMFERENCE BEND FOR APPROXIMAT	ELY 100 DEGREES.					1	L	7	2 	3O	3	O		3A10    	3E1	5	C	P5EA	 
1999031200155	19990312	00155	NE  	1999	3	12	AU990140         	2	19990209	G	7310		LINE            			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					FUEL SYSTEM	LOOSE           	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 							PS0229			(AUS) HIGH PRESSURE FUEL PUMP TO FUEL TANK UNLOADING LINE LOCATED IN THE LT ENGINE NACELLE LOOSE AND LEAKING FUEL.						2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999031700001	19990317	00001	EU  	1999	3	17	AU990141         	2	19990210	G	7240	JR26473A	DIFFUSER        			FOKKER	F28   	F28MK4000   	4990810	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					NR 2 ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							9547			(AUS) NR 2 ENGINE DIFFUSER CASE CRACKED IN SEVERAL PLACES AT THE 6:30 O'CLOCK POSITION.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999031200156	19990312	00156	EU  	1999	3	12	AU990142         	1	19990216	G	5720		BRACKET         			JETAIR	JETSTM	JETSTM4101  	1500501	EU  	GARRTT	TPE331	TPE33114GR  	01514	NE  					WING	CRACKED         	W				O				OTHER                   				F			FLT CONT AFFECTED         			CR	CRUISE         	1			AU	S 										(AUS) DUCKTAIL FAIRING LOCATED UNDER THE RT FLAP VIBRATING DUE TO THE ATTACHMENT BRACKET BEING CRACKED AT THE INBOARD AN	D OUTBOARD FORWARD ENDS.   PART TC:  6,100.					2	L	7	2 	4T	4	T	RT	A41NM   	E18NE				 
1999031200157	19990312	00157	CE  	1999	3	12	AU990143         	1	19990212	G	2710	57150324	CONTROL CABLE   			CESSNA	441   	441         	2076020	CE  						HARTZL	HCB3T	HCB3TN5     	GL  	AILERON	MISINSTALLED    	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) LT AILERON FORWARD CONTROL CABLE (UPPER) FOUND TO BE ON THE WRONG SIDE OF THE CABLE KEEPER.						1	L	7	2 	3T			RT	A28CE   		6	C	P15EA	 
1999031200158	19990312	00158	EU  	1999	3	12	AU990144         	1	19990208	G	2844	415G1007100G14	TRANSMITTER     			BAG   	JETSTM	JETSTM3201  	1500217	EU  	GARRTT	TPE331	TPE33112UAR 	01514	WP  	MCAULY	4HFR34	4HFR34C653  	NE  	FUEL SYSTEM	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) NR 1 FUEL PRESSURE TRANSMITTER FAULTY.   PART TC:  8,971.						2	L	7	2 	4T	4	T	RT	A56EU   	E4WE	6	C	3PNE	 
1999031200159	19990312	00159	NM  	1999	3	12	AU990145         	1	19990208	G	2612	3698	CARD            	GARRTT      	GTCP6604    	BOEING	747   	747312      	1384932	NM  										FIRE DETECTION	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					3698					(AUS) APU FIRE DETECTOR CARD FAULTY.						2	L	7	4 	4F			RT	A20WE   					 
1999031200160	19990312	00160	NM  	1999	3	12	AU990146         	1	19990115	G	2782	256T21516	GEAR            			BOEING	767   	767204      		NM  	GE    	CF6   	CF680A      	30025	NE  					ACTUATOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					23384IB2350					(AUS) NR 3 OUTBOARD AND NR 4 INBOARD LEADING EDGE SLAT ROTARY ACTUATORS CONTAINED INTERNAL CORROSION ON THE RING GEAR BE	ARING SURFACES AND THE PLANET GEAR P/N 256T2152.  FOUND DURING VISUAL INSPECTION IAW ER B76-27-80-27 (AD/B767/095).   PA	RT TC:  51,949.				2	L	7	2 	4F	4	F	RT	A1NM    	E13NE				 
1999031200161	19990312	00161	EU  	1999	3	12	AU990147         	1	19990204	G	5713		STRINGER        			FOKKER	F27   	F27MK50     		EU  										LT & RT WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LT AND RT OUTER WING STRINGERS NR 5 AND NR 6 LOCATED AT THE UPPER AND LOWER SKINS CRACKED AT RIB LOCATIONS.  FOUND	 DURING INSPECTION IAW SERVICE BULLETIN SB F50-57-019 PT2 (AD/F50/78).  PART TC:  19,548.					2	H	7	2 	4T			RT	A817    					 
1999031200162	19990312	00162	NE  	1999	3	12	AU990148         	2	19990211	G	7260	RK19971	SEAL            			FOKKER	F27   	F27MK600    	4990706	EU  	RROYCE	DART  	DART5327R   	54509	NE  	ROTOL	R4304	R1934304    	EU  	NR 2 ENGINE	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 			7490 				13330			(AUS) NR 2 ENGINE AUXILIARY GEARBOX OUTPUT SHAFT SEAL LEAKING.  ENGINE HAD SUFFERED A PREVIOUS AUXILIARY GEARBOX DRIVESH	AFT FAILURE WHICH MAY HAVE CONTRIBUTED TO THE DEFECT.					2	H	7	2 	4T	4	T		A817    	E297	6	C	P899	 
1999031200163	19990312	00163	EU  	1999	3	12	AU990149         	1	19990204	G	5311	9961	FRAME           		11340       	FOKKER	F27   	F27MK50     		EU  										BS 9661 & 11340	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE FRAME 9661 CRACKED ON THE LT AND RT SIDES.  FUSELAGE FRAME 11340 CRACKED ON THE LT AND RT SIDES.  PART TC	:  19,548.					2	H	7	2 	4T			RT	A817    					 
1999031200164	19990312	00164	NM  	1999	3	12	AU990150         	1	19990218	G	2910	82920010265	LINE            			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					HYDRAULIC SYS	CHAFED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) HYDRAULIC PIPE SEVERELY CHAFED ON UNION P/N  824-6D.  PIPE WALL WAS APPROXIMATELY 90 PERCENT WORN THROUGH.  FOUND 	DURING INSPECTION IAW AD/DHC8/47.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999031200165	19990312	00165	EU  	1999	3	12	AU990151         	1	19990214	G	6320	332A32100701	TRANSMISSION    			SNIAS 	AS332 	AS332L      	8680809	EU  	TMECA 	MAKILA	MAKILA1A    	60040	EU  					M/R GEARBOX	MAKING METAL    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1704 		M622					(AUS) MAIN ROTOR GEARBOX METAL CONTAMINATION.  PART TC:  1,704.						2	G	7	2 	4U	4	U		H4EU    	E12NE				 
1999042300374	19990423	00374	WP  	1999	4	23	AU990266         	2	19990209	G	7260	31030351	BEARING         								GARRTT	TPE331	TPE33110UG  	01514	WP  					GEARBOX	FAILED          	W				O				OTHER                   				E			VIBRATION/BUFFET          			CR	CRUISE         	1			AU	S 							P63089			(AUS)  ENGINE ACCESSORY GEARBOX BEARING FAILED ALLOWING LOSS OF DRIVE TO THE FCU FUEL PUMP AND THE ENGINE OIL PUMP.  PAR	T TC:  18,523.										4	T			E4WE				 
1999042300375	19990423	00375	EA  	1999	4	23	AU990287         	2	19990324	G	8530	LW10077	SEAT            								LYC   	O540  	IO540*      	41532	EA  					ENGINE	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS)  INLET VALVE SPRING UPPER SEAT WAS AN INCORRECT PART.  THE SEAT WAS AN EXHAUST VALVE UPPER SEAT, BUT WAS ETCHED WI	TH THE PART NUMBER FOR THE INLET VALVE SPRING.  THE INCORRECT ITEM WAS PART OF A NEW CYLINDER KIT P/N 05K21117.  UNAPPRO	VED PART.									3	O			1E4				 
1999050700213	19990507	00213	CE  	1999	5	7	AU990290         	1	19990319	G	5740	0001101121	FITTING         			BEECH 	33    	F33A        	1151425	CE  	CONT  	O520  	IO520B      	17032	SO  	MCAULY	2A36C	2A36C23     	GL  	LT WING	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT FORWARD LOWER WING ATTACHMENT FITTING CONTAINED SEVERE EXFOLIATION CORROSION IN THE AREA OF THE GUSSET.						1	L	7	1 	3O	3	O		3A15    	E5CE	5	C	P880	 
1999050700214	19990507	00214	SO  	1999	5	7	AU990291         	1	19990320	G	2750	3075001017	CONTROL UNIT    			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  					TE FLAP	FAULTY          	W				O				OTHER                   				F			FLT CONT AFFECTED         			NR	NOT REPORTED   	1			AU	S 					0186					(AUS) FLAP CONTROL UNIT SUSPECT FAULTY.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE				 
1999050700215	19990507	00215	SO  	1999	5	7	AU990292         	1	19990324	G	2510	1MM1110402	SEAT BELT       			GULSTM	AA5   	AA5A        	3960106	SO  	LYC   	O320  	O320E2G     	41508	EA  					FLT COMPARTMENT	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) AUTOMOTIVE SEAT BELT INSTALLED IN REAR SEATS.  SEAT BELTS DO NOT COMPLY WITH AD/RES/10 AMDT4.						1	L	7	1 	3O	3	O		A16EA   	E274				 
1999050700216	19990507	00216	NM  	1999	5	7	AU990293         	1	19990324	G	5415	311T31021	PIN             			BOEING	767   	767277      		NM  	GE    	CF6   	CF680A      	30025	NE  					RT ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT INBOARD ENGINE PYLON MID-SPAR FUSE PIN CRACKED.  CRACK LENGTH 11 MM (0.433 INCH).  FOUND DURING EDDY CURRENT	 INSPECTION.					2	L	7	2 	4F	4	F	RT	A1NM    	E13NE				 
1999050700217	19990507	00217	EU  	1999	5	7	AU990294         	1	19990322	G	5610	3184	WINDSHIELD      			AIRBUS	320   	A320212     		EU  										FLT COMPARTMENT	CRACKED         	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					3184					(AUS) COCKPIT RIGHT NR 1 WINDOW OUTER PANE CRACKED.  SUSPECT CAUSED BY LOCALIZED HEATING AT THE LOWER ANTI-ICE BUS BAR.						2	L	7	2 	4F			RT	A28NM   					 
1999050700218	19990507	00218	SO  	1999	5	7	AU990295         	1	19990323	G	5320	6852300	CHANNEL         			PIPER 	PA32  	PA32300     	7103212	SO  	LYC   	O540  	IO540K1G5   	41532	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	FUSELAGE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE CHANNEL CORRODED.						1	L	7	1 	3O	3	O		A3SO    	1E4	5	C	P920	 
1999050700219	19990507	00219	SO  	1999	5	7	AU990296         	2	19990326	G	7414	M3081	POINTS          	SLICK       	6310        	BEECH 	33    	F33A        	1151425	CE  	CONT  	O520  	IO520B      	17032	SO  	MCAULY	3A32C	3A32C406    	GL  	MAGNETO	WORN            	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					98012583					(AUS) MAGNETO CONTACT POINTS ASSEMBLY WORN EXCESSIVELY ALLOWING THE POINTS GAP TO VARY CONSIDERABLY.						1	L	7	1 	3O	3	O		3A15    	E5CE	5	C	P21E	 
1999050700220	19990507	00220	EU  	1999	5	7	AU990297         	2	19990210	G	7240	JR26473A	DIFFUSER        			FOKKER	F28   	F28MK4000   	4990810	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					NR 2 ENGINE	CRACKED         	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 							9547			(AUS) NR 2 ENGINE DIFFUSER CASE ASSEMBLY CRACKED IN SEVERAL PLACES AT THE 6:30 O'CLOCK POSITION.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999050700221	19990507	00221	EU  	1999	5	7	AU990298         	1	19990303	G	2761	P308450102	ACTUATOR        			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					SPOILER	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					BAEDEPS138					(AUS) LIFT SPOILER ACTUATORS LFO AND LFC FAILED UNLOCKED TEST.  FOUND DURING INSPECTION IAW ER BA6-27-60-16D.  WORKSHOP 	INSPECTION OF THE ACTUATORS COULD FIND NO FAULTS.					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999050700222	19990507	00222	NM  	1999	5	7	AU990300         	1	19990303	G	5312		BULKHEAD        			BOEING	737   	737377      		NM  										FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FORWARD FUSELAGE BULKHEAD CRACKED IN THE FOLLOWING AREAS:  1.  BULKHEAD WEB LOCATED ADJACENT TO THE RIGHT LOWER RA	DAR ANTENNA MOUNT INBOARD UPPER CORNER - CRACK LENGTH 6 MM (0.236 INCH).  2.  SIDE CHORD ANGLE LOCATED AT WL 207 LT SIDE	 AND WL 195 LT SIDE - CRACK LENGTHS 27 MM (1.062 INCH) AND 15 MM (0.590 INCH).  3.  SIDE CHORD ANGLE LOCATED AT WL 207 R	T SIDE - CRACK LENGTH 50 MM  (1.968 IN)CH).  FOUND DURING ULTRASONIC AND EDDY CURRENT INSPECTION.			2	L	7	2 	4F			RT	A16WE   					 
1999050700223	19990507	00223	NM  	1999	5	7	AU990301         	1	19990322	G	2910	82970010415	LINE            			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					HYDRAULIC SYS	CHAFED          	W				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			AU	S 										(AUS) HYDRAULIC PRESSURE PIPE FROM ANTI-SKID VALVE TO THE BRAKE QUANTITY LIMITING VALVE CHAFED.  LOSS OF NR 1 SYSTEM HYD	RAULIC FLUID.  PIPE IS LOCATED IN THE RT NACELLE.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999050700224	19990507	00224	EU  	1999	5	7	AU990302         	1	19990327	G	3246	AHA1489	WHEEL           			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					MLG	DAMAGED         	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) NR 1 MAIN WHEEL DAMAGED.  A PORTION OF THE OUTER RIM HAD BROKEN AWAY.  THE TIRE REMAINED INFLATED.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999050700225	19990507	00225	CE  	1999	5	7	AU990303         	1	19990329	G	2917	991028710	SWITCH          			CESSNA	402   	402C        	207590R	CE  	CONT  	O520  	TSIO520VB   	17040	SO  	MCAULY	3AF32C	3AF32C505   	GL  	HYDRAULIC SYS	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) LEFT HYDRAULIC SYSTEM PRESSURE SWITCH FAULTY.						1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22E	 
1999050700226	19990507	00226	CE  	1999	5	7	AU990304         	1	19990329	G	3233	AN175M22A	BOLT            			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520L      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	RT MLG	SHEARED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					717					(AUS) RIGHT MAIN LANDING GEAR ACTUATOR FORWARD MOUNT BOLT SHEARED.						1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P47G	 
1999050700227	19990507	00227	EU  	1999	5	7	AU990305         	1	19990325	G	5713		STRINGER        			FOKKER	F27   	F27MK50     		EU  										FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WING UPPER AND LOWER NR 5 AND NR 6 STRINGERS CRACKED.  FOUND DURING INCORPORATION OF SB F50-57-019.						2	H	7	2 	4T			RT	A817    					 
1999050700228	19990507	00228	EU  	1999	5	7	AU990306         	1	19990325	G	5313	143B	STRINGER        			FOKKER	F27   	F27MK50     		EU  										BS 12975-14475	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE STRINGER NR 143B CORRODED IN AREA BETWEEN FUSELAGE STATIONS 12975 AND 14475.						2	H	7	2 	4T			RT	A817    					 
1999050700229	19990507	00229	EU  	1999	5	7	AU990307         	1	19990325	G	5313	114B	STRINGER        			FOKKER	F27   	F27MK50     		EU  										BS 11675-12525	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE STRINGER NR 114B CORRODED IN AREA BETWEEN FUSELAGE STATIONS 11675 AND 12525.						2	H	7	2 	4T			RT	A817    					 
1999050700230	19990507	00230		1999	5	7	AU990308         	4	19990301	G	2212	41800302000	ACTUATOR        			AEROSP	SA365 	SA365C      	8680667	EU  	TMECA 	ARRIEL	ARRIEL1A    	60030	NE  					AUTOPILOT	BINDING         	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 			4325 		215					(AUS) AUTOPILOT COMPENSATION ACTUATOR BINDING.						1	G	7	2 	3U	3	U		H10EU   	E19EU				 
1999050700231	19990507	00231	EU  	1999	5	7	AU990309         	1	19990325	G	5313	F5203200003	STRINGER        			FOKKER	F27   	F27MK50     		EU  										BS 13425-14925	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE STRINGER NR 136 CORRODED IN THE AREA BETWEEN FUSELAGE STATIONS 13425 AND 14925.						2	H	7	2 	4T			RT	A817    					 
1999050700232	19990507	00232	SO  	1999	5	7	AU990310         	1	19990123	G	7603	89307000	SWIVEL          			PIPER 	PA34  	PA34200     	7103405	SO  	LYC   	O360  	IO360C1E6   	41514	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	POWER LEVER	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							L906251A	AU2121		(AUS) THROTTLE CONTROL CABLE SWIVEL WORN AND SEPARATED FROM THE BALL JOINT.						1	L	7	2 	3O	3	O		A7SO    	1E10	5	C	P920	 
1999050700233	19990507	00233	NM  	1999	5	7	AU990311         	1	19990324	G	4920		TURBINE         			BOEING	737   	737376      		NM  										APU	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) APU TURBINE SUFFERED A CATASTROPHIC FAILURE.  DAMAGE CAUSED TO THE EXHAUST MUFFLER.						2	L	7	2 	4F			RT	A16WE   					 
1999050700234	19990507	00234	NM  	1999	5	7	AU990313         	1	19990315	G	3233	MHB508	ROD END         		65B0150211  	BOEING	747   	747338      		NM  										MLG	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT BODY LANDING GEAR EXTEND/RETRACT ACTUATOR EYE END BEARING SPLIT AND DISPLACED SIDEWAYS AT THE OLEO END.						2	L	7	2 	4F			RT	A20WE   					 
1999050700235	19990507	00235		1999	5	7	AU990314         	4	19990129	G	3120	C6645030103	CLOCK           			CESSNA	150   	152         	2071835	CE  						MCAULY	1A103	1A103TCM    	GL  	COCKPIT	FAILED          	W				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			AU	S 										(AUS) CLOCK FAULTY.  SMOKE IN CABIN.						1	H	7	1 	3O			NT	3A19    		5	N	P50G	 
1999050700236	19990507	00236		1999	5	7	AU990315         	1	19990211	G	7810		EXHAUST PIPE    								LYC   	O360  	O360A1A     	41514	EA  					ENGINE	FRACTURED       	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 							L852836A			(AUS) NR 2 CYLINDER EXHAUST PIPE FRACTURED AT FLANGE.											3	O			E286				 
1999050700237	19990507	00237	EU  	1999	5	7	AU990316         	1	19990319	G	2435	23079009	STARTER         			BAG   	JETSTM	JETSTM3201  	1500217	EU  						ROTOL	R333	R333482F12  	GL  	NR 1 ENGINE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1529 							(AUS) NR 1 ENGINE STARTER/GENERATOR FAULTY.						2	L	7	2 	4T			RT	A56EU   		6	C	P61G	 
1999050700238	19990507	00238	CE  	1999	5	7	AU990317         	1	19990329	G	2434	WA876	BEARING         	PRESTOLITE  	ALV9407     	CESSNA	402   	402B        	207590P	CE  						MCAULY	3AF32C	3AF32C87    	GL  	ALTERNATOR	FAILED          	W				O				OTHER                   				H			ELECT. POWER LOSS-50 PC   			NR	NOT REPORTED   	1			AU	S 					WA876					(AUS) ALTERNATOR BEARING FAILURE.  ALTERNATOR DAMAGED BEYOND REPAIR.						1	L	7	2 	3O				A7CE    		5	C	P22E	 
1999050700239	19990507	00239	CE  	1999	5	7	AU990318         	1	19990405	G	3230		CABLE           			CESSNA	402   	402C        	207590R	CE  	CONT  	O520  	TSIO520VB   	17040	SO  	MCAULY	3AF32C	3AF32C505   	GL  	MLG	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) LANDING GEAR EMERGENCY EXTENSION SYSTEM ACTUATOR CABLE ASSEMBLY SLIPPING UNDER THE CABLE CLAMP PREVENTING ACTIVATI	ON OF THE NITROGEN BLOW-DOWN BOTTLE.  DURING AN EXTENSION PROBLEM WITH THE LANDING GEAR, THE EMERGENCY UNDERCARRIAGE EXT	ENSION HANDLE WAS PULLED WITHOUT THE REQUIRED RESULT.  THE AIRCRAFT CRASH LANDED CAUSING EXTENSIVE DAMAGE.				1	L	7	2 	3O	3	O	 	A7CE    	E8CE	5	C	P22EA	 
1999050700240	19990507	00240	CE  	1999	5	7	AU990319         	1	19990324	G	5312		BULKHEAD        			CESSNA	172   	172M        	2072418	CE  						MCAULY	1C160	1C160DTM    	GL  	FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) REAR DOOR POST BULKHEAD CRACKED ON BOTH SIDES.						1	H	7	1 	3O			NT	3A12    		5	N	P910	 
1999050700241	19990507	00241	EA  	1999	5	7	AU990320         	2	19990404	G	7322	DL2338	CARBURETOR      	FACET       	105217      	PIPER 	PA28  	PA28161     	7102803	SO  	LYC   	O320  	O320D3G     	41508	EA  					ENGINE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					DL2338		L857639A			(AUS) CARBURETOR FAULTY.  CARBURETOR WAS STRIPPED AND INSPECTED AND FOUND:  1. CARBURETOR FLOAT LEVEL INCORRECTLY SET CA	USING CARBURETOR TO RUN LEAN.   2.  EXCESS MOVEMENT IN THROTTLE SHAFT HAD ALLOWED THROTTLE VALVE PLATE P/N 14-190 TO CON	TACT THROTTLE BODY CAUSING THROTTLE VALVE TO BIND AND SCORE ON THROTTLE BODY.   3.  ATTEMPTS TO REMOVE SCORING IN (2) CA	USED EXCESS CLEARANCE BETWEEN THROTTLE VALVE PLATE AND THROTTLE BODY ALLOWING EXCESSIVE AIR LEAKAGE.  4.  MIXTURE SHAFT 	PN 242-514 TOP END HAD BEEN POLISHED OR GROUND TO BELOW MINIMUM LIMITS AND A BUSHING MANUFACTURED TO COMPENSATE FOR UNDE	RSIZE SHAFT.   A DEEP NICK WAS ALSO FOUND.	1	L	7	1 	3O	3	O		2A13    	E274				 
1999050700242	19990507	00242	SW  	1999	5	7	AU990321         	1	19990318	G	7603	2771031031	THROTTLE        			SWRNGN	SA227 	SA227AC     	8780603	SW  	GARRTT	TPE331	TPE33111U   	01514	WP  	ROTOL	R321	R321482F8   	GL  	POWER LEVER	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT POWER LEVER BROKEN IN TWO DUE TO CHAFING ON THE PEDESTAL.  EVIDENCE OF CORROSION ON THE POWER LEVER.  THE LEV	ER HAD BEEN INCORRECTLY REPAIRED AND WAS HELD TOGETHER WITH LOCKWIRE.					2	L	7	2 	4T	4	T	RT	A8SW    	E4WE	6	C	P61G	 
1999050700243	19990507	00243	NM  	1999	5	7	AU990322         	1	19990403	G	2760		LINKAGE         			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					SPOILER	DISCONNECTED    	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT INBOARD GROUND SPOILER LINKAGE DISCONNECTED FROM ACTUATOR.  LINKAGE HAD BEEN DISCONNECTED DURING MAINTENANCE	 AND NOT CORRECTLY RECONNECTED.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999050700244	19990507	00244	SO  	1999	5	7	AU990323         	1	19990330	G	2750	16423006	BELLCRANK       			PIPER 	PA23  	PA23250     	7102308	SO  	LYC   	O540  	IO540C4B5   	41532	EA  	HARTZL	HCE2Y	HCE2YK2     	GL  	TE FLAP	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FLAP BELLCRANK ASSEMBLY CONTAINED SEVERE EXFOLIATION CORROSION.  OUND DURING INSPECTION IAW AD/PA23/50A.						1	L	7	2 	3O	3	O		1A10    	1E4	5	C	P9EA	 
1999050700245	19990507	00245	NM  	1999	5	7	AU990324         	1	19990404	G	3211	737R3206011	PIN             			BOEING	737   	737376      		NM  										MLG	FRACTURED       	W				K				NONE                    				O			OTHER                     			LD	LANDING        	1			AU	S 					MCO2536P1306					(AUS) RIGHT MAIN LANDING GEAR TRUNNION PIN FRACTURED.						2	L	7	2 	4F			RT	A16WE   					 
1999050700246	19990507	00246	WP  	1999	5	7	AU990325         	1	19990319	G	2430		TERMINAL        			DOUG  	DC3   	DC3CS1C3G   	3021458	WP  	PWA   	R1830 	R183092     	52020	NE  	HAMSTD	23E	23E50       	NE  	DC SYSTEM	FAULTY          	W				O				OTHER                   				H			ELECT. POWER LOSS-50 PC   			NR	NOT REPORTED   	1			AU	S 										(AUS) GENERATOR FIELD TERMINALS FAULTY.						2	L	7	2 	4R	4	R		A669    	5E4	6	C	P603	 
1999050700247	19990507	00247	EU  	1999	5	7	AU990326         	1	19990317	G	2731	DL3827M137	ACTUATOR        			SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT75A2      	30030	NE  	ROTOL	R354	R3544123F13 	NE  	ELEVATOR	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					V1106					(AUS) LEFT MAIN PITCH TRIM ACTUATOR FAULTY.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE6	6	C	P61G	 
1999050700248	19990507	00248		1999	5	7	AU990327         	4	19990402	G	6113	08550303	SUPPORT         			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	SPINNER	BROKEN          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) PROPELLER SPINNER SUPPORT BROKEN IN HALF.						1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22E	 
1999050700249	19990507	00249	NM  	1999	5	7	AU990328         	1	19990406	G	3231	83231020003	SPRING          			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					MLG DOOR	BROKEN          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) RIGHT MAIN LANDING GEAR DOOR SPRING BROKEN AND FOULING ON DOOR ACTUATING ROD PN 83231014-003.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999050700250	19990507	00250	SW  	1999	5	7	AU990329         	1	19990410	G	5400		PIN             			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					COWLING HINGE	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT TRANSMISSION COWLING HINGE PIN MIGRATED OUT AND CONTACTED ALL FOUR MAIN ROTOR PITCH LINK ROD ASSEMBLIES CAUS	ING DAMAGE BEYOND LIMITS.					1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999050700251	19990507	00251	NE  	1999	5	7	AU990330         	2	19990302	G	8530	399354	CYLINDER        			DHAV  	DHC2  	DHC2*       	2800108	EA  	PWA   	R985  	R985AN14B   	52008	NE  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			248  				4219276			(AUS) NR 1 CYLINDER HEAD SEPARATED FROM BARREL.						1	H	7	1 	3R	3	R		A806    	5E1				 
1999050700252	19990507	00252	CE  	1999	5	7	AU990331         	1	19990407	G	3710	212CW	PUMP            			CESSNA	182   	182H        	2072718	CE  	CONT  	O470  	O470K       	17026	SO  	MCAULY	2A34C	2A34C66     	GL  	VACUUM SYSTEM	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) VACUUM PUMP DETERIORATED INTERNALLY.  PUMP VANES WORN AND ROTOR BREAKING UP.						1	H	7	1 	3O	3	O	NT	3A13    	E273	5	C	P3EA	 
1999050700253	19990507	00253	GL  	1999	5	7	AU990332         	2	19990408	G	7320	6875630	LINE            			BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					INLET	BROKEN          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 							CAE832122			(AUS) PC PIPE FROM COMPRESSOR SCROLL TO `TEE' FITTING FRACTURED AND BROKEN OFF AT THE BASE OF THE FLARE BELOW THE `B' NU	T.  THE ENGINE IS FITTED WITH A CECO FUEL SYSTEM.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999050700254	19990507	00254	CE  	1999	5	7	AU990333         	1	19990412	G	3340		CLAMP           			CESSNA	150   	152         	2071835	CE  						MCAULY	1A103	1A103TCM    	GL  	BEACON	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ROTATING BEACON CLAMP LOOSE.  GLASS LOST AND BULB BROKEN.						1	H	7	1 	3O			NT	3A19    		5	N	P50G	 
1999050700255	19990507	00255	CE  	1999	5	7	AU990334         	1	19990412	G	7603		THROTTLE        			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  	MCAULY	1A103	1A103TCM    	GL  	POWER LEVER	MISRIGGED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) THROTTLE CONTROL LEVER INCORRECTLY RIGGED AND NOT SPLIT PINNED.						1	H	7	1 	3O	3	O	NT	3A19    	E223	5	N	P50G	 
1999050700256	19990507	00256	EA  	1999	5	7	AU990335         	2	19990412	G	7420		LEAD            			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  	MCAULY	1A103	1A103TCM    	GL  	IGNITION HARNESS	MISROUTED       	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) ENGINE HIGH TENSION LEADS LYING AGAINST EXHAUST PIPE.						1	H	7	1 	3O	3	O	NT	3A19    	E223	5	N	P50G	 
1999050700257	19990507	00257	EA  	1999	5	7	AU990336         	2	19990412	G	7322		HEATER          			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  	MCAULY	1A103	1A103TCM    	GL  	CARBURETOR	MISRIGGED       	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) CARBURETOR HEATING SYSTEM INCORRECTLY RIGGED.  HEAT `ON' CONTINUOUSLY.						1	H	7	1 	3O	3	O	NT	3A19    	E223	5	N	P50G	 
1999050700258	19990507	00258	EA  	1999	5	7	AU990337         	2	19990412	G	8550		FILTER          			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  	MCAULY	1A103	1A103TCM    	GL  	ENGINE	MISINSTALLED    	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) OIL FILTER NOT LOCKWIRED.						1	H	7	1 	3O	3	O	NT	3A19    	E223	5	N	P50G	 
1999050700259	19990507	00259	CE  	1999	5	7	AU990338         	1	19990412	G	7602		BOLT            			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  	MCAULY	1A103	1A103TCM    	GL  	MIXTURE CONTROL	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) MIXTURE CONTROL SYSTEM BOLT LOOSE.						1	H	7	1 	3O	3	O	NT	3A19    	E223	5	N	P50G	 
1999050700260	19990507	00260	CE  	1999	5	7	AU990339         	1	19990412	G	7921		HOSE            			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  	MCAULY	1A103	1A103TCM    	GL  	OIL COOLER	MISMANUFACTURED 	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) OIL COOLER HOSE TOO LONG.						1	H	7	1 	3O	3	O	NT	3A19    	E223	5	N	P50G	 
1999050700261	19990507	00261	EA  	1999	5	7	AU990341         	2	19990412	G	7322		SHAFT           			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  	MCAULY	1A103	1A103TCM    	GL  	CARBURETOR	MISINSTALLED    	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) CARBURETOR HEAT SHAFT INCORRECTLY SECURED.  SPLIT PIN USED INSTEAD OF THE CORRECT ROLL PIN.						1	H	7	1 	3O	3	O	NT	3A19    	E223	5	N	P50G	 
1999050700262	19990507	00262	CE  	1999	5	7	AU990344         	1	19990303	G	2510	AN9703	WASHER          			CESSNA	172   	172B        	2072406	CE  	CONT  	O300  	O300C       	17022	SO  					SEAT BELT	MISSING         	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) SEAT BELT FLOOR ATTACHMENT FITTINGS HAD THE WASHERS UNDER THE FORWARD NUTS MISSING.						1	H	7	1 	3O	3	O	NT	3A12    	E253				 
1999050700263	19990507	00263	SO  	1999	5	7	AU990345         	1	19990409	G	5711	35168009	SPAR            			PIPER 	PA28  	PA28161     	7102803	SO  	LYC   	O320  	O320D3G     	41508	EA  	SNSNCH	74D	74DM        	EA  	RT WING	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT WING MAIN SPAR CAP CONTAINED EXFOLIATION CORROSION LOCATED IN THE AREA IMMEDIATELY OUTBOARD OF THE LANDING G	EAR LEG.  AREA OF CORROSION APPROXIMATELY 75 MM LONG BY 25 MM WIDE BY 1 MM DEEP (2.95 INCHES LONG BY 0.98 INCH WIDE BY 0	.039 INCH DEEP).				1	L	7	1 	3O	3	O		2A13    	E274	5	N	P886	 
1999050700264	19990507	00264	SW  	1999	5	7	AU990346         	1	19990301	G	6220	206001102017	PILLOW BLOCK    			BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					MAIN ROTOR HEAD	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) MAIN ROTOR HEAD PILLOW BLOCKS CRACKED.  BLOCKS WERE A NEW FIT ITEM AT HEAD OVERHAUL AND WERE CRACK TESTED PRIOR TO	 FITMENT.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999050700265	19990507	00265	SW  	1999	5	7	AU990347         	1	19990414	G	5347	412419001	ARM             		RESCUEHOIST 	BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					HOIST	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					AECHB006					(AUS) RESCUE HOIST MOUNTING ARM ASSEMBLY CRACKED IN THE FORWARD OUTBOARD RADIUS OF THE OUTBOARD MOUNTING FOOT.						1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999050700266	19990507	00266	GL  	1999	5	7	AU990348         	3	19990409	G	6111	90DCA8	BLADE           			CESSNA	182   	182P        	2075816	CE  						MCAULY	2A34C	2A34C203    	GL  	PROPELLER	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 								738032		(AUS) PROPELLER BLADES (2OFF) DAMAGED IN THE BLADE SHANK RETENTION AREA.  THE DAMAGE ON ONE BLADE HAD BEEN ANODIZED OVER	.					1	H	7	1 	3O			NT	TA13    		5	C	P3EA	 
1999050700267	19990507	00267	EU  	1999	5	7	AU990349         	1	19990413	G	3246	AN536A	BOLT            	CLEVELAND   	WHEEL       	BNORM 	BN2   	BN2B20      	1520302	EU  	LYC   	O540  	IO540K1B5   	41532	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	LT MLG	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT MAIN LANDING GEAR INBOARD WHEEL ASSEMBLY BOLTS (2OFF3) BROKEN IN AN AREA APPROXIMATELY 1-2 THREADS ABOVE THE 	SHANK.  WHEN THE WHEEL WAS DISASSEMBLED, THE THIRD BOLT WAS FOUND TO BE CRACKED.					1	H	7	2 	3O	3	O		A17EU   	1E4	5	C	P920	 
1999050700268	19990507	00268	CE  	1999	5	7	AU990350         	1	19990412	G	5711		SPAR            			BEECH 	33    	E33A        	1151424	CE  	CONT  	O520  	IO520B      	17032	SO  	MCAULY	2A36C	2A36C23     	GL  	WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WING CARRY THROUGH SPAR CRACKED.  CRACKS LOCATED IN FRONT RIGHT CORNER AND AT LEFT REAR.  FOUND DURING INSPECTION 	IAW AD/BEECH33E/37.					1	L	7	1 	3O	3	O		3A15    	E5CE	5	C	P880	 
1999050700269	19990507	00269	WP  	1999	5	7	AU990351         	2	19990319	G	7250	30727322	TURBINE         			LEAR  	35    	35A         	5170602	CE  	GARRTT	TFE731	TFE73122B   	01518	WP  					RT ENGINE	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 			218  				P89713			(AUS) RIGHT ENGINE TURBINE FIR TREE ROOT FAILURE RESULTED IN TURBINE BLADE LOSS.  EXTENSIVE FOD AND OUT OF BALANCE DAMAG	E TO HIGH PRESSURE AND LOW PRESSURE TURBINE ASSEMBLIES.					2	L	7	2 	4F	4	F		A10CE   	E6WE				 
1999050700270	19990507	00270	SW  	1999	5	7	AU990352         	1	19990415	G	3310	2719115183	CIRCUIT BOARD   			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UA  	01514	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	COCKPIT LIGHTS	CORRODED        	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 			4685 							(AUS) LEFT AFT CIRCUIT BREAKER PANEL LIGHTING PRINTED CIRCUIT BOARD MOISTURE CONTAMINATED CAUSING TRACKING.  PANEL BURNE	D AND MELTED.					2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999050700271	19990507	00271	EA  	1999	5	7	AU990353         	2	19990408	G	8520	SL13884M03	BEARING         			BNORM 	BN2   	BN2A26      	1520226	EU  	LYC   	O540  	O540E4C5    	41532	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	CRANKSHAFT	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							RL1386540A			(AUS) CRANKSHAFT FRONT BEARING FAULTY.  WHITE METAL BREAKING AWAY FROM THE BEARING.  METAL CONTAMINATION OF OIL SYSTEM.						1	H	7	2 	3O	3	O		A17EU   	E295	5	C	P920	 
1999050700272	19990507	00272	EU  	1999	5	7	AU990354         	1	19990408	G	5753	NB25B143	HINGE           			BNORM 	BN2   	BN2A26      	1520226	EU  	LYC   	O540  	O540E4C5    	41532	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	TE FLAP	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT FLAP CENTER HINGE BRACKETS LOOSE.  HINGE ATTACHMENT BOLTS LOOSE.						1	H	7	2 	3O	3	O		A17EU   	E295	5	C	P920	 
1999050700273	19990507	00273	NE  	1999	5	7	AU990355         	3	19990412	G	6111	4HFR34C663G	BLADE           			FRCHLD	SA227 	SA227DC     	3377521	SW  						MCAULY	4HFR34	4HFR34C652  	NE  	PROPELLER	DAMAGED         	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 								932059		(AUS) RIGHT PROPELLER BLADES DAMAGED DURING GROUND RUN WHEN THE RUBBER MATTING USED AS FOD PROTECTION FROM LOOSE STONES 	LIFTED INTO THE PROPELLER.   HF ANTENNA ALSO DAMAGED BY DEBRIS.  FOD.					2	L	7	2 	4T			RT	A18SW   		6	C	3PNE	 
1999050700274	19990507	00274	NM  	1999	5	7	AU990356         	1	19990405	G	2133		VALVE           			BOEING	737   	737377      		NM  										FUSELAGE	STICKING        	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) FORWARD CABIN OUTFLOW VALVE STICKING IN THE `OPEN' POSITION.						2	L	7	2 	4F			RT	A16WE   					 
1999050700275	19990507	00275		1999	5	7	AU990357         	1	19990419	G	7810	72110D1902	EXHAUST PIPE    								CONT  	O240  	IO240A      		SO  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NR 2 CYLINDER EXHAUST PIPE CRACKED AROUND THE CIRCUMFERENCE IN THE AREA JUST BELOW THE MOUNTING FLANGE.											3	O			E7SO				 
1999050700276	19990507	00276	NM  	1999	5	7	AU990358         	1	19990224	G	2460		HARNESS         			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					BS 296-312	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) BURNED WIRE BUNDLE LOCATED IN THE FORWARD E/E COMPARTMENT AT STN 296-312 IN THE RT SIDE UNDER THE TOILET SERVICE D	UCT.  A TOTAL OF 68 WIRES REPLACED.					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999050700277	19990507	00277	CE  	1999	5	7	AU990359         	1	19990331	G	3710		VACUUM PUMP     			CESSNA	172   	172P        	2072436	CE  	LYC   	O320  	O320D2J     	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	ENGINE	REMOVED         	W				O				OTHER                   				W	K		INADEQUATE Q C            	FLUID LOSS                		NR	NOT REPORTED   	1			AU	S 										(AUS) ENGINE RAN OUT OF OIL.  VACUUM PUMP HAD BEEN REMOVED FOR REPLACEMENT AND PILOT TOOK THE AIRCRAFT WITHOUT EITHER TH	E NEW VACUUM PUMP OR A COVER PLATE FITTED.  THE ENGINE CONSEQUENTLY RAN OUT OF OIL.					1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
1999050700278	19990507	00278	SO  	1999	5	7	AU990360         	1	19990123	G	7603	89307000	SWIVEL          			PIPER 	PA34  	PA34200     	7103405	SO  	LYC   	O360  	IO360C1E6   	41514	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	POWER LEVER	WORN            	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 							L906251A	AU2121		(AUS) THROTTLE CONTROL CABLE SWIVEL WORN AND SEPARATED FROM THE BALL JOINT.						1	L	7	2 	3O	3	O		A7SO    	1E10	5	C	P920	 
1999050700279	19990507	00279	SW  	1999	5	7	AU990361         	1	19990322	G	5520	3036810	TORQUE TUBE     		303689      	AIRTRC	AT500 	AT502B      	0390307	SW  	PWA   	PT6   	PT6A34AG    	52053	NE  	HARTZL	HCB3T	HCB3TN3     	GL  	ELEVATOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							PCE57494	BUA19126		(AUS)  LEFT AND RIGHT ELEVATOR TORQUE TUBES PN  30368-9 (LT) AND PN 30368-10 (RT) CRACKED.						1	L	7	1 	3T	4	T	NC	A17SW   	E4EA	6	C	P15E	 
1999050700280	19990507	00280	SO  	1999	5	7	AU990362         	1	19990417	G	2612		FIRE DETECTOR   			EMB   	110   	EMB110P1    	3260122	SO  	PWA   	PT6   	PT6A34      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	LT ENGINE	CONTAMINATED    	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) LEFT ENGINE FIRE DETECTORS CONTAMINATED WITH MOISTURE.						1	L	7	2 	4T	4	T		A21SO   	E4EA	6	C	P15E	 
1999050700281	19990507	00281	SO  	1999	5	7	AU990363         	1	19990418	G	2612		FIRE DETECTOR   			EMB   	110   	EMB110P1    	3260122	SO  	PWA   	PT6   	PT6A34      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	LT ENGINE	CONTAMINATED    	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) LEFT ENGINE FIRE WARNING DETECTORS CONTAMINATED WITH MOISTURE.  AIRCRAFT FLEW THROUGH LIGHT RAIN.						1	L	7	2 	4T	4	T		A21SO   	E4EA	6	C	P15E	 
1999050700282	19990507	00282	CE  	1999	5	7	AU990364         	1	19990412	G	5730		SKIN            			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WING OUTBOARD SKIN CRACKED IN THE AREA ADJACENT TO THE TIP TANK REAR SUPPORT BRACKET ONTO WING REAR SPAR.  FURTHER	 INVESTIGATION FOUND THE TWO RIVETS ATTACHING THE WING END RIB TO THE REAR SPAR HAD SHEARED ALLOWING THE RIB AND SPAR TO	 FLEX INDEPENDENTLY PLACING SEVERE STRESS ON THE UPPER AND LOWER SKINS AND CORNER DOUBLERS.  UPPER AND LOWER DOUBLERS WE	RE FOUND CRACKED AND A NUMBER OF RIVETS ALONG THE RIB UPPER AND LOWER FLANGES WERE LOOSE AND WORKING.  SUSPECT CAUSED BY	 UPWARDS LOADS IMPOSED ON THE REAR TIP TANK ATTACHMENT DUE TO A LARGE VOLUME OF FUEL FORWARD OF THE MAIN ATTACHMENT POIN	T.	1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22E	 
1999050700283	19990507	00283	SO  	1999	5	7	AU990366         	1	19990415	G	3260	922F2A6NZ735A	SENSOR          			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  					RT MLG	FAILED          	W				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			AU	S 					236					(AUS) RIGHT MAIN LANDING GEAR PROXIMITY SENSOR FAULTY.  SUSPECT INTERNAL SHORT CIRCUIT.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE				 
1999050700284	19990507	00284	CE  	1999	5	7	AU990367         	1	19990412	G	2510	CM402118	BUCKLE          		96503       	CESSNA	402   	402C        	207590R	CE  	CONT  	O520  	TSIO520VB   	17040	SO  	MCAULY	3AF32C	3AF32C93    	GL  	SEAT BELT	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) SEAT BELT BUCKLE LOCKING MECHANISM SPRING BROKEN.						1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22E	 
1999050700285	19990507	00285	NM  	1999	5	7	AU990368         	1	19990408	G	5210	BACN10JC6CM	NUT             			BOEING	747   	747338      		NM  										PASSENGER DOOR	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT AND RIGHT UPPER DECK DOOR NUTS BELOW CORRECT LOCK TORQUE.  FOUND DURING INSPECTION IAW AD/B747/47.						2	L	7	2 	4F			RT	A20WE   					 
1999050700286	19990507	00286	NM  	1999	5	7	AU990369         	1	19990410	G	5753	65B020225	FLAP TRACK      			BOEING	747   	747312      	1384932	NM  										TE FLAP	FRACTURED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT INBOARD FORE FLAP TRACK CENTER BANANNA FITTING BROKEN AND PROTRUDING THROUGH THE FORE FLAP.  FOLLOWING LOWER	ING OF THE FLAPS, THE CAUSE OF DAMAGE WAS FOUND TO BE FAILURE OF THE CENTER PROGRAMMING TRACK ASSEMBLY WHICH HAD FRACTUR	ED INTO SEVERAL SECTIONS.  INITIAL FRACTURE HAD OCCURRED AT APPROXIMATELY 100 MM TO 125 MM (4 INCHES TO 5 INCHES) FROM T	HE AFT END OF THE TRACK RUNNING FROM THE TRACK STOP ATTACHMENT HOLES.			2	L	7	4 	4F			RT	A20WE   					 
1999050700287	19990507	00287	NM  	1999	5	7	AU990370         	1	19990412	G	2560	65C1990115	CABLE           			BOEING	737   	737377      	       	NM  										ESCAPE SLIDE	FRAYED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) BOTH AFT DOOR ESCAPE SLIDE COVER RELEASE CABLES FRAYED AND CORRODED.  FOUND DURING INSPECTION IAW AD/B737/042.						2	L	7	2 	4F			RT	A16WE   					 
1999050700288	19990507	00288	SW  	1999	5	7	AU990371         	1	19990221	G	7921	156F062EO320000	HOSE            			MOONEY	M20   	M20C        	5870208	SW  	LYC   	O360  	O360A1D     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	OIL COOLER	FAILED          	W				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			AU	S 							L2182936A			(AUS) ENGINE OIL COOLER OIL RETURN HOSE FAILED.  LOSS OF ENGINE OIL.  THE AIRCRAFT WAS SEVERELY DAMAGED DURING THE SUBSE	QUENT FORCED LANDING.					1	L	7	1 	3O	3	O		2A3     	E286	5	C	P920	 
1999050700289	19990507	00289	SO  	1999	5	7	AU990372         	1	19990422	G	2612	B232M	FIRE DETECTOR   			EMB   	110   	EMB110P1    	3260122	SO  	PWA   	PT6   	PT6A34      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	LT ENGINE	BROKEN          	W				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			AU	S 										(AUS) LEFT ENGINE FIRE DETECTOR LOCATED IN THE COMPRESSOR INLET AREA FOUND TO HAVE A FAULTY TERMINAL POST (POST BROKE WH	EN THE WIRE WAS REMOVED).  SUSPECT MOISTURE INGRESS CAUSED A SHORT CIRCUIT CAUSING THE FIRE WARNING TO ACTIVATE.					1	L	7	2 	4T	4	T		A21SO   	E4EA	6	C	P15E	 
1999050700290	19990507	00290	SO  	1999	5	7	AU990373         	2	19990323	G	8550		FILTER          			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520L      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	ENGINE OIL	CONTAMINATED    	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 							270300R			(AUS) ENGINE OIL FILTER CONTAMINATED BY METAL.  LIMITED INFORMATION PROVIDED.						1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P47G	 
1999050700291	19990507	00291	NE  	1999	5	7	AU990374         	2	19990317	G	8520	96675	BEARING         			DOUG  	DC4   	C54E        	3021530	WP  	PWA   	R2000 	R2000*      	52023	NE  	HAMSTD	23E	23E50       	NE  	NR 2 ENGINE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			388  		P108591		P108591			(AUS) NR 2 ENGINE MASTER ROD BEARING FAILED. THE MASTER ROD WAS EXTENSIVELY DAMAGED.						2	L	7	4 	4R	4	R		A762    	5E5	6	C	P603	 
1999050700292	19990507	00292		1999	5	7	AU990375         	4	19990421	G	2210	2729B	CONTROL CABLE   		ID363161R   	PIPER 	PA30  	PA30        	7103002	SO  	LYC   	O320  	IO320B1A    	41508	EA  	HARTZL	HCE2Y	HCE2YL2     	GL  	AUTOPILOT SYSTEM	BROKEN          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					2729B					(AUS) AUTOPILOT ACTUATOR CABLE BROKEN.  LIMITED INFORMATION PROVIDED.						1	L	7	2 	3O	3	O	 	A1EA    	1E12	5	C	P9EA	 
1999060400336	19990604	00336	SO  	1999	6	4	AU990376         	2	19990412	G	8520	SA628488	LIFTER          		SA646277    	CESSNA	210   	210M        	2073450	CE  	CONT  	O520  	IO520L      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	EXHAUST VALVE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					A646277		294776R			(AUS) NR 4 CYLINDER EXHAUST VALVE LIFTER DAMAGED DUE TO BREAKING AWAY OF THE HARD FACING ON THE BOTTOM OF THE LIFTER. IN	VESTIGATION FOUND SIMILAR DAMAGE ON NR 1 CYLINDER EXHAUST VALVE LIFTER, NR 5 CYLINDER INLET AND EXHAUST VALVE LIFTERS, A	ND, NR 2 CYLINDER EXHAUST VALVE LIFTER.  THE CORRESPONDING CAMSHAFT LOBES WERE ALSO WORN.   EXHAUST VALVE LIFTER P/N SA 	646277.   INLET VALVE LIFTER P/N SA 628488.			1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P47G	 
1999060400337	19990604	00337	WP  	1999	6	4	AU990377         	2	19990419	G	7210		BEARING         	GARRTT      		FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UA  	01514	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	LT ENGINE	FAILED          	W				E				ENGINE SHUTDOWN         				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			AU	S 					P70212					(AUS) LEFT ENGINE SHUT DOWN IN-FLIGHT.   INVESTIGATION FOUND METAL PARTICLES ON THE CHIP DETECTOR (NO COCKPIT INDICATION	).   SUSPECT GEARBOX IDLER GEAR BEARING FAILURE.					2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999060400338	19990604	00338	SO  	1999	6	4	AU990378         	1	19990423	G	5210	5237600	GUSSETT         			PIPER 	PA31  	PA31350     	7103110	SO  						HARTZL	HCE3Y	HCE3YR2     	GL  	DOOR FRAME	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE UPPER CABIN DOOR HINGE SUPPORT STRUCTURE CRACKED.						1	L	7	2 	3O				A20SO   		5	C	P33E	 
1999060400339	19990604	00339	SO  	1999	6	4	AU990379         	1	19990331	G	3260		SWITCH          			PIPER 	PA23  	PA23250     	7102308	SO  	LYC   	O540  	IO540C4B5   	41532	EA  	HARTZL	HCE2Y	HCE2YK2     	GL  	NLG	OUT OF ADJUST   	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) NOSE LANDING GEAR DOWNLOCK MICROSWITCH OUT OF ADJUSTMENT.						1	L	7	2 	3O	3	O		1A10    	1E4	5	C	P9EA	 
1999060400340	19990604	00340	SO  	1999	6	4	AU990380         	1	19990405	G	3233	HYC50005	MOTOR           			PIPER 	PA32  	PA32R300    	7103213	SO  	LYC   	O540  	IO540K1G5   	41532	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	MLG	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LANDING GEAR ELECTRIC MOTOR BRUSHES WORN BEYOND LIMITS.   HYDRAULIC OIL CONTAMINATION ALSO EVIDENT DUE TO WORN DRI	VE SHAFT `O' RING SEAL.					1	L	7	1 	3O	3	O		A3SO    	1E4	5	C	P920	 
1999060400341	19990604	00341		1999	6	4	AU990382         	1	19990420	G	7714	285TO45817	CARD            								GE    	CF6   	CF680C      		GL  					LT ENGINE	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT ENGINE N2 SPEED CARD FAULTY.   FOUND DURING INSPECTION IAW AD/B767/93 AMDT1.											4	F			E23EA				 
1999060400342	19990604	00342	EA  	1999	6	4	AU990383         	1	19990420	G	5553	C6TFM102227	ADAPTER         			DHAV  	DHC6  	DHC6300     	2802606	EA  	PWA   	PT6   	PT6A27      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	VERT STABILIZER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) VERTICAL STABILIZER ATTACHMENT ADAPTER CRACKED THROUGH THE RIGHT ATTACHMENT BOLT HOLE.						1	H	7	2 	3T	4	T	RT	A9EA    	E4EA	6	C	P15E	 
1999060400343	19990604	00343	NE  	1999	6	4	AU990384         	2	19990419	G	7261	70BM031070	OIL PORT        								TMECA 	ARRIEL	ARRIEL1A    	60030	NE  					NR 1 ENGINE	BLOCKED         	W				O				OTHER                   				E	K		VIBRATION/BUFFET          	FLUID LOSS                		CR	CRUISE         	1			AU	S 					663		663			(AUS) NR 1 ENGINE REAR BEARING OIL SCAVENGE PORT BLOCKED BY CARBON PARTICLE.   ENGINE OIL VENTING FROM THE REAR BEARING 	VENT LINE.										3	U			E19EU				 
1999060400344	19990604	00344	EA  	1999	6	4	AU990385         	1	19990226	G	5553	C6TFM102227	ADAPTER         			DHAV  	DHC6  	DHC6300     	2802606	EA  	PWA   	PT6   	PT6A27      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	VERT STABILIZER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					30160					(AUS) VERTICAL STABILIZER FORWARD ATTACHMENT ADAPTER CRACKED THROUGH RIGHT ATTACHMENT BOLT HOLE.						1	H	7	2 	3T	4	T	RT	A9EA    	E4EA	6	C	P15E	 
1999060400345	19990604	00345	NE  	1999	6	4	AU990386         	2	19990414	G	7200		ENGINE          			BOEING	747   	747312      	1384932	NM  	PWA   	JT9   	JT9D7R4G2   	52054	NE  					NR 1	SEIZED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							P715020			(AUS) NR 1 ENGINE SEIZED.   LIMITED INFORMATION PROVIDED.						2	L	7	4 	4F	4	F	RT	A20WE   	E3NE				 
1999060400346	19990604	00346		1999	6	4	AU990387         	4	19990412	G	2565	G317	PIN             		7A146723    	BOEING	747   	747438      		NM  										ESCAPE SLIDE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					G317					(AUS) SLIDE RAFT UPPER SHEAR PIN FAILED TO SHEAR DURING INFLATION.   FULL DEPLOYMENT OF THE SLIDE COULD NOT OCCUR.						2	L	7	4 	4F			RT	A20WE   					 
1999060400347	19990604	00347	SO  	1999	6	4	AU990388         	2	19990306	G	7420		HARNESS         			CESSNA	182   	182H        	2072718	CE  	CONT  	O470  	O470R       	17026	SO  	MCAULY	2A34C	2A34C66     	GL  	IGNITION SYSTEM	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) ENGINE IGNITION HARNESS LEAD FAILED.						1	H	7	1 	3O	3	O	NT	3A13    	E273	5	C	P3EA	 
1999060400348	19990604	00348	NM  	1999	6	4	AU990389         	1	19990403	G	2710	B544DD	BEARING         			BOEING	737   	737377      		NM  										AILERON	CONTAMINATED    	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					303476					(AUS) AILERON FEEL, CENTERING AND TRIM MECHANISM SUPPORT BEARINGS CONTAMINATED WITH DIRT AND GRIT.						2	L	7	2 	4F			RT	A16WE   					 
1999060400349	19990604	00349	NM  	1999	6	4	AU990391         	1	19990421	G	2760		BRAKE           			BOEING	737   	737376      		NM  										DRAG SYSTEM	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) SPEED BRAKES FAILED TO OPERATE.  SPEED BRAKE LEVER STIFF.   RATIO CHANGER P/N 65-46370-16 AND SPOILER MIXER P/N  6	5-46360-7 CHANGED.					2	L	7	2 	4F			RT	A16WE   					 
1999060400350	19990604	00350	NM  	1999	6	4	AU990392         	1	19990112	G	2520	700002001002	SEAT            			BOEING	767   	767338      		NM  	GE    	CF6   	CF680C      		GL  					ROW 30B	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) PASSENGER SEAT AT POSITION 30B SEAT BACK FRAME/HINGE BROKEN.						2	L	7	2 	4F	4	F	RT	A1NM    	E23EA				 
1999060400351	19990604	00351	EU  	1999	6	4	AU990393         	1	19990414	G	5310	325	STRUCTURE       			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R375	R3754123F21 	NE  	FUSELAGE	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					325					(AUS) AIRCRAFT SUFFERED MAJOR HAIL DAMAGE WHILE PARKED AT SYDNEY AIRPORT.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P17N	 
1999060400352	19990604	00352	EU  	1999	6	4	AU990394         	1	19990416	G	2910	7229151501	LINE            			SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT75A2      	30030	NE  	ROTOL	R354	R3544123F13 	NE  	LT MLG	CRACKED         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT MAIN LANDING GEAR RETRACTION SYSTEM HYDRAULIC PIPE LOCATED IN THE LEFT WING ROOT CRACKED AND LEAKING.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE6	6	C	P61G	 
1999060400353	19990604	00353	SW  	1999	6	4	AU990395         	1	19990423	G	3213	2752544001	CAM             	OZONE       		FRCHLD	SA227 	SA227DC     	3377521	SW  						MCAULY	4HFR34	4HFR34C652  	NE  	NLG	MISINSTALLED    	W				O				OTHER                   				W			INADEQUATE Q C            			NR	NOT REPORTED   	1			AU	S 					001					(AUS) NOSE LANDING GEAR CENTERING CAM FITTED BACK TO FRONT PREVENTING CORRECT RETRACTION.   NOSE LANDING GEAR TORQUE LIN	KS HAD JUST BEEN REPLACED.					2	L	7	2 	4T			RT	A18SW   		6	C	3PNE	 
1999060400354	19990604	00354	CE  	1999	6	4	AU990396         	1	19990405	G	2916	572710118	RESERVOIR       			CESSNA	441   	441         	2076020	CE  						HARTZL	HCB3T	HCB3TN5     	GL  	HYDRAULIC SYSTEM	DAMAGED         	W				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			AU	S 			16529							(AUS) HYDRAULIC RESERVOIR VENT LINE FITTED WITH A BLANKING CAP CAUSING THE RESERVOIR TO OVERPRESSURIZE AND RUPTURE.   LO	SS OF HYDRAULIC FLUID.					1	L	7	2 	3T			RT	A28CE   		6	C	P15E	 
1999060400355	19990604	00355	NM  	1999	6	4	AU990397         	1	19990430	G	4920		APU             	GARRTT      	GTCP85129K  	BOEING	737   	737377      		NM  										APU BAY	FIRE            	W				O				OTHER                   				E	B	J	VIBRATION/BUFFET          	SMOKE/FUMES/ODORS/SPARKS  	WARNING INDICATION        	CR	CRUISE         	1			AU	S 										(AUS) APU FIRE.  DAMAGE WAS FOUND AROUND THE EGT THERMOCOUPLE AND WIRING AND EVIDENCE OF DAMAGE IN THE LOWER EXHAUST SHR	OUD AREA ADJACENT TO THE EGT HARNESS.					2	L	7	2 	4F			RT	A16WE   					 
1999060400356	19990604	00356	NM  	1999	6	4	AU990398         	1	19990426	G	2434	GC1010245DIII	GCU             			DHAV  	DHC8  	DHC8103     	1386005	NM  	PWA   	PW121 	PW121       	52124	NE  					NR 1	FAULTY          	W				O				OTHER                   				H			ELECT. POWER LOSS-50 PC   			TO	TAKEOFF        	1			AU	S 										(AUS) NR 1 GENERATOR CONTROL UNIT (GCU) FAULTY.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999060400357	19990604	00357	SO  	1999	6	4	AU990399         	1	19990219	G	2140	3701326	LINER           	JANITROL    	B3040       	PIPER 	PA31  	PA31P       	7103120	SO  	LYC   	O541  	TIGO541E1A  	41539	EA  					HEATING SYSTEM	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			118  		3701326					(AUS) CABIN HEATER INNER COMBUSTION CAN CRACKED.						1	L	7	2 	3O	3	O		A8EA    	E19EA				 
1999060400358	19990604	00358	EA  	1999	6	4	AU990400         	2	19990423	G	7414	IO349237	GEAR            	BENDIX      	S6LN1208    	PIPER 	PA31  	PA31P       	7103120	SO  	LYC   	O541  	TIGO541E1A  	41539	EA  					MAGNETO	STRIPPED        	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					A267358		L22262			(AUS) LEFT MAGNETO NYLON DISTRIBUTOR GEAR HAD THREE TEETH MISSING.						1	L	7	2 	3O	3	O		A8EA    	E19EA				 
1999060400359	19990604	00359	EU  	1999	6	4	AU990401         	1	19990128	G	5311		FRAME           			REIMS 	406   	F406        		EU  	PWA   	PT6   	PT6A112     	52043	NE  	MCAULY	3G34C7	3GFR34C701  	GL  	BS 177	MISMANUFACTURED 	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) CANTED RIB UPPER CAP AT FS 177.45 CONTAINED MISDRILLED HOLES.   FOUND DURING INSPECTION IAW RHEIMS SERVICE BULLETI	N CAB 98-16.					1	L	7	2 	3T	3	T	RT	A54EU   	E4EA	5	C	P60G	 
1999060400360	19990604	00360	SO  	1999	6	4	AU990402         	1	19990419	G	2410	LW18759	BRACKET         			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  	HARTZL	HCE2Y	HCE2YR2     	GL  	ALTERNATOR	MISINSTALLED    	W				O				OTHER                   				H	W		ELECT. POWER LOSS-50 PC   	INADEQUATE Q C            		CR	CRUISE         	1			AU	S 							L82461			(AUS) RIGHT ENGINE IDLER PULLEY TOP MOUNT BRACKET CRACKED UNDER THE LOCKWIRE.   THE IDLER PULLEY WAS ALSO MOUNTED ON THE	 INCORRECT SHAFT (PN 19760) INSTEAD OF THE CORRECT PN LW-19237 CAUSING APPROXIMATELY 2.54 MM (0.1 INCH) MISALIGNMENT OF 	THE ALTERNATOR BOLT.				1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P9EA	 
1999060400361	19990604	00361	SO  	1999	6	4	AU990403         	2	19990420	G	7414	M3050	IMPULSE COUPLING			CESSNA	182   	182H        	2072718	CE  	CONT  	O470  	O470R       	17026	SO  	MCAULY	2A34C	2A34C66     	GL  	MAGNETO	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					95071603		223546			(AUS) MAGNETO IMPULSE COUPLING DAMAGED.						1	H	7	1 	3O	3	O	NT	3A13    	E273	5	C	P3EA	 
1999060400362	19990604	00362	CE  	1999	6	4	AU990404         	1	19990501	G	2434		WIRE            			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320D3G     	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	DC GENERATOR	BROKEN          	W				O				OTHER                   				H			ELECT. POWER LOSS-50 PC   			CR	CRUISE         	1			AU	S 							L498039C			(AUS) ALTERNATOR FIELD WIRE BROKEN ON AIRCRAFT SIDE OF THE ALTERNATOR CONTROL UNIT CONNECTOR.  BATTERY DISCHARGED CAUSIN	G A TOTAL ELECTRICAL FAILURE.					1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
1999060400363	19990604	00363	CE  	1999	6	4	AU990405         	1	19990427	G	7810	265401818	EXHAUST PIPE    			CESSNA	208   	208B        	2073701	CE  	PWA   	PT6   	PT6A114A    	52043	NE  					ENGINE EXHAUST	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) EXHAUST PIPE REAR UPPER ATTACHMENT BRACKET BROKEN AWAY FROM THE EXHAUST PIPE DUE TO HEAT STRESS AND VIBRATION.						1	H	7	1 	3T	3	T		A37CE   	E4EA				 
1999060400364	19990604	00364	NM  	1999	6	4	AU990406         	1	19990422	G	5610	90297H8338	WINDOW          			BOEING	737   	737377      		NM  										COCKPIT	CRACKED         	W				K				NONE                    				O			OTHER                     			CR	CRUISE         	1			AU	S 					90297H8338					(AUS) CAPTAIN'S NR 1 WINDOW OUTER PANE CRACKED IN NUMEROUS LOCATIONS.   CRACKING ORIGINATED FROM LIGHT BURN MARKS NEAR T	HE UPPER EDGE OF THE WINDOW.					2	L	7	2 	4F			RT	A16WE   					 
1999060400365	19990604	00365	NM  	1999	6	4	AU990407         	1	19990312	G	5754	17891112	WEDGE           			BOEING	767   	767204      		NM  	GE    	CF6   	CF680A      	30025	NE  					SLAT	DISBONDED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES DISBONDED AND CORRODED ON THE FOLLOWING SLATS:  SLAT NR 1.   DISBOND 150 MM	 BY 40 MM (5.905 INCHES BY 1.574 INCH) AT INBOARD END, 30 MM (1.181 INCH) FORWARD OF TRAILING EDGE.  DISBOND 180 MM BY 1	2 MM (7.086 INCHES BY 0.472 INCH) AT OUTBOARD END UPPER SURFACE.   DISBOND 40 MM BY 25 MM (1.574 INCH BY 0.984 INCH) AT 	INBOARD END LOWER SURFACE.  SLAT NR 7.  CORROSION 70 MM BY 30 MM (2.755 INCHES BY 1.181 INCH AT 2510 MM (98.818 INCHES) 	FROM INBOARD END, 230 MM (9.055 INCHES) FORWARD OF TRAILING EDGE.  SLAT NR 8.  DISBOND IN TWO AREAS 50 MM BY 30 MM (1.96	8 INCH BY 1.181 INCH) AND 20 MM (0.787 INCH) IN DIAMETER ON INBOARD END UPPER SURFACE.	2	L	7	2 	4F	4	F	RT	A1NM    	E13NE				 
1999060400366	19990604	00366	WP  	1999	6	4	AU990408         	2	19990401	G	8530		HEAD            			DHAVXX	DH82  	DH82AROBRTSN	2801002	WP  	DHAVXX	GIPSY 	GIPSYMAJOR1 	20004	WP  					ENGINE	MISMANUFACTURED 	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) ENGINE VALVE GUIDES POORLY FITTED.   VALVE SEATING PROBLEMS.						1	Q	7	1 	3I	3	I		A8EU    	A8EU				 
1999060400367	19990604	00367	NM  	1999	6	4	AU990409         	1	19990321	G	2450	6030144	CONNECTOR       			BOEING	737   	737377      		NM  										NR 2 ENGINE	DAMAGED         	W				O				OTHER                   				H			ELECT. POWER LOSS-50 PC   			CR	CRUISE         	1			AU	S 										(AUS) NR 2 ENGINE GENERATOR LEAD PHASE `B' PIN AND SOCKET ON CONNECTOR D5126P/J FAULTY.   PHASE `B' PIN CABLE W144-002-0	6 DAMAGED FOR APPROXIMATELY 50.8 MM (2 INCHES).					2	L	7	2 	4F			RT	A16WE   					 
1999060400368	19990604	00368	NM  	1999	6	4	AU990410         	1	19990427	G	2824	737M28500011	VALVE           			BOEING	737   	737476      		NM  										FUEL TRANSFER	FAULTY          	W				K				NONE                    				K			FLUID LOSS                			CR	CRUISE         	1			AU	S 										(AUS) FUEL CROSSFEED VALVE FAULTY.						2	L	7	2 	4F			RT	A16WE   					 
1999060400369	19990604	00369	EU  	1999	6	4	AU990411         	1	19990328	G	2750		TUBE            			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					TE FLAP	DISBONDED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FLAP SYSTEM TRAILING EDGE WIRING LOOM DAMAGED BY SERRATED EDGES OF THE ALUMINIUM FOIL SCREENING AROUND THE DRAIN H	OLES IN THE WING TRAILING EDGE ZIPPER TUBE.					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999060400370	19990604	00370	WP  	1999	6	4	AU990412         	1	19990501	G	2823	IN80432	KNOB            			GOVT  	N22   	N22B        	3880102	WP  						HARTZL	HCA3V	HCA3VF7     	GL  	FUEL SELECTOR	MISINSTALLED    	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 								DS305		(AUS) FUEL SELECTOR KNOB INCORRECTLY FITTED FOLLOWING REMOVAL FOR ACCESS.  THE KNOB WAS REFITTED 90 DEGREES OFF FROM THE	 CORRECT LOCATION.					1	H	7	2 	3T				A7PC    		5	C	P6EA	 
1999060400371	19990604	00371	SW  	1999	6	4	AU990413         	1	19990503	G	3260	6839	BULB            			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UA  	01514	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	RT MLG INDICATOR	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					167					(AUS) RIGHT MAIN LANDING GEAR COCKPIT LIGHT BULBS (2OFF) BLOWN.						2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999060400372	19990604	00372	NE  	1999	6	4	AU990414         	3	19990506	G	6110	660710398	BOLT            			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R390	R3904123F27 	NE  	PROPELLER	SHEARED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 								DRG272190		(AUS) PROPELLER ATTACHMENT BOLT HEAD SHEARED OFF THROUGH THE LOCKWIRE HOLES WHEN RUN-ON TORQUE WAS APPLIED.  THE BOLT WA	S A NEW ITEM.					2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P31N	 
1999060400373	19990604	00373	EU  	1999	6	4	AU990415         	1	19990407	G	5315		FLOORBEAM       			BAG   	BAE146	BAE146100A  	1500260	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					BS 18	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) CRACKS FOUND IN FLOOR BEAM AT FRAME 18 LOCATED ON THE RIGHT SIDE JUST BELOW THE FLOOR LINE.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999060400374	19990604	00374	CE  	1999	6	4	AU990416         	1	19990429	G	3222	12430211	BEARING         			CESSNA	337   	337A        	2075704	CE  	CONT  	O360  	IO360C      	17025	SO  	MCAULY	2AF34C	D2AF34C61   	GL  	NLG	MISSING         	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 							5503950922	722252736646		(AUS) NOSE LANDING GEAR OLEO STRUT BEARING MISSING.   SUSPECT BEARING HAD BEEN LEFT OUT AT THE LAST INSPECTION WHEN NEW 	SEALS HAD BEEN FITTED.					1	H	7	2 	3O	3	O		A6CE    	E1CE	5	C	P5EA	 
2000021900462	20000219	00462	EU  	2000	2	19	AU990416021      	1	19990124	G	2822	36B079EQN07A	SEAL            	INTERTECHNIQ	2060K       	BRAERO	748   	HS7482B     	1500248	EU  										BOOST PUMP	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA						258					(AU) UPON INSTALLATION IN AIRCRAFT SEAL DRAIN BEGAN LEAKING.  UPON INVESTIGATION BY R&O SHOP LEAK HAD DISSAPPEARED.  THR	EE  SIMILAR INSTANCES HAVE LED TO CONCLUSION THAT EVEN IN A SHORT PERIOD OF TIME THIS SEAL WILL DRY OUT.  SUBMITTER SUGG	ESTS THAT THESE PUMPS BE SOAKED IN FUEL BEFORE INSTALLATION.  PUMPS FOUND ON HS 748, FALCON 20, AND CL-215 AIRCRAFT.				2	L	7	2 	3T				A24EU   					 
2000021900463	20000219	00463	SO  	2000	2	19	AU990416025      	1	19990405	G	7120	STSBG0131	BOLT            		LM2005A14   	LKHEED	382   	382G        	526414U	SO  	ALLSN 	501D  	501D22A     	03006	GL  					ENGINE MOUNT	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA								50224			(AU) PART STSBG013-1 HEX HEAD BOLT FOUND INSTALLED IN THE REAR ENGINE MOUNT.  THE BOLT HAD BEEN SUBSTANTIALLY GROUND DOW	N OF MATERIAL AFT OF THE THREAD AREA.  THE GRINDING HAD BEEN PERFORMED BY A ROTARY DISK AND WAS NOT UNIFORM ON THE CIRCU	MFERENCE.  PART NR 347257 BOLT IS CALLED IN THE MANUFACTURERS IPC.  THERE IS NO SUBSTITUTION ALLOWED.				2	H	7	4 	4T	4	T		A1SO    	E282				 
2000021900465	20000219	00465	EA  	2000	2	19	AU990416035      	2	19990122	G	8530	05K21114	ROCKER BOSS     	LYC         	O235L2C     	PIPER 	PA38  	PA38112     	7103812	SO  	LYC   	O235  	O235L2C     	41505	EA  					CYLINDER	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			400  			L1509115		L1509115			(AU) INSPECTION FOUND THERE WAS EXCESSIVE ROCKER SHAFT TO ROCKER SHAFT BOSS CLEARANCE ON THE INTAKE SIDE OF TWO SEPARATE	 CYLINDERS. THIS CLEARANCE WAS MEASURED AT 0.008 INCH.					1	L	7	1 	3O	3	O		A18SO   	E223				 
2000021900466	20000219	00466	EU  	2000	2	19	AU990416036      	1	19990404	G	7931	9752115207	TRANSMITTER     	PWA         	PT6A67B     	PILATS	PC12  	PC12        	7090550	EU  	PWA   	PT6   	PT6A67      	52043	NE  					OIL PRESSURE	ERRATIC         	W				B				EMER. DESCENT           				N			FALSE WARNING             			CR	CRUISE         	1			CA						PR0012		PR0012			(AU) VERY ERRATIC OIL PRESSURE FLUCTUATIONS.  OIL PRESSURE TRANSMITTER REPLACED.						1	L	7	1 	3T	4	T	RT	A78EU   	E26NE				 
2000021900467	20000219	00467		2000	2	19	AU990416038      	4	19990408	G	6122	57A3107	SPRING          	HARTZL      	F44A        	PIPER 	PA32  	PA32300     	7103212	SO  	LYC   	O540  	IO540K1A5   	41532	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	RELIEF VALVE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						7239U		L1035348	CH8275		(AU) PROPELLER GOVERNOR WAS DISMANTLED AND THE SPRING ON THE RELIEF VALVE WAS FOUND CRACKED AT THE BOTTOM THREE COILS. A	 NEW PART WAS INSTALLED.					1	L	7	1 	3O	3	O		A3SO    	1E4	5	C	P920	 
2000021900468	20000219	00468	SO  	2000	2	19	AU990416039      	1	19990317	G	8120	LW12463	TURBO CHARGER   	GARRETTLTD  		PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					NR 1 ENGINE	SEIZED          	W				D				RETURN TO BLOCK         				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		TX	TAXI/GRND HDL  	1			CA						QLR0142		L175668A			(AU) NR 1 ENGINE WOULD NOT PRODUCE FULL POWER PRIOR TO TAKEOFF.  MAINTENANCE FOUND THE TURBOCHARGER SEIZED.  THE UNIT WA	S REPLACED.					1	L	7	2 	3O	3	O		A20SO   	E14EA				 
2000021900469	20000219	00469	GL  	2000	2	19	AU990416048      	3	19990412	G	6111	82PA6	BLADE           	MCAULY      	B2D34C202   	CESSNA	177   	177B        	2073708	CE  	LYC   	O360  	O360A1F6    	41514	EA  	MCAULY	2D34C	B2D34C202   	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1881 	777  		704186			704186		(AU) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADES WERE FOUND CORRODED ON THE LEADING EDGES AND THE 	BUTTS.  THIS PROPELLER WAS LAST INSPECTED ON 7 NOVEMBER 1990.					1	H	7	1 	3O	3	O		A13CE   	E286	5	C	P7EA	 
2000021900470	20000219	00470	EA  	2000	2	19	AU990416055      	2	19990408	G	8530	69679	BOLT            	LYC         	TIO540J2BD  	PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					NR 1 CYLINDER	BROKEN          	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA				1405 		RL416261A		RL416261A			(AU) OIL LEAK WAS FOUND ON THE NR 1 ENGINE DURING A PROPELLER CHANGE.  FURTHER INSPECTION FOUND A THRU-BOLT BROKEN AT NR	 1 CYLINDER.  THE THRU-BOLT WAS REPLACED AND ALL CYLINDER RETAINING NUTS WERE CHECKED FOR PROPER TORQUE AND FOUND WITHIN	 THE LIMITS.  THE ENGINE WAS GROUND RUN SERVICEABLE AND THE AIRCRAFT RETURNED TO SERVICE.				1	L	7	2 	3O	3	O		A20SO   	E14EA				 
2000021900471	20000219	00471	NE  	2000	2	19	AU990416059      	2	19990324	G	7250	310900301	BLADE           	PWA         	PW121       						PWA   	PW121 	PW121       	52124	NE  					1ST STAGE	SEPARATED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			12728	6034 		121181		121181			(AU) ENG SHUTDOWN IN-FLIGHT AFTER A LOUD BANG, FOLLOWED BY A LOSS OF OIL PRESSURE AND AN INCREASE IN ITT.  POST- FLIGHT 	INSP REVEALED ENG HAD SUFFERED A MAJOR INTERNAL FAILURE.  DISASSY OF ENG REVEALED ENG HAD MAJOR INTERNAL DAMAGE TO ALL R	OTATING ASSY.  DAMAGE INITIATED WITH FAILURE OF A 1ST STAGE POWER TURB BLADE, SENDING DEBRIS UPSTREAM INTO LP TURB AND D	OWNSTREAM INTO 2ND STAGE POWER TURB .  CONSEQUENTIAL UNBALANCE CAUSED VIBRATION AND SUBSEQUENT TIP RUB OF HP TURB BLADES	.  RGB CONTAINED HIGH LEVELS OF RESIDUAL MAGNETISM.  MOST OF BEARING AND GEARS IN RGB WERE SCRAPPED.  BEARINGS WERE SCRA	PPED DUE TO PITTING, GEARS DUE TO FROSTING.  MAGNETISM, IN OPINION OF OVERHAUL SHOP, WAS DUE TO LIGHTNING STRIKE.						4	T			E20NE				 
1999060400375	19990604	00375	CE  	1999	6	4	AU990417         	1	19990421	G	5520	10162001111	HINGE           			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A42      	52043	NE  					ELEVATOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELEVATOR HINGES CONTAINED EXFOLIATION CORROSION.  THE CORROSION WAS MAINLY IN BUT NOT CONFINED TO THE HINGE ATTACH	MENT AREA.					1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999060400376	19990604	00376	CE  	1999	6	4	AU990418         	1	19990421	G	7997		WIRE            			CESSNA	172   	172P        	2072436	CE  	LYC   	O320  	O320D2J     	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	OIL TEMPERATURE	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							11552A39A	MA008		(AUS) ENGINE OIL TEMPERATURE PROBE RESISTOR WIRE BROKEN.						1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
1999060400377	19990604	00377	EA  	1999	6	4	AU990419         	2	19990428	G	7250		TURBINE         			BEECH 	90    	C90         	1152913	CE  	PWA   	PT6   	PT6A20      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	LT ENGINE	DAMAGED         	W				O				OTHER                   				E	B		VIBRATION/BUFFET          	SMOKE/FUMES/ODORS/SPARKS  		CL	CLIMB          	1			AU	S 			3360 				PCE24121			(AUS) LEFT ENGINE FAILED WITH AN EXPLOSIVE SOUND AND SPARKS FROM THE EXHAUST.   INITIAL INVESTIGATION REVEALED EXTENSIVE	 DAMAGE TO THE POWER SECTION.					1	L	7	2 	3T	3	T		3A20    	E4EA	6	C	P15E	 
1999060400378	19990604	00378	SO  	1999	6	4	AU990420         	1	19990406	G	3211	6792630	TRUNNION        		6792631     	PIPER 	PA32  	PA32R301    	7103218	SO  	LYC   	O540  	IO540K1G5   	41532	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					967661696766					(AUS) LEFT AND RIGHT MAIN LANDING GEAR TRUNNION HOUSINGS P/N  67926-30 (LT) AND P/N  67926-31 (RT) BOTH CRACKED ON THE A	FT SIDE AT THE LOWER END OF THE FILLET.   FOUND DURING INSPECTION IAW PIPER SB 787B.					1	L	7	1 	3O	3	O		A3SO    	1E4	5	C	P920	 
2000021900472	20000219	00472	EA  	2000	2	19	AU990420006      	2	19990414	G	8530	3116	STUD            	LYC         	LW15318     	CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	NR 2 CYLINDER	LOOSE           	W				B	A			EMER. DESCENT           	UNSCHED LANDING         			R	E	J	PARTIAL RPM/PWR LOSS      	VIBRATION/BUFFET          	WARNING INDICATION        	CR	CRUISE         	1			CA				1890 				L415576	733708		(AU) DURING DOWN WIND LEG, THE ENGINE BEGAN TO RUN ROUGH.  A FORCED APPROACH AND LANDING, NR 2 CYLINDER INTAKE PUSH ROD 	AND TUBE WERE BENT. THE COVER WAS REMOVED AND THE EXHAUST VALVE ROCKER ARM STUD WAS FOUND TO HAVE WORKED LOOSE. THIS ALL	OWED THE CAP FROM THE EXHAUST VALVE STEM TO FALL OUT.  IT IS SUSPECTED THIS CAP JAMMED THE INTAKE VALVE CAUSING THE ROD 	TO BEND.			1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
2000021900473	20000219	00473	GL  	2000	2	19	AU990420009      	3	19990409	G	6110		PROPELLER ASSY  	MCAULY      	1A102OCM6948	CESSNA	150   	A150L       	2071828	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A102	1A102OCM    	GL  	DOWL AREA	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				957  		G12410		54847AR	G12410		(AU) DURING 5 YEAR INSPECTION CORROSION WAS FOUND OVER THE ENTIRE AREA OF THE PROPELLER.  EXTENSIVE CORROSION WAS FOUND 	IN THE BOLT HOLES AND THE DOWEL AREA, THERE IS NO REPAIR ALLOWED IN THIS AREA.  THE PROPELLER WAS REMOVED FROM SERVICE.					1	H	7	1 	3O	3	O		3A19    	E252	5	N	P918	 
2000021900474	20000219	00474	NE  	2000	2	19	AU990420013      	2	19990328	G	7532	39854221	BLEED VALVE     			BOEING	727   	727260      		NM  	PWA   	JT8   	JT8D17      	52049	NE  					NR 3 ENGINE	STUCK           	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA						P1017		P689960			(AU) NR 3 ENGINE BLEED SHUTOFF VALVE WAS STUCK CLOSED.  THE VALVE WAS REPLACED.						2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
2000021900478	20000219	00478	CE  	2000	2	19	AU990420033      	1	19990222	G	2731	040010730	CONTROL CABLE   			CESSNA	150   	150L        	2071826	CE  	CONT  	O200  	O200A       	17020	SO  					ELEVATOR TRIM	FRAYED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			783  					90010704SO			(AU) ELEVATOR TRIM CABLES FOUND FRAYED AND CORRODED AT 100 HR INSP.  THERE WERE NO INDICATIONS OF THE FRAYING ON THE PRE	VIOUS 100 HR.  FRAYING OCCURRED BETWEEN PULLIES (STRAIGHT RUN) IN AN ACCESSIBLE LOCATION.					1	H	7	1 	3O	3	O	 	3A19    	E252				 
1999060400379	19990604	00379	CE  	1999	6	4	AU990421         	1	19990416	G	2742	0310332	SPROCKET        			CESSNA	185   	185F        	2072820	CE  						MCAULY	D3A34	D3A34C401   	GL  	STABILIZER	BROKEN          	W				O				OTHER                   				F			FLT CONT AFFECTED         			CR	CRUISE         	1			AU	S 										(AUS) STABILIZER RT SCREWJACK ACTUATOR SPROCKET BROKEN AT ROLL PIN HOLES.   INSPECTION OF THE LEFT ACTUATOR REVEALED THA	T THE SPROCKET ROLL PIN HOLES WERE ELONGATED AND STARTING TO CRACK.					1	H	7	1 	3O				3A24    		5	C	P47G	 
1999060400380	19990604	00380	SW  	1999	6	4	AU990422         	1	19990401	G	2910	270810322682	LINE            			FRCHLD	SA227 	SA227DC     	3377521	SW  										RT ENGINE	WORN            	W				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			AU	S 										(AUS) HYDRAULIC PIPE LOCATED IN THE RT ENGINE BAY WORN AND LEAKING.  SUSPECT CAUSED BY A LOOSE CLAMP.						2	L	7	2 	4T			RT	A18SW   					 
1999060400381	19990604	00381	EU  	1999	6	4	AU990423         	1	19990504	G	2160		SWITCH          			BAG   	BAE146	BAE146100A  	1500260	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					A/C PACK	FAULTY          	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			AU	S 										(AUS) AIR CONDITIONING PACK FLOW SWITCH FAULTY.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999060400382	19990604	00382		1999	6	4	AU990424         	4	19990430	G	3414	1143800123	INDICATOR       			BEECH 	1900  	1900C       	1154161	CE  	PWA   	PT6   	PT6A65B     	52043	EA  					COCKPIT	INACCURATE      	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AIRSPEED INDICATOR HAS INCORRECT READINGS.						2	L	7	2 	4T	4	T	RT	A24CE   	E4EA				 
1999060400383	19990604	00383	SO  	1999	6	4	AU990425         	2	19990414	G	8520	555753	ROD             			BEECH 	58    	58          	1152740	CE  	CONT  	O520  	IO520C      	17032	SO  					LT ENGINE	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 			340  				555753			(AUS) LEFT ENGINE'S NR 5 AND NR 6 CONNECTING RODS FAILED.   MAJOR INTERNAL DAMAGE TO THE ENGINE.						1	L	7	2 	3O	3	O		3A16    	E5CE				 
1999060400384	19990604	00384	CE  	1999	6	4	AU990426         	1	19990430	G	3230		CIRCUIT BREAKER 			BEECH 	1900  	1900C       	1154161	CE  	PWA   	PT6   	PT6A65B     	52043	EA  					MLG	FAILED          	W				K				NONE                    				O			OTHER                     			TO	TAKEOFF        	1			AU	S 										(AUS) LANDING GEAR 60 AMP CIRCUIT BREAKER LOCATED IN THE LT ENGINE NACELLE TRIPPED.   SUSPECT CAUSED BY WATER INGRESS.						2	L	7	2 	4T	4	T	RT	A24CE   	E4EA				 
1999060400385	19990604	00385	SW  	1999	6	4	AU990427         	1	19990416	G	5280		BRACKET         			LKHEED	SP2   	SP2H        	5269601	SW  						HAMSTD	43E	43E60       	NE  	MLG DOOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LANDING GEAR DOOR BRACKET SUSPECT CRACKED.  LIMITED INFORMATION PROVIDED.						4	M	7	4 	4R			RT	A15SW   		6	C	P871	 
1999060400386	19990604	00386	EA  	1999	6	4	AU990428         	2	19990420	G	8500		ENGINE          								WRIGHT	R3350 	R3350*      	67040	EA  	HAMSTD	43E	43E60       	NE  	LEFT	MALFUNCTIONED   	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) LEFT ENGINE BACKFIRING.   LIMITED INFORMATION PROVIDED.											4	R			E272	6	C	P871	 
1999060400387	19990604	00387	NM  	1999	6	4	AU990430         	1	19990211	G	5754		WEDGE           			BOEING	767   	767216      	1385121	NM  	GE    	CF6   	CF680A      	30025	NE  					SLAT	DISBONDED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEADING EDGE SLAT T/E WEDGES DISBONDED IN FOLLOWING AREAS:   1.  NR 3 SLAT UPPER SURFACE DISBONDED AT OUTBOARD END	 45 MM (1.771 INCH) FROM T/E .  AREA OF DISBOND 50 MM BY 45 MM (1.968 INCH BY 1.771 INCH).   2.  NR 4 SLAT UPPER SURFACE	 DISBONDED 1440 MM (56.692 INCHES) FROM INBOARD END AND 35 MM (1.377 INCH) FROM TRAILING EDGE.   AREA  OF DISBOND 95 MM 	BY 90 MM (3.740 INCHES BY 3.543 INCHES).   3.  NR 5 SLAT UPPER AND LOWER SURFACES DISBONDED AT INBOARD END 25 MM (0.984 	INCH) FROM T/E.   AREA OF DISBOND 55 MM  BY 35 MM (2.165 INCHES BY 1.377 INCH).   4.  NR 8 SLAT UPPER AND LOWER SURFACES	 DISBONDED AT INBOARD END 85 MM (3.346 INCHES) FROM T/E.  AREA OF DISBOND 130 MM BY 55 MM (5.118 INCHES BY 2.1 INCH).	2	L	7	2 	4F	4	F	TC	A2NM    	E13NE				 
2000021900479	20000219	00479	NE  	2000	2	19	AU990430006      	1	19990413	G	5400		PANEL           	TMECA       	ARRIEL1S1   	SKRSKY	S76   	S76A        	8143006	NE  	TMECA 	ARRIEL	ARRIEL1S    	60030	NE  					ENG INTAKE	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			6817 	756  		15114TEC		15114TEC			(AU) ON WALK-AROUND, A PIECE OF STAINLESS STEEL MEASURING 1.5 INCH BY 2 INCH WHICH HAD BROKEN FREE FROM THE UPPER KEVLAR	 PANEL, BETWEEN NR 1 AND  NR 2 AIRFRAME ENGINE INTAKE AREA HAD BEEN INGESTED INTO THE ENGINE, CAUSING FOD DAMAGE.  THE E	NGINE WAS SENT FOR REPAIR.				1	G	7	2 	3U	3	U		H1NE    	E19EU				 
2000021900480	20000219	00480	SO  	2000	2	19	AU990430010      	2	19990430	G	8520	634503	BEARING         	CONT        	GTSIO520H   	CESSNA	421   	421B        	2076014	CE  	CONT  	O520  	GTSIO520H   	17032	SO  					CRANKCASE	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			1040 			267167R		267167R			(AU) NR 2 MAIN BEARING FAILURE,  POSSIBLY  CAUSED BY FRETTING OF THE CRANKCASE HALVES.  THIS FAILURE ALSO CAUSED TWO MAJ	OR CRACKS IN THE CRANKSHAFT, RADIATING OUT FORWARD AND AFT OF THE OIL HOLE AND NUMEROUS SURFACE CRACKS ON THE FACE OF TH	E MAIN JOURNAL.				1	L	7	2 	3O	3	O		A7CE    	E7CE				 
2000021900481	20000219	00481		2000	2	19	AU990430012      	1	19990419	G	2140	K271B200EL	BEARING         	DYNAMICAIR  	C100B3AA    															BLOWER	UNAPPROVED      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						75					(AU) THE BLOWER WAS RECEIVED FOR OVERHAUL. THE TECHNICIAN NOTICED THE PROPER REPLACEMENT BEARINGS, SUPPLIED BY THE MANUF	ACTURER, WERE DIFFERENT THAN THE BEARINGS REMOVED.  THE MANUFACTURERS BEARINGS HAVE NO MARKINGS AND HAVE BROWN RUBBER SE	ALS.  THE BEARINGS FOUND IN THE BLOWER WERE CLEARLY MARKED AS 3200, MADE IN THE USA, AND HAVE GREEN RUBBER SEALS.  DYNAM	IC AIR ENGINEERING HAVE CONFIRMED THAT THEY HAVE NEVER USED THE DESCRIBED BEARINGS IN ANY OF THEIR MOTORS.  THE UNAPPROV	ED PARTS WERE REPLACED WITH THE PROPER PARTS AND THE UNIT WAS RETURNED TO SERVICE.															 
2000021900482	20000219	00482	GL  	2000	2	19	AU990430015      	3	19990416	G	6111	57A1857T	BEARING         	HARTZL      	HCB3TN3C    											HARTZL	HCB3T	HCB3TN3     	GL  	PROP BLADE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				924  		BUA21664			BUA21664		(AU) DURING INSPECTION, WHILE COMPLYING WITH AD 96-18-14,  NR 1 BLADE BEARINGS AND CLAMP WERE FOUND CORRODED.  THE CORRO	SION WAS IN EXCESS OF THE ALLOWABLE REPAIR LIMITS.  THE PARTS WERE RETIRED FROM SERVICE.															6	C	P15EA	 
2000021900483	20000219	00483	EA  	2000	2	19	AU990430022      	2	19990419	G	7260	3013515	HOUSING         	PWA         		PIPER 	PA31T 	PA31T       	7103124	SO  	PWA   	PT6   	PT6A28      		EA  					GEARBOX	CRACKED         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA				3393 				PCE50650			(AU) DURING PRE-FLIGHT, A SMALL OIL LEAK WAS DISCOVERED ON NR 2 ENGINE.  FURTHER INSPECTION FOUND A 2 INCH  CRACK IN THE	 ACCESSORY GEARBOX HOUSING.  THE CRACK IS IN THE BODY OF THE HOUSING, ADJACENT TO THE ACCESSORY DRIVE PAD.  THIS IS THE 	AIR CONDITIONING PAD.				1	L	7	2 	3T	4	T		A8EA    	E4EA				 
2000021900484	20000219	00484	CE  	2000	2	19	AU990430024      	1	19990324	G	3252	NAS561P518	ROLL PIN        	CESSNA      	26430902    	CESSNA	208   	208B        	2073701	CE  										MLG	BROKEN          	W				O				OTHER                   				E			VIBRATION/BUFFET          			LD	LANDING        	1			CA			1262 	1262 							(AU) PILOT LANDED AND REPORTED NOSE SHIMMY. SUBSEQUENT TEARDOWN REVEALED A BROKEN ROLL PIN SHARD WHICH HELD THE INTERNAL	 METERING PISTON.  RIGGING, STOP BLOCK INSPECTIONS, AND PRIOR LOG BOOK ENTRIES REVEALED NO FAULTS.					1	H	7	1 	3T				A37CE   					 
2000021900485	20000219	00485	SW  	2000	2	19	AU990430026      	1	19990419	G	2913	PV304426	PUMP            			SWRNGN	SA227 	SA227AC     	8780603	SW  	GARRTT	TPE331	TPE33111U   	01514	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	NR 2 ENGINE	WORN            	W				O				OTHER                   				J			WARNING INDICATION        			DE	DESCENT        	1			CA								P44501	930241		(AU) NR 1 ENGINE HYDRAULIC WARNING LIGHT CAME ON PRIOR TO LANDING.  ON NR 2 ENGINE SHUTDOWN, THE HYDRAULIC PRESSURE WENT	 TO ZERO.   FLUID LEVEL CHECKED WITHIN LIMITS.  NR 1 ENGINE HYDRAULIC PUMP DRIVE SPLINES WERE FOUND WORN BEYOND LIMITS D	UE TO PUMP SEIZURE.  NR 1 ENGINE HYDRAULIC PUMP REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.				2	L	7	2 	4T	4	T	RT	A8SW    	E4WE	6	C	3PNE	 
2000021900486	20000219	00486	NE  	2000	2	19	AU990430031      	3	19990412	G	6111	6101A12	BLADE           	HAMSTD      	2D30301     	DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  	HAMSTD	2D	2D30        	NE  	PROPELLER	CUT             	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				247  		T16164		4221546	T16164		(AU) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADES WERE TRIMMED TO ENSURE SERVICEABILITY.						1	H	7	1 	3R	3	R		A806    	5E1	5	C	P206	 
2000021900487	20000219	00487	GL  	2000	2	19	AU990430032      	3	19990419	G	6114		HUB             	MCAULY      	D3A34C404   											MCAULY	D3A34	D3A34C404   	GL  	PROPELLER	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			1960 	373  		790337			790337		(AU) PROPELLER RECEIVED FOR CORROSION INSPECTION.  OVERSIZE BORE CAUSED OIL LEAK INTO THE HUB.																5	C	P47GL	 
2000021900488	20000219	00488	GL  	2000	2	19	AU990430033      	3	19990422	G	6114	B24571	FORK            	HARTZL      	HCC2YK1BF   	ARONCA	15    	S15AC       	0191204	EA  	LYC   	O360  	O360A1A     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	PROPELLER HUB	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				14   		CH5599		RL86436	CH5599		(AU) PROPELLER RECEIVED FOR CORROSION INSPECTION.  FORK WAS FOUND WORN BEYOND LIMITS, PROPELLER HAD NOT BEEN GREASED.						1	H	7	1 	3O	3	O		A802    	E286	5	C	P920	 
2000021900489	20000219	00489	GL  	2000	2	19	AU990430034      	3	19990430	G	6114		HUB             	MCAULY      	1A103TCM6958											MCAULY	1A103	1A103TCM    	GL  	PROPELLER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			5130 	1956 		P773466			P773466		(AU) PROPELLER RECEIVED FOR CORROSION INSPECTION.   CRACKS WERE FOUND IN THE PROPELLER MOUNTING HOLES. AD 89-26-10 HAD N	OT BEEN COMPLIED WITH.															5	N	P50GL	 
2000021900490	20000219	00490	SW  	2000	2	19	AU990430037      	1	19990421	G	5741	1700366	STRAP           	SLINDS      		GULSTM	500   	500S        	0141107	SW  										WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			10937								(AU) AD 98-08-19, SB 223 ACCOMPLISHED.  FUSELAGE TO WING STRAPS REVEALED CRACKS.						1	H	7	2 	3O				6A1     					 
2000021900491	20000219	00491	SW  	2000	2	19	AU990430038      	1	19990421	G	5741	1700366	STRAP           	SLINDS      		GULSTM	500   	500S        	0141107	SW  	LYC   	O540  	IO540E1B5   	41532	EA  					WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			7854 	7854 				RL1280848			(AU) AD 98-08-19, SB 223 ACCOMPLISHED.   FUSELAGE TO WING STRAPS REVEALED CRACKS.						1	H	7	2 	3O	3	O		6A1     	1E4				 
2000021900492	20000219	00492	GL  	2000	2	19	AU990430039      	3	19990423	G	6111	A971	BEARING         	HARTZL      	HCA2VK1DI   	PIPER 	PA24  	PA24250     	7102404	SO  	LYC   	O540  	O540A1D5    	41532	EA  	HARTZL	HCA2V	HCA2V*      	GL  	PROPELLER  BLADE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1908 	117  		J308		L1093540C	J308		(AU) PROPELLER RECEIVED FOR CORROSION INSPECTION.  THE PROPELLER BLADE BEARINGS WERE FOUND CORRODED.						1	L	7	1 	3O	3	O		1A15    	E295	5	C	P24EA	 
2000021900493	20000219	00493	GL  	2000	2	19	AU990430040      	3	19990423	G	6114	C5264	CYLINDER        	CONT        	IO550F      	CESSNA	206   	U206C       	2073332	CE  						MCAULY	D3A34	D3A34C404   	GL  	PROPELLER HUB	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1855 			284761R			931569		(AU) INSPECTION FOUND THE INSIDE DIAMETER OF THE PROPELLER BLADE CYLINDERS PITTED AND CORRODED.  THE CYLINDERS WERE REPL	ACED.					1	H	7	1 	3O				A4CE    		5	C	P47GL	 
2000021900494	20000219	00494	GL  	2000	2	19	AU990430041      	3	19990423	G	6111	C5270	BEARING         	MCAULY      	D3A34C      	CESSNA	206   	U206C       	2073332	CE  						MCAULY	D3A34	D3A34C404   	GL  	PROPELLER BLADE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1855 			931569			931569		(AU) INSPECTION FOUND THE BLADE BEARINGS CORRODED BEYOND LIMITS.  THE BLADE BEARINGS WERE NOT WITHIN REPAIRABLE LIMITS. 	 THE BEARINGS WERE REPLACED.					1	H	7	1 	3O				A4CE    		5	C	P47GL	 
2000021900495	20000219	00495	GL  	2000	2	19	AU990430044      	3	19990423	G	6114	B48202	ACTUATING PIN   	MCAULY      	D3A34C      	CESSNA	206   	U206C       	2073332	CE  						MCAULY	D3A34	D3A34C404   	GL  	PROPELLER HUB	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1855 			931569			931569		(AU) DURING INSPECTION THE PROPELLER BLADE ACTUATING PIN WAS FOUND CORRODED.  IT WAS NOT REUSABLE.  THE PIN WAS REPLACED	.					1	H	7	1 	3O				A4CE    		5	C	P47GL	 
2000021900496	20000219	00496	NE  	2000	2	19	AU990430045      	2	19990422	G	8530	41696	TUBE            	PWA         	R183092     	DOUG  	DC3   	DC3CS1C3G   	3021458	WP  	PWA   	R1830 	R183092     	52020	NE  					NR 9 CYLINDER	BROKEN          	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA				360  		363697		363697			(AU) IN CRUISE, THE NR 1 ENGINE MADE A SOFT BANG AND BEGAN TO RUN ROUGH.  THE AIRCRAFT MADE AN UNSCHEDULED LANDING.  POS	T- FLIGHT INSPECTION FOUND THE NR 9 CYLINDER PUSH ROD CRACKED.  BROKEN AND BANGED UP WITH THE BALL END, AT THE ROCKER AR	M, FULLY DETACHED FROM THE ROD WITH THE ROD END COLLAR CRACKED AND STARTING TO SPREAD.  THE PUSH ROD WAS REPLACED AND TH	E ENGINE WAS GROUND RUN SERVICEABLE.			2	L	7	2 	4R	4	R		A669    	5E4				 
2000021900497	20000219	00497	EA  	2000	2	19	AU990430057      	2	19990329	G	7322	25244405	FCU             			BEECH 	100   	A100        	1152915	CE  	PWA   	PT6   	PT6A28      		EA  	HARTZL	HCB4T	HCB4TN3     	GL  	ENGINE	MALFUNCTIONED   	W				C				ABORTED TAKEOFF         				R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			CA				2936 		A7593		PCE50450	EA225		(AU) PILOT NOTED A LOSS OF POWER ON TAKEOFF.  THE DIFFERENCE IN TORQUE AT 10,000 FEET WAS 200 POUNDS.  ALL ENGINE PARAME	TERS WERE TYPICAL OF LACK OF POWER:   LOW ITT; FUEL FLOW; NG READINGS.  THE FUEL CONTROL UNIT WAS REPLACED AND THE PROBL	EM WAS CORRECTED.				1	L	7	2 	3T	4	T		A14CE   	E4EA	6	C	P40EA	 
1999060400388	19990604	00388	SO  	1999	6	4	AU990431         	1	19990504	G	3230	HYC500S	POWER PACK      			PIPER 	PA34  	PA34200T    	7103406	SO  						HARTZL	HCE2Y	HCE2YK2     	GL  	MLG	MALFUNCTIONED   	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					96166					(AUS) LANDING GEAR POWER PACK INTERNAL FAULT PREVENTING ELECTRIC MOTOR OPERATION.						1	L	7	2 	3O				A7SO    		5	C	P9EA	 
1999060400389	19990604	00389	SO  	1999	6	4	AU990432         	1	19990504	G	3230	4611314520094599	DOWNLOCK        			PIPER 	PA34  	PA34200T    	7103406	SO  						HARTZL	HCE2Y	HCE2YK2     	GL  	LT MLG	SEIZED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					96166					(AUS) LEFT MAIN LANDING GEAR DOWNLOCK TURNBUCKLE AND PIVOT ASSEMBLY SEIZED.						1	L	7	2 	3O				A7SO    		5	C	P9EA	 
1999060400390	19990604	00390	EU  	1999	6	4	AU990433         	1	19990426	G	2730		ELEVATOR        			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					RIGHT	JAMMED          	W				O				OTHER                   				C	F		F.O.D.                    	FLT CONT AFFECTED         		TX	TAXI/GRND HDL  	1			AU	S 										(AUS) RIGHT ELEVATOR JAMMED BY FOD.   INVESTIGATION FOUND A PIECE OF RAG WHICH HAD BEEN USED TO JAM THE ELEVATORS IN THE	 UP POSITION DURING MAINTENANCE THE PREVIOUS NIGHT.					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999060400391	19990604	00391	SW  	1999	6	4	AU990434         	1	19990503	G	7120		MOUNT           			SWRNGN	SA226 	SA226TC     	8780404	SW  	GARRTT	TPE331	TPE3313UW   	01514	WP  	HARTZL	HCB3T	HCB3TN5     	GL  	ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							PO3705			(AUS) LOWER ENGINE MOUNT CRACKED.						2	L	7	2 	4T	4	T	RT	A8SW    	E4WE	6	C	P15E	 
1999060400392	19990604	00392	NM  	1999	6	4	AU990435         	1	19990413	G	5311		FRAME           			BOEING	737   	737377      		NM  										BS 616	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE INNER CHORD LOCATED AT BS 616 LT CRACKED THROUGH THE LOWER FASTENER HOLE.  FOUND DURING EDDY CURRENT INSP	ECTION.					2	L	7	2 	4F			RT	A16WE   					 
1999060400393	19990604	00393	NM  	1999	6	4	AU990436         	1	19990419	G	5313		STRINGER        			BOEING	737   	737377      		NM  										BS 727	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) STRINGER 18A WEB CRACKED FROM THE INBOARD HOLE AT BULKHEAD ATTACHMENT LOCATED AT BS 727 RT SIDE.   FOUND DURING ED	DY CURRENT INSPECTION.					2	L	7	2 	4F			RT	A16WE   					 
1999060400394	19990604	00394	CE  	1999	6	4	AU990437         	1	19990508	G	2434		WIRE            			CESSNA	210   	210H        	2073436	CE  	CONT  	O520  	IO520A      	17032	SO  	MCAULY	3A32C	D3A32C88    	GL  	DC ALTERNATOR	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ALTERNATOR GROUND LEAD HAD COME ADRIFT FROM ITS TERMINAL AT THE ALTERNATOR SOME TIME PREVIOUSLY AND HAD BEEN STOWE	D IN THE LOOM AND HAD NOT BEEN RETERMINATED.   WITHOUT A GROUND, THE ALTERNATOR HAD BEEN GROUNDING THROUGH AN ALUMINIUM 	DUCT RESTING AGAINST IT.  THIS CONDITION CAUSED THE ALTERNATOR ROTOR AND VOLTAGE REGULATOR TO FAIL.				1	H	7	1 	3O	3	O	 	3A21    	E5CE	5	C	P21EA	 
1999060400395	19990604	00395	EU  	1999	6	4	AU990438         	1	19990512	G	5320	TBIO23012101	BRACKET         			SOCATA	TB10  	TB10TOBAGO  	8680696	EU  	LYC   	O360  	O360A1A     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	COCKPIT	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT CONTROL COLUMN SUPPORT BRACKET BROKEN THROUGH THE RADIUS AFT END ATTACHMENT.						1	L	7	1 	3O	3	O	NT	A51EU   	E286	5	C	P920	 
1999060400396	19990604	00396	NE  	1999	6	4	AU990439         	3	19990504	G	6140	3039242	SENSOR          			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  	HAMSTD	14SF	14SF9       	NE  	NR 2 ENGINE	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) NR 2 ENGINE NP SENSOR PROBE RESISTANCE OUT OF TOLERANCE.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	N	P11N	 
1999060400397	19990604	00397	SW  	1999	6	4	AU990440         	2	19990507	G	8530	12921	EXHAUST VALVE   			WACO  	YMF   	YMF         	9600412	EA  	JACOBP	R755  	R755B2      	35007	SW  					ENGINE	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					12921		12921			(AUS) EXHAUST VALVES ON ALL CYLINDERS WERE BADLY DEFORMED ON THE VALVE STEM TIPS.   INVESTIGATION FOUND ABNORMAL WEAR ON	 THE TIPS OF THE INLET VALVES.					1	Q	7	1 	3R	3	R		ATC542  	E237				 
1999060400398	19990604	00398	CE  	1999	6	4	AU990441         	1	19990325	G	3230	99101542	BLOWDOWN BOTTLE 			CESSNA	404   	404CESSNA   	2075901	CE  						MCAULY	3FF32	3FF32C501   	GL  	MLG	FAILED          	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) UNDERCARRIAGE EMERGENCY BLOW-DOWN BOTTLE DISCHARGE VALVE BLEW OFF THE BOTTLE.   SUSPECT THAT THE BOTTLE HAD BEEN C	HARGED WITH OXYGEN INSTEAD OF NITROGEN.					1	L	7	2 	3O				A25CE   		5	C	P45G	 
1999060400399	19990604	00399	EU  	1999	6	4	AU990442         	1	19990506	G	7931	20030405	TRANSDUCER      			BAG   	BAE146	BAE146100A  	1500260	EU  	LYC   	ALF502	ALF502R3A   	41580	NE  					NR 3 ENGINE	MALFUNCTIONED   	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 			19001				LFO50285			(AUS) NR 3 ENGINE OIL PRESSURE TRANSDUCER FAULTY.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999060400400	19990604	00400	CE  	1999	6	4	AU990443         	1	19990508	G	3230	51420021OR3	DRAG BRACE      			CESSNA	402   	402C        	207590R	CE  	CONT  	O520  	TSIO520VB   	17040	SO  	MCAULY	3AF32C	3AF32C505   	GL  	NLG	FRACTURED       	W				K				NONE                    				O			OTHER                     			TO	TAKEOFF        	1			AU	S 										(AUS) NOSE LANDING GEAR DRAG BRACE FRACTURED.						1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22E	 
1999060400401	19990604	00401	CE  	1999	6	4	AU990444         	1	19990416	G	3221	5842000213	TRUNNION        			CESSNA	310   	310Q        	2074242	CE  	CONT  	O470  	IO470V      	17026	SO  	MCAULY	3AF32C	3AF32C87    	GL  	NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					D500					(AUS) NOSE LANDING GEAR TRUNNION CRACKED IN ONE PIVOT AS INDICATED IN AAC1-108.						1	L	7	2 	3O	3	O		3A10    	3E1	5	C	P22E	 
1999060400402	19990604	00402		1999	6	4	AU990445         	1	19990511	G	7732		INDICATOR       		200304005   						LYC   	ALF502	ALF502R3A   	41580	NE  					NR 1 ENGINE	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 							LFO5020			(AUS) NR 1 ENGINE VIBRATION INDICATOR FAULTY.											4	F			E6NE				 
1999060400403	19990604	00403	CE  	1999	6	4	AU990446         	1	19990420	G	5530	12310231	BRACKET         			CESSNA	210   	210J        	2073439	CE  	CONT  	O520  	IO520J      	17032	SO  	MCAULY	3A32C	D3A32C88    	GL  	VERT STABILIZER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LOWER RUDDER ATTACHMENT BRACKET CRACKED IN HORIZONTAL PLANE.						1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P21E	 
1999060400404	19990604	00404	CE  	1999	6	4	AU990447         	1	19990510	G	5753	10516000015	RIB             		16916000519 	BEECH 	76    	76          	1153005	CE  										TE FLAP	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FLAP NOSE RIBS AND FLAP HINGE BRACKET CRACKED AND CORRODED.   EVIDENCE OF PAINT STRIPPER IN THE AREA OF THE CORROS	ION.  THE AIRCRAFT HAD BEEN PAINTED APPROXIMATELY TWELVE MONTHS PREVIOUSLY.					1	L	7	2 	3O				A29CE   					 
1999060400405	19990604	00405	CE  	1999	6	4	AU990448         	1	19990510	G	5753	16916000520	RIB             			BEECH 	76    	76          	1153005	CE  										TE FLAP	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FLAP NOSE RIBS AND FLAP HINGE BRACKET CRACKED AND CORRODED.   EVIDENCE OF PAINT STRIPPER FOUND IN THE AREA.   AIRC	RAFT HAD BEEN PAINTED APPROXIMATELY TWELVE MONTHS PREVIOUSLY.					1	L	7	2 	3O				A29CE   					 
1999060400406	19990604	00406	EU  	1999	6	4	AU990449         	1	19990519	G	5753		BALANCE WEIGHT  			GROB  	G115  	G115C       	1660303	EU  	LYC   	O235  	O235H2C     	41505	EA  	SNSNCH	72C	72CK        	EA  	TE FLAP	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT AND RIGHT FLAP MASS BALANCE WEIGHTS CORRODED.  THE LEFT SIDE WEIGHT HAS CORRODED SUFFICIENTLY TO BURST THROUG	H THE FIBERGLASS CASING.					1	L	7	1 	3O	3	O	NT	A57EU   	E223	5	N	P904	 
1999060400407	19990604	00407	NM  	1999	6	4	AU990450         	1	19990519	G	3097		WIRE            			DHAV  	DHC8  	DHC8103     	1386005	NM  	PWA   	PW121 	PW121       	52124	NE  					NR 2 PITOT	BROKEN          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) NR 2 (RT) PITOT HEAT SYSTEM WIRE CHAFED.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999060400408	19990604	00408	CE  	1999	6	4	AU990451         	1	19990421	G	2150	1143800285	BLOWER          			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					CABIN COOLING	MALFUNCTIONED   	W				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			AU	S 										(AUS) AFT EVAPORATOR BLOWER ROTOR BINDING CAUSING THE HI/LOW SPEED RESISTORS TO BURN OUT.						2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999060400409	19990604	00409	NM  	1999	6	4	AU990452         	1	19990415	G	5101		STRUCTURE       			BOEING	737   	737377      		NM  										AIRFRAME	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AIRCRAFT SUFFERED HAIL DAMAGE TO THE FOLLOWING AREAS:   1.   LT AND RT AILERONS.   2.   RT AILERON TRIM TAB.   3. 	  LT AND RT ELEVATORS.   4.  LT AND RT HORIZONTAL STABILIZERS.   5.  SPOILERS.   6.   RUDDER.					2	L	7	2 	4F			RT	A16WE   					 
1999060400410	19990604	00410	NM  	1999	6	4	AU990453         	1	19990415	G	5101		STRUCTURE       			BOEING	767   	767204      		NM  	GE    	CF6   	CF680A      	30025	NE  					AIRFRAME	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AIRCRAFT SUFFERED HAIL DAMAGE TO THE FOLLOWING AREAS:   1.  LT INBOARD AND OUTBOARD AILERONS.   2.   LT AND RT LEA	DING EDGE SLAT WEDGES.   3.  LT AND RT INBOARD AND OUTBOARD FLAP TRAILING EDGES.   4.   NR 10 SPOILER.   5.  VERTICAL ST	ABILIZER RT SIDE LEADING EDGE.				2	L	7	2 	4F	4	F	RT	A1NM    	E13NE				 
1999060400411	19990604	00411	WP  	1999	6	4	AU990454         	2	19990418	G	7260	31036016	BEARING         	GARRTT      	31038707    	FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UA  	01514	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	LT ENGINE	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					P70212					(AUS) LEFT ENGINE NR 1 ACCESSORY GEAR BEARING LOCATED IN THE ACCESSORY GEARBOX FAILED.						2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999060400412	19990604	00412	EU  	1999	6	4	AU990455         	1	19990415	G	5101		STRUCTURE       			AIRBUS	320   	A320212     		EU  										AIRFRAME	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AIRCRAFT STRUCTURE DAMAGED BY HAIL IN THE FOLLOWING AREAS:   1.  LT AND RT ELEVATOR UPPER SURFACES.   2.  LT AND R	T AILERONS.   3.  LT AND RT INBOARD AND OUTBOARD TRAILING EDGE FLAPS.   4.  NR 1 ENGINE OUTBOARD COWL.   5.  NR 2 ENGINE	 INBOARD COWL.   6.  RT HORIZONTAL STABILIZER.   7.   LT STABILIZER TIP.   8.  LT ELEVATOR.   9.  RADOME.				2	L	7	2 	4F			RT	A28NM   					 
1999060400413	19990604	00413	EU  	1999	6	4	AU990456         	1	19990517	G	2530		OVEN            			BAG   	BAE146	BAE146200A  	1500266	EU  										GALLEY	CONTAMINATED    	W				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			AU	S 										(AUS) OVEN SMOKING.   INVESTIGATION FOUND THAT THE SMOKE WAS CAUSED BY SPILT FOOD AND CLEANING AGENT.						2	H	7	4 	4F			RT	A49EU   					 
1999060400414	19990604	00414	CE  	1999	6	4	AU990457         	1	19990412	G	5753	351650519	SKIN            			BEECH 	58    	58          	1152740	CE  						MCAULY	3AF32C	3AF32C512   	GL  	TE FLAP	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT FLAP SKIN CRACKED IN THE AREA UNDER THE FLAP ACTUATOR ATTACHMENT BRACKET.   RIB P/N 35165050-84 LOCATED BELO	W THE CRACKED AREA OF THE SKIN WAS ALSO CRACKED.					1	L	7	2 	3O				3A16    		5	C	P22E	 
1999060400415	19990604	00415	GL  	1999	6	4	AU990458         	3	19990514	G	6114	D32612	HUB             			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A1A   	41532	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	PROPELLER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 								DJ8188A		(AUS) PROPELLER HUB CRACKED IN THREADS OF GREASE NIPPLE HOLE.						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33E	 
1999060400416	19990604	00416	CE  	1999	6	4	AU990459         	1	19990514	G	3213	358152463	STRUT           		358152461   	BEECH 	95    	D95A        	1153408	CE  	LYC   	O360  	IO360B1B    	41514	EA  	HARTZL	HC92W	HC92WK2     	GL  	LT & RT MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT AND RIGHT MAIN LANDING GEAR CYLINDERS P/N  35815246-1 (LT) AND P/N 35815246-3 (RT) CRACKED IN THE RADIUS OF T	HE LOWER BRACE ATTACHMENT FITTINGS.					1	L	7	2 	3O	3	O		3A16    	1E10	5	C	P16E	 
1999060400417	19990604	00417	GL  	1999	6	4	AU990460         	1	19990510	G	2436		REGULATOR       			AMTR  	LANCAR	LANCAIRIV   	056163V	GL  										DC SYSTEM	MISINSTALLED    	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) INCORRECT VOLTAGE REGULATOR FITTED.						1	L	7	1 	3O			RT	EXPA1L71					 
1999060400418	19990604	00418	GL  	1999	6	4	AU990461         	1	19990510	G	5610		WINDOW          			AMTR  	LANCAR	LANCAIRIV   	056163V	GL  										COCKPIT	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT SIDE WINDOW CRACKED.   WINDOW WAS MODIFIED DURING AIRCRAFT CONSTRUCTION.						1	L	7	1 	3O			RT	EXPA1L71					 
1999060400419	19990604	00419	NM  	1999	6	4	AU990462         	1	19990423	G	5313		STRINGER        			BOEING	737   	737377      		NM  										BS 727	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE STRINGER 18A WEB LOCATED AT BS 727 CRACKED AT THE AFT INBOARD FASTENER HOLES ON THE LT AND RT SIDES.   FO	UND DURING EDDY CURRENT INSPECTION.					2	L	7	2 	4F			RT	A16WE   					 
1999060400420	19990604	00420	NM  	1999	6	4	AU990463         	1	19990511	G	5313		STRINGER        			BOEING	737   	737377      		NM  										BS 727	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE STRINGER 18A LOCATED ON BOTH LT AND RT SIDES AT BS 727 CRACKED AT THE INBOARD HOLES.   FOUND DURING EDDY 	CURRENT INSPECTION.					2	L	7	2 	4F			RT	A16WE   					 
1999060400421	19990604	00421	CE  	1999	6	4	AU990464         	1	19990420	G	3230		DOWNLOCK        			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520F      	17032	SO  	HARTZL	HCJ3Y	PHCJ3YF1    	GL  	MLG	OUT OF ADJUST   	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							280136R	FP401A		(AUS) MAIN LANDING GEAR DOWNLOCKS OUT OF ADJUSTMENT.   DOWNLOCKS HAD NOT BEEN LUBRICATED FOR AN EXTENDED PERIOD CAUSING 	BINDING.					1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P36E	 
1999060400422	19990604	00422	CE  	1999	6	4	AU990465         	1	19990420	G	3231	12170731	ROD END         			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520F      	17032	SO  	HARTZL	HCJ3Y	PHCJ3YF1    	GL  	NLG	MISINSTALLED    	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 							280136R	FP401A		(AUS) NOSE LANDING GEAR DOOR ARM ROD ENDS INSTALLED 180 DEGREES OUT ALLOWING THE DOORS TO FOUL ON THE NACELLE LOWER SKIN	 IN THE FULL DOWN POSITION.   WHEN THE DOORS WERE ADJUSTED TO WITHIN LIMITS, IT WAS FOUND THAT THE DOOR LOCATOR PINS WER	E ALSO MISALIGNED.				1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P36E	 
1999060400423	19990604	00423	CE  	1999	6	4	AU990466         	1	19990420	G	5321		FLOOR  PANEL    			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520F      	17032	SO  	HARTZL	HCJ3Y	PHCJ3YF1    	GL  	CABIN	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							280136R	FP401A		(AUS) FUSELAGE FLOOR CORRODED IN SEVERAL AREAS.  SUSPECT CAUSED BY LEAKING SIDE WINDOWS ALLOWING WATER TO ENTER AND SOAK	 INTO THE CARPET WHICH HAD BEEN DAMP FOR A LONG PERIOD.   AIRCRAFT ALSO OPERATES IN A SALT AIR ENVIRONMENT.					1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P36E	 
1999060400424	19990604	00424	CE  	1999	6	4	AU990467         	1	19990420	G	3242	16401501	DISC            			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520F      	17032	SO  	HARTZL	HCJ3Y	PHCJ3YF1    	GL  	BRAKE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							280136R	FP401A		(AUS) LEFT BRAKE DISC CRACKED IN TWO PLACES ALONG THE FLANGE WHERE IT MEETS THE BRAKE DISC BODY.  THE CRACKS HAD BEEN IN	 THE BRAKE DISC FOR AN EXTENDED PERIOD OF TIME AND THE DISC WAS CLOSE TO FAILURE.					1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P36E	 
1999060400425	19990604	00425	CE  	1999	6	4	AU990468         	1	19990420	G	3230	31NAS464P742	BOLT            			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520F      	17032	SO  	HARTZL	HCJ3Y	PHCJ3YF1    	GL  	MLG	SEIZED          	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 							280136R	FP401A		(AUS) NOSE LANDING GEAR ACTUATOR TO FUSELAGE ATTACHMENT FITTING BOLT SEIZED.   WHEN THE BOLT WAS REMOVED , IT WAS FOUND 	THAT THE BOLT WAS SEVERELY CORRODED.   THE BOLT WAS ALSO THE INCORRECT PART NUMBER.   THE IPC INDICATES THAT AN `AN' TYP	E BOLT SHOULD BE USED WHILE THE BOLT FITTED WAS AN `NAS' TYPE ITEM.				1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P36E	 
1999070900028	19990709	00028	SO  	1999	7	9	AU990469         	2	19990420	G	8530	639272	CYLINDER        	CONT        	IO520FCL    	CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520F      	17032	SO  	HARTZL	HCJ3Y	PHCJ3YF1    	GL  	ENGINE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			13010		280136R		280136R	FP401A		(AUS) ENGINE CYLINDERS CRACKED.   ALL VALVES, PISTONS, PISTON RINGS AND VALVE GUIDES WORN BEYOND LIMITS.  INVESTIGATION 	FOUND THAT NR 2 AND NR 3 CYLINDERS HAD BEEN RELEASED BELOW MINIMUM LIMITS PER AAC 6-32 AMDT1.   FOUND DURING INSPECTION 	IAW AD/ENG/4 AMDT7 PARA 3:1.				1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P36EA	 
1999070900029	19990709	00029	NM  	1999	7	9	AU990470         	1	19990517	G	2130		CONTROLLER      			BOEING	737   	737377      		NM  										CABIN PRESSURE	MALFUNCTIONED   	H				O				OTHER                   				N			FALSE WARNING             			CR	CRUISE         	1			AU	S 										(AUS) EXCESS CABIN ALTITUDE WARNING HORN ACTIVATED.  SUSPECT FAULTY CABIN PRESSURE CONTROLLER.						2	L	7	2 	4F			RT	A16WE   					 
1999070900030	19990709	00030	NM  	1999	7	9	AU990471         	1	19990509	G	2920	2660591	VALVE           			BOEING	767   	767277      		NM  	GE    	CF6   	CF680A      	30025	NE  					HYDRAULIC SYSTEM	FAILED          	H				O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		NR	NOT REPORTED   	1			AU	S 					097					(AUS) RAM AIR TURBINE CHECKOUT MODULE CHECK VALVE FAILED.  LOSS OF CENTER HYDRAULIC SYSTEM FLUID.						2	L	7	2 	4F	4	F	RT	A1NM    	E13NE				 
1999070900031	19990709	00031	CE  	1999	7	9	AU990472         	1	19990520	G	2913	98811241	POWER PACK      			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520F      	17032	SO  	HARTZL	HCJ3Y	PHCJ3YF1    	GL  	HYDRAULIC PUMP	LEAKING         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AU	S 					1066		280136R	FP401A		(AUS) HYDRAULIC POWER PACK LEAKING FROM TOP PUMP SEAL.  INVESTIGATION FOUND THE MOTOR WORN.  THE HYDRAULIC FLUID WAS CON	TAMINATED WITH METAL PARTICLES.					1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P36EA	 
1999070900032	19990709	00032	CE  	1999	7	9	AU990473         	1	19990520	G	3230	9881128	MOTOR           			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520F      	17032	SO  	HARTZL	HCJ3Y	PHCJ3YF1    	GL  	MLG	CONTAMINATED    	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					3383		280136R	FP401A		(AUS) LANDING GEAR MOTOR CONTAMINATED WITH HYDRAULIC OIL CAUSING HIGH RESISTANCE AND FRICTION IN THE ARMATURE.  THE LAND	ING GEAR CIRCUIT BREAKER HAD TO BE CONTINUALLY RESET.					1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P36EA	 
1999070900033	19990709	00033	CE  	1999	7	9	AU990474         	1	19990520	G	7820	65043	MUFFLER         			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520F      	17032	SO  	HARTZL	HCJ3Y	PHCJ3YF1    	GL  	EXHAUST	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							280136R	FP401A		(AUS) LEFT EXHAUST MUFFLER CRACKED AROUND THE TAILPIPE FLANGE.  BULGES FOUND ON THE MUFFLER CAN.						1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P36EA	 
1999070900034	19990709	00034	CE  	1999	7	9	AU990475         	1	19990420	G	7810	12502632	COLLECTOR       	CONT        	IO520FCL    	CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520F      	17032	SO  	HARTZL	HCJ3Y	PHCJ3YF1    	GL  	EXHAUST	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					280136R		280136R	FP401A		(AUS) LEFT EXHAUST COLLECTOR CRACKED ALONG EXHAUST STUB SLIP JOINT.  THE COLLECTOR HAD BEEN ILLEGALLY WELD REPAIRED.  UN	APPROVED REPAIR.					1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P36EA	 
1999070900035	19990709	00035	CE  	1999	7	9	AU990476         	1	19990420	G	5523	12346281	TRIM TAB        			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520F      	17032	SO  	HARTZL	HCJ3Y	PHCJ3YF1    	GL  	ELEVATOR	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							280136R	FP401A		(AUS) ELEVATOR TRIM TAB CORRODED AND DAMAGED DUE TO FOD. THE TRIM TAB HAD ALSO BEEN REPAIRED AT SOME TIME PREVIOUSLY DUE	 TO TIP DAMAGE.					1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P36EA	 
1999070900036	19990709	00036	NM  	1999	7	9	AU990477         	1	19990521	G	7712		CONNECTOR       			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					SIGNAL CONDITION	CONTAMINATED    	H				C				ABORTED TAKEOFF         				E			VIBRATION/BUFFET          			TO	TAKEOFF        	1			AU	S 										(AUS) RIGHT ENGINE TORQUE SIGNAL CONDITIONER CONNECTOR CONTAMINATED WITH OIL.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999070900037	19990709	00037	WP  	1999	7	9	AU990478         	1	19990512	G	5311	A02020	FRAME           			ROBSIN	R22   	R22ALPHA    	7640104	WP  	LYC   	O320  	O320B2C     	41508	EA  					FUSELAGE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE UPPER FRAME ASSEMBLY CRACKED AT THE EDGE OF THE WELDED JOINT ON THE DIAGONAL STRUT BETWEEN THE UPPER AND 	LOWER FRAME HEXAGONAL BOLT ATTACHMENT POINT AND THE REAR RIGHT MAIN ROTOR TRANSMISSION MOUNTING BOLT TRUNNION.  INVESTIG	ATION OF WITNESS MARKS FOUND THAT A SMALL PORTION OF THE CRACK HAD EXISTED ON THE TOP INNER SURFACE OF THE TUBE FOR SOME	 TIME.			1	G	7	1 	3O	3	O		H10WE   	E274				 
1999070900038	19990709	00038	CE  	1999	7	9	AU990479         	1	19990515	G	5711	501100033	SPAR            			BEECH 	55    	D55         	1152730	CE  	CONT  	O520  	IO520C      	17032	SO  	MCAULY	3AF32C	3AF32C75    	GL  	RT WING	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT WING TOP SPAR CAP CONTAINED EXFOLIATION CORROSION IN THREE AREAS.						1	L	7	2 	3O	3	O		3A16    	E5CE	5	C	P22EA	 
1999070900039	19990709	00039	NM  	1999	7	9	AU990480         	1	19990519	G	3230		UPLOCK HOOK     			DHAV  	DHC8  	DHC8103     	1386005	NM  	PWA   	PW121 	PW121       	52124	NE  					RT MLG	WORN            	H				K				NONE                    				O			OTHER                     			DE	DESCENT        	1			AU	S 										(AUS) RIGHT MAIN LANDING GEAR UPLOCK HOOK WORN EXCESSIVELY.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999070900040	19990709	00040	SW  	1999	7	9	AU990481         	1	19990515	G	2133	2686017001	VENT            			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UA  	01514	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	CABIN PRESSURE	BLOCKED         	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) OUTFLOW VALVE STATIC PORT LOCATED ON THE LEFT LOWER EMPENNAGE COVERED WITH MASKING TAPE FOLLOWING REPAINT.  THE TA	PE HAD BEEN PAINTED OVER AND WAS DIFFICULT TO SEE.					2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999070900041	19990709	00041	SO  	1999	7	9	AU990482         	1	19990521	G	7334	1103P1892	SWITCH          			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  					RT ENGINE	FAILED          	H				K				NONE                    				E			VIBRATION/BUFFET          			CL	CLIMB          	1			AU	S 										(AUS) RIGHT ENGINE FUEL PRESSURE SWITCH FAULTY.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE				 
1999070900042	19990709	00042	GL  	1999	7	9	AU990483         	2	19990430	G	7260	6889700	GEAR            	ALLSN       	6894171     	BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	WRONG PART      	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 			4754 		CAG36047		CAE832194			(AUS) ENGINE ACCESSORY GEARBOX 2.5 BEARING INCORRECTLY POSITIONED DUE TO THE INCORRECT FITMENT OF THE HELICAL GEAR.  THE	 GEAR HAD BEEN INSTALLED IN THE REVERSE POSITION.  THE GEARBOX HAD JUST BEEN RECEIVED FROM THE OVERHAUL FACILITY FOLLOWI	NG REPAIRS AND WAS BEING INSPECTED PRIOR TO FITMENT.				1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999070900043	19990709	00043	NM  	1999	7	9	AU990484         	1	19990511	G	5313		STRINGER        			BOEING	737   	737377      		NM  										BS 727	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE STRINGER 18A LOCATED AT BS 727, LT AND RT SIDES CRACKED AT THE INBOARD HOLES.   FOUND DURING EDDY CURRENT	 INSPECTION.					2	L	7	2 	4F			RT	A16WE   					 
1999070900044	19990709	00044	NM  	1999	7	9	AU990485         	1	19990415	G	5700		STRUCTURE       			BOEING	767   	767216      	1385121	NM  	GE    	CF6   	CF680A      	30025	NE  					WING	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AIRCRAFT SUFFERED HAIL DAMAGE TO THE FOLLOWING AREAS:  1.  LT OUTBOARD AILERON, RT INBOARD AND OUTBOARD AILERONS. 	 2.  LT AND RT ELEVATORS.  3.  NR 1, NR 2, NR 3, NR 4, NR 5, NR 7, NR 8, NR 9, NR 10, NR 11, NR 12 LEADING EDGE SLATS.  	4.  NR 2, NR 3, NR 4, NR 5, NR 7, NR 8, NR 9, NR 10, NR 11 SPOILER PANELS.   5.  LT INBOARD, RT INBOARD AND LT OUTBOARD 	TRAILING EDGE FLAPS.			2	L	7	2 	4F	4	F	TC	A2NM    	E13NE				 
1999070900045	19990709	00045	NM  	1999	7	9	AU990486         	1	19990419	G	5312		BULKHEAD        			BOEING	737   	737377      		NM  										BS 178	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FORWARD PRESSURE BULKHEAD LOCATED AT STA 178 CRACKED IN THE FOLLOWING LOCATIONS:  1.  CRACK LOCATED ON THE INBOARD	 SIDE RADIUS OF THE LT VERTICAL CHORD (LBL 5.7) AND WL184 ON THE AFT SIDE OF THE BULKHEAD -  CRACK LENGTH 9.525 MM (0.37	5 INCH).   2.  CRACK LOCATED IN THE RT SIDE CHORD RADIUS AT WL 207 ABOVE AND  BELOW FLOOR LEVEL - CRACK LENGTH 31.75 MM 	(1.25 INCH) FOUND DURING EDDY CURRENT INSPECTION IAW ER B73-53-10-39D.			2	L	7	2 	4F			RT	A16WE   					 
1999070900046	19990709	00046	SW  	1999	7	9	AU990487         	1	19990414	G	5320	2060312012915	FITTING         			BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					FUSELAGE	MISREPAIRTED    	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) CENTER BOX SECTION STIFFENER AND FITTING INCORRECTLY REPAIRED.  REPAIR DID NOT COMPLY WITH THE REPAIR SCHEME STATE	D IN BELL 206 STRUCTURAL REPAIR MANUAL.  UNAPPROVED REPAIR.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999070900047	19990709	00047	NM  	1999	7	9	AU990489         	1	19990415	G	5700		STRUCTURE       			BOEING	737   	737377      		NM  										WING	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AIRCRAFT SUFFERED HAIL DAMAGE IN THE FOLLOWING LOCATIONS:  1.  LT AILERON AND LT AND RT AILERON TAB.   2.  LT AND 	RT ELEVATOR.   3.  SPOILERS.   4. RUDDER.					2	L	7	2 	4F			RT	A16WE   					 
1999070900048	19990709	00048	EU  	1999	7	9	AU990490         	1	19990527	G	3030	E370405	SENSOR          			BAG   	BAE146	BAE146300A  	1500267	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					PITOT/STATIC	FAULTY          	H				O				OTHER                   				J			WARNING INDICATION        			CR	CRUISE         	1			AU	S 										(AUS) RT PITOT HEAT UNDERCURRENT SENSOR FAULTY.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999070900049	19990709	00049	EU  	1999	7	9	AU990491         	1	19990523	G	5700		STRUCTURE       			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					WING	MISREPAIRED     	H				O				OTHER                   				W			INADEQUATE Q C            			NR	NOT REPORTED   	1			AU	S 										(AUS) STEEL SCREWS USED IN THE LEADING EDGE ADJACENT TO THE COMPASS SYSTEM FLUX VALVE.   A STEEL SCRIBER WAS ALSO FOUND 	IN THE CHANNEL ADJACENT TO THE FLUX VALVE.  THE STEEL ITEMS PREVENTED THE NR 2 COMPASS SYSTEM FROM CORRECT OPERATION.  U	NAPPROVED PART.  FOD.				2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999070900050	19990709	00050	EU  	1999	7	9	AU990492         	1	19990523	G	2722		ACTUATOR        			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					RUDDER	FAULTY          	H				C				ABORTED TAKEOFF         				F	J		FLT CONT AFFECTED         	WARNING INDICATION        		TO	TAKEOFF        	1			AU	S 										(AUS) RUDDER SERVO CONTROL/ACTUATOR FAULTY.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999070900051	19990709	00051	GL  	1999	7	9	AU990493         	2	19990506	G	7210	406340104101	SEAL            			BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE GEARBOX	DAMAGED         	H				O				OTHER                   				E	K		VIBRATION/BUFFET          	FLUID LOSS                		CR	CRUISE         	1			AU	S 					CAG36047		CAE832194			(AUS) ENGINE ACCESSORY GEARBOX REAR DOUBLE LIP SEAL FAULTY.  INVESTIGATION FOUND THE SEALING LIP TORN.  THE GEARBOX HAD 	BEEN RECENTLY REPAIRED AND IT IS SUSPECTED THAT THE SEAL WAS DAMAGED DUE TO INCORRECT INSTALLATION.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999070900052	19990709	00052	NM  	1999	7	9	AU990494         	1	19990524	G	2910	A22535	COVER           		NAS1611029  	BOEING	767   	767277      		NM  	GE    	CF6   	CF680A      	30025	NE  					HYDRAULIC SYSTEM	CRACKED         	H				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			AU	S 					0038					(AUS) RT LATERAL CENTRAL CONTROL ACTUATOR FILTER COVER `O' RING SEAL DISPLACED.  LOSS OF CENTER HYDRAULIC SYSTEM FLUID. 	 INVESTIGATION FOUND THAT THE FILTER COVER CONTAINED A CIRCUMFERENTIAL CRACK INTHE THREADED PORTION EXPOSING THE SEAL TO	 HYDRAULIC PRESSURE WHICH THEN LED TO THE FAILURE OF THE `O' RING SEAL P/N NAS1611029.				2	L	7	2 	4F	4	F	RT	A1NM    	E13NE				 
1999070900053	19990709	00053	NM  	1999	7	9	AU990495         	1	19990519	G	3030		WIRE            			DHAV  	DHC8  	DHC8103     	1386005	NM  	PWA   	PW121 	PW121       	52124	NE  					PITOT/STATIC	WORN            	H				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			AU	S 										(AUS) RT PITOT HEATER WIRE CHAFED.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999070900054	19990709	00054	SO  	1999	7	9	AU990496         	1	19990523	G	3213		AXLE            			PIPER 	PA28  	PA28140     	7102802	SO  	LYC   	O320  	O320E3D     	41508	EA  	SNSNCH	74DM	M74DM       	EA  	MLG	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LANDING GEAR STUB AXLE DAMAGED.  SUSPECT HEAVY LANDING.  LIMITED INFORMATION PROVIDED.						1	L	7	1 	3O	3	O		2A13    	E274	5	N	P88614	 
1999070900055	19990709	00055	SO  	1999	7	9	AU990497         	2	19990424	G	8540	641368	BEARING         			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	RT ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					PARTNO642083		555873			(AUS) RT ENGINE NR 1, NR 2 AND NR 3 CONNECTING ROD BIG END BEARINGS WORN.  INVESTIGATION FOUND THE STARTER ADAPTER WORM 	GEAR NEEDLE ROLLER BEARING HAD FAILED CONTAMINATING THE OIL SYSTEM AND PARTIALLY BLOCKING OIL SUPPLY TO THE CONNECTING R	OD BIG END BEARINGS.				1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22EA	 
1999070900056	19990709	00056	CE  	1999	7	9	AU990498         	1	19990526	G	5312		BULKHEAD        			CESSNA	172   	172P        	2072436	CE  						MCAULY	1C160	1C160DTM    	GL  	FUSELAGE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AFT LOWER DOORPOST BULKHEAD CRACKED ON BOTH SIDES. CRACK LENGTH 19.05 MM (0.75 INCH).						1	H	7	1 	3O			NT	3A12    		5	N	P910	 
1999070900057	19990709	00057	SW  	1999	7	9	AU990499         	1	19990522	G	2130		CONTROLLER      			FRCHLD	SA227 	SA227DC     	3377521	SW  						MCAULY	4HFR34	4HFR34C652  	NE  	CABIN PRESSURE	FAULTY          	H				O				OTHER                   				J			WARNING INDICATION        			CR	CRUISE         	1			AU	S 										(AUS) PRESSURIZATION SYSTEM CONTROLS SEIZED.  SUSPECT CAUSED BY ICING OF THE CONTROLS.  DURING INVESTIGATION, A LINE TO 	THE HORIZONTAL STABILIZER DE-ICE BOOTS WAS FOUND TO BE DISCONNECTED.					2	L	7	2 	4T			RT	A18SW   		6	C	3PNE	 
1999070900058	19990709	00058	NE  	1999	7	9	AU990500         	2	19990520	G	7321	87043354	PLUG            	HAMSTD      	7918094004  						PWA   	PWA120	PW125B      		NE  					FUEL CONTROL	CONTAMINATED    	H				O				OTHER                   				E			VIBRATION/BUFFET          			CL	CLIMB          	1			AU	S 					87043354		124019			(AUS) LT ENGINE ELECTRONIC CONTROL TORQUE SENSOR PLUGS CONTAMINATED.											4	T			E20NE				 
1999070900059	19990709	00059		1999	7	9	AU990501         	1	19990307	G	5751		BRACKET         			AMTR  		MUSTANG2    								HARTZL		HCC2YK1     		AILERON	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AILERON MASS BALANCE ATTACHMENT BRACKET CRACKED.									0 										 
1999070900060	19990709	00060	NM  	1999	7	9	AU990502         	1	19990423	G	5312		BULKHEAD        			BOEING	737   	737377      		NM  										FUSELAGE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING LOCATIONS:  1.  VERTICAL CHORD AT LBL 5.7 WL 184 - CRACK LENGTH	 35 MM (1.377 INCH) IN INBOARD RADIUS AND 14 MM (0.551 INCH) IN OUTBOARD RADIUS.  2.  WEB ON FORWARD FACE AT WL 218 LOCA	TED 90 MM (3.543 INCH) OUTBOARD  OF RBL 5.5.  CRACK LENGTH 6 MM (0.236 INCH).  3.  RT SIDE CHORD RADIUS AT WL 207 - CRAC	K LENGTH 16 MM (0.629 INCH ).  FOUND DURING ULTRASONIC AND EDDY CURRENT INSPECTION.			2	L	7	2 	4F			RT	A16WE   					 
1999070900061	19990709	00061	SO  	1999	7	9	AU990503         	2	19990503	G	8530		CYLINDER        			CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	3A32C	D3A32C90    	GL  	ENGINE	CRACKED         	H				O				OTHER                   				E			VIBRATION/BUFFET          			CR	CRUISE         	1			AU	S 							572674			(AUS) NR 6 CYLINDER HEAD SEPARATED FROM THE CYLINDER BARREL. THE HEAD CRACKED FROM THE FORWARD SIDE AND PROGRESSED RAPID	LY AROUND AND THROUGH THE BOTTOM SPARK PLUG HOLE.   A COMPRESSION LEAK CHECK HAD BEEN CARRIED OUT DURING THE 100 HOUR IN	SPECTION APPROXIMATELY ONE WEEK PREVIOUSLY WITH NO SIGN OF CRACKING OR LEAKAGE.  THE CYLINDER WAS A CHROMED ITEM.				1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P21EA	 
1999070900062	19990709	00062	EU  	1999	7	9	AU990504         	1	19990519	G	7603	MTC100JH2P22	PLUG            		P2B18       	SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT75A2      	30030	NE  					POWER LEVER	FAULTY          	H				O				OTHER                   				F			FLT CONT AFFECTED         			LD	LANDING        	1			AU	S 										(AUS) PLUG P2B18 FAULTY.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE6				 
1999070900063	19990709	00063	NM  	1999	7	9	AU990506         	1	19990421	G	5311		FRAME           			BOEING	737   	737377      		NM  										BS 639	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LT FUSELAGE FRAME INNER CHORD LOCATED AT STS 639 CRACKED DOWNWARDS FROM THE LOWER FASTENER HOLE.   FOUND DURING ED	DY CURRENT INSPECTION.					2	L	7	2 	4F			RT	A16WE   					 
1999070900064	19990709	00064	EU  	1999	7	9	AU990507         	1	19990524	G	5610	7256100502	WINDSHIELD      			SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT75A2      	30030	NE  	ROTOL	R354	R3544123F13 	NE  	COCKPIT	CRACKED         	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) RT FRONT WINDSHIELD CRACKED.   WINDSHIELD HEATING WAS `ON'.  OAT WAS 11 DEGREES AND RAINING.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE6	6	C	P61GL	 
1999070900065	19990709	00065		1999	7	9	AU990508         	4	19990526	G	3418	18617	LIFT DETECTOR   																	STALL WARNING	FAULTY          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					15530					(AUS) LIFT DETECTORS SUPPLIED FROM OVERHAUL FACILITY WERE INCORRECTLY SPRUNG.  MANUFACTURING ERROR.																			 
1999070900066	19990709	00066	SO  	1999	7	9	AU990509         	2	19990528	G	8520	649985	CRANKSHAFT      			CESSNA	402   	402B        	207590P	CE  	CONT  	O520  	TSIO520E    	17040	SO  	MCAULY	3AF32C	3AF32C87    	GL  	ENGINE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							812613R			(AUS) RT ENGINE CRANKSHAFT CRACKED IN THE AREA OF THE COUNTERWEIGHT BUSHING.  FOUND DURING ULTRASONIC INSPECTION IAW TCM	 CSB99-3A AND AD/CON/79.					1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22EA	 
1999070900067	19990709	00067	CE  	1999	7	9	AU990510         	1	19990530	G	2913	AN8156	FITTING         		99103541    	CESSNA	441   	441         	2076020	CE  						HARTZL	HCB3T	HCB3TN5     	GL  	HYDRAULIC PUMP	WORN            	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AU	S 					541					(AUS) LT ENGINE DRIVEN HYDRAULIC PUMP PRESSURE LINE FITTING TO FLEXIBLE HOSE ASSEMBLY WORN AND DAMAGED ON THE FLARE.  HY	DRAULIC FLUID LEAKING FROM THE FITTING.					1	L	7	2 	3T			RT	A28CE   		6	C	P15EA	 
1999070900068	19990709	00068	SO  	1999	7	9	AU990511         	2	19990428	G	8530	646985	SEAL            	CONT        	IO520L      	CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520L      	17032	SO  	MCAULY	3A32C	D3A32C88    	GL  	ENGINE	MISSING         	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 					291130R		291130R			(AUS) ALL INLET VALVE SEALS MISSING.  OIL LEAKING FROM MANIFOLD DRAINS.  THE ENGINE WAS COMPLETING GROUND RUNS FOLLOWING	 INSTALLATION OF AN OVERHAULED ENGINE.  SEVERAL OTHER DEFECTS WERE FOUND DURING THE INVESTIGATION OF THE OIL LEAKAGE.  T	HESE DEFECTS WERE:  1.  THE TOP SUPPORT BRACKET FOR THE THROTTLE BODY WAS AN INCORRECT TYPE.   2.  OIL PRESSURE OUTLET U	NION AND ELBOW MISSING FROM CASE - NO  BLANK WAS LEFT IN THE HOLE FOR THE UNION FITTING.   3.  INCORRECT TYPE OF SUMP FI	TTED.  UNAPPROVED PART.		1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P21EA	 
1999070900069	19990709	00069	EU  	1999	7	9	AU990512         	1	19990528	G	2760		WARNING SYSTEM  			BAG   	BAE146	BAE146100A  	1500260	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					DRAG CONTROL SYS	ILLUMINATED     	H				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			AU	S 										(AUS) MANUAL SPOILER FAULT LIGHT ILLUMINATED.  INVESTIGATION COULD FIND NO DEFECT.  PCB CHX6 RE-RACKED.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999070900070	19990709	00070		1999	7	9	AU990513         	1	19990527	G	6123	C5328	SPRING          	MCAULY      	4HFR34C653  											MCAULY	4HFR34	4HFR34C653  	NE  	PROPELLER	MISINSTALLED    	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 					881158					(AUS) FEATHERING SPRING WAS THE INCORRECT LENGTH.  THE SPRING FITTED WAS 13.8125 INCH (350.837 MESM) WITH THE CORRECT LE	NGTH AS SPECIFIED IN THE OVERHAUL MANUAL BEING 12.265 INCH (311.531 MES).  INVESTIGATION FOUND THAT THE SPRINGS WERE THE	 CORRECT P/N C5328 AS SUPPLIED BY THE MANUFACTURER.  THE SPRING IN A RECENTLY ASSEMBLED SPARE PROPELLER WAS ALSO CHECKED	 AND FOUND TO BE THE INCORRECT LENGTH.													6	C	3PNE	 
1999070900071	19990709	00071	NM  	1999	7	9	AU990514         	1	19990410	G	5753	65B020225	TRACK           			BOEING	747   	747312      	1384932	NM  										TE FLAP	FRACTURED       	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RT INBOARD FORE FLAP CENTER BANANA FITTING BROKEN AND PROTRUDING THROUGH FLAP.  SUSPECT CAUSED BY FRACTURE OF THE 	CENTER PROGRAMMING TRACK.					2	L	7	4 	4F			RT	A20WE   					 
1999070900072	19990709	00072	SO  	1999	7	9	AU990515         	1	19990520	G	5751	U4188100	HINGE           			PIPER 	PA25  	PA25235     	7102504	SO  	LYC   	O540  	O540H2A5    	41532	EA  	MCAULY	1A200	1A200FA     	GL  	AILERON	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AILERON AND FLAP HINGES CORRODED.  AIRCRAFT HAD BEEN USED FOR CROP DUSTING.						1	L	7	1 	3O	3	O		2A10    	E295	5	N	P874	 
1999070900073	19990709	00073	EU  	1999	7	9	AU990516         	1	19990510	G	5753	6191	BRACKET         			PARTEN	P68   	P68B        		EU  	LYC   	O360  	IO360A1B6   	41514	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	TE FLAP	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RT WING FLAP BRACKET CORRODED.						1	H	7	2 	3O	3	O		A31EU   	1E10	5	C	P920	 
1999070900074	19990709	00074	SW  	1999	7	9	AU990517         	1	19990527	G	5511		RIB             			AIRTRC	AT500 	AT502       	0390303	SW  	PWA   	PT6   	PT6A15AG    	52043	NE  	HARTZL	HCB3T	HCB3TN3     	GL  	HORIZONTAL STAB	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) HORIZONTAL STABILIZER NOSE RIBS CRACKED AT THE FORWARD EDGE ALONG THE FLANGE RADIUS.						1	L	7	1 	3T	4	T	NC	A9SW    	E4EA	6	C	P15EA	 
1999070900075	19990709	00075		1999	7	9	AU990518         	4	19990603	G	2562	MN1300	BATTERY         	ACK         	E01         	BEECH 	58    	58          	1152740	CE  						MCAULY	3AF32C	3AF32C512   	GL  	ELT	LEAKING         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AU	S 										(AUS) ELT BATTERY LEAKING CAUSING CORROSION ON THE BATTERY CASE.  THE BATTERY WAS LEAKING ALONG A DETERIORATED `POWER CH	ECK STRIP'P.  THE BATTERIES WERE FITTED ON THE 15TH SEPTEMBER 1998 WITH A BEST IF INSTALLED BEFORE JANUARY 2002 DATE.					1	L	7	2 	3O				3A16    		5	C	P22EA	 
1999070900076	19990709	00076	CE  	1999	7	9	AU990519         	1	19990413	G	3320	1013800841	LIGHT           			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A42      	52043	NE  	HARTZL	HCB3T	HCB3TN3     	GL  	CABIN	OVERHEAT        	H				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			AU	S 										(AUS) WINDOW FLUORESCENT LIGHT TRANSFORMER OVERHEATED CAUSING THE VELCRO ATTACHMENT TOUCHING THE TRANSFORMER TO MELT.  S	USPECT VELCRO INCORRECTLY FITTED.					1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15EA	 
1999070900077	19990709	00077	EU  	1999	7	9	AU990520         	1	19990602	G	5711	BN2A20	SPAR            			BNORM 	BN2   	BN2A20      	1520220	EU  	LYC   	O540  	IO540K1B5   	41532	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	WING	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WING MAIN SPAR CRACKED IN TWO PLACES ON THE LT SIDE AND IN THREE PLACES ON THE RT SIDE IN THE AREA COVERED BY AD/B	N2/62 AND SB BN2/SB237.  THE AIRCRAFT STILL HAD 111 CYCLES TO RUN BEFORE THE NEXT AD INSPECTION WAS DUE.					1	H	7	2 	3O	3	O		A17EU   	1E4	5	C	P920	 
1999070900078	19990709	00078	SO  	1999	7	9	AU990521         	2	19990522	G	8530	TM649317	CYLINDER        	CONT        	TSIO520K    	CESSNA	340   	340CESSNA   	2076404	CE  	CONT  	O520  	TSIO520K    	17040	SO  	MCAULY	3AF32C	3AF32C93    	GL  	ENGINE	SEPARATED       	H				O				OTHER                   				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		NR	NOT REPORTED   	1			AU	S 			1200 				21787173K			(AUS) LT ENGINE NR 1 CYLINDER HEAD SEPARATED FROM THE CYLINDER BARREL.  METAL CONTAMINATION OF OIL SYSTEM.						1	L	7	2 	3O	3	O		3A25    	E8CE	5	C	P22EA	 
1999070900079	19990709	00079		1999	7	9	AU990522         	4	19990526	G	6122	P70211	GOVERNOR        			FRCHLD	SA227 	SA227DC     	3377521	SW  						MCAULY	4HFR34	4HFR34C652  	NE  	PROPELLER	OUT OF ADJUST   	H				C				ABORTED TAKEOFF         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		TO	TAKEOFF        	1			AU	S 					P70211					(AUS) LT ENGINE PROPELLER GOVERNOR OUT OF ADJUSTMENT.   GOVERNOR WAS INTERFERING WITH THE OPERATION OF THE FCU.						2	L	7	2 	4T			RT	A18SW   		6	C	3PNE	 
1999070900080	19990709	00080	EU  	1999	7	9	AU990524         	1	19990528	G	2760		SPOILER         			BAG   	BAE146	BAE146100A  	1500260	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					DRAG CONTROL SYS	FAULTY          	H				A				UNSCHED LANDING         				F	N		FLT CONT AFFECTED         	FALSE WARNING             		CL	CLIMB          	1			AU	S 										(AUS) MANUAL SPOILER CAUTION LIGHT ILLUMINATED AFTER TAKEOFF.  THE FAULT WAS UNABLE TO BE REPRODUCED ON THE GROUND AND T	HE AIRCRAFT HAS SINCE FLOWN SERVICEABLE.  DEFECT NOT CONFIRMED.					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999070900081	19990709	00081	NM  	1999	7	9	AU990526         	1	19990522	G	2910	DSC252B60150	HOSE            			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					LT MLG	FAILED          	H				O				OTHER                   				K			FLUID LOSS                			AP	APPROACH       	1			AU	S 										(AUS) LT MAIN LANDING GEAR DOWN HOSE RUPTURED.  LOSS OF FLUID FROM NR 2 HYDRAULIC SYSTEM.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999070900082	19990709	00082	NM  	1999	7	9	AU990527         	1	19990423	G	5313		STRINGER        			BOEING	737   	737377      		NM  										BS 727	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) STRINGER 18A WEB LOCATED AT BS 727 CRACKED FROM THE LT AND RT SIDE AFT INBOARD FASTENER HOLES.  FOUND DURING EDDY 	CURRENT INSPECTION.					2	L	7	2 	4F			RT	A16WE   					 
1999070900083	19990709	00083	NM  	1999	7	9	AU990528         	1	19990112	G	5311		FRAME           			BOEING	737   	737377      		NM  										BS 842	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE FRAME LOCATED IN THE AFT CARGO COMPARTMENT AT BS 842 RT SEVERELY CORRODED BETWEEN STRINGERS S25R AND S26R	 AT AFT CARGO DOOR APERTURE.					2	L	7	2 	4F			RT	A16WE   					 
1999070900084	19990709	00084	NE  	1999	7	9	AU990529         	1	19990530	G	7921	5F224000	GASKET          			SKRSKY	S76   	S76A        	8143006	NE  	TMECA 	ARRIEL	ARRIEL1S    	60030	NE  					OIL COOLER	LEAKING         	H				A				UNSCHED LANDING         				E	K	J	VIBRATION/BUFFET          	FLUID LOSS                	WARNING INDICATION        	CR	CRUISE         	1			AU	S 							15069			(AUS) RT OIL COOLER TO OIL TANK GASKET LEAKING.  OIL COOLER AND GASKET HAD BEEN REPLACED PRIOR TO THE FLIGHT.  GROUND RU	NS HAD FOUND NO EVIDENCE OF LEAKAGE.					1	G	7	2 	3U	3	U		H1NE    	E19EU				 
1999070900085	19990709	00085	EU  	1999	7	9	AU990531         	1	19990524	G	5610	7256100502	WINDSHIELD      			SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT75A2      	30030	NE  	ROTOL	R354	R3544123F13 	NE  	COCKPIT	CRACKED         	H				O				OTHER                   				O			OTHER                     			DE	DESCENT        	1			AU	S 										(AUS) RT WINDSHIELD CRACKED AND DELAMINATED.  SUSPECT CAUSED BY CONTINUAL USE OF WINDSHIELD HEATING.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE6	6	C	P61GL	 
1999070900086	19990709	00086	EU  	1999	7	9	AU990532         	1	19990601	G	2620		FIRE EXTING     			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NR 2 ENGINE	MISINSTALLED    	H				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) NR 2 ENGINE OUTBOARD FIRE EXTINGUISHER INCORRECTLY WIRED.   WIRING FROM FIRE HANDLE SWITCH TO FIRE BOTTLE WAS FOUN	D TO BE CONNECTED TO THE SIGNAL CONDITIONING PCB.					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999070900087	19990709	00087	EU  	1999	7	9	AU990533         	1	19990601	G	2751		WARNING LIGHT   			BAG   	BAE146	BAE146300A  	1500267	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					TE FLAP	ILLUMINATED     	H				A				UNSCHED LANDING         				F	N		FLT CONT AFFECTED         	FALSE WARNING             		CR	CRUISE         	1			AU	S 										(AUS) FLAP FAULT LIGHT ILLUMINATED.  NIL FAULT FOUND AND FLAP COMPUTER RESET.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999070900088	19990709	00088	EA  	1999	7	9	AU990534         	2	19990412	G	8520	LW18837	CAMSHAFT        	LYC         	O320E2D     	CESSNA	172   	172M        	2072418	CE  	LYC   	O320  	O320E2D     	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	ENGINE	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1666 		RL3621127A		RL3621127A			(AUS) CAMSHAFT REAR LOBE WORN EXTENSIVELY.						1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
1999070900089	19990709	00089	EU  	1999	7	9	AU990535         	1	19990601	G	2751		WARNING LIGHT   			BAG   	BAE146	BAE146300A  	1500267	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					TE FLAP	ILLUMINATED     	H				A				UNSCHED LANDING         				F	N		FLT CONT AFFECTED         	FALSE WARNING             		CL	CLIMB          	1			AU	S 										(AUS) FLAP FAULT INDICATION.  FLAP COMPUTER RERACKED AND CIRCUIT BREAKERS RESET.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999070900090	19990709	00090		1999	7	9	AU990536         	1	19990604	G	3213	33050239	PINTLE          			AMTR  		SPITFIRE    												MLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) MAIN LANDING GEAR PINTLE CRACKED.  PART WAS A USED ITEM AND WAS BEING NDT INSPECTED BEFORE FITMENT.									0 										 
1999070900091	19990709	00091	EU  	1999	7	9	AU990537         	1	19990309	G	3320	HC252B2173015	PANEL           			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					CABIN	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) CABIN ROOF LIGHTING REFLECTOR PANELS SHOWED EVIDENCE OF HEAT DAMAGE RANGING FROM MINOR DISCOLORATION TO BLACK CHAR	 LIKE DEPOSITS AT THE FLUORESCENT TUBE FITTINGS.  THE TUBE END FITTINGS HAD BECOME BRITTLE.					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999070900092	19990709	00092	CE  	1999	7	9	AU990538         	1	19990521	G	7921	8406F	OIL COOLER      			CESSNA	172   	172RG       	2072438	CE  	LYC   	O360  	O360F1A6    	41514	EA  	MCAULY	2D34C	B2D34C220   	GL  	ENGINE	LEAKING         	H				A				UNSCHED LANDING         				E	K		VIBRATION/BUFFET          	FLUID LOSS                		CR	CRUISE         	1			AU	S 							L2854036A			(AUS) ENGINE OIL COOLER LEAKING FROM THE CORE ADJACENT TO THE UPPER FITTING BOSS.  THE BOSS WAS SLIGHTLY DISTORTED.   TH	E COOLER WAS A REPAIRED ITEM AND HAD BEEN INSTALLED FOR APPROXIMATELY 1.5 HOURS.  THE ITEM HAD BEEN IN STORAGE IN EXCESS	 OF FIFTEEN YEARS.				1	H	7	1 	3O	3	O		3A17    	E286	5	C	P7EA	 
1999070900093	19990709	00093	CE  	1999	7	9	AU990539         	1	19990522	G	2822	476411	PUMP            			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  					BOOST PUMP	SEIZED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELECTRIC FUEL PUMPS FAULTY.  SUSPECT CONTACTS IN PUMPS ARE WELDING TOGETHER GIVING A LIMITED LIFE.						1	L	7	2 	3O	3	O		3A10    	E5CE				 
1999070900094	19990709	00094	NE  	1999	7	9	AU990540         	2	19990608	G	7200		ENGINE          			STBROS	SD3   	SD360       	8100606	EU  	PWA   	PT6   	PT6A67R     	52043	NE  	HARTZL	HCA6A	HCA6A3      	NE  	LEFT	FAILED          	H				A				UNSCHED LANDING         				E	X	J	VIBRATION/BUFFET          	ENGINE FLAMEOUT           	WARNING INDICATION        	CL	CLIMB          	1			AU	S 							106223			(AUS) LT ENGINE FAILURE.  SUSPECT BEARING FAILURE.						2	H	7	2 	4T	4	T		A41EU   	E26NE	6	C	P14NE	 
1999070900095	19990709	00095	NM  	1999	7	9	AU990541         	1	19990602	G	2731		TRIM            			DHAV  	DHC8  	DHC8202     	2809007	NM  										ELEVATOR	JAMMED          	H				A				UNSCHED LANDING         				F			FLT CONT AFFECTED         			CR	CRUISE         	1			AU	S 										(AUS) ELEVATOR TRIM SYSTEM JAMMED.  THE JAMMING FREED ITSELF DURING LANDING.  INVESTIGATION COULD FIND NO FAULTS IN THE 	TRIM SYSTEM.  SYSTEM LUBRICATED AND SYSTEM CHECKED OK THROUGH THE FULL RANGE.					2	H	7	2 	4T			RT	A13NM   					 
1999070900096	19990709	00096	SO  	1999	7	9	AU990542         	1	19990611	G	5743	9536302	BRACKET         	PIPER       	SUPPORT     	PIPER 	PA28  	PA28R180    	7102809	SO  	LYC   	O360  	IO360B1E    	41514	EA  	HARTZL	HCC2Y	HCC2YR1     	GL  	MLG	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) MAIN LANDING GEAR SIDE BRACE BRACKET CORRODED.						1	L	7	1 	3O	3	O		2A13    	1E10	5	C	P920	 
1999070900097	19990709	00097	SO  	1999	7	9	AU990543         	1	19990610	G	5743	AN3209	NUT             	PIPER       	BRACKET     	PIPER 	PA28  	PA28R180    	7102809	SO  	LYC   	O360  	IO360B1E    	41514	EA  	HARTZL	HCC2Y	HCC2YR1     	GL  	LT & RT MLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LT AND RT MAIN LANDING GEAR SIDE BRACKET SUPPORT NUTS CRACKED.  FOUND DURING MAGNETIC PARTICLE INSPECTION.						1	L	7	1 	3O	3	O		2A13    	1E10	5	C	P920	 
1999070900098	19990709	00098	NM  	1999	7	9	AU990544         	1	19990514	G	2612		WARNING LIGHT   			BOEING	737   	737377      		NM  										FIRE DETECTION	ILLUMINATED     	H				A				UNSCHED LANDING         				N			FALSE WARNING             			CR	CRUISE         	1			AU	S 										(AUS) APU FIRE WARNING LIGHT ILLUMINATED.  FIRE BOTTLE DISCHARGED AND WARNING LIGHT EXTINGUISHED.  SEVERAL MINUTES LATER	, THE WARNING LIGHT ACTIVATED AGAIN AND INTERMITTENTLY ACTIVATED FOR THE REMAINDER OF THE FLIGHT.  INVESTIGATION COULD F	IND NO CAUSE FOR THE WARNING LIGHT ACTIVATION.				2	L	7	2 	4F			RT	A16WE   					 
1999070900099	19990709	00099	EU  	1999	7	9	AU990545         	2	19990424	G	7321	365AQ	CIRCUIT BOARD   	TMECA       	ECU         						TMECA 	MAKILA	MAKILA1A    	60040	EU  					FUEL CONTROL	FAULTY          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					365AQ					(AUS) NR 2 ENGINE ELECTRONIC CONTROL UNIT (ECU) CHANNEL SELECTOR PRINTED CIRCUIT BOARD FAULTY.											4	U			E12NE				 
1999070900100	19990709	00100	EA  	1999	7	9	AU990546         	2	19990604	G	8530	60828	PLUG            	LYC         	AE10360B2F  	MUDRY 	10    	CAP10B      		EU  	LYC   	O360  	AEIO360B2F  	41514	EA  	HOFMAN	HO29	HO29HM180   	EU  	ENGINE	WORN            	H				C				ABORTED TAKEOFF         				R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			AU	S 			455  		L2597551A		L2597551A			(AUS) NR 2 CYLINDER PISTON PIN PLUG WORN.  PISTON OIL RING LANDS DAMAGED.   METAL CONTAMINATION OF THE ENGINE OIL SYSTEM	.					1	L	7	1 	3O	3	O		A36EU   	1E10	5	N	P3EU	 
1999070900101	19990709	00101	EA  	1999	7	9	AU990547         	2	19990604	G	8500		ENGINE          			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	LEFT	FIRE            	H				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			AU	S 										(AUS) LT ENGINE FIRE CAUSED BY MAIN ALTERNATOR WIRE TO NOISE FILTER BEING DAMAGED AND IGNITING OIL IN THE COWLING.  DAMA	GE CAUSED TO THE ALTERNATOR WIRE, FILTER BOWL AND TWO HOSES.					1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
1999070900102	19990709	00102		1999	7	9	AU990548         	4	19990604	G	6113		SPINNER         			PIPER 	PA31  	PA31350     	7103110	SO  						HARTZL	HCE3Y	HCE3YR2     	GL  	PROPELLER	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RT PROPELLER SPINNER CRACKED.  ONE SCREW MISSING AND SPINNER SKIN PEELING BACK.   CRACK LENGTH 50.8 MM (2 INCHES).						1	L	7	2 	3O				A20SO   		5	C	P33EA	 
1999070900103	19990709	00103	SO  	1999	7	9	AU990549         	1	19990604	G	3222		LEG             			PIPER 	PA31  	PA31350     	7103110	SO  						HARTZL	HCE3Y	HCE3YR2     	GL  	NLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR LEG CRACKED.   CRACK LENGTH 25.4  MM (1 INCH).						1	L	7	2 	3O				A20SO   		5	C	P33EA	 
1999070900104	19990709	00104	NM  	1999	7	9	AU990550         	1	19990326	G	2530	DPXAMA2633S	CONNECTOR       			BOEING	737   	737377      		NM  										GALLEY OVEN	DAMAGED         	H				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			AU	S 										(AUS) NR 2 OVEN CONNECTOR SOCKETS AND CONTROLLER CONNECTOR PINS HAD ARCING DAMAGE.						2	L	7	2 	4F			RT	A16WE   					 
1999070900105	19990709	00105	NM  	1999	7	9	AU990551         	1	19990326	G	2530	DPXAMA2634P	CONNECTOR       			BOEING	737   	737377      		NM  										GALLEY OVEN	DAMAGED         	H				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			AU	S 										(AUS) NR 2 OVEN CONTROLLER CONNECTOR SOCKET AND PINS HAD ARCING DAMAGE.  SEE ALSO MDR AU990550.						2	L	7	2 	4F			RT	A16WE   					 
1999070900106	19990709	00106	NE  	1999	7	9	AU990552         	2	19990422	G	7321		SENSOR          								GE    	CF6   	CF680C2A5   		NE  					RT ENGINE	FAULTY          	H				A				UNSCHED LANDING         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CL	CLIMB          	1			AU	S 										(AUS) RT ENGINE N1 HYDROMECHANICAL SENSORS (2OFF) FAULTY.											4	F			E13NE				 
1999070900107	19990709	00107	SO  	1999	7	9	AU990553         	1	19990608	G	2750	P1761	PLUG            			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  					TE FLAP	FAULTY          	H				C				ABORTED TAKEOFF         				F			FLT CONT AFFECTED         			TO	TAKEOFF        	1			AU	S 										(AUS) LT OUTBOARD FLAP ACTUATOR PLUG CONTAINED BROKEN WIRES INSIDE THE PLUG BACK SHELL POTTING.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE				 
1999070900108	19990709	00108	NM  	1999	7	9	AU990554         	1	19990613	G	2910	82970010175	PIPE            			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					HYDRAULIC SYSTEM	WORN            	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) HYDRAULIC PIPE WORN THROUGH.   LOSS OF HYDRAULIC PRESSURE TO THE FORWARD LT LANDING GEAR DOOR ACTUATOR ALLOWING TH	E LT LANDING GEAR TO PUSH THE FORWARD DOOR OPEN AND SHEARING THE FORWARD DOOR CONNECTING ROD P/N 83231027-001.  DAMAGE A	LSO TO THE FORWARD LT DRAG LINK FAIRING.				2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999070900109	19990709	00109	NM  	1999	7	9	AU990555         	1	19990527	G	5320		DOOR SILL       			BOEING	737   	737377      		NM  										FUSELAGE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FORWARD SERVICE DOOR SILL LOWER AFT CORNER RADIUS CRACKED FROM EDGE CUTOUT THROUGH A FASTENER AND SCREW HOLE INTO 	ANOTHER FASTENER HOLE.  CRACK LENGTH 69.85 MM (2.75 INCH).					2	L	7	2 	4F			RT	A16WE   					 
1999070900110	19990709	00110	NM  	1999	7	9	AU990556         	1	19990609	G	2910	82950010271	PIPE            			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					HYDRAULIC SYSTEM	CRACKED         	H				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			AU	S 										(AUS) LT WING INBOARD ROLL SPOILER HYDRAULIC PIPE CRACKED ON A RADIUS.  LOSS OF HYDRAULIC FLUID.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999070900111	19990709	00111	NE  	1999	7	9	AU990557         	2	19990605	G	7320	7918094004	EEC             								PWA   	PWA120	PW125B      		NE  					RT ENGINE	FAULTY          	H				A				UNSCHED LANDING         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CR	CRUISE         	1			AU	S 					7043354		124076			(AUS) RT ENGINE ELECTRONIC CONTROL UNIT FAILED.											4	T			E20NE				 
1999070900112	19990709	00112	SW  	1999	7	9	AU990559         	1	19990601	G	2910	2781032135	PIPE            			FRCHLD	SA227 	SA227DC     	3377521	SW  						MCAULY	4HFR34	4HFR34C652  	NE  	HYDRAULIC SYSTEM	FAILED          	H				A				UNSCHED LANDING         				K			FLUID LOSS                			CL	CLIMB          	1			AU	S 										(AUS) FLAPS UP HYDRAULIC PRESSURE PIPE FAILED.  LOSS OF HYDRAULIC FLUID.						2	L	7	2 	4T			RT	A18SW   		6	C	3PNE	 
1999070900113	19990709	00113	NM  	1999	7	9	AU990560         	1	19990518	G	2751	W474230224B	WIRE            			BOEING	747   	747438      	       	NM  										TE FLAP	SHORTED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) TE FLAP POSITION WIRING LOCATED IN THE FORWARD CARGO HOLD CEILING ADJACENT TO STA 690 HAD SHORTED TO GROUND.						2	L	7	4 	4F			RT	A20WE   					 
1999070900114	19990709	00114	NM  	1999	7	9	AU990561         	1	19990409	G	2897	07881590	WIRE            		60B890049   	BOEING	747   	747312      	1384932	NM  										BOOST PUMP	FAULTY          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					07881590					(AUS) NR 2 MAIN AFT BOOST PUMP WIRING INSULATION FAULTY.						2	L	7	4 	4F			RT	A20WE   					 
1999070900115	19990709	00115	EU  	1999	7	9	AU990562         	1	19990318	G	5210	A5211079000251	CASING          			AIRBUS	320   	A320212     		EU  										PASSENGER DOOR	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) L1 DOOR LOCK UNIT CASING CRACKED BETWEEN A HOOK PIVOT BOLT HOLE AND THE CASING EDGE.						2	L	7	2 	4F			RT	A28NM   					 
1999070900116	19990709	00116	SO  	1999	7	9	AU990563         	1	19990603	G	3231	12012347001003	HANDLE          			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  					LT MLG	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LT MAIN LANDING GEAR OUTBOARD DOOR HANDLE WORN.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE				 
1999070900117	19990709	00117	NE  	1999	7	9	AU990564         	2	19990604	G	7200	0292005250	ENGINE          			SKRSKY	S76   	S76C        	8143008	NE  	TMECA 	ARRIEL	ARRIEL1S    	60030	NE  					NR 1	MAKING METAL    	H				A				UNSCHED LANDING         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CR	CRUISE         	1			AU	S 							15085			(AUS) NR 1 ENGINE REAR BEARING CHIP DETECTOR CONTAMINATED WITH METAL CHIPS.  ENGINE REMOVED.  SUSPECT BEARING FAILURE.						1	G	7	2 	3U	3	U	NC	H1NE    	E19EU				 
1999070900118	19990709	00118		1999	7	9	AU990565         	4	19990604	G	3444	9650476088	COMPUTER        			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  					E/E BAY	MALFUNCTIONED   	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) GROUND PROXIMITY WARNING SYSTEM (GPWS) COMPUTER INTERMITTENT IN OPERATION.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE				 
1999070900119	19990709	00119	EU  	1999	7	9	AU990566         	1	19990608	G	5610	7256100502	WINDSHIELD      			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R375	R3754123F21 	NE  	COCKPIT	DELAMINATED     	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RT WINDSHIELD CRACKED ACROSS THE TOP CORNER OF THE OUTER PANE.  SUSPECT CAUSED BY THERMAL STRESS.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P17NE	 
1999070900120	19990709	00120	SO  	1999	7	9	AU990567         	2	19990409	G	8520	459221	CRANKSHAFT      	CONT        	O470R       						CONT  	O470  	O470R       	17026	SO  					ENGINE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					459221		459221			(AUS) CRANKSHAFT CRACKED IN TWO PLACES FROM THE CRANK GEAR DOWEL HOLE.  CRANKCASE MAIN TUNNEL MEASUREMENTS OUT OF LIMITS	.   CAMSHAFT LOBES BREAKING UP.										3	O			E273				 
1999070900121	19990709	00121	SO  	1999	7	9	AU990568         	2	19990521	G	8520	551451	CRANKSHAFT      	CONT        	TSIO520E    						CONT  	O520  	TSIO520E    	17040	SO  					ENGINE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					551451					(AUS) CRANKSHAFT CRACKED FROM CRANK GEAR DOWEL.  CRANKCASE TUNNEL MEASUREMENTS OUT OF LIMITS.											3	O			E8CE				 
1999070900122	19990709	00122	EA  	1999	7	9	AU990569         	2	19990508	G	8550		ENGINE          			PARTEN	P68   	P68B        		EU  	LYC   	O360  	IO360A1B6   	41514	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	OIL SYSTEM	OVERSERVICED    	H				C				ABORTED TAKEOFF         				B			SMOKE/FUMES/ODORS/SPARKS  			TO	TAKEOFF        	1			AU	S 										(AUS) SMOKE IN COCKPIT.  INVESTIGATION FOUND A SMALL QUANTITY OF OIL AROUND THE MUFFLER SHROUD.  SUSPECT OIL HAD BEEN SP	ILT DURING ENGINE OIL TOP UP.					1	H	7	2 	3O	3	O		A31EU   	1E10	5	C	P920	 
1999070900123	19990709	00123	CE  	1999	7	9	AU990570         	1	19990610	G	7120	96910023	BOLT            			BEECH 	58    	58          	1152740	CE  	CONT  	O520  	IO520C      	17032	SO  	HARTZL	HCJ2Y	BHCJ2YF2    	GL  	ENGINE MOUNT	BROKEN          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							299016R	DZ403		(AUS) ENGINE MOUNT BOLT BROKEN.						1	L	7	2 	3O	3	O		3A16    	E5CE	5	C	P37EA	 
1999070900124	19990709	00124	CE  	1999	7	9	AU990571         	1	19990608	G	3222	1018200741	SHOCK ABSORBER  			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A42      	52043	NE  	HARTZL	HCB3T	HCB3TN3     	GL  	NLG	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			16   							(AUS) NOSE LANDING GEAR SHOCK ABSORBER CRACKED.  FOUND DURING INSPECTION IAW AD/BEECH200/45 AMDT2 (BEECH SB 2102 REV III	).					1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15EA	 
1999070900125	19990709	00125	NE  	1999	7	9	AU990572         	2	19990601	G	7200	115093	ENGINE          	PWA         	PW118A      	EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  	HAMSTD	14RF	14RF9       	NE  	RIGHT	FAILED          	H				A				UNSCHED LANDING         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CR	CRUISE         	1			AU	S 					115093		115093			(AUS) RT ENGINE FAILED.   INVESTIGATION FOUND METAL ON THE REDUCTIONG GEARBOX CHIP DETECTOR.  THE REDUCTION GEARBOX WAS 	FOUND TO BE UNCOUPLED FROM THE POWER TURBINE.  ALL POWER TURBINE BLADES MISSING.  LOW PRESSURE COMPRESSOR JAMMED.  TORQU	E SENSOR DAMAGED.  TORQUE SHAFT DAMAGED.   FRONT AIR INLET CASE CRACKED AND DAMAGED.  MINOR DAMAGE TO EXHAUST DUCT FROM 	EXITING TURBINE BLADES.			2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	C	P11NE	 
1999070900126	19990709	00126	EU  	1999	7	9	AU990573         	1	19990616	G	5610		SEAL            			BAC   	146   	AVRO146RJ70A	1500095	EU  										WINDSHIELD	DAMAGED         	H				C				ABORTED TAKEOFF         				O			OTHER                     			TO	TAKEOFF        	1			AU	S 										(AUS) FIRST OFFICER'S `C' WINDSHIELD SEAL DAMAGED.						2	H	7	4 	4F			RT	A49EU   					 
1999070900127	19990709	00127		1999	7	9	AU990574         	4	19990617	G	6122	MWD20E1	DIODE           			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	PROP GOVERNOR	INTERMITTENT    	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LT ENGINE PROPELLER FEATHER VALVE DIODE BLOCK INTERMITTENT IN OPERATION.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
1999070900128	19990709	00128	NM  	1999	7	9	AU990575         	1	19990604	G	2910		PIPE            			DHAV  	DHC8  	DHC8103     	1386005	NM  	PWA   	PW121 	PW121       	52124	NE  					HYDRAULIC SYSTEM	LEAKING         	H				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			AU	S 										(AUS) HYDRAULIC SYSTEM PIPE TO HYDRAULIC ANTI-SKID PRESSURE SYSTEM CHAFED AND LEAKING IN THE LT NACELLE AREA.  THE PIPE 	HAD RECENTLY BEEN FITTED AS PART OF SB 8-29-29 (AD/DHC8/047).					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999070900129	19990709	00129	CE  	1999	7	9	AU990576         	1	19990610	G	7120	57510088	MOUNT           			CESSNA	441   	441         	2076020	CE  	GARRTT	TPE331	TPE3318     	01514	WP  	HARTZL	HCB3T	HCB3TN5     	GL  	LT ENGINE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LT ENGINE MOUNT ASSEMBLY CRACKED.						1	L	7	2 	3T	4	T	RT	A28CE   	E4WE	6	C	P15EA	 
1999070900130	19990709	00130	EA  	1999	7	9	AU990577         	2	19990607	G	8530	60828	PLUG            			MUDRY 	10    	CAP10B      		EU  	LYC   	O360  	AEIO360B2F  	41514	EA  	HOFMAN	HO29	HO29HM180   	EU  	ENGINE	FAILED          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							L2597551A			(AUS) NR 2 PISTON PIN PLUG WORN AWAY.   PLUG HAD WORN INTO THE PISTON OIL RING LAND.  THE ENGINE WAS INSPECTED AND ALL O	THER PISTON PIN PLUGS WERE FOUND WITH VARIOUS DEGREES OF WEAR.  THE ENGINE HAD BEEN FITTED WITH NEW CYLINDER KITS IN APR	IL 1998.				1	L	7	1 	3O	3	O		A36EU   	1E10	5	N	P3EU	 
1999070900131	19990709	00131	GL  	1999	7	9	AU990578         	2	19990623	G	7250	23004540	BLADE           	ALLSN       	TURBINEASSY 	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30      	03013	GL  					TURBINE	DAMAGED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					CAT90220		CAE8900288			(AUS) NR 2 ENGINE FIRST STAGE TURBINE BLADES SEVERELY DAMAGED.						1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999070900132	19990709	00132	EU  	1999	7	9	AU990579         	1	19990619	G	2910	MS21908D6	FITTING         			FOKKER	F27   	F27MK50     		EU  										HYDRAULIC SYSTEM	CRACKED         	H				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AU	S 										(AUS) LT MAIN LANDING GEAR-UP UNION FITTING CRACKED.   LOSS OF HYDRAULIC FLUID.						2	H	7	2 	4T			RT	A817    					 
1999070900133	19990709	00133	EA  	1999	7	9	AU990580         	2	19990618	G	8530	05K21232	CYLINDER        								LYC   	O235  	O235H2C     	41505	EA  	SNSNCH	72C	72CK        	EA  	ENGINE	CRACKED         	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							L2451315			(AUS) NR 3 CYLINDER CRACKED AROUND THE CIRCUMFERENCE OF THE CYLINDER BASE.											3	O			E223	5	N	P9045	 
1999070900134	19990709	00134	EU  	1999	7	9	AU990581         	1	19990616	G	7700	785226	SENSOR          	GE          	CT79B       	SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R375	R3754123F21 	NE  	ENGINE	FAULTY          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					785226					(AUS) LT ENGINE NP SENSOR SUSPECT FAULTY.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P17NE	 
1999070900135	19990709	00135	GL  	1999	7	9	AU990582         	1	19990612	G	7603		SPRING          			AMTR  	COZY  	COZY        	05613R8	GL  										POWER LEVER	BROKEN          	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) THROTTLE OPERATING (RETURN) SPRING BROKEN.						1	M	7	1 	3O			NT	EXPA1M71					 
1999070900136	19990709	00136	CE  	1999	7	9	AU990583         	1	19990617	G	7120		TRUSS           			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  	HARTZL	HCE4A	HCE4A3A     	NE  	ENGINE MOUNT	WORN            	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RT SIDE ENGINE TRUSS INBOARD TUBE WORN BEYOND LIMITS BY TEFLON OIL COOLER HOSE.						2	L	7	2 	4T	4	T	RT	A24CE   	E26NE	5	C	P10NE	 
1999070900137	19990709	00137	NE  	1999	7	9	AU990584         	2	19990618	G	7200		ENGINE          			BOEING	737   	737377      		NM  	GE    	CFM56 	CFM563B1    	13802	NE  					NR 2	MALFUNCTIONED   	H				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 							720904			(AUS) NR 2 ENGINE VIBRATION.  INVESTIGATION FOUND OIL CONTAMINATION IN THE TAILPIPE AND METAL CONTAMINATION OF THE AFT S	UMP CHIP DETECTOR.					2	L	7	2 	4F	4	F	RT	A16WE   	E2GL				 
1999070900138	19990709	00138	CE  	1999	7	9	AU990585         	1	19990515	G	5532	04310045	SKIN            			CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A102	1A102OCM    	GL  	VERTICAL STAB	CORRODED        	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					PNO04310042					(AUS) VERTICAL STABILIZER SKIN CORRODED INTERNALLY.						1	H	7	1 	3O	3	O		3A19    	E252	5	N	P918	 
1999070900139	19990709	00139	SW  	1999	7	9	AU990587         	1	19990613	G	3242	212033	BRAKE           	OZONE       	LHMLG       	SWRNGN	SA227 	SA227AC     	8780603	SW  	GARRTT	TPE331	TPE33111U   	01514	WP  					LT MLG	FAULTY          	H				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			142  		NSN					(AUS) LT MAIN LANDING GEAR BRAKE ASSEMBLY OVERHEATED AND CAUSED PAINT AND GREASE ON THE WHEEL TO CATCH FIRE.  SUSPECT CA	USED BY A PINCHED PISTON SEAL WHICH OCCURRED DURING ASSEMBLY.					2	L	7	2 	4T	4	T	RT	A8SW    	E4WE				 
1999091700032	19990917	00032	EU  	1999	9	17	AU990615         	1	19990701	G	2120	8540153569	DUCT            			FOKKER	F27   	F27MK500    	4990629	EU  						ROTOL	R4304	R1934304    	EU  	AIR DISTRIBUTION	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT CABIN COMPRESSOR AIR DUCT LOCATED BETWEEN THE SILENCER AND THE WING REAR SPAR P/N 8540-153-569 CRACKED AROUND	 THE FLANGE FOR APPROXIMATELY 85 PERCENT OF THE CIRCUMFERENCE.  THE CRACK HAD PENETRATEDTHE FULL DEPTH OF THE FLANGE AND	 EXHIBITED DELAMINATION AND CORROSION OF THE FLANGE MATERIAL.				2	H	7	2 	4T				A817    		6	C	P899	 
1999091700033	19990917	00033	NM  	1999	9	17	AU990673         	1	19990507	G	5312		BULKHEAD        			BOEING	737   	737377      		NM  										FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FWD PRESSURE BULKHEAD FWD AND AFT FACES CRACKED IN FOLLOWING AREAS:  1.  2 CRACKS IN BULKHEAD WEB ON FWD SIDE OF B	ULKHEAD.  A.  ONE CRACK BENEATH HORIZ STRAP IN WEB AT WL 218 OUTBOARD OF RBL 5.7.  CRACK LENGTH 9.525 MM (0.375 INCH).  	B.  CRACK UNDER INBOARD BOTTOM CORNER OF BRACKET AT WL195 AND RBL 5.7.  CRACK LENGTH 15.875 MM (0.625 INCH).  2.  CRACK 	IN RT SIDE INTERCOSTAL AT STN 178 AND RBL 24.  3.  CRACK IN LT VERTICAL CHORD LBL 5.7 OUTBOARD SIDE AT WL184 - CRACK LEN	GTH 15.875 MM (0.625 INCH).  4.  CRACK IN RT SIDE BULKHEAD CHORD JUST ABOVE COCKPIT FLOOR AT WL 207.  CRACK LENGTH APPRO	XIMATELY 15.875 MM (0.625 INCH).  FOUND DURING ULTRASONIC AND EDDY CURRENT INSPS IAW ER B73-53-10-39.	2	L	7	2 	4F			RT	A16WE   					 
1999091700034	19990917	00034	NM  	1999	9	17	AU990674         	1	19990506	G	5311		FRAME           			BOEING	737   	737377      		NM  										BS 616	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE FRAME INNER CHORD LOCATED AT STN 616 LEFT CRACKED IN LOWER FASTENER HOLE AFT FACE.  FOUND DURING EDDY CUR	RENT INSPECTION.					2	L	7	2 	4F			RT	A16WE   					 
1999091700035	19990917	00035	SO  	1999	9	17	AU990675         	1	19990611	G	3230		DOWNLOCK        			PIPER 	PA31  	PA31350     	7103110	SO  						HARTZL	HCE3Y	HCE3YR2     	GL  	RT MLG	LACK OF LUBE    	W				K				NONE                    				O			OTHER                     			LD	LANDING        	1			AU	S 										(AUS) RIGHT MAIN LANDING GEAR DOWNLOCK STICKING DUE TO LACK OF LUBRICATION.  CAUSED BY OPERATING IN HEAVY RAIN.						1	L	7	2 	3O				A20SO   		5	C	P33EA	 
1999091700036	19990917	00036	SO  	1999	9	17	AU990676         	1	19990624	G	8120	ZFO19677	IMPELLER        	GARRTT      	4091709001  	PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	TURBOCHARGER	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			198  		ZFO19677		L565961A			(AUS) ENGINE TURBOCHARGER IMPELLER DAMAGED BY FOD.						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
1999091700037	19990917	00037	CE  	1999	9	17	AU990677         	1	19990712	G	3246	40135	WHEEL           		16101901    	CESSNA	402   	402C        	207590R	CE  	CONT  	O520  	TSIO520VB   	17040	SO  	MCAULY	3AF32C	3AF32C505   	GL  	MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WHEEL HALF BEAD SECTION CRACKED AND SEPARATED.  LENGTH OF SEPARATED SECTION APPROXIMATELY 152.4 MM (6 INCHES).						1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22EA	 
1999091700038	19990917	00038	EU  	1999	9	17	AU990678         	1	19990623	G	7602	11043	ROD END         			PARTEN	P68   	P68B        		EU  	LYC   	O360  	IO360A1B6   	41514	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	MIXTURE CONTROL	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 							L1627151A			(AUS) LEFT ENGINE MIXTURE CONTROL TO FCU CONTROL ROD ROD END AND ATTACHING HARDWARE SUSPECT UNAPPROVED PARTS.						1	H	7	2 	3O	3	O		A31EU   	1E10	5	C	P920	 
1999091700039	19990917	00039	GL  	1999	9	17	AU990679         	3	19990617	G	6111		BLADE           	MCAULY      	D3A34C401   	CESSNA	206   	U206G       	2073356	CE  						MCAULY	D3A34	D3A34C401   	GL  	PROPELLER	MISRIGGED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 								940641		(AUS) PROPELLER BLADE SETTINGS INCORRECT.  FINE PITCH SET AT 12.5 DEGREES INSTEAD OF AT 11.2 DEGREES.						1	H	7	1 	3O				A4CE    		5	C	P47GL	 
1999091700040	19990917	00040	NM  	1999	9	17	AU990680         	1	19990712	G	3230	B4706640192	HOSE            			BOEING	737   	737377      		NM  										RT MLG	FAILED          	W				O				OTHER                   				K			FLUID LOSS                			CL	CLIMB          	1			AU	S 										(AUS) RIGHT MAIN LANDING GEAR UPLOCK ACTUATOR HYDRAULIC HOSE FAILED ADJACENT TO THE END FITTING.  LOSS OF SYSTEM 'A' HYD	RAULIC FLUID.  DRY RUNNING OF ELECTRICAL AND ENGINE DRIVEN HYDRAULIC PUMPS DAMAGED THE PUMPS.					2	L	7	2 	4F			RT	A16WE   					 
1999091700041	19990917	00041	NE  	1999	9	17	AU990681         	2	19990724	G	7320		SENSOR          								GE    	CF6   	CF680A      	30025	NE  					LT ENGINE	FAULTY          	W				O				OTHER                   				R	E		PARTIAL RPM/PWR LOSS      	VIBRATION/BUFFET          		DE	DESCENT        	1			AU	S 							580242			(AUS) LEFT ENGINE FAILED TO ACCELERATE ABOVE FLIGHT IDLE.  NR 1 COMPRESSOR INLET TEMPERATURE SENSOR CHANGED.											4	F			E13NE				 
1999091700042	19990917	00042	SO  	1999	9	17	AU990682         	2	19990616	G	8520	270020	BEARING         			CESSNA	210   	210M        	2073450	CE  	CONT  	O520  	IO520L      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	CRANKSHAFT	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					270020		270020			(AUS) CRANKSHAFT BEARING FAILED. THE BEARING FELL OUT OF THE SUMP PLUG HOLE DURING ENGINE OIL DRAIN.  LIMITED INFORMATIO	N PROVIDED.					1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P47GL	 
1999101300001	19991013	00001	NE  	1999	10	13	AU990683         	3	19990714	G	6111	HCC3YR2UF	BLADE           	HARTZL      	HCC3YR2UF   	GULSTM	500   	500B        	0141106	SW  	LYC   	O540  	IO540E1B5   	41532	EA  	HARTZL	HCC3Y	HCC3YR2     	NE  	PROPELLER	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			556  		CK4456A			CK4456A		(AUS) LEFT PROPELLER BLADE LOOSE.						1	H	7	2 	3O	3	O		6A1     	1E4	5	C	P25EA	 
1999091700043	19990917	00043	EA  	1999	9	17	AU990684         	2	19990411	G	7310		LINE            			BNORM 	BN2   	BN2A21      	1520221	EU  	LYC   	O540  	IO540K1B5   	41532	EA  	HARTZL	HCC2Y	HCC2YR2     	GL  	FUEL SYSTEM	LOOSE           	W				O				OTHER                   				K	R	E	FLUID LOSS                	PARTIAL RPM/PWR LOSS      	VIBRATION/BUFFET          	NR	NOT REPORTED   	1			AU	S 										(AUS) NR 2 CYLINDER FUEL INJECTOR LINE BETWEEN DISTRIBUTION VALVE AND INJECTOR NOZZLE DISCONNECTED AT BOTH ENDS.  THE 'P	' CLAMPS WERE  ALSO UNDONE.  FUEL LEAKING INTO ENGINE BAY.					1	H	7	2 	3O	3	O		A17EU   	1E4	5	C	P920	 
1999091700044	19990917	00044	NM  	1999	9	17	AU990685         	1	19990414	G	5313		STRINGER        			BOEING	747   	747312      	1384932	NM  										BS 1630&1650	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) STRINGER 47R CORRODED IN AREA BETWEEN BS 1630 AND BS 1650.  LENGTH OF CORROSION 254 MM (10 INCHES) - WIDTH OF CORR	OSION 52.8 MM (2 INCHES) - DEPTH OF CORROSION 1.524 MM (0.060 INCH).					2	L	7	4 	4F			RT	A20WE   					 
1999091700045	19990917	00045	SO  	1999	9	17	AU990686         	2	19990714	G	8520	294573R	CAMSHAFT LOBE   								CONT  	O520  	IO520L      	17032	SO  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					294573R		294573R			(AUS) CRANKCASE MAIN TUNNEL DIMENSIONS OUT OF LIMITS.  CAMSHAFT LOBE CRACKED.											3	O			E5CE				 
1999091700046	19990917	00046	SO  	1999	9	17	AU990687         	1	19990706	G	6120		CONTROL CABLE   	HARTZL      	HCE2YR2     	PIPER 	PA23  	PA23250     	7102308	SO  	LYC   	O540  	IO540K1A5   	41532	EA  	HARTZL	HCE2Y	HCE2YR2     	GL  	PROP CONTROL	WRONG PART      	W				O				OTHER                   				W			INADEQUATE Q C            			DE	DESCENT        	1			AU	S 			5    							(AUS) LEFT PROPELLER CONTROL CABLE SEIZED.  INVESTIGATION FOUND THE CABLE IS USED IN A MARINE APPLICATION AND WAS PLASTI	C COATED WITH A LABEL PART NUMBER F.D.A. (FLEX DRIVE AUSTRALIA). UNAPPROVED PART.					1	L	7	2 	3O	3	O	 	1A10    	1E4	5	C	P9EA	 
1999091700047	19990917	00047	SO  	1999	9	17	AU990688         	2	19990715	G	8530	SA2000A20P	CYLINDER        			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							176901			(AUS) CYLINDER BARREL CRACKED IN EXTENSION BELOW BASE FLANGE.						1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P47GL	 
1999091700048	19990917	00048	CE  	1999	9	17	AU990689         	1	19990319	G	3213		SPACER          			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	MLG	MISINSTALLED    	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) MAIN LANDING GEAR CENTER SCISSOR LINK SPACERS INCORRECTLY INSTALLED CAUSING TOE-IN ON THE MAIN WHEELS LEADING TO R	APID TIRE WEAR.					1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22EA	 
1999091700049	19990917	00049	CE  	1999	9	17	AU990690         	1	19990319	G	3213	NAS43H158	SPACER          			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	MLG	MISSING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT MAIN LANDING GEAR CENTER SCISSOR LINK SPACERS MISSING. THE SPACERS WERE FOUND LAYING ON TOP OF THE SPAR.						1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22EA	 
1999091700050	19990917	00050	NM  	1999	9	17	AU990691         	1	19990715	G	7922	53E19600	VALVE           			ROBSIN	R22   	R22BETA     		NM  	LYC   	O320  	O320B2C     	41508	EA  					ENGINE OIL	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					L1591139A		L1591139A			(AUS) ENGINE THERMOSTATIC OIL COOLER BYPASS VALVE (VERNATHERM) CRIMP NUT LOOSE.						1	G	7	1 	3O	3	O		H10WE   	E274				 
1999091700051	19990917	00051	NM  	1999	9	17	AU990692         	1	19990713	G	3211	2000171	FITTING         		2000181     	PIPER 	PA60  	PA60600A    	7106002	NM  	LYC   	O540  	IO540K1J5   	41532	EA  					MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) MAIN LANDING GEAR ATTACHMENT FITTINGS P/N 200017-1 AND P/N O200018-1 CRACKED THROUGH WEB SECTION.						1	M	7	2 	3O	3	O	RT	A17WE   	1E4				 
1999091700052	19990917	00052	EU  	1999	9	17	AU990693         	1	19990323	G	2130	P264	BLEED VALVE     			FOKKER	F28   	F28MK4000   	4990810	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					CABIN PRESSURE	FAULTY          	W				O				OTHER                   				O			OTHER                     			CL	CLIMB          	1			AU	S 					P264					(AUS) MAIN AIR BLEED VALVES FAULTY.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999091700053	19990917	00053	EU  	1999	9	17	AU990694         	1	19990323	G	2130	861	BLEED VALVE     			FOKKER	F28   	F28MK4000   	4990810	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					CABIN PRESSURE	FAULTY          	W				O				OTHER                   				O			OTHER                     			CL	CLIMB          	1			AU	S 					861					(AUS) PRESSURIZATION SYSTEM BLEED AIR SHUTOFF VALVES FAULTY.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999091700054	19990917	00054	NM  	1999	9	17	AU990695         	1	19990727	G	2421	31708001A	GENERATOR       			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					NR 2	FAILED          	W				O				OTHER                   				J	H		WARNING INDICATION        	ELECT. POWER LOSS-50 PC   		CL	CLIMB          	1			AU	S 			519  		PCE		PLE120282			(AUS) NR 2 ALTERNATE CURRENT GENERATOR FAILED INTERNALLY.  DEBRIS FROM FAILED GENERATOR CONTAMINATED THE ENGINE OIL SYST	EM.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999091700055	19990917	00055	SO  	1999	9	17	AU990696         	2	19990613	G	7314	6533512A2	PUMP            								CONT  	O240  	IO240B      	17063	SO  					FUEL SYSTEM	FAULTY          	W				C				ABORTED TAKEOFF         				R	E		PARTIAL RPM/PWR LOSS      	VIBRATION/BUFFET          		TO	TAKEOFF        	1			AU	S 					H289725B		806938			(AUS) ENGINE DRIVEN FUEL PUMP FAULTY.  INVESTIGATION FOUND THE FOLLOWING DEFECTS:  1.  STAIN MARK ON RELIEF VALVE SEAT I	N PUMP HOUSING.  2. FINE SEDIMENT IN AREA OF PUMP ROTOR.  3.  LIGHT SCORING ON METERING SHAFT OUTSIDE DIAMETER AND BUSH 	INSIDE DIAMETER.  4.  EXCESS SEALANT ON THREAD OF HIGH RPM ADJUSTER LOCATED INSIDE  PUMP HOUSING.									3	O			E7SO				 
1999091700056	19990917	00056	SO  	1999	9	17	AU990697         	2	19990613	G	7322	6538981A1	FCU             								CONT  	O240  	IO240B      	17063	SO  					ENGINE	FAULTY          	W				C				ABORTED TAKEOFF         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		TO	TAKEOFF        	1			AU	S 					I289723A		806938			(AUS) FUEL CONTROL UNIT FAULTY.  INVESTIGATION FOUND SCORING ON THE SURFACES OF THE METERING PLUG AND SHAFT.											3	O			E7SO				 
1999091700057	19990917	00057		1999	9	17	AU990698         	1	19990714	G	7820	7200D1701	MUFFLER         								CONT  	O240  	IO240A      		SO  					EXHAUST	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) EXHAUST MUFFLER CRACKED IN THREE PLACES FROM SHROUD SUPPORT WELDS.   CRACK LENGTHS ALL LESS THAN 12.7 MM (0.5 INCH	).										3	O			E7SO				 
1999091700058	19990917	00058	CE  	1999	9	17	AU990699         	1	19990701	G	5711	501100032	CAP             			BEECH 	95    	95B55       	1152729	CE  	CONT  	O470  	IO470L      	17026	SO  	MCAULY	2AF34C	2AF34C55    	GL  	LT WING SPAR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT WING UPPER SPAR CAP CONTAINED EXFOLIATION CORROSION.						1	L	7	2 	3O	3	O	RT	3A16    	3E1	5	C	P5EA	 
1999091700059	19990917	00059	NM  	1999	9	17	AU990700         	1	19990713	G	3260		SENSOR          			DHAV  	DHC8  	DHC8103     	1386005	NM  	PWA   	PW121 	PW121       	52124	NE  					MLG	FAULTY          	W				O				OTHER                   				N			FALSE WARNING             			LD	LANDING        	1			AU	S 										(AUS) LANDING GEAR PROXIMITY SENSOR FAULTY.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999091700060	19990917	00060	NE  	1999	9	17	AU990701         	2	19990716	G	7314	2893A	PUMP            			BOEING	747   	747312      	1384932	NM  	PWA   	JT9   	JT9D7R4G2   	52054	NE  					FUEL SYSTEM	FAULTY          	W				C				ABORTED TAKEOFF         				R	E		PARTIAL RPM/PWR LOSS      	VIBRATION/BUFFET          		TO	TAKEOFF        	1			AU	S 					2893A		715202			(AUS) NR 4 ENGINE MAIN FUEL PUMP SUSPECT FAULTY.						2	L	7	4 	4F	4	F	RT	A20WE   	E3NE				 
1999091700061	19990917	00061	NE  	1999	9	17	AU990702         	2	19990713	G	7322	WYG33180	FCU             								GE    	CF6   	CF680A      	30025	NE  					NR 2 ENGINE	FAULTY          	W				O				OTHER                   				R	E		PARTIAL RPM/PWR LOSS      	VIBRATION/BUFFET          		DE	DESCENT        	1			AU	S 			5258 		WYG33180		580233			(AUS) NR 2 ENGINE MAIN ENGINE CONTROL SUSPECT FAULTY.											4	F			E13NE				 
1999091700062	19990917	00062	NM  	1999	9	17	AU990703         	1	19990715	G	5320	85330272103	COAMING         			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE COAMING CRACKED.  SIGNS OF IMPACT DAMAGE SUGGEST DAMAGE WAS CAUSED BY A BAGGAGE TUG.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999091700063	19990917	00063	EA  	1999	9	17	AU990704         	2	19990707	G	7322	32448343	FCU             			EMB   	110   	EMB110P1    	3260122	SO  	PWA   	PT6   	PT6A34      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	ENGINE	FAULTY          	W				C				ABORTED TAKEOFF         				X			ENGINE FLAMEOUT           			TO	TAKEOFF        	1			AU	S 			4058 		A66081		56574			(AUS) FUEL CONTROL UNIT SUSPECT FAULTY.						1	L	7	2 	4T	4	T		A21SO   	E4EA	6	C	P15EA	 
1999091700064	19990917	00064	NM  	1999	9	17	AU990705         	1	19990112	G	5313		WEB             			BOEING	737   	737377      		NM  										BS 727	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) STRINGER 18A WEB LOCATED AT BS 727 CRACKED ON LT AND RT SIDES RUNNING AFT FROM FASTENER.  FOUND DURING EDDY CURREN	T INSPECTION IAW ER B73-53-10-40A.					2	L	7	2 	4F			RT	A16WE   					 
1999091700065	19990917	00065	EA  	1999	9	17	AU990706         	2	19990629	G	7322		CARBURETOR      			PIPER 	PA28  	PA28151     	7102805	SO  	LYC   	O320  	O320E3D     	41508	EA  	SNSNCH	74D	74DM        	EA  	ENGINE	FIRE            	W				O				OTHER                   				A			FLAME/FIRE                			TX	TAXI/GRND HDL  	1			AU	S 							L3777127A	A42672		(AUS) ENGINE FIRE.  THE ENGINE STOPPED ON TOUCHDOWN AND WHEN A RESTART WAS ATTEMPTED A FIRE STARTED IN THE BOTTOM OF THE	 CARBURETOR AIR BOX WHICH SPREAD UP THE SCAT HOSES TO THE FRONT OF THE ENGINE COMPARTMENT.  SUSPECT THE HOT ENGINE WAS O	VERPRIMED DURING THE RESTART.				1	L	7	1 	3O	3	O		2A13    	E274	5	N	P88614	 
1999091700066	19990917	00066	NM  	1999	9	17	AU990707         	1	19990617	G	3250	450516801	COLLAR          			PIPER 	PA60  	PA60601P    	7106012	NM  	LYC   	O540  	IO540S1A5   	41532	EA  					NLG STEERING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					0765					(AUS) NOSE LANDING GEAR STEERING COLLAR FAILED AT THE STEERING ACTUATING MECHANISM ATTACHMENT LUG.   INVESTIGATION FOUND	 THAT THE CRACK HAD EXISTED FOR SOME TIME FINALLY FAILING DUE TO OVERLOAD.  THE COLLAR HAD GENERAL PITTING CORROSION.  F	URTHER INVESTIGATION FOUND CRACKING ON THE OTHER ATTACHMENT LUG WHICH WAS NOT VISIBLE TO THE NAKED EYE.				1	M	7	2 	3O	3	O	RT	A17WE   	1E4				 
1999091700067	19990917	00067	NE  	1999	9	17	AU990708         	2	19990517	G	7200		ENGINE          			SKRSKY	S76   	S76A        	8143006	NE  	TMECA 	ARRIEL	ARRIEL1S    	60030	NE  					NR 1	FAILED          	W				O				OTHER                   				Y			ENGINE STOPPAGE           			NR	NOT REPORTED   	1			AU	S 							15528			(AUS) NR 1 ENGINE INDICATIONS FLUCTUATED FOLLOWED BY AN UNCOMMANDED SHUTDOWN.						1	G	7	2 	3U	3	U		H1NE    	E19EU				 
1999091700068	19990917	00068	SO  	1999	9	17	AU990709         	2	19990701	G	8520	653906	LIFTER          								CONT  	O240  	IO240B      	17063	SO  					ENGINE	FAULTY          	W				O				OTHER                   				R	E		PARTIAL RPM/PWR LOSS      	VIBRATION/BUFFET          		CR	CRUISE         	1			AU	S 							806938			(AUS) HYDRAULIC VALVE LIFTERS (8OFF) FAULTY.											3	O			E7SO				 
1999091700069	19990917	00069	NM  	1999	9	17	AU990710         	1	19990408	G	5210		LEVER           			BOEING	747   	747438      		NM  	GE    	CF6   	CF680C2A5   		NE  					PASSENGER DOOR	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) DOOR EMERGENCY POWER ASSIST BOTTLE TOGGLES ON DOORS 3L AND 4R WERE NOT CONNECTED TO THE ACTIVATION CABLE LINKAGE. 	 THE CONNECTING BOLT WAS FITTED, BUT DID NOT CAPTURE THE TOGGLE LEVER.					2	L	7	4 	4F	4	F	RT	A20WE   	E13NE				 
1999091700070	19990917	00070	GL  	1999	9	17	AU990711         	3	19990714	G	6114		HUB             	MCAULY      	3GFR34C702  	BEECH 	200   	B200C       	1152924	CE  	PWA   	PT6   	PT6A42      	52043	NE  	MCAULY	3G34C7	3GFR34C701  	GL  	PROPELLER	FOD             	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 			3707 					870400		(AUS) PROPELLER FOD.   A SMALL BRIDING TOOL WAS  FOUND INSIDE THE PROPELLER CAUSING DAMAGE TO PARTS.  METAL CONTAMINATIO	N OF OIL SYSTEM.					1	L	7	2 	4T	4	T		A24CE   	E4EA	5	C	P60GL	 
1999091700071	19990917	00071	CE  	1999	9	17	AU990712         	1	19990712	G	5230		DOOR            			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A42      	52043	NE  	MCAULY	4HFR34	4HFR34C754  	NE  	CARGO DOOR	MISREPAIRED     	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) BAGGAGE DOOR MODIFICATION POOR WORKMANSHIP PREVENTED CORRECT CLOSURE OF BAGGAGE DOOR.   DOOR TOP HINGES HITTING DO	OR FRAME WHEN FULLY OPEN CAUSING DEFORMATION AND TWISTING OF TOP OF FRAME.  DOOR ALSO SIDE LOADED BY GUIDE BLOCK.					1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	3PNE	 
1999091700072	19990917	00072	CE  	1999	9	17	AU990713         	1	19990712	G	2700		CONTROL CABLE   			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A42      	52043	NE  	MCAULY	4HFR34	4HFR34C754  	NE  	FLIGHT CONTROL	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) CONTROL CABLES, WIRING AND COAXIAL CABLES LOCATED BEHIND THE INSTRUMENT PANEL AND CENTER CONSOLE CORRODED.  CORROS	ION AND SURFACE CORROSION ON MOST EXPOSED STEEL AND CADMIUM PLATED SURFACES.  THE AIRCRAFT HAD BEEN TAXIED WITH THE NLG 	BAY AFT ACCESS PANEL LEFT OFF ALLOWING RUNWAY DE-ICE SOLUTION TO CONTAMINATE THE AREA.				1	L	7	2 	4T	4	T	 	A24CE   	E4EA	6	C	3PNE	 
1999091700073	19990917	00073	CE  	1999	9	17	AU990714         	1	19990713	G	5711		SPAR            			BEECH 	33    	35C33       	1151408	CE  	CONT  	O470  	IO470K      	17026	SO  	MCAULY	2A36C	2A36C23     	GL  	LT & RT WING	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT AND RIGHT WING UPPER SPARS CONTAINED SEVERE INTERGRANNULAR CORROSION.  ON THE LT WING A SECTION OF THE REAR H	INGE HAD BEEN REMOVED WITH NO MATERIAL REPLACED.  ON THE RT WING A SUSPECT REPAIR HAD BEEN CARRIED OUT WITH A DOUBLER AD	DED. SUBMITTER SUSPECTED UNAPPROVED REPAIRS.				1	L	7	1 	3O	3	O		3A15    	3E1	5	C	P880	 
1999091700074	19990917	00074	WP  	1999	9	17	AU990716         	2	19990714	G	7320		SENSOR          								GARRTT	TPE331	TPE33110UG  	01514	WP  	ROTOL	R333	R333482F12  	GL  	LT ENGINE	FAULTY          	W				C				ABORTED TAKEOFF         				R	E		PARTIAL RPM/PWR LOSS      	VIBRATION/BUFFET          		TO	TAKEOFF        	1			AU	S 							P63095			(AUS) LEFT ENGINE T2/P2 SENSOR SUPECT FAULTY.											4	T			E4WE	6	C	P61GL	 
1999091700075	19990917	00075	CE  	1999	9	17	AU990717         	1	19990720	G	5711	1011200352	FITTING         			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	RT WING SPAR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT AFT SPAR FITTING CRACKED.   FOUND DURING FLUORESCENT DYE PENETRANT INSPECTION.						1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15EA	 
1999091700076	19990917	00076	CE  	1999	9	17	AU990718         	1	19990720	G	5711	1011100313	CAP             			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	LT WING SPAR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT FORWARD UPPER SPAR CAP CORRODED.  FOUND DURING VISUAL INSPECTION.						1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15EA	 
1999091700077	19990917	00077	SO  	1999	9	17	AU990719         	2	19990720	G	8520	578470	CRANKCASE       								CONT  	O520  	IO520B      	17032	SO  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					578470		578470			(AUS) CRANKCASE CRACKED IN AREA BETWEEN NR 5 CYLINDER AND ALTERNATOR PAD.											3	O			E5CE				 
1999091700078	19990917	00078	SO  	1999	9	17	AU990720         	1	19990715	G	2400		ELECTRICAL POWER			PIPER 	PA31  	PA31350     	7103110	SO  						HARTZL	HCE3Y	HCE3YR2     	GL  	ELECTRICAL SYS	FAILED          	W				C				ABORTED TAKEOFF         				H			ELECT. POWER LOSS-50 PC   			TO	TAKEOFF        	1			AU	S 										(AUS) AIRCRAFT SUFFERED A TOTAL ELECTRICAL FAILURE FOLLOWED BY A PARTIAL RETURN OF POWER.  INVESTIGATION COULD FIND NO S	PECIFIC CAUSE OF THE PROBLEM.  VARIOUS COMPONENTS WERE REPLACED AS A PRECAUTION.					1	L	7	2 	3O				A20SO   		5	C	P33EA	 
1999091700079	19990917	00079	SO  	1999	9	17	AU990721         	1	19990806	G	5712	4A221301	RIB             			EMB   	110   	EMB110P1    	3260122	SO  	PWA   	PT6   	PT6A34      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	RT WING	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT WING INBOARD RIB CORRODED IN THE AREA BETWEEN THE FRONT AND REAR SPARS.  FOLLOWING REMOVAL OF THE RIB A SMAL	L AMOUNT OF INTERGRANULAR/FILIFORM CORROSION WAS FOUND ON THE REAR SPAR WEB UNDER THE STAINLESS STEEL SHIMS LOCATED BETW	EEN THE RIB REAR FLANGE AND THE REAR SPAR RIB.				1	L	7	2 	4T	4	T		A21SO   	E4EA	6	C	P15EA	 
1999091700080	19990917	00080	EU  	1999	9	17	AU990722         	1	19990722	G	7120	68120251	FITTING         	PARTEN      	P68B        	PARTEN	P68   	P68B        		EU  	LYC   	O360  	IO360A1B6   	41514	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	LT ENGINE MOUNT	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					124					(AUS) LEFT ENGINE MOUNT UPPER INBOARD ATTACHMENT FITTING CRACKED IN THE VERTICAL FLANGE.						1	H	7	2 	3O	3	O		A31EU   	1E10	5	C	P920	 
1999091700081	19990917	00081		1999	9	17	AU990723         	1	19990709	G	5540		RUDDER          			AMTR  		MUSTANG2    			LYC   		IO360B1E    			HARTZL		HCC2YK1     		VERTICAL STAB	SEPARATED       	W				O				OTHER                   				F			FLT CONT AFFECTED         			DE	DESCENT        	1			AU	S 							2424151A	CH2257		(AUS) RUDDER FLUTTER CAUSED THE RUDDER TO SEPARATE FROM THE FIN REAR SPAR AT THE HINGE POINT.									0 										 
1999091700082	19990917	00082	NM  	1999	9	17	AU990724         	1	19990725	G	7931	BN	CONNECTOR       			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					LT ENGINE	CONTAMINATED    	W				C				ABORTED TAKEOFF         				E	K		VIBRATION/BUFFET          	FLUID LOSS                		TO	TAKEOFF        	1			AU	S 										(AUS) LEFT ENGINE OIL PRESSURE SENDER UNIT CONNECTOR CONTAMINATED WITH OIL.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999091700083	19990917	00083	GL  	1999	9	17	AU990725         	3	19990716	G	6110	3GFR34C702	PROPELLER ASSY  	MCAULY      	3GFR34C702  	BEECH 	200   	B200C       	1152924	CE  	PWA   	PT6   	PT6A42      	52043	NE  	MCAULY	3G34C7	3GFR34C701  	GL  	FORWARD	FOD             	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			3707 					870400		(AUS) PROPELLER CONTAINED FOD LEFT OVER FROM THE LAST ASSEMBLY.  A BRIDGING TOOL USED TO PREVENT CUTTING OF THE PISTON O	-RING  DURING ASSEMBLY WAS FOUND ON THE PRESSURE SIDE OF THE PISTON.  THE PISTON SKIRT HAD BEEN DAMAGED AND THE CYLINDER	 SCORED.  FOD.				1	L	7	2 	4T	4	T		A24CE   	E4EA	5	C	P60GL	 
1999091700084	19990917	00084	EU  	1999	9	17	AU990726         	1	19990722	G	2720	54069	CONTROL CABLE   			PARTEN	P68   	P68B        	6780104	EU  	LYC   	O360  	IO360A1B6   	41514	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	RUDDER	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT FORWARD RUDDER CABLE EXCESSIVELY WORN IN THE AREA OF THE FORWARD PULLEY LOCATED AT FRAME NR 3.						1	H	7	2 	3O	3	O	 	A31EU   	1E10	5	C	P920	 
1999091700085	19990917	00085	CE  	1999	9	17	AU990727         	1	19990719	G	2810	MS2951310	SEAL            		08234102    	CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	FUEL CAP	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUEL TANK CAP SEALS P/N MS29513-10 AND P/N  MS29513-232 IN POOR CONDITION.  FUEL TANKS CONTAMINATED WITH WATER.						1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22EA	 
1999091700086	19990917	00086	CE  	1999	9	17	AU990728         	1	19990728	G	2120	57155278CM361210	CLAMP           			CESSNA	441   	441         	2076020	CE  						HARTZL	HCB3T	HCB3TN5     	GL  	AIR DISTRIBUTION	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) DUCT CLAMP SECURING THE DUCT FROM THE AIR CYCLE MACHINE (ACM) TO THE WATER SEPARATOR LOOSE.  THE ACM HAD BEEN FITT	ED ON THE 27TH APRIL 1999.					1	L	7	2 	3T			RT	A28CE   		6	C	P15EA	 
1999091700087	19990917	00087	SO  	1999	9	17	AU990729         	1	19990710	G	7603	31747000	COUPLING        			PIPER 	PA34  	PA34200     	7103405	SO  	LYC   	O360  	IO360C1E6   	41514	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	POWER LEVER	BROKEN          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) RIGHT ENGINE THROTTLE BALL COUPLING FAILED IN THE AREA BENEATH THE BALL.  INVESTIGATION FOUND THAT THE BALL STUD W	AS WORN APPROXIMATELY 40 PERCENT THROUGH.					1	L	7	2 	3O	3	O		A7SO    	1E10	5	C	P920	 
1999091700088	19990917	00088	NE  	1999	9	17	AU990730         	2	19990712	G	7261	310349011	OIL SYSTEM      			JETAIR	JETSTM	JETSTM4101  	1500501	EU  	GARRTT	TPE331	TPE33114GR  	01514	NE  	MCAULY	5JFR	B5JFR36C1101	GL  	NR 1 ENGINE	CONTAMINATED    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			2194 				P75051			(AUS) NR 1 ENGINE OIL SYSTEM METAL CONTAMINATION.						2	L	7	2 	4T	4	T	RT	A41NM   	E18NE	5	C	P15WE	 
1999091700089	19990917	00089	CE  	1999	9	17	AU990731         	1	19990712	G	5311		FRAME           			CESSNA	206   	P206B       	2073309	CE  	CONT  	O520  	IO520A      	17032	SO  	MCAULY	3A32C	D3A32C88    	GL  	FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							270346R	725001		(AUS) LEFT DOORPOST FRAME CRACKED.  FUSELAGE SKIN RIVETS LOOSE IN AREA ADJACENT TO THE WING STRUT.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P21EA	 
1999091700090	19990917	00090	CE  	1999	9	17	AU990732         	1	19990712	G	5312		BULKHEAD        			CESSNA	206   	P206B       	2073309	CE  	CONT  	O520  	IO520A      	17032	SO  	MCAULY	3A32C	D3A32C88    	GL  	BS 209	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							270346R	725001		(AUS) FUSELAGE AFT BULKHEAD LOCATED AT STN 209.0 CRACKED IN THE UPPER RT CORNER ADJACENT TO THE RT HORIZONTAL STABILIZER	 ATTACHMENT FITTING.					1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P21EA	 
1999091700091	19990917	00091	CE  	1999	9	17	AU990733         	1	19990726	G	3297		WIRE            			CESSNA	401   	401A        	207590D	CE  						MCAULY	3AF32C	3AF32C505   	GL  	MLG	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LANDING GEAR MOTOR CONNECTION LOOSE.						1	L	7	2 	3O			 	A7CE    		5	C	P22EA	 
1999091700092	19990917	00092	EA  	1999	9	17	AU990734         	2	19990423	G	8520	LW13521	BEARING         			BEECH 	76    	76          	1153005	CE  	LYC   	O360  	O360A1G     	41514	EA  					ENGINE	SPALLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							L2612436A			(AUS) NR 2 AND NR 3 CYLINDER CONNECTING ROD BIG END BEARINGS SPALLED.  SUSPECT CAUSED BY PARTIAL BREAK-UP OF HYDRAULIC T	APPET.  METAL CONTAMINATION OF ENGINE OIL SYSTEM.					1	L	7	2 	3O	3	O		A29CE   	E286				 
1999091700093	19990917	00093	CE  	1999	9	17	AU990735         	1	19990728	G	2822	4765411	PUMP            			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	FUEL BOOST	SHORTED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUEL BOOST PUMP FAULTY.  SHORT CIRCUIT AT PUMP BODY CONNECTION.  CIRCUIT BREAKER TRIPPED.						1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22EA	 
1999091700094	19990917	00094	NM  	1999	9	17	AU990736         	1	19990618	G	2497		WIRE            			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					AC SYSTEM	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) SEVEN ELECTRICAL CABLES DAMAGED AT THE OUTER INSULATION JACKET.  NO EVIDENCE OF EXPOSED CONDUCTORS.						2	L	7	3 	4F	4	F	 	A3WE    	E2EA				 
1999091700095	19990917	00095	EA  	1999	9	17	AU990737         	2	19990730	G	7414	IO5136029	MAGNETO         			AVIONS	R2160 	R2160       	0960101	EU  	LYC   	O320  	O320D2A     	41508	EA  	SNSNCH	74D	74DM        	EA  	ENGINE	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					L1308839A		L1308839A	A56962		(AUS) MAGNETO FAULTY.  ENGINE WAS JUST RECEIVED FROM OVERHAUL.						1	L	7	1 	3O	3	O	RT	A48EU   	E274	5	N	P88614	 
1999091700096	19990917	00096	NM  	1999	9	17	AU990738         	1	19990621	G	2120	31739394	PISTON RING     			BOEING	737   	737377      		NM  										AIR DISTRIBUTION	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					567C					(AUS) RIGHT PRESSURE REGULATING AND SHUTOFF VALVE FAULTY.   WORKSHOP INSPECTION FOUND THAT THE CONTROL PISTON RING SET W	AS CRACKED AND THE ACTUATOR COVER PACKING WAS TORN.					2	L	7	2 	4F			RT	A16WE   					 
1999091700097	19990917	00097	EU  	1999	9	17	AU990739         	1	19990217	G	3230	HC3236H0108000	PIN             			BAG   	BAE146	BAE146300A  	1500267	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR RETRACTION JACK ATTACHMENT PIN CRACKED.  FOUND DURING MAGNETIC PARTICLE INSPECTION.  CRACK LENGT	H 19.05 MM (0.75 INCH).					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999091700098	19990917	00098	EU  	1999	9	17	AU990740         	1	19990217	G	3230	HC3236H0108000	PIN             			BAG   	BAE146	BAE146300A  	1500267	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR RETRACTION JACK ATTACHMENT PIN CRACKED.  FOUND DURING MAGNETIC PARTICLE INSPECTION.  CRACK LENGT	HS 19.05 MM AND 12.7 MM.					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999091700099	19990917	00099	EU  	1999	9	17	AU990741         	1	19990217	G	3230	HC3236H010800	PIN             			BAG   	BAE146	BAE146300A  	1500267	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR RETRACTION JACK ATTACHMENT PIN CRACKED.  FOUND DURING MAGNETIC PARTICLE INSPECTION.  CRACK LENGT	H 15.875 MM (0.625 INCH).					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999091700100	19990917	00100	EU  	1999	9	17	AU990742         	1	19990217	G	3230	HC3236H0108000	PIN             			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR RETRACTION JACK ATTACHMENT PIN CRACKED.  FOUND DURING MAGNETIC PARTICLE INSPECTION.  CRACK LENGT	HS 15.875 MM AND 4.762 MM (0.625 INCH AND 0.187 INCH).					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999091700101	19990917	00101	EU  	1999	9	17	AU990743         	1	19990217	G	3230	HC3236H0108000	PIN             			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR RETRACTION JACK ATTACHMENT PIN CRACKED.  FOUND DURING MAGNETIC PARTICLE INSPECTION.  CRACK LENGT	H 9.525 MM (0.375 INCH).					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999091700102	19990917	00102	EU  	1999	9	17	AU990744         	1	19990217	G	3230	HC3236H0108000	PIN             			BAG   	BAE146	BAE146300A  	1500267	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR RETRACTION JACK ATTACHMENT PIN CRACKED.  FOUND DURING MAGNETIC PARTICLE INSPECTION.  CRACK LENGT	H 76.2 MM (3 INCHES).					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999091700103	19990917	00103	EU  	1999	9	17	AU990745         	1	19990217	G	3230	HC3236H0108000	PIN             			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR RETRACTION JACK ATTACHMENT PIN CRACKED.  FOUND DURING MAGNETIC PARTICLE INSPECTION. CRACK LENGTH	 9.525 MM (0.375 INCH).					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999091700104	19990917	00104	NE  	1999	9	17	AU990746         	2	19990618	G	7230	3053556220	BEARING         			BOEING	737   	737377      		NM  	GE    	CFM56 	CFM563B1    	13802	NE  					NR 2 ENGINE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			6260 				720904			(AUS) NR 2 ENGINE NR 4 BEARING FAILED.  SECONDARY DAMAGE TO HPC, HPT AND LPT MODULES.  AFT SUMP CHIP DETECTOR HAD HEAVY 	CONTAMINATION.					2	L	7	2 	4F	4	F	RT	A16WE   	E2GL				 
1999091700105	19990917	00105	NM  	1999	9	17	AU990747         	1	19990707	G	5311		FRAME           			BOEING	737   	737377      		NM  										BS 616	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT FRAME INNER CHORD LOCATED AT FS 616 ABOVE THE CENTER FUEL TANK CRACKED IN LOWER RIVET HOLE.  FOUND DURING EDD	Y CURRENT INSPECTION.					2	L	7	2 	4F			RT	A16WE   					 
1999091700106	19990917	00106	EA  	1999	9	17	AU990748         	2	19990428	G	7250	PCE24121	BLADE           			BEECH 	90    	C90         	1152913	CE  	PWA   	PT6   	PT6A20      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	LT ENGINE	FAILED          	W				O				OTHER                   				X	J		ENGINE FLAMEOUT           	WARNING INDICATION        		NR	NOT REPORTED   	1			AU	S 					PCE24121		PCE24121			(AUS) LEFT ENGINE FAILED.  INVESTIGATION FOUND FAILURE OF ONE COMPRESSOR TURBINE BLADE DUE TO FATIGUE.  DAMAGE CAUSED TO	 THE OTHER BLADES.					1	L	7	2 	3T	3	T		3A20    	E4EA	6	C	P15EA	 
1999091700107	19990917	00107	CE  	1999	9	17	AU990749         	1	19990721	G	5411	075100113	FRAME           			CESSNA	180   	180C        	2072608	CE  	CONT  	O470  	O470R       	17026	SO  					NACELLE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							130879			(AUS) ENGINE MOUNT FRAME CRACKED IN THE AREA AT THE TOP OF THE CLUSTER GUSSET ON THE LEFT SIDE.  CRACK LENGTH 13 MM (0.5	1 INCH).  FOUND DURING INSPECTION IAW AD/CESSNA180/4 (ITEM IS NOT PART OF THIS INSPECTION).					1	H	7	1 	3O	3	O		5A6     	E273				 
1999091700108	19990917	00108	GL  	1999	9	17	AU990750         	3	19990730	G	6111	S90AT4	BLADE           	MCAULY      	D2A34C58NO  											MCAULY	2A34C	D2A34C58    	GL  	PROPELLER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					941776			941776		(AUS) PROPELLER BLADES CRACKED IN THE FOLLOWING LOCATIONS:  1.  ONE BLADE CRACKED IN TWO LOCATIONS IN THE FOURTH THREAD 	FROM THE BASE OF THE BLADE - CRACK LENGTHS 63.5 MM (2.5 INCHES) AT THE LEADING EDGE AND 25.4 MM (1 INCH) AT THE TRAILING	 EDGE.  2.  ONE BLADE CRACKED IN THE THIRD THREAD FROM THE BASE OF THE BLADE - CRACK LENGTH 25.4 MM (1 INCH) AT THE LEAD	ING EDGE.													5	C	P3EA	 
1999091700109	19990917	00109	CE  	1999	9	17	AU990751         	1	19990716	G	5720		ANGLE           			CESSNA	182   	182F        	2072714	CE  	CONT  	O470  	O470K       	17026	SO  	MCAULY	2A34C	2A34C66     	GL  	WS 76	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							490274KR	741890		(AUS) RIGHT WING SPAR CAP TOP ANGLE CONTAINED INTERGRANNULAR CORROSION IN THE AREA FROM WS 76 TO WS 118.						1	H	7	1 	3O	3	O	NT	3A13    	E273	5	C	P3EA	 
1999091700110	19990917	00110	NE  	1999	9	17	AU990752         	2	19990804	G	7200	200304010	ENGINE          								LYC   	ALF502	ALF502R5    	41580	NE  					NACELLE	FAILED          	W				E				ENGINE SHUTDOWN         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			AU	S 							LF0531SA			(AUS) ENGINE OVERSPEED RESULTING IN SHUTDOWN.  INSPECTION FOUND THE FAN DECOUPLED FROM THE LP TURBINE.  THE CHIP DETECTO	R WAS INSPECTED AND FOUND TO BE CONTAMINATED AND THE ENGINE OIL WAS BLACK.										4	F			E6NE				 
1999091700111	19990917	00111	CE  	1999	9	17	AU990753         	1	19990726	G	5523		TAB             			BEECH 	76    	76          	1153005	CE  	LYC   	O360  	IO360A1G6   	41514	EA  					ELEVATOR	DISBONDED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELEVATOR TRIM TAB TRAILING EDGES DISBONDED.						1	L	7	2 	3O	3	O		A29CE   	1E10				 
1999091700112	19990917	00112	SO  	1999	9	17	AU990754         	2	19990731	G	7322	15A21	SCREW           	FACET       	MA45        	CESSNA	182   	182D        	2072710	CE  	CONT  	O470  	O470L       	17026	SO  	MCAULY	2A34C	2A34C66     	GL  	CARBURETOR	LOOSE           	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AU	S 			1165 		4025411		L81143			(AUS) CARBURETOR FLOAT TO BODY ATTACHMENT SCREWS LOOSE ALLOWING THE FLOAT TO CONTACT THE BODY AND PREVENT CLOSING OF THE	 NEEDLE AND SEAT. CARBURETOR FLOODING.					1	H	7	1 	3O	3	O	NT	3A13    	E273	5	C	P3EA	 
1999091700113	19990917	00113	NM  	1999	9	17	AU990755         	1	19990506	G	5320		BEAM            			BOEING	737   	737377      		NM  										FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) STABILIZER CUT-OUT BEAMS IN FUSELAGE CONTAINED TWO CRACKS ON THE LT SIDE AND ONE CRACK ON THE RT SIDE.  FOUND DURI	NG EDDY CURRENT INSPECTION IAW ER B73-53-30-10D.					2	L	7	2 	4F			RT	A16WE   					 
1999091700114	19990917	00114	GL  	1999	9	17	AU990756         	3	19990730	G	6114	C4716C58	HUB             	MCAULY      	D2A34C58NO  											MCAULY	2A34C	D2A34C58    	GL  	PROPELLER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					941776			941776		(AUS) PROPELLER HUB CRACKED IN TWO AREAS IN NR 2 BLADE SOCKET EXTENDING ACROSS ALL THREADS BETWEEN THE 5 O'CLOCK AND 7 O	'CLOCK POSITIONS.															5	C	P3EA	 
1999091700115	19990917	00115	NE  	1999	9	17	AU990757         	2	19990730	G	7261	133	CHIP DETECTOR   								TMECA 	ARRIEL	ARRIEL1A    	60030	NE  					NR 1 ENGINE	CONTAMINATED    	W				O				OTHER                   				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		NR	NOT REPORTED   	1			AU	S 			112  		133		133			(AUS) NR 1 ENGINE REAR BEARING RETURN ELECTRICAL MAGNETIC CHIP DETECTOR CONTAMINATED WITH A SMALL SLIVER OF METAL.  ENGI	NE WAS GROUND RUN IAW MAINTENANCE MANUAL WITH NO FURTHER FAULTS FOUND.										3	U			E19EU				 
1999091700116	19990917	00116	SO  	1999	9	17	AU990758         	1	19990728	G	5210	5329602	PIN             			PIPER 	PA31  	PA31350     	7103110	SO  						HARTZL	HCE3Y	HCE3YR2     	GL  	PASSENGER DOOR	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LOWER CABIN DOOR LOCK PIN BENT. PIN WAS CAUGHT BY SUPPORT CABLE AND BENT WHEN PASSENGERS USED THE DOOR.						1	L	7	2 	3O				A20SO   		5	C	P33EA	 
1999091700117	19990917	00117	GL  	1999	9	17	AU990759         	3	19990727	G	6111	R1075	BLADE           	MCAULY      	1C235LFA757 											MCAULY	1C235	1C235LFA    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					R1075					(AUS) PROPELLER BLADE SURFACES CONTAINED INTERGRANNULAR CORROSION MAINLY IN THE AREA OF THE LEADING EDGES.																5	N	P12EA	 
1999091700118	19990917	00118	SO  	1999	9	17	AU990760         	2	19990727	G	8520	570647	CRANKCASE       								CONT  	O520  	IO520F      	17032	SO  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					570647		570647			(AUS) ENGINE CRANKCASE CRACKED.  CAMSHAFT LOBE HARDENING CRACKED.  STARTER SHAFT CRACKED.											3	O			E5CE				 
1999091700119	19990917	00119	NE  	1999	9	17	AU990761         	1	19990804	G	6710		CYCLIC STICK    			SKRSKY	S76   	S76A        	8143006	NE  	TMECA 	ARRIEL	ARRIEL1S    	60030	NE  					M/R CONTROL	JAMMED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) CYCLIC CONTROL STICK JAMMED BY FOD.  INVESTIGATION FOUND THAT A SCREW BECAME TRAPPED BETWEEN THE CYCLIC TORQUE TUB	E FITTING AND THE TORQUE TUBE SUPPORT BRACKET PREVENTING FULL AFT CYCLIC MOVEMENT.  THE ORIGIN OF THE SCREW COULD NOT BE	 CONFIRMED.				1	G	7	2 	3U	3	U		H1NE    	E19EU				 
1999091700120	19990917	00120	CE  	1999	9	17	AU990762         	1	19990723	G	3230	11581002918	NUT             			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	LT MLG	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT MAIN LANDING GEAR NUT ASSEMBLY FAILED.  THE FAILURE WAS CAUSED BY A CRACK LOCATED APPROXIMATELY 31.75 (1.25 I	NCHES) FROM THE END OF THE NUT HOUSING EXTENDING FOR 360 DEGREES CIRCUMFERENTIALLY WITH 100 PERCENT PENETRATION.  FURTHE	R INVESTIGATION FOUND THAT THE NLG AND RT MLG NUT ASSEMBLIES WERE SIMILARLY CRACKED.				1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15EA	 
1999091700121	19990917	00121	CE  	1999	9	17	AU990763         	1	19990723	G	3230	908200151	NUT             			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			4406 							(AUS) NOSE LANDING GEAR NUT ASSEMBLY CRACKED.  CRACK LOCATED APPROXIMATELY 25.4 MM (1 INCHES) FROM THE END OF THE NUT HO	USING AND EXTENDING FOR APPROXIMATELY 100 DEGREES CIRCUMFERENTIALLY.  SEE OPER CONTROL NR AU990762 FOR FURTHER INFORMATI	ON.				1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15EA	 
1999091700122	19990917	00122	SO  	1999	9	17	AU990764         	1	19990710	G	3230	1092	DOWNLOCK        	OZONE       	OAS29233    	PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	LT MLG	CONTAMINATED    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					1092					(AUS) LEFT MAIN LANDING GEAR DOWNLOCK HOOK CONTAMINATED WITH MUD AND DIRT PREVENTING ACTUATION OF MICROSWITCH.						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
1999091700123	19990917	00123	SO  	1999	9	17	AU990765         	1	19990710	G	3230	755277	HANDLE          	OZONE       	OAS29233    	PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	MLG	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					1092					(AUS) LANDING GEAR EMERGENCY HAND PUMP LEVER BROKEN.  CAUSED BY OVER EXTENSION OF LEVER DURING OPERATION OF THE PUMP.						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
1999091700124	19990917	00124	CE  	1999	9	17	AU990766         	1	19990723	G	3230	11581002917	NUT             			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	RT MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			3744 							(AUS) RIGHT MAIN LANDING GEAR NUT ASSEMBLY CRACKED APPROXIMATELY 38.1 MM (1.5 INCHES) FROM THE END OF THE NUT HOUSING EX	TENDING FOR APPROXIMATELY 180 DEGREES CIRCUMFERENTIALLY.  SEE OPER CONTROL NR AU990762 FOR FURTHER INFORMATION.					1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15EA	 
1999091700125	19990917	00125	CE  	1999	9	17	AU990767         	1	19990720	G	5711	351150595	FITTING         			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	RT WING SPAR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT WING AFT SPAR FITTING CORRODED.						1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15EA	 
1999091700126	19990917	00126	EU  	1999	9	17	AU990768         	1	19990810	G	3230	7229152692	PIPE            			SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT75A2      	30030	NE  	ROTOL	R354	R3544123F13 	NE  	MLG	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LANDING GEAR DOWNLOCK RELEASE HYDRAULIC PIPE CHAFING ON FITTING P/N 7257162-004 CAUSING REDUCED WALL THICKNESS.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE6	6	C	P61GL	 
1999091700127	19990917	00127	SO  	1999	9	17	AU990769         	2	19990613	G	8530		CYLINDER        			CESSNA	182   	182Q        	2072732	CE  	CONT  	O470  	O470U       	17026	SO  	MCAULY	2A34C	2A34C203    	GL  	ENGINE	SEPARATED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) CYLINDER HEAD SEPARATED FROM BARREL.						1	H	7	1 	3O	3	O	NT	3A13    	E273	5	C	P3EA	 
1999091700128	19990917	00128	CE  	1999	9	17	AU990770         	1	19990705	G	5330	15279888	SKIN            			CESSNA	150   	152         	2071835	CE  						MCAULY	1A103	1A103TCM    	GL  	FUSELAGE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					15279888					(AUS) AIRCRAFT CONTAINED MAJOR CORROSION. AIRCRAFT HAD BEEN STRIPPED AND REPAINTED APPROXIMATELY FOUR MONTHS PREVIOUSLY 	AND IT IS SUSPECTED THAT THE AIRCRAFT WAS INCORRECTLY STRIPPED AND TREATED BEFORE PAINTING.					1	H	7	1 	3O			NT	3A19    		5	N	P50GL	 
1999091700129	19990917	00129	SO  	1999	9	17	AU990771         	1	19990804	G	2844	306000017	TRANSDUCER      		486439      	PIPER 	PA38  	PA38112     	7103812	SO  						SNSNCH	74D	74DM        	EA  	FUEL PRESSURE	MISREPAIRED     	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 					11583					(AUS) FUEL PRESSURE TRANSDUCER FAULTY.  FOUND DURING INSPECTION IAW AD/INST/8.  SUBMITTER STATED INSPECTION OF THE TRANS	DUCER REVEALED EVIDENCE OF PREVIOUS UNAUTHORIZED REPAIRS.					1	L	7	1 	3O				A18SO   		5	N	P88614	 
1999091700130	19990917	00130	NM  	1999	9	17	AU990772         	1	19990408	G	5720		STIFFENER       			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					RT WING	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT WING FRONT SPAR STIFFENER CONTAINED LEVEL 2 CORROSION.						2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700131	19990917	00131	NM  	1999	9	17	AU990773         	1	19990416	G	5330		SKIN            			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					BS 1192 & 1212	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) INTERIOR SKIN CONTAINED CORROSION IN THE FOLLOWING AREAS:  1.  BS 1192 - AREA OF CORROSION 25.4 MM BY 177.8 MM (1 	INCH BY 7 INCH).  2.  BS 1212 - AREA OF CORROSION 38.1 MM BY 101.6 MM (1.5 INCHES BY 4 INCHES).  3.  BS 1232 - AREA OF C	ORROSION 38.1 MM BY 50.8 MM (1.5 INCHES BY 2 INCHES).				2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700132	19990917	00132	NM  	1999	9	17	AU990774         	1	19990526	G	5522		SKIN            			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					ELEVATOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELEVATOR SKIN CORRODED AT STN 40, STN 73, STN 84, STN 106 AND STN 166.  RT STABILIZER UPPER SKIN ABOVE REAR SPAR C	ONTAINED FIVE AREAS OF REPAIR.					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700133	19990917	00133	NM  	1999	9	17	AU990775         	1	19990407	G	5522		SKIN            			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					ELEVATOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LET ELEVATOR LOWER SKIN BULGED AND CORRODED BETWEEN SEVEN RIVETS AT STN 159 TRAILING EDGE.						2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700134	19990917	00134	NM  	1999	9	17	AU990776         	1	19990407	G	5511		SPAR            			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					HORIZONTAL STAB	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT STABILIZER REAR SPAR UPPER CHORD BULGED AND CORRODED FOR APPROXIMATELY 177.8 MM (7 INCHES) BETWEEN STN 176 A	ND STN 186.					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700135	19990917	00135	NM  	1999	9	17	AU990777         	1	19990407	G	5510		BEAM            			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					HORIZONTAL STAB	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM CORRODED FOR APPROXIMATELY 127 MM (5 INCHES) BETWEEN STN 200 	AND STN 209.					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700136	19990917	00136	NM  	1999	9	17	AU990778         	1	19990807	G	5522		SKIN            			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					ELEVATOR	DELAMINATED     	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT ELEVATOR TRAILING EDGE INBOARD SKIN DELAMINATED FOR APPROXIMATELY 50.8 MM (2 INCHES).						2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700137	19990917	00137	NM  	1999	9	17	AU990779         	1	19990421	G	5311		PLATE           			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					BS 227	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FRAME REINFORCEMENT PLATE LOCATED AT STN 227.8 AT THE COCKPIT SIDEWALL CORRODED.						2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700138	19990917	00138	NM  	1999	9	17	AU990780         	1	19990415	G	5315		FLOORBEAM       			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					BS 344	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE FLOORBEAM LOCATED AT STN 344 LBL 2 CORRODED.						2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700139	19990917	00139	NM  	1999	9	17	AU990781         	1	19990414	G	5320		BRACKET         			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					BS 375	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) MAIN CARGO BARRIER LOWER FITTING SUPPORT BRACKET LOCATED AT STN 375 RBL 39 CORRODED.						2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700140	19990917	00140	NM  	1999	9	17	AU990782         	1	19990414	G	5320		FLANGE          			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					BS 968-1072	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) MAIN CARGO COMPARTMENT TIEDOWN TRACK FLANGE CORRODED AT BS 968, BS 1002, BS 1027, BS 1043 AND BS 1072 AT RBL 63.						2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700141	19990917	00141	NM  	1999	9	17	AU990783         	1	19990409	G	5347		FLANGE          			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					BS 968-1072	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) MAIN CARGO COMPARTMENT TIEDOWN TRACK FLANGE CORRODED AT BS 968, BS 1002, BS 1027, BS 1043 AND BS 1072 AT RBL 63.						2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700142	19990917	00142	NM  	1999	9	17	AU990784         	1	19990409	G	5347		FLANGE          			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					BS 847	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) MAIN CARGO COMPARTMENT TIEDOWN TRACK FLANGE CORRODED AT STN 847 RBL 63.						2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700143	19990917	00143	NM  	1999	9	17	AU990785         	1	19990409	G	5312		BULKHEAD        			BOEING	727   	72777C      	1380420	NM  	PWA   	JT8   	JT8D7A      	52053	NE  					BS 350	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) E/E COMPARTMENT BULKHEAD LOCATED AT STN BS 350.2, BL RBL 36 CORRODED.   AREA OF CORROSION 1935.48 SQMM (3 SQUARE I	NCHES).					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999091700144	19990917	00144	EU  	1999	9	17	AU990786         	1	19990710	G	2750	866108	SOLENOID        		8661C       	BAG   	JETSTM	JETSTM3107  	1500215	EU  						ROTOL	R333	R333482F12  	GL  	TE FLAP	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					DS386T					(AUS) LIFT DUMP SOLENOID SUSPECT FAULTY.						2	L	7	2 	4T			RT	BA15CAA 		6	C	P61GL	 
1999091700145	19990917	00145	EU  	1999	9	17	AU990787         	1	19990809	G	5330		SKIN            			BAG   	BAE146	BAE146100A  	1500260	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					BS 29	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE SKIN CRACKED IN THE AREA OF FRAME 29 LOCATED BETWEEN STRINGER NR 12 AND STRINGER NR 13.  FOUND DURING INS	PECTION IAW AD/BAE/146/70.  LIMITED INFORMATION PROVIDED.					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999091700146	19990917	00146	SO  	1999	9	17	AU990788         	2	19990805	G	8520	642135	CRANKCASE       			CESSNA	404   	404CESSNA   	2075901	CE  	CONT  	O520  	GTSIO520M   	17032	SO  	MCAULY	3FF32	3FF32C501   	GL  	RT ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					606731		60631			(AUS) RIGHT ENGINE CRANKCASE CRACKED AT THE 5 O'CLOCK POSITION ON NR 6 CYLINDER FLANGE.						1	L	7	2 	3O	3	O		A25CE   	E7CE	5	C	P45GL	 
1999091700147	19990917	00147	CE  	1999	9	17	AU990789         	1	19990824	G	2750	C160401	GEARBOX         			BEECH 	58    	58          	1152740	CE  	CONT  	O520  	IO520C      	17032	SO  	MCAULY	3AF34C	3AF34C502   	GL  	TE FLAP	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FLAP GEARBOX DRIVE TEETH SHEARED.						1	L	7	2 	3O	3	O		3A16    	E5CE	5	C	P22EA	 
1999091700148	19990917	00148	EU  	1999	9	17	AU990790         	1	19990808	G	3030		PITOT HEAT      			SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT75A2      	30030	NE  					PITOT/STATIC SYS	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) STANDBY PITOT TUBE, PITOT HEAT SWITCH, AND/OR CIRCUIT BREAKER FAULTY.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE6				 
1999091700149	19990917	00149	CE  	1999	9	17	AU990791         	1	19990728	G	6120	5038901023	CONTROL CABLE   			BEECH 	58    	58          	1152740	CE  	CONT  	O520  	IO520C      	17032	SO  	MCAULY	3AF34C	3AF34C502   	GL  	RT PROPELLER	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							22316673C			(AUS) RIGHT ENGINE PROPELLER CSU CONTROL CABLE INNER CABLE SEPARATED APPROXIMATELY 117.8 MM (7 INCHES) FROM CSU END OF C	ABLE.					1	L	7	2 	3O	3	O	 	3A16    	E5CE	5	C	P22EA	 
1999091700150	19990917	00150	NE  	1999	9	17	AU990792         	2	19990804	G	7200	200304010	ENGINE          								LYC   	ALF502	ALF502R3A   	41580	NE  					NACELLE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1464 				LFO5315A			(AUS) ENGINE FAN DECOUPLED FROM LP TURBINE.  FULL FLOW CHIP DETECTOR CONTAMINATED AND OIL COLORED BLACK.											4	F			E6NE				 
1999091700151	19990917	00151	EA  	1999	9	17	AU990793         	2	19990810	G	8550	CH48110	FILTER          	CHAMPION    	CH48110     	PIPER 	PA23  	PA23250     	7102308	SO  	LYC   	O540  	IO540K1A5   	41532	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	ENGINE	MISINSTALLED    	W				K				NONE                    				W	K		INADEQUATE Q C            	FLUID LOSS                		IN	INSP/MAINT     	1			AU	S 										(AUS) ENGINE OIL FILTER FAULTY.  FILTER WAS INCORRECTLY LOCKWIRED.  THE SEAL WAS ALSO PROTRUDING.  THE THREADED INSERT H	AD COME LOOSE AND SEPARATED FROM THE FILTER WHEN IT WAS REMOVED FROM THE ENGINE.					1	L	7	2 	3O	3	O		1A10    	1E4	5	C	P920	 
1999091700153	19990917	00153	CE  	1999	9	17	AU990795         	1	19990729	G	3252	NAS561P414	PIN             		04425121    	CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320D2G     	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	MLG	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) INCORRECT SHIMMY DAMPER PISTON ROLL PIN FITTED.  A BRASS SCREW WAS USED INSTEAD OF THE CORRECT STEEL ROLL PIN.  TH	E BRASS SCREW SHEARED CAUSING COMPLETE FAILURE OF THE DAMPER WITH ASSOCIATED NOSE WHEEL SHIMMY.  UNAPPROVED PART.					1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
1999091700154	19990917	00154	SO  	1999	9	17	AU990796         	1	19990802	G	3230	10035002A	ACCUMULATOR     			EMB   	110   	EMB110P1    	3260122	SO  	PWA   	PT6   	PT6A34      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	NLG	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					022					(AUS) NOSE LANDING GEAR CENTERING ACCUMULATOR FOUND TO HAVE NIL CHARGE.						1	L	7	2 	4T	4	T		A21SO   	E4EA	6	C	P15EA	 
1999091700155	19990917	00155	SO  	1999	9	17	AU990797         	1	19990727	G	3231	4A11364002	ROD             			EMB   	110   	EMB110P1    	3260122	SO  	PWA   	PT6   	PT6A34      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	NLG DOOR	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					022					(AUS) NOSE LANDING GEAR DOOR ROD BROKEN.						1	L	7	2 	4T	4	T		A21SO   	E4EA	6	C	P15EA	 
1999091700156	19990917	00156	EA  	1999	9	17	AU990798         	3	19990730	G	6111	74DM6060	BLADE           	SNSNCH      	74DM6060    	PIPER 	PA28  	PA28140     	7102802	SO  						SNSNCH	74D	74DM        	EA  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					A45202			A45202		(AUS) PROPELLER HUB BOSSES AND BLADES CORRODED.  DYE CHECK REVEALED CRACK INDICATIONS IN TWO MOUNTING BOLT HOLES AND COR	ROSION ON MOUNTING FACE AND DOWEL HOLES.					1	L	7	1 	3O				2A13    		5	N	P88614	 
1999091700157	19990917	00157	CE  	1999	9	17	AU990799         	1	19990730	G	3242	RFS1030	DISC            			BEECH 	200   	B200C       	1152924	CE  	PWA   	PT6   	PT6A42      	52043	NE  					BRAKE	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) BRAKE ROTATING DISC BROKEN.  SUSPECT CAUSED BY OVERHEATING.						1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999091700158	19990917	00158	EU  	1999	9	17	AU990800         	1	19990710	G	2611	7211121100	SMOKE DETECTOR  			BAG   	JETSTM	JETSTM3107  	1500215	EU  	GARRTT	TPE331	TPE33112UA  	01514	WP  	ROTOL	R333	R333482F12  	GL  	CARGO BAY	FAULTY          	W				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			AU	S 										(AUS) BAGGAGE POD SMOKE DETECTOR FAULTY.						2	L	7	2 	4T	4	T	RT	BA15CAA 	E4WE	6	C	P61GL	 
1999091700159	19990917	00159	EU  	1999	9	17	AU990801         	1	19990811	G	5610	F5105324409	WINDOW          			FOKKER	F27   	F27MK50     		EU  										COCKPIT	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) COPILOT'S SLIDING WINDOW CRACKED AND DELAMINATED.						2	H	7	2 	4T			RT	A817    					 
1999091700160	19990917	00160	EU  	1999	9	17	AU990802         	1	19990811	G	5210	F5106043425	SEAL            			FOKKER	F27   	F27MK50     		EU  										PASSENGER DOOR	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) PASSENGER DOOR SEAL FAULTY.						2	H	7	2 	4T			RT	A817    					 
1999091700161	19990917	00161	NE  	1999	9	17	AU990803         	2	19990812	G	8500		SUMP            			DHAV  	DHC2  	DHC2*       	2800108	EA  	PWA   	R985  	R985AN14B   	52008	NE  					ENGINE	CONTAMINATED    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							23112			(AUS) METAL CONTAMINATION OF ENGINE SUMP.						1	H	7	1 	3R	3	R		A806    	5E1				 
1999091700162	19990917	00162	EU  	1999	9	17	AU990804         	1	19990726	G	2424		GCU             			BAG   	BAE146	BAE146100A  	1500260	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NR 2	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NR 2 AC BUS FAILED.  GENERATOR CONTROL UNIT REPLACED.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999091700163	19990917	00163	NE  	1999	9	17	AU990805         	2	19990804	G	7510	44E202A	SEPARATOR       			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  					LT ENGINE	FAULTY          	W				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			AU	S 										(AUS) LEFT ENGINE BLEED AIR LINE INTO DE-ICE SYSTEM WATER SEPARATOR BROKEN.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE				 
1999091700164	19990917	00164	SO  	1999	9	17	AU990806         	2	19990729	G	8540	537721	BEARING         			CESSNA	404   	404CESSNA   	2075901	CE  	CONT  	O520  	GTSIO520M   	17032	SO  	MCAULY	3FF32	3FF32C501   	GL  	LT ENGINE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					606656		606656			(AUS) LEFT ENGINE STARTER ADAPTER FRONT ROLLER BEARING FAILED.  METALCONTAMINATION OF ENGINE OIL SYSTEM.						1	L	7	2 	3O	3	O		A25CE   	E7CE	5	C	P45GL	 
1999091700165	19990917	00165	WP  	1999	9	17	AU990807         	2	19990803	G	7261	P70166	CHIP DETECTOR   			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UA  	01514	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	ENGINE	CONTAMINATED    	W				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			AU	S 					P70166					(AUS) ENGINE CHIP DETECTOR CONTAMINATED BY A SMALL PARTICLE OF METAL.						2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999091700166	19990917	00166	EU  	1999	9	17	AU990808         	1	19990729	G	5400		NACELLE         			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R375	R3754123F21 	NE  	RIGHT	FOD             	W				K				NONE                    				W	C		INADEQUATE Q C            	F.O.D.                    		IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT ENGINE FIRE DECK FOD.  A SCREWDRIVER WAS FOUND DURING THE PRE-FLIGHT INSPECTION.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P17NE	 
1999091700167	19990917	00167	EA  	1999	9	17	AU990809         	2	19990621	G	8500	IO540K1G5	ENGINE          			PIPER 	PA32  	PA32300     	7103212	SO  	LYC   	O540  	IO540K1G5   	41532	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	FORWARD	MAKING METAL    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			384  		L1252348A		L1252348A			(AUS) ENGINE OIL SYSTEM AND FILTER CONTAMINATED WITH METAL PARTICLES.						1	L	7	1 	3O	3	O		A3SO    	1E4	5	C	P920	 
1999091700168	19990917	00168	CE  	1999	9	17	AU990810         	1	19990806	G	3230	1013880073	CIRCLIP         		207006      	BEECH 	200   	B200C       	1152924	CE  	PWA   	PT6   	PT6A42      	52043	NE  					MLG	SEPARATED       	W				K				NONE                    				O			OTHER                     			LD	LANDING        	1			AU	S 					1475					(AUS) EMERGENCY UNDERCARRIAGE HAND PUMP PISTON RETAINING CIRCLIP DISLODGED ALLOWING LOSS OF HYDRAULIC FLUID.						1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999091700169	19990917	00169	SW  	1999	9	17	AU990811         	1	19990802	G	5520		TORQUE TUBE     			AIRTRC	AT500 	AT502       	0390303	SW  	PWA   	PT6   	PT6A15AG    	52043	NE  	HARTZL	HCB3T	HCB3TN3     	GL  	ELEVATOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELEVATOR TORQUE TUBE CRACKED.						1	L	7	1 	3T	4	T	NC	A9SW    	E4EA	6	C	P15EA	 
1999091700170	19990917	00170	NM  	1999	9	17	AU990812         	1	19990809	G	7120	87110016009	STRUT           			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					ENGINE MOUNT	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ENGINE MOUNT VERTICAL STRUT CRACKED.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999091700171	19990917	00171	EU  	1999	9	17	AU990813         	1	19990721	G	2750		SOLENOID        			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					TE FLAP	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FLAP EXTENSION SOLENOID FAULTY.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999091700172	19990917	00172		1999	9	17	AU990814         	1	19990817	G	7810	7210D1903	EXHAUST PIPE    								CONT  	O240  	IO240A      		SO  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ENGINE EXHAUST PIPE CRACKED IN THE AREA BELOW THE MOUNT FLANGE ATTACHMENT WELD. THE CRACK HAD PROGRESSED FOR APPRO	XIMATELY HALF OF THE PIPE CIRCUMFERENCE.										3	O			E7SO				 
1999091700173	19990917	00173	EA  	1999	9	17	AU990815         	2	19990817	G	7414	IO5136029	MAGNETO         			AVIONS	R2160 	R2160       	0960101	EU  	LYC   	O320  	O320D2A     	41508	EA  	SNSNCH	74D	74DM        	EA  	RIGHT	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			642  		L11633394		L1163339A	A57396		(AUS) RIGHT MAGNETO FAULTY.						1	L	7	1 	3O	3	O	RT	A48EU   	E274	5	N	P88614	 
1999091700174	19990917	00174	NE  	1999	9	17	AU990816         	2	19990810	G	7320	304355901	ACCUMULATOR     			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					NR 1 ENGINE	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					PS63295		PS63295			(AUS) NR 1 ENGINE FUEL SURGE ACCUMULATOR FAULTY. VISUAL POP-OUT ACTIVATED.						1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999091700175	19990917	00175	CE  	1999	9	17	AU990817         	1	19990813	G	5753		ROLLER          			CESSNA	500   	550         	2076604	CE  										TE FLAP	MISMANUFACTURED 	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT FLAP INBOARD AFT ROLLER ASSEMBLY AND ATTACHING HARDWARE MISSING.  SUSPECT LOCKING SPLIT PIN WAS NOT FITTED D	URING MANUFACTURE.					1	L	7	2 	4F				A22CE   					 
1999091700176	19990917	00176	EA  	1999	9	17	AU990818         	2	19990811	G	8550		HOSE            			PIPER 	PA28  	PA28R200    	7102811	SO  	LYC   	O360  	IO360C1C    	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	ENGINE OIL	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 							L1015951A			(AUS) PROPELLER GOVERNOR TO CRANKCASE OIL HOSE, INCORRECT PART.  THE HOSE WAS AN AEROQUIP TYPE 303 HOSE AND WAS AN UNAPP	ROVED PART IAW AD/LYC/86 AMDT2.					1	L	7	1 	3O	3	O		2A13    	1E10	5	C	P920	 
1999091700177	19990917	00177	SW  	1999	9	17	AU990819         	1	19990817	G	2910	27810322683	PIPE            			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UA  	01514	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	LT NACELLE	WORN            	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AU	S 										(AUS) HYDRAULIC PRESSURE PIPE LOCATED IN THE LEFT ENGINE BAY CHAFED AND LEAKING.						2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999091700178	19990917	00178	CE  	1999	9	17	AU990820         	1	19990812	G	2497		WIRE            			BEECH 	200   	B200C       	1152924	CE  	PWA   	PT6   	PT6A42      	52043	NE  					AC SYSTEM	WORN            	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) WIRE BUNDLE CHAFING ON PITOT/STATIC LINE IN AREA BELOW THE CIRCUIT BREAKER PANEL.						1	L	7	2 	4T	4	T	 	A24CE   	E4EA				 
1999091700179	19990917	00179	EA  	1999	9	17	AU990821         	2	19990813	G	7414	M3548	ROTOR           	SLICK       	4370        	PIPER 	PA28  	PA28161     	7102803	SO  	LYC   	O320  	O320D3G     	41508	EA  	SNSNCH	74D	74DM        	EA  	MAGNETO	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					96030002		L1112439A			(AUS) MAGNETO ROTOR BROKEN.						1	L	7	1 	3O	3	O		2A13    	E274	5	N	P88614	 
1999091700180	19990917	00180	EA  	1999	9	17	AU990822         	2	19990716	G	8520	L1575948A	CRANKCASE       								LYC   	O540  	IO540T4B5   	41532	EA  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					L1575948A		L1575948A			(AUS) CRANKCASE CRACKED.  CAMSHAFT LOBES CRACKED.											3	O			1E4				 
1999091700181	19990917	00181	EA  	1999	9	17	AU990823         	2	19990716	G	8530	L1575948A	CYLINDER        								LYC   	O540  	IO540T4B5   	41532	EA  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					L1575948A		L1575948A			(AUS) TWO CYLINDERS CRACKED IN THE AREA OF THE EXHAUST PORTS.											3	O			1E4				 
1999091700182	19990917	00182	NE  	1999	9	17	AU990824         	2	19990818	G	7261	0235230920	RECEPTACLE      								TMECA 	ARRIEL	ARRIEL1A    	60030	NE  					NR 2 ENGINE	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1748 		298		298			(AUS) NR 2 ENGINE GAS GENERATOR REAR BEARING MAGNETIC PLUG RECEPTACLE FAULTY.											3	U			E19EU				 
1999091700183	19990917	00183	NM  	1999	9	17	AU990825         	1	19990814	G	2421	31708001A	GENERATOR       			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					NR 1	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 			6148 		1135					(AUS) NR 1 AC GENERATOR FAILED.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999091700184	19990917	00184	CE  	1999	9	17	AU990826         	1	19990811	G	7710	70HF10	DIODE           			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	RT POWER SUPPLY	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) RIGHT POWER SUPPLY DIODE FAULTY.						1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15EA	 
1999112500001	19991125	00001	CE  	1999	11	25	AU990827         	1	19990819	G	7120	085112120	BEAM            			CESSNA	340   	340A        	2076405	CE  	CONT  	O520  	TSIO520N    	17040	SO  	MCAULY	3AF32C	3AF32C505   	GL  	ENGINE MOUNT	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ENGINE BEAM CORRODED.						1	L	7	2 	3O	3	O		3A25    	E8CE	5	C	P22EA	 
1999112500002	19991125	00002	CE  	1999	11	25	AU990828         	1	19990819	G	7120	085112131	BEAM            			CESSNA	340   	340A        	2076405	CE  	CONT  	O520  	TSIO520N    	17040	SO  	MCAULY	3AF32C	3AF32C505   	GL  	ENGINE MOUNT	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ENGINE BEAM CORRODED.						1	L	7	2 	3O	3	O		3A25    	E8CE	5	C	P22EA	 
1999112500003	19991125	00003	SW  	1999	11	25	AU990829         	1	19990818	G	3250	2752544003	ARM             			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UA  	01514	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	NLG STEERING	LOOSE           	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) NOSE WHEEL STEERING SYSTEM CENTERING ARM CAM FOLLOWER BACKED OUT AND BINDING ON THE CENTERING CAM RETAINING CAP SC	REWS.					2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999112500004	19991125	00004	EU  	1999	11	25	AU990830         	2	19990819	G	7250		TURBINE BLADE   			FOKKER	F28   	F28MK4000   	4990810	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					LT ENGINE	SEPARATED       	W				O				OTHER                   				E	F		VIBRATION/BUFFET          	FLT CONT AFFECTED         		CL	CLIMB          	1			AU	S 							9037			(AUS) LEFT ENGINE LOW PRESSURE TURBINE BLADE SEPARATED.   REMAINING BLADES AND GUIDE VANES DAMAGED.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999112500005	19991125	00005	EU  	1999	11	25	AU990831         	1	19990509	G	7712	7239060505	CONTROL PANEL   			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R375	R3754123F21 	NE  	COCKPIT	FAULTY          	W				C				ABORTED TAKEOFF         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		TO	TAKEOFF        	1			AU	S 					853716					(AUS) LEFT ENGINE CONSTANT TORQUE ON TAKEOFF (CTOT) PANEL FAULTY.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P17NE	 
1999112500006	19991125	00006	CE  	1999	11	25	AU990832         	1	19990507	G	5711		SPAR            			CESSNA	172   	172F        	2072414	CE  	CONT  	O300  	O300C       	17022	SO  					RT WING	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT WING MAIN SPAR AND SPAR CAP CONTAINED EXTENSIVE CORROSION.  RIBS AND SKIN ALSO CORRODED.						1	H	7	1 	3O	3	O	NT	3A12    	E253				 
1999112500007	19991125	00007	CE  	1999	11	25	AU990833         	1	19990701	G	2730		BRACKET         			CESSNA	172   	172F        	2072414	CE  	CONT  	O300  	O300C       	17022	SO  					ELEVATOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELEVATOR BELLCRANK ATTACHMENT BRACKET SUPPORT CRACKED.						1	H	7	1 	3O	3	O	NT	3A12    	E253				 
1999112500008	19991125	00008	EU  	1999	11	25	AU990834         	1	19990823	G	2752	951D10011	ACTUATOR        	VICKERS     	951D10011   	PILATS	PC12  	PC12        	7090550	EU  	PWA   	PT6   	PT6A67B     	52043	NE  					TE FLAP	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					0792A0716A					(AUS) TWO OF FOUR FLAP ACTUATORS HAD EXCESSIVE GEAR BACKLASH.						1	L	7	1 	3T	4	T	RT	A78EU   	E26NE				 
1999112500009	19991125	00009	EU  	1999	11	25	AU990835         	1	19990819	G	5520	TB203402113	HINGE           		TB10        	SOCATA	TB10  	TB10TOBAGO  	8680696	EU  	LYC   	O360  	O360A1A     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	ELEVATOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT ELEVATOR HINGE CRACKED FROM ATTACHMENT BOLT HOLES.						1	L	7	1 	3O	3	O	RT	A51EU   	E286	5	C	P920	 
1999112500010	19991125	00010	SO  	1999	11	25	AU990836         	1	19990817	G	2140	5751546	LINER           	JANITROL    	B3040       	PIPER 	PA34  	PA34200T    	7103406	SO  	CONT  	O360  	TSIO360E    	17025	SO  	HARTZL	HCC2Y	BHCC2YF2    	GL  	HEATING SYSTEM	UNSERVICEABLE   	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			138  		5751546					(AUS) CABIN HEATER COMBUSTION LINER FAILED.  FOUND DURING INSPECTION IAW AD/AIRCON/9 AMDT5.						1	L	7	2 	3O	3	O		A7SO    	E9CE	5	C	P920	 
1999112500011	19991125	00011	EU  	1999	11	25	AU990837         	1	19990818	G	5743	CAP10	FITTING         	MUDRY       	CAP10B      	MUDRY 	10    	CAP10B      		EU  	LYC   	O360  	AEIO360B2F  	41514	EA  					RT MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					262					(AUS) RIGHT MAIN LANDING GEAR ATTACHMENT BLOCK CRACKED FROM LOWER FORWARD INBOARD ATTACHMENT HOLE.						1	L	7	1 	3O	3	O		A36EU   	1E10				 
1999112500012	19991125	00012	EU  	1999	11	25	AU990838         	1	19990429	G	7712	7239060503	CONTROL PANEL   			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R390	R3904123F27 	NE  	COCKPIT	INOPERATIVE     	W				C				ABORTED TAKEOFF         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		TO	TAKEOFF        	1			AU	S 					0314					(AUS) RIGHT ENGINE CONSTANT TORQUE ON TAKEOFF (CTOT) CONTROL PANEL FAULTY.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P31NE	 
1999112500013	19991125	00013	NE  	1999	11	25	AU990839         	3	19990225	G	6111	DAP0066	BLADE           			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R390	R3904123F27 	NE  	PROPELLER	LIGHTNING STRIKE	W				O				OTHER                   				C			F.O.D.                    			CR	CRUISE         	1			AU	S 			7070 					DAP0066		(AUS) PROPELLER BLADE TIP DAMAGED BY LIGHTNING STRIKE CAUSING LOCALIZED BURNING TO THE COMPOSITE STRUCTURE.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P31NE	 
1999112500014	19991125	00014	EU  	1999	11	25	AU990840         	1	19990225	G	2420	51539007A	GCU             			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R390	R3904123F27 	NE  	DC REGULATOR	FAILED          	W				O				OTHER                   				C	H		F.O.D.                    	ELECT. POWER LOSS-50 PC   		CR	CRUISE         	1			AU	S 					2545					(AUS) RIGHT DC GENERATOR CONTROL UNIT FAILED. AIRCRAFT EXPERIENCED LIGHTNING STRIKE ON RIGHT PROPELLER.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P31NE	 
1999112500015	19991125	00015	CE  	1999	11	25	AU990841         	1	19990809	G	2720	0024100397	BELLCRANK       			BEECH 	58    	58          	1152740	CE  	CONT  	O550  	IO550C      		SO  	MCAULY	3AF32C	3AF32C512   	GL  	RUDDER	BROKEN          	W				C				ABORTED TAKEOFF         				F			FLT CONT AFFECTED         			TO	TAKEOFF        	1			AU	S 										(AUS) RUDDER CONTROL BELLCRANK LOCATED IMMEDIATELY AFT OF THE COPILOT'S RUDDER PEDALS FAILED.  INVESTIGATION FOUND EVIDE	NCE OF A PRE-EXISTING CRACK.					1	L	7	2 	3O	3	O		3A16    	E3SO	5	C	P22EA	 
1999112500016	19991125	00016	SW  	1999	11	25	AU990842         	1	19990706	G	2435	03601018	BEARING         		23079010    	FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UA  	01514	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	STARTER/GEN	FAILED          	W				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			AU	S 			865  		95041					(AUS) STARTER/GENERATOR REAR BEARING FAILED.  SUBMITTER SUSPECTED CAUSED BY LACK OF LUBRICATION.						2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999112500017	19991125	00017	NM  	1999	11	25	AU990843         	1	19990729	G	5311		FRAME           			BOEING	737   	73733A      	1384673	NM  										BS 616	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE FRAME LOCATED AT BS 616 LEFT CRACKED AT THE INNER CHORD.  CRACK LENGTH APPROXIMATELY 32 MM (1.259 INCHES)	.  FOUND DURING EDDY CURRENT INSPECTION.					2	L	7	2 	4F			RT	A16WE   					 
1999112500018	19991125	00018	NM  	1999	11	25	AU990844         	1	19990731	G	7830		SENSOR          			BOEING	767   	767277      		NM  	GE    	CF6   	CF680A      	30025	NE  					THRUST REVERSER	OUT OF ADJUST   	W				O				OTHER                   				E	N		VIBRATION/BUFFET          	FALSE WARNING             		CL	CLIMB          	1			AU	S 							580191			(AUS) RIGHT ENGINE THRUST REVERSER LOCK PROXIMITY SENSOR OUT OF ADJUSTMENT.						2	L	7	2 	4F	4	F	RT	A1NM    	E13NE				 
1999112500019	19991125	00019	EU  	1999	11	25	AU990845         	1	19990805	G	7603		CABLE           			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					POWER LEVER	STIFF           	W				O				OTHER                   				O			OTHER                     			DE	DESCENT        	1			AU	S 							LF05507AC			(AUS) NR 3 ENGINE POWER LEVER STIFF.  SUSPECT LOWER CONTROL CABLE RUBBER THERMOFIT SLEEVE FOULING OR LACK OF LUBRICATION	 AND/OR DIRT CONTAMINATION OF THE CABLE.					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999112500020	19991125	00020	NM  	1999	11	25	AU990846         	1	19990729	G	5313		STRINGER        			BOEING	737   	73733A      	1384673	NM  										BS 727	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE STRINGER 18A LT AND RT LOCATED AT BS 727 CRACKED IN THE INBOARD HOLE.   FOUND DURING EDDY CURRENT INSPECT	ION.					2	L	7	2 	4F			RT	A16WE   					 
1999112500021	19991125	00021		1999	11	25	AU990848         	4	19990322	G	6122	C290D4GT4	CSU             			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520L      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	PROP GOVERNOR	FAILED          	W				O				OTHER                   				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CL	CLIMB          	1			AU	S 					840886					(AUS) PROPELLER GOVERNOR (CSU) FAILED.   PROPELLER REMAINED IN COARSE PITCH.   STRIP INVESTIGATION FOUND EXTENSIVE DAMAG	E IN GEAR POCKETS AND IDLER GEAR SHAFT.   IDLER GEAR DAMAGED AND BEARING CENTER AND ROLLERS MISSING.  BASE FACEPLATE SCO	RED AND DRIVE GEAR BEARING  SURFACES ALSO CONTAIN SLIGHT SCORING.				1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P47GL	 
1999112500022	19991125	00022	CE  	1999	11	25	AU990849         	1	19990116	G	5720	SA00487SE	VORTEX GENERATOR			CESSNA	441   	441         	2076020	CE  	GARRTT	TPE331	TPE3318     	01514	WP  	HARTZL	HCB3T	HCB3TN5     	GL  	WING	MISINSTALLED    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) VORTEX GENERATOR KIT INCORRECTLY INSTALLED.						1	L	7	2 	3T	4	T	RT	A28CE   	E4WE	6	C	P15EA	 
1999112500023	19991125	00023	NM  	1999	11	25	AU990850         	1	19990809	G	2460		HARNESS         			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	LT ENGINE	WORN            	W				O				OTHER                   				H			ELECT. POWER LOSS-50 PC   			DE	DESCENT        	1			AU	S 										(AUS) WIRING LOOM LOCATED IN FLAP RECESS INBOARD OF THE LT ENGINE WAS CHAFED AND BADLY BURNT.  TWO POWER WIRES FOR THE L	T STANDBY HYDRAULIC PUMP AND ONE POWER WIRE FOR THE RT STANDBY HYDRAULIC PUMP OPEN CIRCUITED.   WIRE 7611-10006D22-2 (EC	U WIRING) WAS ALSO OPEN CIRCUITED.   OTHER WIRES IN THE LOOM WERE CHAFED OR HEAT AFFECTED.				2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
1999112500024	19991125	00024	EA  	1999	11	25	AU990851         	2	19990811	G	8500	L1415515	ENGINE          			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  	MCAULY	1A103	1A103TCM    	GL  	FORWARD	NOISY           	W				O				OTHER                   				E			VIBRATION/BUFFET          			CL	CLIMB          	1			AU	S 					L1415515		L1415515			(AUS) ENGINE EXPERIENCED UNUSUAL NOISES.   INSPECTION AND GROUND RUN COULD FIND NO EVIDENCE OF DEFECT.  DEFECT NOT CONFI	RMED.					1	H	7	1 	3O	3	O	NT	3A19    	E223	5	N	P50GL	 
1999112500025	19991125	00025	CE  	1999	11	25	AU990852         	1	19990815	G	5540		BRACKET         			BEECH 	55    	D55         	1152730	CE  	CONT  	O520  	IO520C      	17032	SO  	MCAULY	2AF34C	2AF34C55    	GL  	RUDDER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							1259307CLH	782991LH6945		(AUS) CENTER RUDDER SUPPORT BRACKET CONTAINED SEVERE EXFOLIATION CORROSION.  TWO RIVETS MISSING. MAIN FUEL CELLS ALSO LE	AKING.					1	L	7	2 	3O	3	O		3A16    	E5CE	5	C	P5EA	 
1999112500026	19991125	00026	EA  	1999	11	25	AU990853         	2	19990826	G	7261		FILTER          			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	ENGINE OIL	CONTAMINATED    	W				A				UNSCHED LANDING         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CR	CRUISE         	1			AU	S 			13   				PCE81520			(AUS) ENGINE CHIP DETECTOR AND OIL FILTER METAL CONTAMINATION.   SUBMITTER SUSPECTED THE ENGINE HAD BEEN DROPPED FOLLOWI	NG OVERHAUL.					1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15EA	 
1999112500027	19991125	00027	SO  	1999	11	25	AU990854         	1	19990818	G	2560		CO2 DETECTOR    		TSIO360E    	PIPER 	PA34  	PA34200T    	7103406	SO  	CONT  	O360  	TSIO360E    	17025	SO  	HARTZL	HCC2Y	BHCC2YF2    	GL  	CABIN	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) CARBON DIOXIDE DETECTOR FAULTY.						1	L	7	2 	3O	3	O		A7SO    	E9CE	5	C	P920	 
1999112500028	19991125	00028	NE  	1999	11	25	AU990855         	2	19990815	G	7321	6071T20P17	DECU            			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R375	R3754123F21 	NE  	RT ENGINE	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							GEC087325			(AUS) RT ENGINE DIGITAL ENGINE CONTROL UNIT INTERNAL FAILURE.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P17NE	 
1999112500029	19991125	00029	SO  	1999	11	25	AU990856         	1	19990824	G	5610	11595CB31023	WINDSHIELD      			GULSTM	G1159 	GIV         	3980115	SO  	RROYCE	TAY   	TAY6118     		EU  					COCKPIT	CONTAMINATED    	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			AU	S 										(AUS) MOISTURE INGRESS INTO LOWER INBOARD CORNER OF LT CAPTAIN'S WINDSHIELD.						2	L	7	2 	4F	4	F	RT	A12EA   	E25NE				 
1999112500030	19991125	00030	SO  	1999	11	25	AU990857         	1	19990818	G	7170	1159P417569	PIPE            			GULSTM	G1159 	GIV         	3980115	SO  	RROYCE	TAY   	TAY6118     		EU  					ACCESSORY G/B	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ACCESSORY GEARBOX DRIVE PAD DRAIN PIPE CRACKED.  PIPE IS MANUFACTURED FROM STAINLESS STEEL.						2	L	7	2 	4F	4	F	RT	A12EA   	E25NE				 
1999112500031	19991125	00031	SO  	1999	11	25	AU990858         	2	19990722	G	8520		CRANKCASE       								CONT  	O520  	IO520C      	17032	SO  					ENGINE	FRETTED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							29887612			(AUS) CRANKCASE SADDLE FRETTED AND TUNNEL MEASUREMENTS OUT OF LIMITS.  COUNTERWEIGHTS ALSO UNSERVICEABLE IAW CONTINENTAL	 SB 93-4.										3	O			E5CE				 
1999112500032	19991125	00032	CE  	1999	11	25	AU990859         	1	19990824	G	5730		SKIN            			CESSNA	340   	340A        	2076405	CE  	CONT  	O520  	TSIO520N    	17040	SO  	MCAULY	3AF32C	3AF32C93    	GL  	RT & LT WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT AND RIGHT WING TOP SKINS CRACKED IN THE AREA ADJACENT TO THE WING LOCKERS.						1	L	7	2 	3O	3	O		3A25    	E8CE	5	C	P22EA	 
1999112500033	19991125	00033	EA  	1999	11	25	AU990860         	2	19990827	G	8520	LW10290	GEAR            								LYC   	O540  	IO540K1G5   	41532	EA  					ENGINE	MISMARKED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					L1454048A		L1454048A			(AUS) TIMING GEAR INCORRECTLY MARKED.  THE TIMING MARK ON THE NEW PN OLW-10290 GEAR WAS ONE TOOTH OUT.											3	O			1E4				 
1999112500034	19991125	00034	CE  	1999	11	25	AU990861         	1	19990707	G	5711	501100032	SPAR            		N35         	BEECH 	35    	N35         	1151528	CE  	CONT  	O470  	IO470N      	17026	SO  	MCAULY	2A36C	2A36C23     	GL  	LT WING	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					D6776					(AUS) LEFT WING SPAR CAP CONTAINED SEVERE INTERGRANULAR CORROSION ON THE VERTICAL FLANGE.						1	L	7	1 	3O	3	O		3A15    	3E1	5	C	P880	 
1999112500035	19991125	00035	CE  	1999	11	25	AU990862         	1	19990812	G	2140	8259DL	SWITCH          			CESSNA	411   	411         	2075902	CE  	CONT  	O520  	GTSIO520C   	17032	SO  	MCAULY	3AF34C	3AF34C74    	GL  	HEATING SYSTEM	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					247					(AUS) COMBUSTION HEATER FAULTY.   AIR VALVE SWITCH JAMMED IN THE ON POSITION.  VENT MOTOR MAIN POSITIVE LEAD NOT LOCKED 	TO THE POWER SOURCE CAUSING ARCING ON THE POST.   MAIN HEAD GASKET CRACKED AND PERISHED.  FUEL NOZZLE CONTAMINATED WITH 	RUST AND SCUM.  OVERHEAT SWITCH FAULTY WITH NO GASKET FITTED.				1	L	7	2 	3O	3	O		A7CE    	E7CE	5	C	P22EA	 
1999112500036	19991125	00036	CE  	1999	11	25	AU990863         	1	19990803	G	3246		SPRING          			CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	WATER RUDDER	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT WATER RUDDER SPRING BROKEN.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
1999112500037	19991125	00037	CE  	1999	11	25	AU990864         	1	19990803	G	3250		CONTROL CABLE   			CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	NLG STEERING	SEIZED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT WATER RUDDER CONTROL CABLE SEIZED.						1	H	7	1 	3O	3	O	 	A4CE    	E5CE	5	C	P47GL	 
1999112500038	19991125	00038	SO  	1999	11	25	AU990865         	2	19990826	G	8530	649168P15	CYLINDER        			CESSNA	182   	182Q        	2072732	CE  	CONT  	O470  	O470U       	17026	SO  	MCAULY	2A34C	C2A34C204   	GL  	ENGINE	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AU	S 					273081R		273081R			(AUS) ALL ENGINE CYLINDERS LEAKING BETWEEN THE BARREL AND HEAD.						1	H	7	1 	3O	3	O	NT	3A13    	E273	5	C	P3EA	 
1999112500039	19991125	00039	SO  	1999	11	25	AU990866         	2	19990826	G	8530	649168P15	CYLINDER        								CONT  	O470  	O470U       	17026	SO  					ENGINE	MISOVERHAULED   	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) TWO OVERHAULED CYLINDERS WERE NOT WITHIN SERVICE LIMITS.  THE CYLINDERS CONTAINED SERVICEABLE TAGS.  THESE CYLINDE	RS WERE TO BE USED AS REPLACEMENT CYLINDERS FOR MDR 99/0865.										3	O			E273				 
1999112500040	19991125	00040	EU  	1999	11	25	AU990867         	1	19990326	G	5552	TB203402113	HINGE           			SOCATA	TB10  	TB10TOBAGO  	8680696	EU  	LYC   	O360  	O360A1A     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	RT ELEVATOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT ELEVATOR HINGE CRACKED FROM ATTACHMENT BOLT HOLE.						1	L	7	1 	3O	3	O	RT	A51EU   	E286	5	C	P920	 
1999112500041	19991125	00041	NM  	1999	11	25	AU990868         	1	19990807	G	7830	32785002	SHAFT           			BOEING	767   	767324      		NM  	GE    	CF6   	CF680C2*    		GL  					THRUST REVERSER	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							704303			(AUS) THRUST REVERSER LEFT UPPER INBOARD FLEXSHAFT LOCATED BETWEEN THE ELECTRO MECHANICAL BRAKE AND THE UPPER ANGLE GEAR	BOX BROKEN.					2	L	7	2 	4F	4	F	RT	A1NM    	E23EA				 
1999112500042	19991125	00042	SO  	1999	11	25	AU990870         	1	19990819	G	2810		FUEL TANK       			PIPER 	PA28  	PA28181     	7102807	SO  	LYC   	O360  	O360A4M     	41514	EA  	SNSNCH	76E	76EM8       	EA  	WING	MISMARKED       	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) EACH FUEL TANK HELD THREE LITRES LESS CONTENTS THAN FACTORY SPECIFICATIONS (TOTAL OF SIX LITRES LESS OVERALL).  IN	SPECTION OF TANKS FOUND NIL DAMAGE OR NON-STANDARD CONSTRUCTION.   FOUND DURING FUEL CALIBRATION TEST.					1	L	7	1 	3O	3	O		2A13    	E286	5	N	P4EA	 
1999112500043	19991125	00043	SO  	1999	11	25	AU990871         	2	19990821	G	8530	464099	CYLINDER        			CESSNA	182   	182P        	2075816	CE  	CONT  	O470  	O470S       	17026	SO  	MCAULY	2A34C	2A34C203    	GL  	ENGINE	FAILED          	W				O				OTHER                   				E	Y		VIBRATION/BUFFET          	ENGINE STOPPAGE           		CR	CRUISE         	1			AU	S 					464099		464099	772577		(AUS) NR 2 CYLINDER CONNECTING ROD BROKEN.  CRANKCASE HOLED IN THE AREA BELOW THE MAGNETOS.  NR 2 CYLINDER AND THE SURRO	UNDING AREA DAMAGED.  SUBMMITTER SUSPECTED CAUSED BY INCOMPATIBILITY BETWEEN THE CYLINDER BORE SURFACE TREATMENT AND THE	 PISTON RING MATERIAL.				1	H	7	1 	3O	3	O	NT	TA13    	E273	5	C	P3EA	 
1999112500044	19991125	00044	NE  	1999	11	25	AU990872         	2	19990812	G	7510	2351A000	VALVE           			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					NR 3 ENGINE	FAULTY          	W				C				ABORTED TAKEOFF         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		TO	TAKEOFF        	1			AU	S 			14727		02801357					(AUS) NR 3 ENGINE INTAKE ANTI-ICING VALVE FAULTY.						2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999112500045	19991125	00045	SO  	1999	11	25	AU990873         	1	19990830	G	7797		WIRE            			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      	 	NE  	HAMSTD	14SF	14SF9       	NE  	LT ENGINE	LOOSE           	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			AU	S 										(AUS) LEFT ENGINE THERMOCOUPLE WIRE LOOSE AT JUNCTION BOX LOCATED IN INBOARD AFT NACELLE.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	N	P11NE	 
1999112500046	19991125	00046	SO  	1999	11	25	AU990874         	2	19990830	G	8550	606199	FILTER          			CESSNA	404   	404CESSNA   	2075901	CE  	CONT  	O520  	GTSIO520M   	17032	SO  	MCAULY	3FF32	3FF32C501   	GL  	ENGINE OIL	CONTAMINATED    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					606199		606199			(AUS) ENGINE OIL FILTER CONTAMINATED WITH FERROUS METAL PARTICLES.   SUBMITTER SUSPECTED BEARING FAILURE.						1	L	7	2 	3O	3	O		A25CE   	E7CE	5	C	P45GL	 
1999112500047	19991125	00047	SO  	1999	11	25	AU990875         	2	19990830	G	8530	653443A13	CYLINDER        			CESSNA	182   	182P        	2075816	CE  	CONT  	O470  	O470R       	17026	SO  	MCAULY	2A34C	2A34C66     	GL  	ENGINE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					459135		459135			(AUS) CYLINDER EXHAUST VALVE AND VALVE GUIDE WORN PREMATURELY.  THE CYLINDER HAD TWO VALVE AND VALVE GUIDE REPLACEMENTS 	FOR WORN ITEMS IN 474 HOURS OF OPERATION.					1	H	7	1 	3O	3	O	NT	TA13    	E273	5	C	P3EA	 
1999112500048	19991125	00048	SO  	1999	11	25	AU990876         	1	19990725	G	5311		FRAME           			PIPER 	PA25  	PA25150     	7102503	SO  	LYC   	O320  	O320A2B     	41508	EA  	MCAULY	1A170	1A170GM     	GL  	FUSELAGE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE FRAME TUBE CORRODED AS INDICATED IN AD/PA25/17 AMDT4.						1	H	7	1 	3O	3	O		EXPA1H71	E274	5	N	P857	 
1999112500049	19991125	00049	CE  	1999	11	25	AU990877         	1	19990803	G	3340		LIGHT           			CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	TAIL	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) TAIL NAVIGATION LIGHT LENS BROKEN.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
2000010800530	20000108	00530	SO  	2000	1	8	AU990878         	2	19990820	G	8530		ROCKER ARM      			PAC   	CT4   	CT4A        	05623UC	GL  	CONT  	O360  	IO360HB     	17025	SO  					ENGINE	FRACTURED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			442  				265116R			(AUS) NR 5 CYLINDER EXHAUST VALVE ROCKER ARM FRACTURED.  SUBMITTER SUSPECTED ROCKER ARM BUSHING INCORRECTLY FITTED, COVE	RING THE OIL HOLE AND PREVENTING LUBRICATION.  (X)					1	Q	7	1 	3I	3	O	RT	A9PC    	E1CE				 
1999112500050	19991125	00050	EU  	1999	11	25	AU990879         	1	19990902	G	3211	7257500181	FITTING         			SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  	ROTOL	R375	R3754123F21 	NE  	MLG	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LANDING GEAR SUPPORT FITTING CORRODED.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE	6	C	P17NE	 
1999112500051	19991125	00051	SW  	1999	11	25	AU990880         	1	19990902	G	5711	2733000	SPAR            			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UHR 		WP  	MCAULY	4HFR34	4HFR34C652  	NE  	WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WING SPAR WEB CRACKED IN THE AREA BETWEEN STRINGER NR 14 CUT-OUT AND THE ADJACENT TRIM CABLE CUT-OUT.  CRACK LENGT	H 1.016 MM (0.040 INCH).					2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999112500052	19991125	00052	NM  	1999	11	25	AU990881         	1	19990902	G	2435	300SGL127Q1	STARTER/GEN     			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	DC SYSTEM	MISOVERHAULED   	W				O				OTHER                   				H	J		ELECT. POWER LOSS-50 PC   	WARNING INDICATION        		NR	NOT REPORTED   	1			AU	S 			351  							(AUS) STARTER/GENERATOR BRUSH HOLDER RUBBED THROUGH BY PIGTAIL.  SUBMITTER SUSPECTED INCORRECT FITMENT OF BRUSH HOLDER D	URING OVERHAUL.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
1999112500053	19991125	00053	NE  	1999	11	25	AU990882         	2	19990824	G	7321	7086M60G11	DECU            			SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT75A2      	30030	NE  	ROTOL	R354	R3544123F13 	NE  	RT ENGINE	FAULTY          	W				C				ABORTED TAKEOFF         				E			VIBRATION/BUFFET          			TO	TAKEOFF        	1			AU	S 			10253		NOECDE5018		367412			(AUS) RIGHT ENGINE CONTROL UNIT FAULTY.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE6	6	C	P61GL	 
1999112500054	19991125	00054	SW  	1999	11	25	AU990883         	1	19990823	G	6320	206040562101	GEAR            		206040002029	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					M/R GEARBOX	FRACTURED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1500 		BKW12156		CAE832928			(AUS) MAIN TRANSMISSION UPPER SPLINE GEAR TOOTH FRACTURED.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999112500055	19991125	00055	EU  	1999	11	25	AU990884         	1	19990902	G	5520	TB203402112	HINGE           		TB10        	SOCATA	TB10  	TB10TOBAGO  	8680696	EU  	LYC   	O360  	O360A1A     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	ELEVATOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT ELEVATOR HINGE CRACKED THROUGH FROM THE ATTACHMENT BOLT HOLE.						1	L	7	1 	3O	3	O	RT	A51EU   	E286	5	C	P920	 
1999112500056	19991125	00056	NM  	1999	11	25	AU990885         	1	19990611	G	3230	BACB10A554	BEARING         			BOEING	737   	737377      		NM  										NLG	SEIZED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR MANUAL EXTENSION SYSTEM LEFT AND RIGHT TORQUE TUBE SUPPORT BEARINGS SEIZED.  SUBMITTER SUSPECTED	 CAUSED BY LACK OF LUBRICATION CAUSED BY WASHING.					2	L	7	2 	4F			RT	A16WE   					 
1999112500057	19991125	00057	NM  	1999	11	25	AU990886         	1	19990727	G	2997	216268	WIRE            			BOEING	737   	737377      	       	NM  										HYDRAULIC PUMP	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1671 		216268					(AUS) SYSTEM 'B' ELECTRIC HYDRAULIC PUMP OUTPUT PRESSURE LINE CHAFING ON POWER CABLE W0334 WIRE BUNDLE CAUSING SHORT CIR	CUIT.					2	L	7	2 	4F			RT	A16WE   					 
1999112500058	19991125	00058	NM  	1999	11	25	AU990887         	1	19990901	G	2910	82950010291	PIPE            			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	HYDRAULIC SYSTEM	CRACKED         	W				K				NONE                    				O	K		OTHER                     	FLUID LOSS                		IN	INSP/MAINT     	1			AU	S 										(AUS) NR 1 HYDRAULIC SYSTEM PRESSURE PIPE TO THE OUTBOARD ROLL SPOILER ACTUATOR CRACKED AT PIPE RADIUS LOCATED SLIGHTLY 	INBOARD OF WING STATION Y347.70.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
1999112500059	19991125	00059	WP  	1999	11	25	AU990888         	1	19990829	G	3220	H36566A	TUBE            			DHAVXX	DH82  	DH82AROBRTSN	2801002	WP  	DHAVXX	GIPSY 	GIPSYMAJOR1 	20004	WP  					TAIL SKID	BROKEN          	W				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			AU	S 										(AUS) TAIL SKID VERTICAL PIVOT TUBE FAILED AT WELD.						1	Q	7	1 	3I	3	I		A8EU    	A8EU				 
1999112500060	19991125	00060	EU  	1999	11	25	AU990889         	1	19990902	G	5541	A06020403	SHAFT           		AB6000401   	FOKKER	F28   	F28MK4000   	4990810	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					RUDDER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					0232					(AUS) RUDDER POST CORRODED IN AREA OF LOWER BUSHING.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999112500061	19991125	00061	CE  	1999	11	25	AU990890         	1	19990803	G	5520		BEARING         			CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	ELEVATOR	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELEVATOR BEARING WORN.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
1999112500062	19991125	00062	CE  	1999	11	25	AU990891         	1	19990720	G	5720	95110014295	ANGLE           			BEECH 	58    	58          	1152740	CE  	CONT  	O520  	IO520C      	17032	SO  					LT WING	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT WING SPAR UPPER REAR SPAR CAP ANGLE CORRODED.  AN ATTEMPT HAD BEEN MADE TO HIDE THE CORROSION USING MASKING T	APE AND PAINT.					1	L	7	2 	3O	3	O		3A16    	E5CE				 
1999112500063	19991125	00063	CE  	1999	11	25	AU990892         	1	19990908	G	7111	991026815	CONTROL UNIT    		IO520M      	CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	COWL FLAP	SEIZED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) BOTH COWL FLAP CONTROLS UNSERVICEABLE.  ONE CONTROL SEIZED.  ONE CONTROL BROKEN WITH THE 'T' HANDLE REPLACED.						1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22EA	 
1999112500064	19991125	00064	CE  	1999	11	25	AU990893         	1	19990908	G	2710		CONTROL CABLE   		310R        	CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	AILERON	MISINSTALLED    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AILERON CABLES INCORRECTLY INSTALLED AT LEFT AND RIGHT BELLCRANKS IN WINGS.  CABLES CROSSED BETWEEN WING STATIONS 	47.83 AND 73.50 AND ALSO BETWEEN WING STATIONS 122.50 AND 133.50.					1	L	7	2 	3O	3	O	 	3A10    	E5CE	5	C	P22EA	 
1999112500065	19991125	00065	NM  	1999	11	25	AU990894         	1	19990825	G	2910	82950010173	PIPE            			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	HYDRAULIC SYSTEM	FAILED          	W				K				NONE                    				K			FLUID LOSS                			LD	LANDING        	1			AU	S 										(AUS) NR 1 HYDRAULIC SYSTEM RETURN LINE FROM THE OUTBOARD ROLL SPOILER ACTUATOR LOCATED OUTBOARD OF LEFT WING STATION Y2	79 SEPARATED FROM A PREVIOUS PERMASWAGE REPAIR.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
1999112500066	19991125	00066	CE  	1999	11	25	AU990895         	1	19990803	G	2731		TRIM            			CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	ELEVATOR	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELEVATOR TRIM SYSTEM WORN BEYOND LIMITS.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
1999112500067	19991125	00067	NE  	1999	11	25	AU990896         	3	19990903	G	6111	L106FA0	BLADE           			BAG   	JETSTM	JETSTM3201  	1500217	EU  	GARRTT	TPE331	TPE33112UA  	01514	WP  	MCAULY	4HFR34	4HFR34C653  	NE  	PROPELLER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			3995 		920167		P66114C	920167		(AUS) PROPELLER BLADE CRACKED ON THE CAMBER SIDE OF THE BLADE IN THE MID-SPAN POSITION.  THE CRACK RUNS IN A CHORDWISE D	IRECTION APPROXIMATELY 381 MM (15 INCHES) FROM THE TIP.					2	L	7	2 	4T	4	T	RT	A56EU   	E4WE	6	C	3PNE	 
1999112500068	19991125	00068	EA  	1999	11	25	AU990897         	2	19990825	G	8520	L14068A	CYLINDER STUD   			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	LTIO540J2BD 	41533	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	RT ENGINE	SHEARED         	W				O				OTHER                   				E	K		VIBRATION/BUFFET          	FLUID LOSS                		CR	CRUISE         	1			AU	S 			1529 		L14068A		L14068A			(AUS) RIGHT ENGINE NR 2 CYLINDER ATTACHMENT STUDS (4 OFF) SHEARED.						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
1999112500069	19991125	00069	NM  	1999	11	25	AU990898         	1	19990902	G	3297	82455027001	WIRE            			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      	 	NE  	HAMSTD	14SF	14SF7       	NE  	LT MLG	BROKEN          	W				O				OTHER                   				N			FALSE WARNING             			DE	DESCENT        	1			AU	S 										(AUS) LEFT MAIN LANDING GEAR WEIGHT ON WHEELS SYSTEM WIRE BROKEN AT CONNECTOR 3261-P16.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
1999112500070	19991125	00070	NM  	1999	11	25	AU990899         	1	19990901	G	6320	A1843	BEARING         			ROBSIN	R22   	R22BETA     		NM  	LYC   	O320  	O320B2C     	41508	EA  					M/R GEARBOX	COLLAPSED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) TRANSMISSION SPRAG CLUTCH BEARING OVERHEATED WITH SUBSEQUENT FAILURE AND DISINTEGRATION OF TWO BALLS.						1	G	7	1 	3O	3	O		H10WE   	E274				 
1999112500071	19991125	00071	EU  	1999	11	25	AU990900         	1	19990910	G	2612	899253	DETECTOR WIRE   			SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT75A2      	30030	NE  	ROTOL	R320	R3204123F1  	NE  	RT ENGINE	DAMAGED         	W				O				OTHER                   				N			FALSE WARNING             			DE	DESCENT        	1			AU	S 										(AUS) RIGHT ENGINE FIRE DETECTOR SYSTEM AFT DETECTOR WIRE KINKED.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE6	6	C	P5NE	 
1999112500072	19991125	00072	EU  	1999	11	25	AU990902         	1	19990831	G	2752	951010011	ACTUATOR        			PILATS	PC12  	PC12        	7090550	EU  	PWA   	PT6   	PT6A67B     	52043	NE  					TE FLAP	MALFUNCTIONED   	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					0809AAND0804					(AUS) FLAP ACTUATOR EXCEEDED BACKLASH LIMITS IAW PILATUS AMM TR 27-12 P9 WITH ONE ACTUATOR EXHIBITING HIGH GREASE LEAKAG	E.					1	L	7	1 	3T	4	T	RT	A78EU   	E26NE				 
1999112500073	19991125	00073	SO  	1999	11	25	AU990903         	2	19990819	G	8530	S643767	VALVE GUIDE     			CESSNA	210   	210N        	2073453	CE  	CONT  	O520  	IO520L      	17032	SO  	MCAULY	3A32C	D3A32C88    	GL  	NR 2 CYLINDER	BROKEN          	W				O				OTHER                   				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		DE	DESCENT        	1			AU	S 							294578R			(AUS) NR 2 CYLINDER EXHAUST VALVE GUIDE BROKEN.						1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P21EA	 
1999112500074	19991125	00074	NE  	1999	11	25	AU990904         	2	19990827	G	7321	78249046	EEC             			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  	HAMSTD	14SF	14SF9       	NE  	NR 1 ENGINE	FAULTY          	W				C				ABORTED TAKEOFF         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		TO	TAKEOFF        	1			AU	S 			5159 		90013401					(AUS) NR 1 ENGINE ELECTRONIC CONTROL UNIT FAILED.  PROPELLER CONTROL UNIT ALSO CHANGED.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	N	P11NE	 
1999112500075	19991125	00075	SO  	1999	11	25	AU990905         	2	19990830	G	8530	653443A13	CYLINDER        			CESSNA	182   	182P        	2075816	CE  	CONT  	O470  	O470R       	17026	SO  	MCAULY	2A34C	2A34C66     	GL  	ENGINE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					459135		459135			(AUS) CYLINDER EXHAUST VALVE AND VALVE GUIDE WORN.  CYLINDER HAD TWO VALVES AND VALVE GUIDES REPLACED IN ONLY 474 HOURS 	OF OPERATION.					1	H	7	1 	3O	3	O	NT	TA13    	E273	5	C	P3EA	 
1999112500076	19991125	00076	SO  	1999	11	25	AU990906         	1	19990908	G	2460		CONNECTOR       			GULSTM	GA7   	GA7         	3960401	SO  	LYC   	O320  	O320D1D     	41508	EA  					DC SYSTEM	FAULTY          	W				K				NONE                    				H			ELECT. POWER LOSS-50 PC   			CL	CLIMB          	1			AU	S 										(AUS) FIREWALL ELECTRICAL CONNECTOR FAULTY.  TOTAL ELECTRICAL FAILURE.						1	L	7	2 	3O	3	O		A17SO   	E274				 
1999112500077	19991125	00077		1999	11	25	AU990907         	4	19990902	G	3418	0179	STALL WARNING   			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  	HAMSTD	14SF	14SF9       	NE  	COCKPIT	FAULTY          	W				A				UNSCHED LANDING         				N			FALSE WARNING             			CR	CRUISE         	1			AU	S 					0179					(AUS) STALL WARNING ALARM SYSTEM FAILED.  ALARM PANEL REPLACED AND INSPECTED WITH NIL FAULT FOUND.  NR 1 AND NR 2 STALL 	WARNING COMPUTERS REPLACED AS A PRECAUTION.					2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	N	P11NE	 
1999112500078	19991125	00078	SW  	1999	11	25	AU990908         	1	19990908	G	7330		WIRE            			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UHR 	 	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	FUEL INDICATOR	WORN            	W				A				UNSCHED LANDING         				E	N		VIBRATION/BUFFET          	FALSE WARNING             		CL	CLIMB          	1			AU	S 							P70052			(AUS) ENGINE FUEL BYPASS VALVE WIRE WORN AND SHORT CIRCUITING.						2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
2000010800529	20000108	00529		2000	1	8	AU990909         	1	19990906	G	7820	7200D1701	MUFFLER         			AMTR  		EAGLEXTS150 												EXHAUST	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS)  EXHAUST MUFFLER CRACKED AT SHROUD SUPPORT WELD.  CRACK LENGTH 6.35 MM (0.25 INCH).  PART TOTAL CYCLES:  494.  (X)									0 										 
1999112500079	19991125	00079	WP  	1999	11	25	AU990910         	2	19990906	G	7230	8682201	IMPELLER        			AIRTRC	AT300 	AT301       	0390103	SW  	GARRTT	TPE331	TPE3312201A 		WP  	HARTZL	HCB3T	HCB3TN5     	GL  	COMPRESSOR	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							P90201			(AUS) COMPRESSOR SECOND STAGE IMPELLER VANES (2 OFF) FRACTURED AND SEPARATED.  CAUSED BY EROSION OF VANES.   DAMAGE TO I	NTERNAL COMPONENTS.					1	L	7	1 	3R	4	T		A9SW    	E3WE	6	C	P15EA	 
1999112500080	19991125	00080	EU  	1999	11	25	AU990911         	1	19990907	G	2421	6043T28P05	STATOR          			SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT75A2      	30030	NE  	ROTOL	R354	R3544123F13 	NE  	LT ENGINE	FAILED          	W				K				NONE                    				E			VIBRATION/BUFFET          			CL	CLIMB          	1			AU	S 					367412		367412			(AUS) LEFT ENGINE DRIVEN ALTERNATOR STATOR FAULTY.						2	L	7	2 	4T	4	T	RT	A52EU   	E8NE6	6	C	P61GL	 
1999112500081	19991125	00081	CE  	1999	11	25	AU990912         	1	19990908	G	2720	965240261	MOUNT           			BEECH 	58    	58          	1152740	CE  						MCAULY	3AF32C	3AF32C512   	GL  	RUDDER	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RUDDER BELLCRANK SUPPORT MOUNT BROKEN.						1	L	7	2 	3O				3A16    		5	C	P22EA	 
1999112500082	19991125	00082	EU  	1999	11	25	AU990913         	1	19990811	G	6730	1090110424	ACTUATOR        		0128007REV  	AGUSTA	A109  	A109C       	0260118	EU  	ALLSN 	250C  	250C20R1    	03013	GL  					HYDRAULIC SYSTEM	CRACKED         	W				O				OTHER                   				K			FLUID LOSS                			LD	LANDING        	1			AU	S 					1994					(AUS) HYDRAULIC SERVO ACTUATOR LOCATED ON THE LEFT SIDE OF THE GEARBOX CRACKED ON THE UPPER BODY.  LOSS OF NR 2 HYDRAULI	C SYSTEM FLUID.					1	G	7	2 	3U	3	U		H7EU    	E4CE				 
1999112500083	19991125	00083	GL  	1999	11	25	AU990914         	3	19990902	G	6110	C4903	NUT             			BEECH 	95    	95          	1153402	CE  						MCAULY	2AF34C	2AF34C55    	GL  	PROPELLER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			293  		790501			790501		(AUS) PROPELLER RETENTION NUT CRACKED.  EVIDENCE OF CRACK HIGHLIGHTED BY MARKER PEN.  SUBMITTER SUSPECTED CRACK HAD BEEN	 FOUND PREVIOUSLY AND THE UNSERVICEABLE NUT HAD BEEN REUSED.					1	L	7	2 	3O				3A16    		5	C	P5EA	 
1999112500084	19991125	00084	EU  	1999	11	25	AU990915         	1	19990607	G	5320	A24003703	ANGLE           			FOKKER	F28   	F28MK4000   	4990810	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					COCKPIT WINDOW	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT COCKPIT WINDOW LOWER ATTACHMENT ANGLE CORRODED.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999112500085	19991125	00085	EU  	1999	11	25	AU990916         	1	19990615	G	5313	A34165	STRINGER        			FOKKER	F28   	F28MK4000   	4990810	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					BS 16495 / 17845	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) STRINGER 58 DIMPLED LAP JOINT LOCATED IN THE RIGHT REAR FUSELAGE SKIN BETWEEN FS 16495 AND FS 17845 CORRODED.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999112500086	19991125	00086	EU  	1999	11	25	AU990917         	1	19990530	G	5314	A34070	BEAM            			FOKKER	F28   	F28MK4000   	4990810	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					BS 13345	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE MAIN KEEL BEAM CORRODED AT LEFT FUSELAGE FRAME 13345.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999112500087	19991125	00087	EU  	1999	11	25	AU990918         	1	19990527	G	5551	A03035411	BRACKET         			FOKKER	F28   	F28MK4000   	4990810	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					HORIZONTAL STAB	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) HORIZONTAL STABILIZER ACTUATOR MOUNT BRACKETS CORRODED.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999112500088	19991125	00088	EU  	1999	11	25	AU990919         	1	19990510	G	5751	A78811002	BRACKET         			FOKKER	F28   	F28MK4000   	4990810	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					AILERON	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT AILERON CONTROL UNIT LOWER MOUNT BRACKET CORRODED.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999112500089	19991125	00089	SO  	1999	11	25	AU990920         	1	19990908	G	7120	LW18459	BRACKET         			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	LTIO540J2BD 	41533	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	ENGINE MOUNT	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			239  		RL21168A		RL21168A			(AUS) ENGINE BRACKET CRACKED FROM WELD OF LT ATTACHMENT LUG.  CRACKED LENGTH APPROXIMATELY 19.05 MM (0.75 INCH).						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
1999112500090	19991125	00090	EA  	1999	11	25	AU990921         	2	19990801	G	8530		PISTON          		6A4165B3    	UNIVAR	108   	1083        	9230408	NM  	FRNKLN	6A4165	6A4165B3    	27025	EA  	MCAULY	1A170	1A170FFA    	GL  	ENGINE	OUT OF LIMITS   	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							30592			(AUS) PISTON TO CYLINDER CLEARANCE OUT OF LIMITS.  SUBMITTER SUSPECTED PISTON WAS A MADE TO ORDER ITEM.						1	H	7	1 	3O	3	O		A767    	E238	5	N	P857	 
1999112500091	19991125	00091	SO  	1999	11	25	AU990922         	1	19990909	G	5540	6534100	DOUBLER         		65342       	PIPER 	PA32  	PA32R301T   	7103220	SO  	LYC   	O540  	TIO540S1AD  	41532	EA  	HARTZL	HCE2Y	HCE2YR1     	GL  	RUDDER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					R301T6001					(AUS) RUDDER LT AND RT DOUBLER ANGLES CRACKED.   CRACK LENGTH LT ANGLE -19.050 MM (0.75 INCH).  CRACK LENGTH RT ANGLE - 	12.7 MM (0.5 INCH).					1	L	7	1 	3O	3	O		A3SO    	E14EA	5	C	P9EA	 
1999112500092	19991125	00092	SO  	1999	11	25	AU990923         	1	19990909	G	5541	63543	SPAR            		653422      	PIPER 	PA32  	PA32R301T   	7103220	SO  	LYC   	O540  	TIO540S1AD  	41532	EA  	HARTZL	HCE2Y	HCE2YR1     	GL  	RUDDER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					R301T6001					(AUS) RUDDER SPAR CRACKED.   REF:  SEE MDR AU990922 FOR FURTHER INFORMATION.						1	L	7	1 	3O	3	O		A3SO    	E14EA	5	C	P9EA	 
1999112500093	19991125	00093	SW  	1999	11	25	AU990924         	1	19990915	G	7330	2764024083	PIPE            			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UHR 		WP  	MCAULY	4HFR34	4HFR34C652  	NE  	FUEL SYSTEM	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							P70164			(AUS) LEFT FUEL FILTER BYPASS LINE 'B' NUT LOOSE AT FUEL FILTER END.						2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999112500094	19991125	00094	NE  	1999	11	25	AU990925         	2	19990821	G	7260	3010674	BEARING         			AIRTRC	AT500 	AT502B      	0390307	SW  	PWA   	PT6   	PT6A34AG    	52053	NE  	HARTZL	HCB3T	HCB3TN3     	GL  	TURBINE ENGINE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							PCEPHOOO7			(AUS) NR 6 ACCESSORY DRIVE GEAR REAR BEARING BRONZE CARRIER DAMAGED.  SUBMITTER SUSPECTED CAUSED BY OIL STARVATION DUE T	O BLOCKED OIL GALLERY WHICH WAS CAUSED BY AN INCORRECTLY  FITTED SEAL.  METAL CONTAMINATION OF ENGINE OIL SYSTEM.					1	L	7	1 	3T	4	T	NC	A17SW   	E4EA	6	C	P15EA	 
1999112500095	19991125	00095	SW  	1999	11	25	AU990926         	1	19990825	G	3242	50116402	BRAKE           		50116402    	FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UHR 		WP  	MCAULY	4HFR34	4HFR34C652  	NE  	BRAKE	OVERHEATED      	W				O				OTHER                   				M			OVER TEMP                 			LD	LANDING        	1			AU	S 					SPR94646					(AUS) NR 2 BRAKE PACKING BINDING AND OVERHEATING.  WATER ALSO FOUND IN BRAKE MASTER CYLINDERS.						2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999112500096	19991125	00096		1999	11	25	AU990927         	4	19990806	G	3418	18617	STALL WARNING   			REIMS 	406   	F406        		EU  	PWA   	PT6   	PT6A112     	52043	NE  	MCAULY	3G34C7	3GFR34C701  	GL  	FUSELAGE	FAULTY          	W				A				UNSCHED LANDING         				N			FALSE WARNING             			CL	CLIMB          	1			AU	S 										(AUS) STALL WARNING VANE TIGHT TO MOVE IN BEARINGS CAUSING INTERMITTENT STALL WARNING INDICATIONS.						1	L	7	2 	3T	3	T	RT	A54EU   	E4EA	5	C	P60GL	 
1999112500097	19991125	00097	SW  	1999	11	25	AU990928         	1	19990910	G	3242	M834611216	O RING          			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UHR 		WP  	MCAULY	4HFR34	4HFR34C652  	NE  	BRAKE	DAMAGED         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AU	S 			5312 		92326					(AUS) LEFT MAIN LANDING GEAR INBOARD BRAKE UNIT O-RING SEAL LEAKING.  SUBMITTER SUSPECTED CAUSED BY BRAKE OVERHEATING DU	RING TAXI.					2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999112500098	19991125	00098	CE  	1999	11	25	AU990929         	1	19990909	G	2910	5100111095	PIPE            			CESSNA	402   	402C        	207590R	CE  	CONT  	O520  	TSIO520VB   	17040	SO  	MCAULY	3AF32C	3AF32C93    	GL  	HYDRAULIC SYSTEM	CRACKED         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT MAIN LANDING GEAR HYDRAULIC PIPE CRACKED ON THE BEND OF THE PIPE.  CRACK LENGTH 15 MM (0.590 INCH).  LOSS OF 	HYDRAULIC FLUID.					1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22EA	 
1999112500099	19991125	00099	CE  	1999	11	25	AU990931         	1	19990803	G	3250		CONTROL CABLE   			CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	WATER RUDDER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WATER RUDDER CABLE CORRODED.						1	H	7	1 	3O	3	O	 	A4CE    	E5CE	5	C	P47GL	 
1999112500100	19991125	00100	CE  	1999	11	25	AU990932         	1	19990803	G	3213		BEARING         			CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	MLG	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LANDING GEAR BEARING WORN AND LOOSE.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
1999112500101	19991125	00101	CE  	1999	11	25	AU990933         	1	19990803	G	5347		SEAT TRACK      			CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	CABIN	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT SEAT RAIL WORN BEYOND LIMITS.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
1999112500102	19991125	00102	CE  	1999	11	25	AU990934         	1	19990825	G	3233	571304031	FITTING         			CESSNA	425   	425         	2076018	CE  	PWA   	PT6   	PT6A112     	52043	NE  	MCAULY	3G34C7	3GFR34C701  	GL  	NLG	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR ACTUATOR SUPPORT CHANNEL FASTENERS FAILED.						1	L	7	2 	3T	3	T	RT	A7CE    	E4EA	5	C	P60GL	 
1999112500103	19991125	00103	EU  	1999	11	25	AU990935         	1	19990726	G	3211	201160702	BOLT            			AIRBUS	320   	A320212     		EU  	GE    	CFM56 	CFM565A     	13802	NE  					LT MLG	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT MAIN LANDING GEAR FORWARD PINTLE PIN LOCK BOLT SHOWED EVIDENCE OF ROTATION.						2	L	7	2 	4F	4	F	RT	A28NM   	E29NE				 
1999112500104	19991125	00104		1999	11	25	AU990936         	4	19990617	G	2565		VALVE           		7A12492     	BOEING	747   	747SP38     		NM  										ESCAPE SLIDE	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT UPPER DECK ESCAPE SLIDE TURBO-FAN FLAPPER VALVE BROKEN.						2	L	7	4 	4F			RT	A20WE   					 
1999112500105	19991125	00105		1999	11	25	AU990937         	4	19990617	G	2565	60B503248	CYLINDER        			BOEING	747   	747SP38     		NM  										ESCAPE SLIDE	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AU	S 										(AUS) UPPER DECK ESCAPE SLIDE INFLATION CYLINDER LEAKING AT THE HEAD FITTING.  DEPLOYMENT ACTUATOR LEAKING OIL.						2	L	7	4 	4F			RT	A20WE   					 
1999112500106	19991125	00106	NM  	1999	11	25	AU990938         	1	19990825	G	5311		FRAME           			BOEING	737   	737377      		NM  										BS 616 / 639	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FUSELAGE FRAME INNER CHORDS LOCATED AT FR 616 AND FR 639 LEFT CRACKED AT THE LOWER RIVET HOLES.  FOUND DURING EDDY	 CURRENT INSPECTION.					2	L	7	2 	4F			RT	A16WE   					 
1999112500107	19991125	00107	EA  	1999	11	25	AU990939         	2	19990902	G	8530		VALVE SEAT      			ROBSIN	R22   	R22BETA     		NM  	LYC   	O320  	O320B2C     	41508	EA  					ENGINE	LOOSE           	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			AU	S 							L1663739A			(AUS) NR 1 CYLINDER EXHAUST VALVE SEAT DISLODGED AND HELD THE EXHAUST VALVE OPEN ALLOWING IT TO BE CONTACTED BY THE PIST	ON WHICH THEN SNAPPED THE VALVE HEAD OFF.  DAMAGE TO NR 1 CYLINDER AND CONNECTING ROD.					1	G	7	1 	3O	3	O		H10WE   	E274				 
1999112500108	19991125	00108	CE  	1999	11	25	AU990940         	1	19990911	G	3230	35815077	UPLOCK HOOK     			BEECH 	35    	35BEECH     	1151502	CE  	CONT  	E185  	E1858       	17014	SO  	BEECH	215	215107      	CE  	LT MLG	CORRODED        	W				K				NONE                    				O			OTHER                     			LD	LANDING        	1			AU	S 							4235DC	43568		(AUS) LEFT MAIN LANDING GEAR UPLOCK HOOK CORRODED AND STIFF TO OPERATE.						1	L	7	1 	3O	3	O		A777    	E246	5	C	P873	 
1999112500109	19991125	00109	SO  	1999	11	25	AU990941         	1	19990911	G	5610	PPGNP1513112	WINDSHIELD      			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  	HAMSTD	14SF	14SF9       	NE  	COCKPIT	FAILED          	W				O				OTHER                   				O			OTHER                     			CL	CLIMB          	1			AU	S 										(AUS) OUTER RIGHT FRONT WINDSHIELD SHATTERED BUT REMAINED INTACT.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	N	P11NE	 
1999112500110	19991125	00110	SW  	1999	11	25	AU990942         	1	19990916	G	7120	NAS147DH22	BOLT            			FRCHLD	SA227 	SA227DC     	3377521	SW  	GARRTT	TPE331	TPE33112UA  	01514	WP  	MCAULY	4HFR34	4HFR34C652  	NE  	ENGINE MOUNT	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							P70141			(AUS) RIGHT ENGINE INBOARD MOUNT LOWER BOLT HEAD BROKEN OFF.						2	L	7	2 	4T	4	T	RT	A18SW   	E4WE	6	C	3PNE	 
1999112500111	19991125	00111	CE  	1999	11	25	AU990943         	1	19990907	G	3260	B72RQ181A2	SWITCH          			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A42      	52043	NE  	HARTZL	HCD4N3	HCD4N3A     	GL  	MLG	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) UPLIMIT MICROSWITCH ACTUATOR HEAD LOOSE ON SWITCH BODY.  MICROSWITCH WAS A NEW ITEM.						1	L	7	2 	4T	4	T		A24CE   	E4EA	5	C	STC	 
1999112500112	19991125	00112	NE  	1999	11	25	AU990944         	2	19990829	G	7200		ENGINE          			CESSNA	500   	550         	2076604	CE  	PWA   	JT15  	JT15D4      	52112	NE  					LEFT	BIRD STRIKE     	W				C				ABORTED TAKEOFF         				E	C		VIBRATION/BUFFET          	F.O.D.                    		TO	TAKEOFF        	1			AU	S 							PCE70332			(AUS) LEFT ENGINE BIRD STRIKE.  THE ENGINE SUFFERED SUBSTANTIAL DAMAGE.   INDICATIONS OF IMPACT ALSO EVIDENT ON THE INBO	ARD LEADING EDGE OF THE LEFT WING.					1	L	7	2 	4F	4	F		A22CE   	E1NE				 
1999112500113	19991125	00113	NM  	1999	11	25	AU990945         	1	19990811	G	5311	85320058	FRAME           			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	BS 354	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT FUSELAGE FRAME LOCATED AT STN 354.25 CRACKED.  THE CRACK RAN FROM THE CUT-OUT FOR STRINGER NR 22 AND PROGRES	SED COMPLETELY THROUGH THE FRAME.  CRACK LENGTH APPROXIMATELY 76.2 MM TO 101.6 MM (3 INCHES TO 4 INCHES).					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
1999112500114	19991125	00114	SO  	1999	11	25	AU990946         	1	19990920	G	6120	MS210453	NUT             			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  	HARTZL	HCC3Y	HCC3YR2     	NE  	PROP CONTROL	WORN            	W				O				OTHER                   				O			OTHER                     			CL	CLIMB          	1			AU	S 										(AUS) PITCH CONTROL ROD END LOCKNUT VIBRATED LOOSE CAUSING DISCONNECTION OF THE PITCH CONTROL CABLE.  INVESTIGATION FOUN	D THE LOCKING FUNCTION ON THE NUT WAS NON-EXISTENT.					1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P25EA	 
1999112500115	19991125	00115	SW  	1999	11	25	AU990947         	1	19990825	G	6410	HAC473	PITCH HORN      		HAC473      	BELL  	47    	47G3B       	1181026	SW  	LYC   	O435  	TVO435D1B   	41516	EA  					TAIL ROTOR BLADE	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					00115					(AUS) TAIL ROTOR BLADE PITCH HORN LOOSE.						1	G	7	1 	3O	3	O		2H3     	1E13				 
1999121000039	19991210	00039	CE  	1999	12	10	AU990948         	1	19990907	G	3260	BZ2R0181A2	SWITCH          			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A42      	52043	NE  					MLG	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LANDING GEAR DOWN LIMIT MICROSWITCH FAULTY.  DOWEL PINS HOLDING THE SWITCH BODY AND THE ACTUATOR HEAD TOGETHER HAD	 PARTIALLY WORKED ITS WAY OUT.					1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999112500116	19991125	00116	NE  	1999	11	25	AU990949         	2	19990914	G	7250	3023411	TURBINE DISC    								PWA   	PT6   	PT6A15AG    	52043	NE  					COMPRESSOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							PCE14156			(AUS) COMPRESSOR TURBINE DISC CRACKED ON THE TRAILING EDGE SIDE ADJACENT TO THE BALANCE RIM IN THE WEB AREA.  ONE CONFIR	MED CRACK AND ONE SUSPECT CRACK.   FOUND DURING NDI.										4	T			E4EA				 
1999112500117	19991125	00117	SO  	1999	11	25	AU990950         	2	19990914	G	8520		CAMSHAFT        								CONT  	O520  	IO520L      	17032	SO  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					567809		567809			(AUS) CRANKCASE TUNNEL DIMENSIONS OUT OF LIMITS.  CAMSHAFT CRACKED.											3	O			E5CE				 
1999112500118	19991125	00118	CE  	1999	11	25	AU990951         	1	19990907	G	3260	BZ2RQ181A2	SWITCH          			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A42      	52043	NE  	HARTZL	HCD4N3	HCD4N3A     	GL  	MLG	FAULTY          	W				O				OTHER                   				O			OTHER                     			DE	DESCENT        	1			AU	S 										(AUS) LANDING GEAR UPLIMIT MICROSWITCH FAULTY.  INSPECTION FOUND THAT THE DOWEL PINS HOLDING THE MICROSWITCH BODY TO THE	 ACTUATOR HEAD HAD COME OUT.  THE LANDING GEAR MOTOR CONTROL CIRCUIT BREAKER BLEW WHEN THE GEAR OVERRAN.					1	L	7	2 	4T	4	T		A24CE   	E4EA	5	C	STC	 
1999112500119	19991125	00119		1999	11	25	AU990952         	4	19990830	G	2565		CABLE           			BOEING	737   	737377      	       	NM  										ESCAPE SLIDE	FRAYED          	W			QS7R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) CABIN DOOR ESCAPE SLIDE COVER LATCH RELEASE CABLES FRAYED.  THE ESCAPE SLIDES AFFECTED WERE LOCATED AT DOORS R1, R	2, AND L2.					2	L	7	2 	4F			RT	A16WE   					 
1999112500120	19991125	00120	EU  	1999	11	25	AU990953         	1	19990820	G	5280	HC321B0040000	HINGE           			BAG   	BAE146	BAE146300A  	1500267	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					RT & LT MLG DOOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT AND RIGHT MAIN LANDING GEAR DOOR REAR HINGE BRACKETS CORRODED IN THE AREA ADJACENT TO THE BONDING LEAD ATTACH	MENT POINTS ON THEFORWARD BRACKET SEGMENTS.					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
1999112500121	19991125	00121	NM  	1999	11	25	AU990954         	1	19990910	G	2730	183	COMPUTER        			BOEING	737   	73733A      	1384673	NM  										ELEVATOR	FAULTY          	W				O				OTHER                   				F			FLT CONT AFFECTED         			NR	NOT REPORTED   	1			AU	S 					183					(AUS) ELEVATOR FEEL COMPUTER FAULTY.  INVESTIGATION COULD FIND NO FAULTS WITH THE COMPUTER.						2	L	7	2 	4F			RT	A16WE   					 
1999112500122	19991125	00122	SW  	1999	11	25	AU990955         	1	19990922	G	2613		WIRE            			SWRNGN	SA227 	SA227AC     	8780603	SW  	GARRTT	TPE331	TPE33111U   	01514	WP  	ROTOL	R321	R321482F8   	GL  	LT ENGINE	FAILED          	W				O				OTHER                   				N			FALSE WARNING             			LD	LANDING        	1			AU	S 							P44434			(AUS) LEFT ENGINE OVERHEAT DETECTOR WIRING HARNESS CHAFED AND SHORT CIRCUITED BENEATH HEAT SHRINK.  FALSE FIRE WARNING R	ESULTED IN DISCHARGE OF FIRE EXTINGUISHER.					2	L	7	2 	4T	4	T	RT	A8SW    	E4WE	6	C	P61GL	 
1999112500123	19991125	00123	EU  	1999	11	25	AU990956         	1	19990826	G	2730	NB451051	CONTROL ROD     			BNORM 	BN2   	BN2A26      	1520226	EU  	LYC   	O540  	O540E4C5    	41532	EA  	HARTZL	HCC2Y	HCC2YK2     	GL  	ELEVATOR	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELEVATOR CONTROL ROD WORN PAST LIMITS IN THE AREA OF THE GUIDE ROLLERS.  ROD HAD BEEN ILLEGALLY REPAIRED USING MET	AL FILLER OR SIMILAR MATERIAL.					1	H	7	2 	3O	3	O		A17EU   	E295	5	C	P920	 
2000011500256	20000115	00256	EA  	2000	1	15	AU990957         	2	19990907	G	8520		CRANKCASE       			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1545 				L347561A			(AUS) CRANKCASE CRACKED ON FRONT RIGHT SIDE BELOW THE CYLINDER.  CRACK LENGTH 50.8 MM (2 IN)CHES).						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
2000011500257	20000115	00257	SO  	2000	1	15	AU990958         	2	19991006	G	7322	6329168	FCU             			CESSNA	402   	402A        	207590M	CE  	CONT  	O520  	TSIO520E    	17040	SO  	MCAULY	3AF32C	3AF32C87    	GL  	LT ENGINE	FAILED          	W				O				OTHER                   				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			AU	S 			1204 				502423			(AUS) LEFT ENGINE FUEL CONTROL UNIT FAULTY.						1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22EA	 
2000011500258	20000115	00258	NM  	2000	1	15	AU990959         	1	19990727	G	5312		BULKHEAD        			BOEING	737   	73733A      	1384673	NM  										FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING AREAS:  1.   BULKHEAD WEB LHS AT WL 218 - CRACK LENGTH 15 MM (0	.590 INCHES).   2.   LT AND RT CHORDS AT WL 207 FLOOR LEVEL FOUND DURING ULTRASONIC INSPECTION IAW ER B73-53-1-39D.					2	L	7	2 	4F			RT	A16WE   					 
2000011500259	20000115	00259	NM  	2000	1	15	AU990960         	1	19990602	G	5312		BULKHEAD        			BOEING	737   	737377      		NM  										FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FORWARD PRESSURE BULKHEAD CRACKED IN THE FOLLOWING AREAS:  1.   FORWARD SIDE WEB - TWO CRACKS.  2.  LOWER AFT SIDE	 WEB - TWO CRACKS.   3.  VERTICAL CHORD AFT SIDE - ONE CRACK.   4.   RT SIDE CHORD RADIUS - ONE CRACK FOUND DURING ULTRA	SONIC AND EDDY CURRENT INSPECTION IAW ER B73-53-10-39.				2	L	7	2 	4F			RT	A16WE   					 
2000011500260	20000115	00260	NM  	2000	1	15	AU990961         	1	19990629	G	5312		BULKHEAD        			BOEING	737   	737377      		NM  										FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FORWARD PRESSURE BULKHEAD RT SIDE CHORD RADIUS CRACKED AT FLOOR LEVEL.   FOUND DURING EDDY CURRENT INSPECTION IAW 	ER B73-53-10-39.					2	L	7	2 	4F			RT	A16WE   					 
2000011500261	20000115	00261	EU  	2000	1	15	AU990963         	2	19991012	G	7200		ENGINE          			BOEING	737   	737476      		NM  	CFMINT	CFM56 	CFM563C1    	13802	EU  					ENGINE BAY	OVERTEMP        	W				O				OTHER                   				E	M		VIBRATION/BUFFET          	OVER TEMP                 		CR	CRUISE         	1			AU	S 										(AUS) ENGINE OVERHEAT CONDITION EVIDENT.  LIMITED INFORMATION PROVIDED.						2	L	7	2 	4F	4	F	RT	A16WE   	E21EU				 
2000011500262	20000115	00262	NM  	2000	1	15	AU990964         	1	19991018	G	2510		LOCK            			BOEING	737   	737476      		NM  										COCKPIT SEAT	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) CAPTAIN'S SEAT LOCKING MECHANISM PLUNGER BRACKET SCREW SHEARED AND A LOOSE BOLT FITTED IN PLACE OF THE SECOND SCRE	W.   UNAPPROVED PART.					2	L	7	2 	4F			RT	A16WE   					 
2000011500263	20000115	00263	CE  	2000	1	15	AU990965         	1	19990917	G	2620	7122011	SWITCH          		1143800523  	BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					LT ENGINE	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					1169					(AUS) LEFT ENGINE FIRE EXTINGUISHING SYSTEM FIRE PULL T-HANDLE  MICROSWITCH PIN 8 TO PIN 9 HAD NO CONTINUITY.						2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
2000011500264	20000115	00264	CE  	2000	1	15	AU990966         	1	19990919	G	2620	7122011	SWITCH          		1143800523  	BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  	HARTZL	HCE4A	HCE4A3A     	NE  	RT ENGINE	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					700					(AUS) RIGHT ENGINE FIRE EXTINGUISHING SYSTEM FIRE PULL T-HANDLE  MICROSWITCH FAULTY.   EVIDENCE OF WEAR WAS FOUND ON ONE	 OF THE MICROSWITCH CONTACT PLATES.					2	L	7	2 	4T	4	T	RT	A24CE   	E26NE	5	C	P10NE	 
2000011500265	20000115	00265	NM  	2000	1	15	AU990967         	1	19990817	G	3810	237226	HEATING ELEMENT 			BOEING	747   	747438      		NM  										POTABLE WATER	WORN            	W				K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			AU	S 										(AUS) POTABLE WATER LEVEL SENSOR HEATER RIBBON ELEMENT LOCATED IN THE AFT END OF THE FORWARD CARGO HOLD WAS FOUND TO BE 	SMOULDERING.  INVESTIGATION FOUND CHAFING OF THE RIBBON ELEMENT WIRING.					2	L	7	4 	4F			RT	A20WE   					 
2000011500266	20000115	00266	NM  	2000	1	15	AU990968         	1	19990814	G	2497	292110005A12C1	WIRE            			DHAV  	DHC8  	DHC8201     	2809001	NM  						HAMSTD	14SF	14SF23      	NE  	AC ELECTRICAL	WORN            	W				O				OTHER                   				H			ELECT. POWER LOSS-50 PC   			CR	CRUISE         	1			AU	S 										(AUS) WIRE LOCATED IN LEFT AC CONTACTOR BOX SHORT CIRCUITING TO EARTH.  LT AC GCU FOUND TO BE FAULTY.						2	H	7	2 	4T			RT	A13NM   		6	C	P7NE	 
2000011500267	20000115	00267	NM  	2000	1	15	AU990969         	1	19991014	G	2450	82450067001	BRACKET         			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	AC ELECTRICAL	BROKEN          	W				O				OTHER                   				H			ELECT. POWER LOSS-50 PC   			CR	CRUISE         	1			AU	S 										(AUS) CIRCUIT BREAKER PANEL LOCATED IN LT AC CONTACTOR BOX BROKEN ALLOWING THE TERMINALS TO SHORT CIRCUIT TO THE BOX AND	 CAUSING THE AC GENERATOR TO FAIL.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
2000011500268	20000115	00268	SO  	2000	1	15	AU990970         	1	19990929	G	8120	4091709001	TURBOCHARGER    			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	ENGINE	FAULTY          	W				A				UNSCHED LANDING         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CL	CLIMB          	1			AU	S 			10   							(AUS) ENGINE TURBOCHARGER FAULTY.						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
2000011500269	20000115	00269	EU  	2000	1	15	AU990971         	1	19991014	G	2910		VALVE PIN       			BAG   	JETSTM	JETSTM3201  	1500217	EU  	GARRTT	TPE331	TPE33112UA  	01514	WP  	ROTOL	R333	R333482F12  	GL  	HYD SYSTEM	POPPED          	W				C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			AU	S 										(AUS) LANDING GEAR FAILED TO RETRACT.   A POPPED BUTTON IN THE HYDRAULIC SYSTEM (EMERGENCY SELECTOR VALVE PIN) WAS FOUND	.  THE BUTTON WAS RESET AND THE SYSTEM TESTED SERVICEABLE.					2	L	7	2 	4T	4	T	RT	A56EU   	E4WE	6	C	P61GL	 
2000011500270	20000115	00270	NM  	2000	1	15	AU990972         	1	19991010	G	6120	8210176	PUMP            	HAMSTD      	14SF7       	DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	PROP  CONTROL	FAULTY          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			AU	S 							PCE120155			(AUS) NR 1 PROPELLER OIL PUMP FAULTY.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
2000011500271	20000115	00271	NE  	2000	1	15	AU990973         	3	19990930	G	6140	005WS00	WEU             	ROTOL       	R3544123F13 	SAAB  	SF340 	SF340A      	7850100	EU  						ROTOL	R354	R3544123F13 	NE  	PROP INDICATOR	FAULTY          	W				C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			AU	S 										(AUS) WARNING ELECTRONIC UNIT (WEU) FAULTY.						2	L	7	2 	4T			RT	A52EU   		6	C	P61GL	 
2000011500272	20000115	00272	SO  	2000	1	15	AU990974         	1	19991016	G	3230	18190003	VALVE           		1203859400  	EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  	HAMSTD	14SF	14SF9       	NE  	MLG	FAULTY          	W				C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			AU	S 					120115					(AUS) LANDING GEAR SOLENOID VALVE AND/OR LANDING GEAR SELECTOR CONTROL UNIT SUSPECT FAULTY.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	N	P11NE	 
2000011500273	20000115	00273	EU  	2000	1	15	AU990976         	1	19991004	G	5730		SKIN            			GROB  	G115  	G115C       	1660303	EU  	LYC   	O360  	O360A1F6    	41514	EA  	HARTZL	HCF2Y	HCF2YR1     	GL  	LT WING	DISBONDED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT WING LOWER SKIN DISBONDED FROM REAR SPAR IN THE AREA ADJACENT TO THE AILERON OUTBOARD HINGE.  DISBOND APPEARS	 TO ORIGINATE FROM THE OUTBOARD END IN THE AREA OF THE AILERON MASS BALANCE CUT-OUT ON THE WING.					1	L	7	1 	3O	3	O	NT	A57EU   	E286	5	C	P27EA	 
2000011500274	20000115	00274	CE  	2000	1	15	AU990977         	1	19990916	G	3250	58130441	STRUCTURE       		581353      	CESSNA	404   	404CESSNA   	2075901	CE  						MCAULY	3FF32	3FF32C501   	GL  	NLG STEERING	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AIRCRAFT STRUCTURE FAILED IN THE AREA OF THE NOSE LANDING GEAR STEERING SYSTEM ATTACHMENT.  PARTS AFFECTED ARE:  1	.  P/N 5813044-1 (2 OFF).   2.   ANGLE P/N 581353.   3.   SUPPORT P/N 5813045.1.					1	L	7	2 	3O				A25CE   		5	C	P45GL	 
2000011500275	20000115	00275	EU  	2000	1	15	AU990978         	1	19991007	G	5712	TB1011015003	RIB             			SOCATA	TB10  	TB10TOBAGO  	8680696	EU  	LYC   	O360  	O360A1A     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	WING	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WING RIB CONTAINED SEVERE EXFOLIATION CORROSION ALONG THE BOTTOM RIVET LINE.  THE RIB IS THE ONE TO WHICH THE LAND	ING GEAR OLEO STRUT IS ATTACHED.					1	L	7	1 	3O	3	O	RT	A51EU   	E286	5	C	P920	 
2000011500276	20000115	00276	EU  	2000	1	15	AU990979         	1	19991007	G	5712	TB1011015002	RIB             			SOCATA	TB10  	TB10TOBAGO  	8680696	EU  	LYC   	O360  	O360A1A     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	WING	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WING RIB CONTAINED SEVERE EXFOLIATION CORROSION ALONG THE BOTTOM RIVET LINE.  CORROSION ALSO EVIDENT IN OTHER AREA	S OF THE RIB.					1	L	7	1 	3O	3	O	RT	A51EU   	E286	5	C	P920	 
2000011500277	20000115	00277	EU  	2000	1	15	AU990980         	1	19990819	G	3710		PUMP            			GROB  	G115  	G115C       	1660303	EU  	LYC   	O360  	O360A1F6    	41514	EA  	HARTZL	HCF2Y	HCF2YR1     	GL  	VACUUM SYSTEM	MISINSTALLED    	W				O				OTHER                   				W			INADEQUATE Q C            			NR	NOT REPORTED   	1			AU	S 							L3623836A			(AUS) VACUUM PUMP LOOSE ON MOUNT.  WHEN THE PUMP WAS REMOVED THE DRIVESHAFT WAS FOUND TO BE MISALIGNED CAUSING DAMAGE TO	 THE CAMSHAFT DRIVE GEAR.  METAL CONTAMINATION OF THE ENGINE OIL SYSTEM.  ENGINE WAS RECEIVED FROM THE GROB FACTORY WITH	 THE PUMP ALREADY FITTED.				1	L	7	1 	3O	3	O	NT	A57EU   	E286	5	C	P27EA	 
2000011500278	20000115	00278	EA  	2000	1	15	AU990981         	2	19991006	G	8520	LW10345	CRANKSHAFT      			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	LTIO540J2BD 	41533	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	LT ENGINE	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 			1371 				L16068A			(AUS) LEFT ENGINE CRANKSHAFT HAD AN INCORRECT CRANKSHAFT FITTED.						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
2000011500279	20000115	00279	GL  	2000	1	15	AU990982         	1	19991008	G	3500		OXYGEN SYSTEM   			AMTR  	LANCAR	LANCAIRIV   	056163V	GL  	CONT  		TSIO550E    							CABIN	UNAPPROVED PART 	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) OXYGEN SYSTEM FOUND INSTALLED IN AIRCRAFT WITH NO INSTALLATION CERTIFICATION OR WEIGHT/BALANCE DATA IN THE AIRCRAF	T LOG BOOK.  THE OXYGEN SYSTEM IS NOT APPROVED FOR AIRCRAFT USE AND THE INSTALLATION DOES NOT COMPLY WITH FAR REQUIREMEN	TS.  UNAPPROVED PART.				1	L	7	1 	3O			RT	EXPA1L71					 
2000011500280	20000115	00280	GL  	2000	1	15	AU990983         	1	19991006	G	5520	EL40304	TORQUE TUBE     			AMTR  	LANCAR	LANCAIRIV   	056163V	GL  	CONT  		TSIO550E    							ELEVATOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELEVATOR TORQUE TUBE CORRODED.  THE AREA IS COVERED WITH EXHAUST GAS DEPOSITS.						1	L	7	1 	3O			RT	EXPA1L71					 
2000011500281	20000115	00281	CE  	2000	1	15	AU990985         	1	19990926	G	2434	9800943	SENSOR          	PRESTOLITE  	ALV9510     	CESSNA	404   	404CESSNA   	2075901	CE  						MCAULY	3FF32	3FF32C501   	GL  	DC ALTERNATOR	FAULTY          	W				A				UNSCHED LANDING         				H	J		ELECT. POWER LOSS-50 PC   	WARNING INDICATION        		CR	CRUISE         	1			AU	S 			12   		86272					(AUS) ALTERNATOR FAULTY.   ELECTRICAL SENSOR FAILED.						1	L	7	2 	3O				A25CE   		5	C	P45GL	 
2000011500282	20000115	00282	SO  	2000	1	15	AU990986         	1	19991002	G	2750	3472001001C	CONTROL UNIT    			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  	HAMSTD	14SF	14SF9       	NE  	TE FLAP	FAULTY          	W				C				ABORTED TAKEOFF         				F	J		FLT CONT AFFECTED         	WARNING INDICATION        		TO	TAKEOFF        	1			AU	S 					0123					(AUS) FLAP CONTROL UNIT SUSPECT FAULTY.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	N	P11NE	 
2000011500283	20000115	00283	SO  	2000	1	15	AU990987         	1	19990929	G	3260	ICH214	SWITCH          			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	RT MLG	FAULTY          	W				K				NONE                    				O	J		OTHER                     	WARNING INDICATION        		DE	DESCENT        	1			AU	S 										(AUS) RIGHT MAIN LANDING GEAR DOWNLOCK MICROSWITCH FAULTY.						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
2000011500284	20000115	00284	WP  	2000	1	15	AU990988         	2	19990925	G	7200	P66354	ENGINE          			BAG   	JETSTM	JETSTM3201  	1500217	EU  	GARRTT	TPE331	TPE33112UHR 		WP  	ROTOL	R333	R333482F12  	GL  	NR 2	OVERTEMP        	W				A				UNSCHED LANDING         				E	R	M	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	OVER TEMP                 	CL	CLIMB          	1			AU	S 							P66354C			(AUS) NR 2 ENGINE OVERTEMPED TO 700 DEGREES CELSIUS.  INSPECTION IAW GARRETT MM.  FOUND NO DEFECTS.   EGT CONNECTOR (2KR	31) FOUND TO HAVE A DISLODGED PIN.					2	L	7	2 	4T	4	T	RT	A56EU   	E4WE	6	C	P61GL	 
2000011500285	20000115	00285	CE  	2000	1	15	AU990989         	1	19990911	G	7603	1250317	BRACKET         			CESSNA	207   	207A        	2073604	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	3A32C	D3A32C90    	GL  	ENGINE CONTROL	BROKEN          	W				O				OTHER                   				E			VIBRATION/BUFFET          			LD	LANDING        	1			AU	S 			1237 				574572			(AUS) THROTTLE CABLE AND MIXTURE CONTROL CABLE SUPPORT BRACKET BROKEN IN THE AREA OF THE ATTACHMENT BOLT TO  THE INTAKE 	RISER.					1	H	7	1 	3O	3	O		A16CE   	E5CE	5	C	P21EA	 
2000011500286	20000115	00286	CE  	2000	1	15	AU990990         	1	19990304	G	5753	26111447	BRACKET         		26111446    	CESSNA	208   	208B        	2073701	CE  						MCAULY	3AF34C	3GFR34C703  	GL  	TE FLAP	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FLAP ACTUATOR SUPPORT BRACKETS P/N 261114-6 (FORWARD) AND P/N 261114-7 (AFT) CRACKED AND DISTORTED.  SUBMITTER SUS	PECTED CAUSED BY MISRIGGING OF THE FLAP POSITION SWITCH ASSEMBLY.					1	H	7	1 	3T				A37CE   		5	C	P60GL	 
2000011500287	20000115	00287	EU  	2000	1	15	AU990991         	1	19991002	G	6420	360A33103427	FAIRING         		360A33100209	AEROSP	SA365 	SA365C      	8680667	EU  	TMECA 	ARRIEL	ARRIEL1A    	60030	NE  					TAIL ROTOR	CRACKED         	W				O				OTHER                   				E	F		VIBRATION/BUFFET          	FLT CONT AFFECTED         		DE	DESCENT        	1			AU	S 					PAW2					(AUS) TAIL ROTOR FENESTRON ASSEMBLY ROTATING FAIRING CRACKED.						1	G	7	2 	3U	3	U		H10EU   	E19EU				 
2000011500288	20000115	00288	GL  	2000	1	15	AU990992         	3	19991001	G	6111	A106GAD	BLADE           	MCAULY      	3GFR34C703B 	CESSNA	208   	208B        	2073701	CE  						MCAULY	3AF34C	3GFR34C703  	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1152 		960719			96719		(AUS) PROPELLER BLADES CONTAINED EXFOLIATION CORROSION.						1	H	7	1 	3T				A37CE   		5	C	P60GL	 
2000011500289	20000115	00289	EU  	2000	1	15	AU990993         	1	19991007	G	5320	TB1042010001	MOUNT           			SOCATA	TB10  	TB10TOBAGO  	8680696	EU  	LYC   	O360  	O360A1A     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR RIGHT TOP OLEO MOUNT CRACKED ON THE TOP WELD ADJACENT TO THE STEERING STOP.  THE CRACK EXTENDS F	OR APPROXIMATELY 66 PERCENT OF THE TUBE CIRCUMFERENCE.					1	L	7	1 	3O	3	O	RT	A51EU   	E286	5	C	P920	 
2000011500290	20000115	00290	EU  	2000	1	15	AU990994         	1	19991007	G	5510		MOUNT           			SOCATA	TB10  	TB10TOBAGO  	8680696	EU  	LYC   	O360  	O360A1A     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	HORIZONTAL STAB	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) REAR RIGHT TAILPLANE HINGE MOUNT CONTAINS SLIGHT INTERGRANULAR CORROSION.						1	L	7	1 	3O	3	O	RT	A51EU   	E286	5	C	P920	 
2000011500291	20000115	00291	EU  	2000	1	15	AU990995         	1	19991007	G	5712	TB1011015008	RIB             			SOCATA	TB10  	TB10TOBAGO  	8680696	EU  	LYC   	O360  	O360A1A     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	WING	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WING RIB CONTAINS EXFOLIATION CORROSION ALONG THE BOTTOM RIVET LINE AND AT OTHER LOCATIONS ON THE RIB.						1	L	7	1 	3O	3	O	RT	A51EU   	E286	5	C	P920	 
2000011500292	20000115	00292	EU  	2000	1	15	AU990996         	1	19991008	G	6120		PCU             	ROTOL       	R3894123F   	SAAB  	SF340 	SF340A      	7850100	EU  										PROPELLER	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) PROPELLER, BETA TUBE AND PROPELLER CONTROL UNIT (PCU) DAMAGED DURING MAINTENANCE DUE TO AN ATTEMPT BY MAINTENANCE 	PERSONNEL TO FEATHER THE PROPELLER WITH THE RIGGING PIN INSTALLED CONTRARY TO THE MAINTENANCE MANUAL.					2	L	7	2 	4T			RT	A52EU   					 
2000011500293	20000115	00293	GL  	2000	1	15	AU990997         	2	19991010	G	7230	23057142	STATOR          			BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			514  				CAE830380			(AUS) COMPRESSOR SECOND STAGE STATOR VANE FAILED AND ENTERED THE THIRDSTAGE COMPRESSOR ROTOR CAUSING SIGNIFICANT IMPACT 	DAMAGE TO THE THIRD STAGE ROTOR AND FURTHER DOWNSTREAM STAGES.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
2000011500294	20000115	00294	NM  	2000	1	15	AU990998         	1	19990905	G	5230	B20676	ACTUATOR        			BOEING	747   	747SP38     		NM  										CARGO DOOR	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) AFT CARGO DOOR ROTARY ACTUATOR FAULTY.  MOUNT BOLTS SHEARED AND ACTUATOR OUT OF POSITION.   DAMAGE CAUSED TO SURRO	UNDING STRUCTURE.  MOUNT BEAM CRACKED, DOUBLER PLATE BUCKLED, AND FLOOR BEAM CRACKED.					2	L	7	4 	4F			RT	A20WE   					 
2000011500295	20000115	00295	NM  	2000	1	15	AU990999         	1	19990808	G	2750		CONNECTOR       			BOEING	747   	747438      		NM  										TE FLAP	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT TRAILING EDGE FLAP ALTERNATE DRIVE ELECTRICAL CONNECTOR WAS FOUND TO BE DISCONNECTED.						2	L	7	4 	4F			RT	A20WE   					 
2000011500296	20000115	00296	NM  	2000	1	15	AU991000         	1	19990811	G	2550		INSULATION      			BOEING	767   	767338      	1385151	NM  	GE    	CF6   	CF680C      		GL  					BS 400	FIRE            	W				K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			AU	S 										(AUS) FORWARD CARGO HANDLING SYSTEM CIRCUIT BREAKERS P35 AND L169 TRIPPED.  THE BREAKERS WERE RESET AND SUBSEQUENT OPERA	TION OF THE HANDLING SYSTEM RESULTED IN A SMALL FIRE IN THE INSULATION BLANKETS AT STA 400 CENTERLINE BELOW THE CARGO HO	LD FLOOR LINE.  ADJACENT WIRING WAS ALSO DAMAGED.  THE BREAKERS WERE AGAIN FOUND TO HAVE TRIPPED.				2	L	7	2 	4F	4	F	RT	A1NM    	E23EA				 
2000011500297	20000115	00297	NM  	2000	1	15	AU991002         	1	19990325	G	5415		FUSE PIN        			BOEING	767   	767238      		NM  	PWA   	JT9   	JT9D7R4E    	52054	NE  					NR 2 ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NR 2 ENGINE STRUT INBOARD MID-SPAR FUSE PIN CRACKED.  CRACK LENGTH 0.508 MM (0.020 INCH).  NR 2 ENGINE OUTBOARD MI	D-SPAR FUSE PIN CRACKED.  CRACK LENGTH 38.1 MM (1.5 INCH).  FOUND DURING INSPECTION IAW QANTAS ENGINEERING INSTRUCTION E	I 767-054-0026.				2	L	7	2 	4F	4	F	RT	A1NM    	E3NE				 
2000011500298	20000115	00298	NM  	2000	1	15	AU991003         	1	19990817	G	4900	38162	HOUSING         			BOEING	747   	747338      		NM  										GEARBOX	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					38162					(AUS) APU COOLING AIR FAN SEIZED AND GEARBOX CASE SHATTERED.						2	L	7	2 	4F			RT	A20WE   					 
2000011500299	20000115	00299	NM  	2000	1	15	AU991004         	1	19990904	G	2530		WIRE            			BOEING	737   	737476      	       	NM  										GALLEY	FAILED          	W				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			CR	CRUISE         	1			AU	S 										(AUS) AFT GALLEY POWER SUPPLY CABLES DAMAGED AND SHORT CIRCUITING SUSPECT DUE TO INSULATION BREAKDOWN.						2	L	7	2 	4F			RT	A16WE   					 
2000011500300	20000115	00300	NM  	2000	1	15	AU991005         	1	19990916	G	7110		PANEL           			BOEING	767   	767338      	1385151	NM  	GE    	CF6   	CF680C      		GL  					LT ENGINE COWL	SEPARATED       	W				A				UNSCHED LANDING         				D	J		INFLIGHT SEPARATION       	WARNING INDICATION        		CL	CLIMB          	1			AU	S 										(AUS) LEFT ENGINE NOSE COWL ANTI-ICE PANEL LOCATED AT THE 12 O'CLOCK POSITION SEPARATED FROM THE ENGINE. THE AIRCRAFT HA	D JUST COMPLETED A C-CHECK.					2	L	7	2 	4F	4	F	RT	A1NM    	E23EA				 
2000011500301	20000115	00301	NM  	2000	1	15	AU991006         	1	19990913	G	7160		CONNECTOR       			BOEING	747   	747438      		NM  										ENGINE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NR 1 STRUT BULKHEAD CONNECTORS ARCING.  FURTHER INVESTIGATION FOUND THE WIRING LOOM CONDUIT D8451P DRAIN HOLE INCO	RRECTLY POSITIONED ALLOWING A BUILD UP OF HYDRAULIC FLUID AT THE REAR OF THE CONNECTOR WHICH CAUSED DETERIORATION OF THE	 RUBBER INSERT WHICH ALLOWED THE PINS TO SHORT CIRCUIT.				2	L	7	4 	4F			RT	A20WE   					 
2000011500302	20000115	00302	EU  	2000	1	15	AU991007         	2	19990914	G	7230		BEARING         			BOEING	737   	737376      		NM  	CFMINT	CFM56 	CFM563C1    	13802	EU  					NR 1 ENGINE	FAILED          	W				A				UNSCHED LANDING         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CR	CRUISE         	1			AU	S 										(AUS) NR 1 ENGINE NR 4 BEARING FAILED.						2	L	7	2 	4F	4	F	RT	A16WE   	E21EU				 
2000011500303	20000115	00303	NE  	2000	1	15	AU991008         	2	19991002	G	7320		LINE            			BOEING	767   	767238      		NM  	PWA   	JT9   	JT9D7R4E    	52054	NE  					RT ENGINE	LOOSE           	W				A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			AU	S 										(AUS) RIGHT ENGINE T2 SENSOR PTT2 FUEL LINE LOOSE AND LEAKING FUEL.						2	L	7	2 	4F	4	F	RT	A1NM    	E3NE				 
2000011500304	20000115	00304	EA  	2000	1	15	AU991009         	2	19991015	G	7310	2524172	VALVE           			GULSTM	500   	500S        	0141107	SW  	LYC   	O540  	IO540E1B5   	41532	EA  	HARTZL	HCC3Y	HCC3YR2     	NE  	FUEL MANIFOLD	FAULTY          	W				A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			AU	S 			857  				L595548			(AUS) FUEL MANIFOLD VALVE FAULTY.						1	H	7	2 	3O	3	O		6A1     	1E4	5	C	P25EA	 
2000011500305	20000115	00305	EU  	2000	1	15	AU991010         	2	19991002	G	7310	737M285001	VALVE           			BOEING	737   	737376      		NM  	CFMINT	CFM56 	CFM563C1    	13802	EU  					FUEL SYSTEM	FAULTY          	W				D				RETURN TO BLOCK         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		TX	TAXI/GRND HDL  	1			AU	S 					477					(AUS) NR 2 ENGINE FUEL SPAR VALVE FAULTY.						2	L	7	2 	4F	4	F	RT	A16WE   	E21EU				 
2000011500306	20000115	00306	GL  	2000	1	15	AU991011         	2	19991010	G	7230	23057142	CASE            			BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	FAILED          	W				O				OTHER                   				T	R	J	ENGINE CASE PENETRATION   	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	DE	DESCENT        	1			AU	S 			514  				CAE830380			(AUS) COMPRESSOR CASE DAMAGED IN THE AREA OF THE THIRD AND FOURTH STAGE OF THE COMPRESSOR DUE TO STATOR FAILURE.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
2000011500307	20000115	00307	NM  	2000	1	15	AU991012         	1	19991004	G	2497		WIRE            			BOEING	767   	767338      	1385151	NM  	GE    	CF6   	CF680C      	 	GL  					AC POWER SYSTEM	CHAFED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) ELECTRICAL FEEDER CABLE ARCING DUE TO CHAFING ON HINGED SUPPORT CLAMPS.						2	L	7	2 	4F	4	F	RT	A1NM    	E23EA				 
2000011500308	20000115	00308	GL  	2000	1	15	AU991013         	3	19991015	G	6111	TC005	BLADE           	MCAULY      	1A1036958   	CESSNA	150   	A152        	2071836	CE  	LYC   	O235  	O235L2C     	41505	EA  	MCAULY	1A103	1A103TCM    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					TC005			TC5		(AUS) PROPELLER BLADE CONTAINED EXFOLIATION CORROSION.  AREA OF CORROSION APPROXIMATELY 6 MM (0.236 INCH) BY 4 MM (0.157	 INCH) BY 1 MM (0.039 INCH) DEEP.  THE PROPELLER WAS INSTALLED NEW ON THE 7/14/99.					1	H	7	1 	3O	3	O		3A19    	E223	5	N	P50GL	 
2000011500309	20000115	00309	CE  	2000	1	15	AU991014         	1	19991011	G	2822	476411	PUMP            			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C*     	GL  	FUEL BOOST	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							277564R	9682		(AUS) RIGHT MAIN FUEL TANK TRANSFER PUMP FAILED.  INVESTIGATION FOUND THE PUMP TO BE OPEN CIRCUITED. THE  PUMP HAD COMPL	ETED 227 HOURS TIME IN SERVICE SINCE NEW.					1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22EA	 
2000011500310	20000115	00310	NM  	2000	1	15	AU991015         	1	19990930	G	5400		ROD             			BOEING	767   	76733A      	1385209	NM  	PWA   	4056  	PW4056      		NE  					RT PYLON	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) FOLLOWING REMOVAL OF THE RT PYLON BOAT FAIRING FOR REPAIR THE FOLLOWING DEFECTS WERE FOUND:  1.  RT ENGINE DRIVEN 	HYDRAULIC PUMP PRESSURE AND SUPPLY LINE  ELBOW JAM NUTS BACKED OFF AND ELBOW FRETTING IN PYLON RECEPTACLES2S.   2.   INB	OARD VERTICAL STRAKE RIVET HEAD MISSING.   3.   INBOARD PYLON FAIRING SUPPORT ROD ATTACHMENT FITTING WORN DUE TO FRETTIN	G BEARING.  4.  RT PYLON AFT FAIRING STAINLESS STEEL HEAT SHIELDS/CLOSING PANELS HAD NUMEROUS LOOSE AND MISSING FASTENER	S.		2	L	7	2 	4F	4	F	RT	A1NM    	E24NE				 
2000011500311	20000115	00311	NM  	2000	1	15	AU991016         	1	19990709	G	2910	654468114	ACTUATOR        			BOEING	737   	737476      		NM  										HYDRAULIC SYS	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) STANDBY HYDRAULIC MODULE STANDBY RUDDER SHUTOFF ACTUATOR FAULTY.						2	L	7	2 	4F			RT	A16WE   					 
2000022300014	20000223	00014	NM  	2000	2	23	AU991017         	1	19990908	G	2597		WIRE            			BOEING	747   	747238B     	1384828	NM  										GALLEY	CONTAMINATED    	W				A				UNSCHED LANDING         				H	B	J	ELECT. POWER LOSS-50 PC   	SMOKE/FUMES/ODORS/SPARKS  	WARNING INDICATION        	CR	CRUISE         	1			AU	S 										(AUS) REAR GALLEY HOTPLATE WIRING AND TERMINAL BLOCK DETERIORATED.  WATER CONTAMINATION OF WIRING.						2	L	7	4 	4F			 	A20WE   					 
2000011500312	20000115	00312	NM  	2000	1	15	AU991018         	1	19991002	G	2520	737M25503011	SEAT            			BOEING	737   	737476      		NM  										CABIN	FAILED          	W				A				UNSCHED LANDING         				O			OTHER                     			CL	CLIMB          	1			AU	S 										(AUS) REAR FLIGHT ATTENDANT'S SEAT COLLAPSED.  AIRCRAFT WAS EXPERIENCING MODERATE TURBULENCE AT THE TIME.  THE SEAT WAS 	OCCUPIED.					2	L	7	2 	4F			RT	A16WE   					 
2000011500313	20000115	00313	NM  	2000	1	15	AU991019         	1	19990926	G	4920		TURBINE         			BOEING	737   	737376      		NM  										APU	DISINTEGRATED   	W				O				OTHER                   				T	J		ENGINE CASE PENETRATION   	WARNING INDICATION        		NR	NOT REPORTED   	1			AU	S 										(AUS) APU TURBINE DISINTEGRATED.  TURBINE PIECES STOPPED BY CONTAINMENT SHROUD.						2	L	7	2 	4F			RT	A16WE   					 
2000011500314	20000115	00314	CE  	2000	1	15	AU991023         	1	19991008	G	5610	101384025021	WINDSHIELD      			BEECH 	200   	B200C       	1152924	CE  	PWA   	PT6   	PT6A41      	52043	EA  	HARTZL	HCD4N3	HCD4N3A     	GL  	COCKPIT	BROKEN          	W				A				UNSCHED LANDING         				O			OTHER                     			CR	CRUISE         	1			AU	S 			773  		97342H2576					(AUS) INNER PANEL ON PILOT'S WINDSHIELD SHATTERED.						1	L	7	2 	4T	4	T		A24CE   	E4EA	5	C	STC	 
2000011500315	20000115	00315	CE  	2000	1	15	AU991025         	1	19991005	G	6120	565580004	CONTROL CABLE   	MCAULY      	B2D34C220   	CESSNA	172   	172RG       	2072438	CE  	LYC   	O360  	O360F1A6    	41514	EA  	MCAULY	2D34C	B2D34C220   	GL  	PITCH CONTROL	FAULTY          	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			AU	S 			23   				L2992536A	814995		(AUS) PROPELLER PITCH CONTROL CABLE FAULTY.						1	H	7	1 	3O	3	O	 	3A17    	E286	5	C	P7EA	 
2000022300015	20000223	00015	CE  	2000	2	23	AU991026         	1	19991016	G	3233	481	ACTUATOR        			BEECH 	200   	B200C       	1152924	CE  	PWA   	PT6   	PT6A42      	52043	NE  					MLG	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 			20451		516A					(AUS) LANDING GEAR MOTOR FAULTY.						1	L	7	2 	4T	4	T		A24CE   	E4EA				 
2000011500316	20000115	00316	CE  	2000	1	15	AU991027         	1	19991008	G	2731	12601491	ACTUATOR        			CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	ELEVATOR TAB	WORN            	W				A				UNSCHED LANDING         				F			FLT CONT AFFECTED         			CL	CLIMB          	1			AU	S 										(AUS) ELEVATOR TAB ACTUATOR SPROCKET LOCATING PINS MIGRATED PREVENTING THE TAB FROM MOVING.  INVESTIGATION FOUND WEAR IN	 THE GROOVE PIN HOLES.					1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
2000011500317	20000115	00317	EU  	2000	1	15	AU991028         	1	19991021	G	5343	880214561	BRACKET         		880214562   	SOCATA	MS893 	MS893E      	8402838	EU  	LYC   	O360  	O360A1A     	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR LEFT (P/N 880-21-456-1) AND RIGHT (P/N 880-21-456-2) ATTACHMENT BRACKETS CRACKED.						1	L	7	1 	3O	3	O		7A14    	E286	5	C	P920	 
2000011500318	20000115	00318	NM  	2000	1	15	AU991029         	1	19991015	G	3230	BACB30EK5A24C	BOLT            			BOEING	737   	737376      		NM  										MLG	SHEARED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) MAIN LANDING GEAR WALKING BEAM HANGER BRACKET LOWER ATTACHMENT BOLTS (2 OFF) SHEARED.  THE UPPER BOLTS (2 OFF) WER	E STILL INTACT.					2	L	7	2 	4F			RT	A16WE   					 
2000011500319	20000115	00319	EU  	2000	1	15	AU991030         	1	19991001	G	5530		BRACKET         			BNORM 	BN2   	BN2A20      	1520220	EU  	LYC   	O540  	IO540K1B5   	41532	EA  	HARTZL	HCC2Y	HCC2YR2     	GL  	VERTICAL STAB	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) CENTER RUDDER ATTACHMENT BRACKET DAMAGED.						1	H	7	2 	3O	3	O		A17EU   	1E4	5	C	P920	 
2000011500320	20000115	00320	SO  	2000	1	15	AU991032         	1	19991013	G	7810	12033750004	EXHAUST PIPE    			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  	HAMSTD	14RF	14RF9       	NE  	RT ENGINE	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							PCE115644			(AUS) RIGHT ENGINE EXHAUST EXIT DUCT CRACKED AND DAMAGED.  INVESTIGATION FOUND THAT THE COWL FITTED OVER THE EXHAUST WAS	 INCORRECTLY  FITTED AND WAS RUBBING ON THE DUCT.					2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	C	P11NE	 
2000011500321	20000115	00321	SO  	2000	1	15	AU991033         	1	19991013	G	2612	PCE115644	SENSOR          			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  	HAMSTD	14RF	14RF9       	NE  	RT ENGINE	CHAFED          	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 							PCE115644			(AUS) RIGHT ENGINE CONTAINED THE FOLLOWING DEFICIENCIES FOUND DURING SCHEDULED MAINTENANCE:  1.  INTAKE TO ENGINE V-BAND	 COUPLING LOOSE.   2.   AUXILIARY GENERATOR COOLING AIR OUTLET DRAIN NOT CONNECTED.   3.  FIRE DETECTION SENSOR CHAFING 	IN SEVERAL PLACES.   4. FIRE DETECTION SENSOR ELECTRICAL CONNECTOR  LOOSE AND NOT LOCKWIRED.   5.   MAIN ENGINE CONTROLL	ER ELECTRICAL CONNECTOR  LOOSE AND NOT LOCKWIRED.  THE ENGINE HAD BEEN INSTALLED THREE DAYS PREVIOUS.			2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	C	P11NE	 
2000011500322	20000115	00322	NM  	2000	1	15	AU991034         	1	19991020	G	2510	D9981J	CONNECTOR       		D9981P      	BOEING	747   	747338      		NM  										COCKPIT	FAILED          	W				K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			AU	S 										(AUS) CREW REST INTERFACE MODULE CONNECTOR PINS SHORT CIRCUITED.  SUBMITTER SUSPECTED CONNECTORS CONTAMINATED BY WATER.						2	L	7	2 	4F			RT	A20WE   					 
2000011500323	20000115	00323	SO  	2000	1	15	AU991035         	2	19991014	G	7414	1034922004	MAGNETO         			CESSNA	404   	404CESSNA   	2075901	CE  	CONT  	O520  	GTSIO520M   	17032	SO  	MCAULY	3AF34C	3AF34C74    	GL  	LT ENGINE	FAILED          	W				A				UNSCHED LANDING         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CR	CRUISE         	1			AU	S 			105  				243455			(AUS) LEFT ENGINE LEFTMAGNETO FAULTY.   POINTS CONTAMINATED WITH OIL AND PRIMARY COIL LEAD CHAFED.						1	L	7	2 	3O	3	O		A25CE   	E7CE	5	C	P22EA	 
2000011500324	20000115	00324	SO  	2000	1	15	AU991036         	2	19991014	G	7414	103492607	MAGNETO         			CESSNA	404   	404CESSNA   	2075901	CE  	CONT  	O520  	GTSIO520M   	17032	SO  	MCAULY	3AF34C	3AF34C74    	GL  	LT ENGINE	FAILED          	W				A				UNSCHED LANDING         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CR	CRUISE         	1			AU	S 			105  				243455			(AUS) LEFT ENGINE RIGHT MAGNETO FAULTY.  POINTS BURNT AND COIL PRIMARY RESISTANCE OUT OF TOLERANCE.  SIGNS OF PITTING ON	 THE DISTRIBUTOR BLOCK.  SEE MDR AU991035 FOR FURTHER INFORMATION.					1	L	7	2 	3O	3	O		A25CE   	E7CE	5	C	P22EA	 
2000011500325	20000115	00325		2000	1	15	AU991037         	4	19990826	G	3418		STALL WARNING   			PIPER 	PA34  	PA34200T    	7103406	SO  	CONT  	O360  	TSIO360E    	17025	SO  	HARTZL	HCC2Y	BHCC2YF2    	GL  	COCKPIT	MALFUNCTIONED   	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) STALL WARNING SYSTEM FAULTY.  SYSTEM WORKS PERFECTLY ON THE GROUND BUT FAILS TO OPERATE IN THE AIR.  THE SYSTEM HA	S BEEN THOROUGHLY CHECKED WITH NUMEROUS COMPONENT CHANGES TO NO AVAIL.					1	L	7	2 	3O	3	O		A7SO    	E9CE	5	C	P920	 
2000011500326	20000115	00326	NM  	2000	1	15	AU991038         	1	19990622	G	2780		ROD             			BOEING	767   	767277      		NM  	GE    	CF6   	CF680A      	30025	NE  					LE FLAP	OUT OF ADJUST   	W				O				OTHER                   				F	J		FLT CONT AFFECTED         	WARNING INDICATION        		NR	NOT REPORTED   	1			AU	S 										(AUS) OUTBOARD SLAT PDU INPUT ROD OUT OF ADJUSTMENT.						2	L	7	2 	4F	4	F	RT	A1NM    	E13NE				 
2000011500327	20000115	00327	EU  	2000	1	15	AU991039         	1	19991001	G	5730		TAPE            			BNORM 	BN2   	BN2A20      	1520220	EU  	LYC   	O540  	IO540K1B5   	41532	EA  	HARTZL	HCC2Y	HCC2YR2     	GL  	WING	UNAPPROVED PART 	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) LEADING EDGE TAPES FITTED TO WINGS HAD NO DOCUMENTATION.  MANUFACTURER DOES NOT APPROVE OF TAPE FITMENT. TAPE WAS 	ALSO POORLY FITTED AND WAS NOT ADHERING CORRECTLY.   UNAPPROVED PART.					1	H	7	2 	3O	3	O		A17EU   	1E4	5	C	P920	 
2000011500328	20000115	00328	NM  	2000	1	15	AU991040         	1	19991023	G	7712	575	TSCU            			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	RT ENGINE	FAULTY          	W				A				UNSCHED LANDING         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CL	CLIMB          	1			AU	S 							120038			(AUS) RIGHT ENGINE TORQUE SIGNAL CONDITIONER (TSCU) FAULTY.  THE FAILURE WAS FOUND TO BE IN THE ENGINE INDICATION SYSTEM	 OF THE TSCU.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
2000011500329	20000115	00329	CE  	2000	1	15	AU991041         	1	19990729	G	2822	476411	PUMP            			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	2D34C	B2D34C214   	GL  	FUEL BOOST	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							277602	1678		(AUS) LEFT MAIN FUEL TANK FUEL TRANSFER PUMP FAULTY.  INVESTIGATION FOUND THE PUMP TO BE OPEN CIRCUITED.  SUSPECT BURNT 	OUT CONTACTS.					1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P7EA	 
2000011500330	20000115	00330	CE  	2000	1	15	AU991042         	1	19991018	G	2822	476411	PUMP            			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C*     	GL  	FUEL BOOST	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							277331	95679		(AUS) RIGHT MAIN FUEL TANK FUEL TRANSFER PUMP FAULTY.  INVESTIGATION FOUND THE PUMP OPEN CIRCUITED.  SUSPECT BURNT OUT C	ONTACTS.					1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22EA	 
2000011500331	20000115	00331	CE  	2000	1	15	AU991043         	1	19991018	G	2822	476411	PUMP            			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C*     	GL  	FUEL BOOST	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							277548R	9568		(AUS) LEFT MAIN FUEL TANK FUEL TRANSFER PUMP FAULTY. INVESTIGATION FOUND THE PUMP OPEN CIRCUITED.  SUSPECT CAUSED BY BUR	NT OUT CONTACTS.					1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22EA	 
2000022300016	20000223	00016		2000	2	23	AU991044         	4	19991020	G	2565	71124831	SLIDE           			BOEING	747   	747238B     	1384828	NM  										PAX DOOR	FAILED          	W				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT UPPER DECK ESCAPE SLIDE FAILED TO FULLY DEPLOY DUE TO THE FORWARD BELLCRANK CONTACTING A DOOR FITTING.						2	L	7	4 	4F				A20WE   					 
2000011500332	20000115	00332	EU  	2000	1	15	AU991045         	2	19991023	G	7230		BEARING         			BOEING	737   	737476      		NM  	CFMINT	CFM56 	CFM563C1    	13802	EU  					RT ENGINE	LEAKING         	W				C				ABORTED TAKEOFF         				E	B	J	VIBRATION/BUFFET          	SMOKE/FUMES/ODORS/SPARKS  	WARNING INDICATION        	TO	TAKEOFF        	1			AU	S 										(AUS) RIGHT ENGINE OIL LEAKING INTO COMPRESSOR.  SUSPECT NR 4 BEARING LEAKING.						2	L	7	2 	4F	4	F	RT	A16WE   	E21EU				 
2000011500333	20000115	00333	NM  	2000	1	15	AU991046         	1	19990814	G	2497	292110005A12C1	WIRE            			DHAV  	DHC8  	DHC8201     	2809001	NM  						HAMSTD	14SF	14SF23      	NE  	AC POWER SYSTEM	CHAFED          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			AU	S 										(AUS) WIRING IN LEFT AC CONTACTOR BOX SHORT CIRCUITING DUE TO CHAFING.  LEFT AC GCU FOUND TO BE FAULTY.						2	H	7	2 	4T			RT	A13NM   		6	C	P7NE	 
2000011500334	20000115	00334	SO  	2000	1	15	AU991047         	1	19991011	G	2710	24166002	ROD END         			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	AILERON	SEIZED          	W				C				ABORTED TAKEOFF         				F			FLT CONT AFFECTED         			TO	TAKEOFF        	1			AU	S 										(AUS) AILERON CONTROL ROD ROD END SEIZED AND BROKEN.						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
2000011500335	20000115	00335		2000	1	15	AU991048         	4	19991014	G	2320	82450067001	BRACKET         			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	FUSELAGE	BROKEN          	W				A				UNSCHED LANDING         				H	J		ELECT. POWER LOSS-50 PC   	WARNING INDICATION        		CR	CRUISE         	1			AU	S 										(AUS) LEFT AC CONTACTOR BOX CIRCUIT BREAKER PANEL BROKEN ALLOWING THE CIRCUIT BREAKER TERMINALS TO SHORT CIRCUIT ONTO TH	E CONTACTOR BOX AND CAUSING THE NR 1 AC GENERATOR TO FAIL.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
2000011500336	20000115	00336	GL  	2000	1	15	AU991049         	2	19991018	G	7250	23031938	DIAPHRAGM       			HUGHES	369   	369E        	4470707	WP  	ALLSN 	250C  	250C20R1    	03013	GL  					GAS PRODUCER	FAILED          	W				C				ABORTED TAKEOFF         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		TO	TAKEOFF        	1			AU	S 										(AUS) GAS PRODUCER TURBINE SECOND STAGE NOZZLE DIAPHRAGM FAILED AND RUBBING ON THE FIST AND SECOND STAGE TURBINE WHEELS.						1	G	7	1 	3U	3	U		H3WE    	E4CE				 
2000011500337	20000115	00337	NM  	2000	1	15	AU991050         	1	19991023	G	2810	A7131	STRAP           			ROBSIN	R22   	R22BETA     		NM  	LYC   	O320  	O320B2C     	41508	EA  					FUEL STORAGE	MISSING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			250  							(AUS) ROTOR CONTROL PUSH/PULL TUBE P/N A121-7 WORN.  INVESTIGATION FOUND THAT THE FUEL TANK RETAINING STRAP P/N A713-1 H	AD NOT BEEN FITTED DURING AIRCRAFT REBUILD ALLOWING THE TANK TO MOVE AND RUB ON THE CONTROL RODS.  AN EFFORT HAD BEEN MA	DE TO HIDE THE DAMAGE BY USING HEAT SHRINK ON THE CONTROL TUBE AND BY FILING AWAY THE FUEL TANK.				1	G	7	1 	3O	3	O		H10WE   	E274				 
2000011500338	20000115	00338		2000	1	15	AU991051         	4	19991027	G	3442	6222504001	ANTENNA         	COLLINS     	6222504001  	DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	WEATHER RADAR	FAILED          	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			AU	S 					1004					(AUS) WEATHER RADAR ANTENNA FAILED.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
2000011500339	20000115	00339	EU  	2000	1	15	AU991052         	1	19991027	G	6123	3048000011	CONTROL UNIT    	ROTOL       	R352        	FOKKER	F27   	F27MK50     		EU  	PWA   	PWA120	PW125B      		NE  					PROP FEATHER	FAULTY          	W				C				ABORTED TAKEOFF         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		TO	TAKEOFF        	1			AU	S 					150		124051			(AUS) RIGHT ENGINE AUTOFEATHER UNIT FAILED.						2	H	7	2 	4T	4	T	RT	A817    	E20NE				 
2000011500340	20000115	00340	NM  	2000	1	15	AU991054         	1	19990815	G	2612		CONNECTOR       			BOEING	737   	737377      		NM  										NR 2 ENGINE	LOOSE           	W				C				ABORTED TAKEOFF         				N			FALSE WARNING             			TO	TAKEOFF        	1			AU	S 										(AUS) NR 2 ENGINE FIRE DETECTOR SYSTEM CONNECTOR PLUG D1208 LOOSE.  FALSE FIRE WARNING RESULTED IN DISCHARGE OF BOTH FIR	E BOTTLES.					2	L	7	2 	4F			RT	A16WE   					 
2000011500341	20000115	00341		2000	1	15	AU991056         	4	19991009	G	3442	3718637902903	TRANSISTOR      		MI585205    	AEROSP	SA365 	SA365C      	8680667	EU  	TMECA 	ARRIEL	ARRIEL1A    	60030	NE  					WEATHER RADAR	FAILED          	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			AU	S 			2972 		1020					(AUS) RADAR ANTENNA FAILED.  INVESTIGATION FOUND TWO TRANSISTORS ON THE ANTENNA MOTOR DRIVE BOARD WERE DEFECTIVE.						1	G	7	2 	3U	3	U		H10EU   	E19EU				 
2000011500342	20000115	00342	EU  	2000	1	15	AU991057         	1	19991014	G	8012	31860000	VALVE           			AEROSP	SA365 	SA365C      	8680667	EU  	TMECA 	ARRIEL	ARRIEL1A    	60030	NE  					NR 1 ENGINE	LEAKING         	W				O				OTHER                   				E	K		VIBRATION/BUFFET          	FLUID LOSS                		NR	NOT REPORTED   	1			AU	S 							133			(AUS) NR 1 ENGINE IGNITION SOLENOID VALVE LEAKING FUEL.						1	G	7	2 	3U	3	U		H10EU   	E19EU				 
2000011500343	20000115	00343	EU  	2000	1	15	AU991058         	1	19991013	G	5280	HC321B004000	BRACKET         			BAG   	BAE146	BAE146300A  	1500267	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					MLG DOOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT AND RIGHT MAIN LANDING GEAR DOOR REAR HINGE BRACKETS CORRODED ON THE FORWARD SEGMENTS ADJACENT TO THE BONDING	 LEAD ATTACHMENT HOLES.  FOUND DURING INSPECTION IAW AD/BAE146/035, SB 32-A119 AND ER BA6-32-10-30.					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
2000011500344	20000115	00344	CE  	2000	1	15	AU991059         	1	19990510	G	3220		ROD END         		3500A       	CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	NLG	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR CLEVIS ROD ENDS WORN AND DISTORTED.  ROD ENDS ALSO APPEAR TO BE REWORKED.  AN481 PARTS GIVEN A N	EW PART NUMBER.					1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
2000011500345	20000115	00345	CE  	2000	1	15	AU991060         	1	19990510	G	3246		SEAL            		3500A       	CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	MLG	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AU	S 										(AUS) WHEEL SEALS INEFFECTIVE. THE AIRCRAFT IS EQUIPPED WITH FLOATS ANDTHE SEALS ARE USED TO KEEP THE GREASE IN AN THE W	AD THE WATER OUT.  THE SEALS ARE DISLODGED WHEN ATTEMPTING TO GREASE THE WHEELS.  SUSPECT UNAPPROVED PART.					1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
2000011500346	20000115	00346	NM  	2000	1	15	AU991061         	1	19991031	G	2910	DSC252B40124	HOSE            			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	HYDRAULIC SYS	FAILED          	W				C				ABORTED TAKEOFF         				K	J		FLUID LOSS                	WARNING INDICATION        		TO	TAKEOFF        	1			AU	S 										(AUS) FLEXIBLE HYDRAULIC HOSE FAILED.   LOSS OF NR 2 HYDRAULIC SYSTEM FLUID.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
2000011500347	20000115	00347	EA  	2000	1	15	AU991062         	2	19990922	G	8520		CRANKSHAFT      			PIPER 	PA30  	PA30        	7103002	SO  	LYC   	O320  	IO320B1A    	41508	EA  	HARTZL	HCE2Y	HCE2YR2     	GL  	ENGINE	FAILED          	W				O				OTHER                   				E	K		VIBRATION/BUFFET          	FLUID LOSS                		DE	DESCENT        	1			AU	S 							L30855			(AUS) CRANKSHAFT BROKEN AT NR 1 CONNECTING ROD POSITION.  NR 1 CONNECTING ROD BEARING SPINNING. CRANKCASE THRUST FACE WO	RN.  INVESTIGATION FOUND THAT THE FAILURE WAS A RESULT OF FATIGUE INITIATING FROM A SMALL DEFECT ON THE CRANKSHAFT CHEEK	 ADJACENT TO THE SLUDGE TUBE  HOLE.				1	L	7	2 	3O	3	O		A1EA    	1E12	5	C	P9EA	 
2000011500348	20000115	00348	WP  	2000	1	15	AU991063         	2	19991014	G	7230	89452810	STATOR          								GARRTT	TPE331	TPE331*     	01514	WP  					ENGINE	UNSERVICEABLE   	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) SECOND STAGE STATOR FAULTY.  STATOR WAS RECEIVED FROM THE OVERHAUL FACILITY WITH ZERO HOURS TSN.  UPON INSPECTION 	ONLY ONE SCREW HOLE OUT OF TWELVE WAS ABLE TO ACCEPT A BOLT.  THE BOLTS ATTACH THE ITT HARNESS.										3	T			E2WE				 
2000011500349	20000115	00349	CE  	2000	1	15	AU991064         	1	19990528	G	3211	514110313	TRUNNION        			CESSNA	402   	402C        	207590R	CE  	CONT  	O520  	TSIO520VB   	17040	SO  	MCAULY	3AF32C	3AF32C*     	GL  	LT MLG	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT MAIN LANDING GEAR TRUNNION ASSEMBLY ACTUATOR ATTACHMENT LUG CONTAINED A FAULT LINE.  CONFIRMED USING DYE PENE	TRANT AND EDDY CURRENT INSPECTIONS.					1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22EA	 
2000011500350	20000115	00350	GL  	2000	1	15	AU991065         	2	19990922	G	7532	23001789	BLEED VALVE     								ALLSN 	250C  	250C30P     	03013	GL  					COMPRESSOR	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					FF36036					(AUS) ENGINE BLEED VALVE PC PORT CONTAINED DAMAGED THREADS DUE TO CORROSION.  THE BLEED VALVE WAS AN OVERHAULED EXCHANGE	 ITEM BEING INSPECTED BEFORE FITMENT.										3	U			E1GL				 
2000011500351	20000115	00351	NM  	2000	1	15	AU991066         	1	19990615	G	5330		SKIN            			BOEING	737   	737377      		NM  										FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT SERVICE DOOR AFT LOWER CORNER RADIUS CRACKED.  CRACK LENGTH APPROXIMATELY 25.4 MM (1 INCH) RUNNING THROUGH T	WO THICKNESSES OF SKIN.  CRACK FOUND AFTER THE DOOR SCUFF PLATE WAS REMOVED.					2	L	7	2 	4F			RT	A16WE   					 
2000011500352	20000115	00352	CE  	2000	1	15	AU991067         	1	19991007	G	3110	07601316	COLLAR          			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	INSTRUMENT PANEL	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT INSTRUMENT PANEL LOCK COLLAR CRACKED.						1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
2000011500353	20000115	00353	NE  	2000	1	15	AU991068         	2	19991003	G	7322	786394	FCU             			EMB   	120   	EMB120      	3260201	SO  	PWA   	118   	PW118A      		NE  	HAMSTD	14RF	14RF9       	NE  	RT ENGINE	FAULTY          	W				A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			AU	S 			1    				115710			(AUS) RIGHT ENGINE FUEL CONTROL UNIT FAULTY.						2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	C	P11NE	 
2000011500354	20000115	00354		2000	1	15	AU991069         	4	19990726	G	3421	10076301	ADIRU           			AIRBUS	320   	A320212     		EU  										COCKPIT	FAULTY          	W				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			AU	S 					HG1150AC0513					(AUS) ATTITUDE GYRO INDICATOR REMOTE UNIT (ADIRU) FAULTY.						2	L	7	2 	4F			RT	A28NM   					 
2000011500355	20000115	00355	SO  	2000	1	15	AU991070         	2	19990908	G	8530	652956	EXHAUST VALVE   			CESSNA	182   	182R        	2072731	CE  	CONT  	O470  	O470S       	17026	SO  	MCAULY	2A34C	2A34C203    	GL  	ENGINE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							470266			(AUS) NR 1 CYLINDER EXHAUST VALVE P/N 652956 AND EXHAUST VALVE GUIDE P/N 643767 WORN BEYOND LIMITS.						1	L	7	1 	3O	3	O	NT	3A13    	E273	5	C	P3EA	 
2000011500356	20000115	00356	EA  	2000	1	15	AU991071         	2	19991012	G	7320	4708849010	CONTROLLER      			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	LTIO540J2BD 	41533	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	FUEL SYSTEM	LEAKING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			298  				RL21168A			(AUS) DENSITY CONTROLLER LEAKING INTERNALLY FROM CAPSULE AREA.						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
2000011500357	20000115	00357	SO  	2000	1	15	AU991072         	2	19991003	G	8520	6295183H	PLUG            			CESSNA	210   	210L        	2073448	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	3A32C	D3A32C88    	GL  	CRANKCASE	MISSING         	W				C				ABORTED TAKEOFF         				E	K		VIBRATION/BUFFET          	FLUID LOSS                		TO	TAKEOFF        	1			AU	S 							28197R			(AUS) CRANKCASE OIL GALLERY PLUG FELL OUT OF THE SUCTION SIDE OF THE OIL PUMP ALLOWING AIR INTO THE SUCTION LINE.  SUSPE	CT PLUG INCORRECTLY FITTED DURING OVERHAUL.					1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P21EA	 
2000011500358	20000115	00358	SO  	2000	1	15	AU991073         	1	19991012	G	8011	MHB4014	STARTER         			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	LTIO540J2BD 	41533	EA  	HARTZL	HCE3Y	HCE3YR2     	GL  	ENGINE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			298  				RL21168A			(AUS) STARTER MOTOR FAILED.  SUSPECT ARMATURE OR BUSHING PROBLEM.						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
2000011500359	20000115	00359	CE  	2000	1	15	AU991074         	1	19990814	G	2913	98807101	PRESSURE SWITCH 		POWERPACK   	CESSNA	210   	210L        	2073448	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	3A32C	D3A32C88    	GL  	HYD POWERPACK	FAULTY          	W				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			AU	S 			50   		303					(AUS) HYDRAULIC POWER PACK PRESSURE SWITCH FAULTY.						1	H	7	1 	3O	3	O		3A21    	E5CE	5	C	P21EA	 
2000011500360	20000115	00360	GL  	2000	1	15	AU991075         	1	19990730	G	2460	W23X1AG50	CIRCUIT BREAKER 			AMTR  	LANCAR	LANCAIRIV   	056163V	GL  	CONT  		TSIO550E    							DC POWER SYS	FAILED          	W				A				UNSCHED LANDING         				H	J		ELECT. POWER LOSS-50 PC   	WARNING INDICATION        		CR	CRUISE         	1			AU	S 										(AUS) INCORRECT RATED CIRCUIT BREAKER INSTALLED.  CIRCUIT BREAKER RATED AT 50 AMPS CONNECTED TO A 70 AMP ALTERNATOR.  CI	RCUIT BREAKER FAILED DURING FLIGHT.   UNAPPROVED PART.					1	L	7	1 	3O			RT	EXPA1L71					 
2000011500361	20000115	00361	EU  	2000	1	15	AU991076         	1	19991011	G	3213	201072383	FITTING         	ROTOL       	LHMLG       	FOKKER	F28   	F28MK1000   	4990808	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					MLG	BROKEN          	W				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			AU	S 					DRG374690					(AU) LEFT MAIN LANDING GEAR UPPER TORQUE LINK FITTING PIVOT PIN BOSS FAILED.  THE FAILURE WAS DIAGONAL FROM THE REAR OF 	THE INBOARD SIDE OF THE BOSS TO THE FRONT OF THE OUTBOARD SIDE.  THE BREAK TRAVERSED THROUGH THE PIVOT PIN LOCATING HOLE	.				2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
2000011500362	20000115	00362	WP  	2000	1	15	AU991077         	2	19991007	G	7230		BEARING         			BAG   	JETSTM	JETSTM3201  	1500217	EU  	GARRTT	TPE331	TPE33112UA  	01514	WP  	MCAULY	4HFR34	4HFR34C653  	NE  	ENGINE	FAILED          	W				O				OTHER                   				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		DE	DESCENT        	1			AU	S 							P66231C			(AUS) ENGINE OIL FILTER CONTAMINATED WITH METAL.  SUSPECT COMPRESSOR BEARING FAILURE.						2	L	7	2 	4T	4	T	RT	A56EU   	E4WE	6	C	3PNE	 
2000011500363	20000115	00363	CE  	2000	1	15	AU991078         	1	19990430	G	2820		NUT             			CESSNA	421   	421B        	2076014	CE  						MCAULY	3AF34C	3AF34C92    	GL  	RT WING	LOOSE           	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) ENGINE FUEL VAPOR RETURN LINE LOCATED IN THE RIGHT WING LEADING EDGE HAD A LOOSE CONNECTION NUT.  FUEL VAPORS EXPL	ODED CAUSING DAMAGE TO THE RIGHT WING LEADING EDGE.					1	L	7	2 	3O				A7CE    		5	C	P22EA	 
2000011500364	20000115	00364	CE  	2000	1	15	AU991079         	1	19991004	G	2710	0510105365	CONTROL CABLE   			CESSNA	172   	172R        	2072401	CE  						MCAULY	1C235	1C235LFA    	GL  	AILERON	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT AILERON CABLE WORN ON PHENOLIC BLOCK.						1	H	7	1 	3O			NT	3A12    		5	N	P12EA	 
2000011500365	20000115	00365	SO  	2000	1	15	AU991080         	2	19990910	G	8530	286365R	PISTON PIN      			CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	3A32C	D3A32C90    	GL  	NR 2 CYLINDER	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							286365R			(AUS) NR 2 CYLINDER PISTON PIN END CAP SHEARED OFF.  ENGINE OIL SYSTEM CONTAMINATED WITH METAL.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P21EA	 
2000011500366	20000115	00366	NE  	2000	1	15	AU991081         	2	19991031	G	7230		BEARING         			STBROS	SD3   	SD360       	8100606	EU  	PWA   	PT6   	PT6A67R     	52043	NE  	HARTZL	HCA6A	HCA6A3      	NE  	ENGINE	FAILED          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			AU	S 							PCE106003			(AUS) ENGINE FAILURE.  SUSPECT BEARING FAILURE.						2	H	7	2 	4T	4	T		A41EU   	E26NE	6	C	P14NE	 
2000011500367	20000115	00367		2000	1	15	AU991082         	1	19991023	G	7120	H2640200YZ	MOUNT           			AMTR  		CJ6A        												ENGINE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT AND RIGHT ENGINE MOUNT BRACKETS SEVERELY CORRODED.									0 										 
2000011500368	20000115	00368	SO  	2000	1	15	AU991083         	1	19991013	G	2434		ALTERNATOR      			PIPER 	PA32  	PA32R300    	7103213	SO  	LYC   	O540  	IO540K1G5   	41532	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	DC SYSTEM	FAILED          	W				O				OTHER                   				H			ELECT. POWER LOSS-50 PC   			LD	LANDING        	1			AU	S 							L1489748A			(AUS) ALTERNATOR FAILED INTERNALLY AND SEIZED CAUSING INTERNAL AND EXTERNAL DAMAGE.						1	L	7	1 	3O	3	O		A3SO    	1E4	5	C	P920	 
2000011500369	20000115	00369	CE  	2000	1	15	AU991084         	1	19990510	G	3246		BOLT            		3500A       	CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	MLG	UNAPPROVED PART 	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AU	S 										(AUS) MAIN AND NOSE LANDING GEAR PIVOT BOLTS HAVE THE HEADS GROUND TO APPEAR LIKE A CLEVIS BOLT HEAD.  THE AIRCRAFT IS F	ITTED WITH FLOATS.   UNAPPROVED PART. UNAPPROVED MODIFICATION.					1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
2000011500370	20000115	00370	CE  	2000	1	15	AU991085         	1	19990510	G	3246	4020603449	BEARING         			CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	MLG WHEEL	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					4020603449					(AUS) WHEEL BEARINGS CORRODED.  SUSPECT CAUSED BY DISLODGED WHEEL SEALS.  THE AIRCRAFT IS FITTED WITH FLOATS.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
2000011500371	20000115	00371	CE  	2000	1	15	AU991086         	1	19990510	G	3246		WHEEL           		3500A       	CESSNA	206   	U206F       	2073333	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	MLG	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) WHEEL RIM DAMAGED.  RIM HAS WORN AWAY.  AIRCRAFT IS EQUIPPED WITH FLOATS.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
2000011500372	20000115	00372	EU  	2000	1	15	AU991087         	2	19991101	G	7250	9547	BLADE           			FOKKER	F28   	F28MK4000   	4990810	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					TURBINE	DAMAGED         	W				K				NONE                    				O		K	OTHER                     		FLUID LOSS                	IN	INSP/MAINT     	1			AU	S 							9547			(AUS) LEFT ENGINE SECOND STAGE LP TURBINE BLADES CONTAIN IMPACT MARKS ON THE TRAILING EDGES.  FINE SLIVERS OF METAL IN T	HE TAILPIPE.  THE ENGINE WAS ALSO USING EXCESSIVE OIL.					2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
2000011500373	20000115	00373	WP  	2000	1	15	AU991088         	2	19991029	G	7200	P66329	ENGINE          			BAG   	JETSTM	JETSTM3201  	1500217	EU  	GARRTT	TPE331	TPE33112UHR 		WP  	MCAULY	4HFR34	4HFR34C653  	NE  	LEFT	SEIZED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							P66329			(AUS) LEFT ENGINE HARD TO TURN.   METAL CONTAMINATION OF ENGINE OIL SYSTEM.   FURTHER INVESTIGATION FOUND PROPELLER AND 	OIL COOLER ALSO METAL CONTAMINATED.					2	L	7	2 	4T	4	T	RT	A56EU   	E4WE	6	C	3PNE	 
2000011500374	20000115	00374	EA  	2000	1	15	AU991089         	2	19991025	G	7414	10382681	CAPACITOR       	BENDIX      	D6LN2000    	PIPER 	PA32  	PA32RT300T  	7103216	SO  	LYC   	O540  	TIO540S1AD  	41532	EA  	HARTZL	HCE3Y	HCE3YR1     	GL  	MAGNETO	FAULTY          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					85410133K		L537461A			(AUS) LEFT MAGNETO CAPACITOR OPEN CIRCUITED AND POINTS CAM FOLLOWER MELTED.						1	L	7	1 	3O	3	O		A3SO    	E14EA	5	C	P33EA	 
2000011500375	20000115	00375	CE  	2000	1	15	AU991090         	1	19990923	G	2750	RHFLAP	PUSHROD         			CESSNA	182   	182E        	2072712	CE  	CONT  	O470  	O470R       	17026	SO  	HARTZL	HCC2Y	BHCC2YF1    	GL  	TE FLAP	BROKEN          	W				O				OTHER                   				F			FLT CONT AFFECTED         			LD	LANDING        	1			AU	S 										(AUS) RIGHT PUSHROD BENT AND BROKEN.   INVESTIGATION FOUND RESTRICTION IN ONE OF THE FLAP TRACK ROLLERS.						1	H	7	1 	3O	3	O	NT	3A13    	E273	5	C	P920	 
2000011500376	20000115	00376	NM  	2000	1	15	AU991091         	1	19990912	G	7500	9354M37G01	DUCT            			BOEING	767   	767277      		NM  	GE    	CF6   	CF680A      	30025	NE  					BLEED  AIR	BURST           	W				O				OTHER                   				E			VIBRATION/BUFFET          			CL	CLIMB          	1			AU	S 							380342			(AUS) RIGHT ENGINE HP AIR DUCT ELBOW RUPTURED.						2	L	7	2 	4F	4	F	RT	A1NM    	E13NE				 
2000011500377	20000115	00377	NM  	2000	1	15	AU991092         	1	19990912	G	7500	9358M60G01	BRACKET         			BOEING	767   	767277      		NM  	GE    	CF6   	CF680A      	30025	NE  					BLEED AIR	BROKEN          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			AU	S 							380342			(AUS) RIGHT ENGINE BLEED AIR DUCT SUPPORT BRACKET BROKEN.  SUSPECT BROKEN BRACKET CAUSED BLEED AIR DUCT TO FAIL.   SEE M	DR AU991091.					2	L	7	2 	4F	4	F	RT	A1NM    	E13NE				 
2000011500378	20000115	00378	CE  	2000	1	15	AU991093         	1	19991103	G	7120	12921004701	MOUNT           			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  	HARTZL	HCE4A	HCE4A3I     	NE  	ENGINE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					S2697					(AUS) RIGHT ENGINE TRUSS CHAFED BY A CONNECTION ON THE AIR CONDITIONING COMPRESSOR SUCTION LINE.						2	L	7	2 	4T	4	T	RT	A24CE   	E26NE	5	C	P10NE	 
2000011500379	20000115	00379	EU  	2000	1	15	AU991094         	1	19991020	G	5280	HC321B0040000	BRACKET         			BAG   	BAE146	BAE146200A  	1500266	EU  	LYC   	ALF502	ALF502R5    	41580	NE  					MLG DOOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) LEFT AND RIGHT MAIN LANDING GEAR DOOR REAR HINGE BRACKETS CORRODED IN THE AREAS DESCRIBED IN SB 32-A119 (AD/BAE146	/035).					2	H	7	4 	4F	4	F	RT	A49EU   	E6NE				 
2000011500380	20000115	00380		2000	1	15	AU991095         	4	19990808	G	2340		PA SYSTEM       			BOEING	747   	747SP38     		NM  										CABIN	FAULTY          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 										(AUS) CABIN PUBLIC ADDRESS SYSTEM FAULTY.  INVESTIGATION FOUND THAT THE WIRING WAS INCORRECTLY CONFIGURED.						2	L	7	4 	4F			RT	A20WE   					 
2000011500381	20000115	00381	CE  	2000	1	15	AU991096         	1	19991004	G	2710	0510105362	CONTROL CABLE   			CESSNA	172   	172R        	2072401	CE  						MCAULY	1C235	1C235LFA    	GL  	AILERON	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) RIGHT AILERON CABLE WORN DUE TO CONTACT WITH THE PHENOLIC RUBBING BLOCK LOCATED OUTBOARD OF THE RIGHT FLAP ACTUATO	R.					1	H	7	1 	3O			NT	3A12    		5	N	P12EA	 
2000011500382	20000115	00382	SO  	2000	1	15	AU991097         	2	19991005	G	8520	6525402	CRANKCASE       			BEECH 	33    	F33A        	1151425	CE  	CONT  	O520  	IO520B      	17032	SO  	MCAULY	2A36C	2A36C23     	GL  	ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			1523 				578463			(AUS) RIGHT CRANKCASE HALF CRACKED FROM THE ALTERNATOR MOUNT FLANGE TOWARDS NR 5 CYLINDER.						1	L	7	1 	3O	3	O		3A15    	E5CE	5	C	P880	 
2000011500383	20000115	00383	SO  	2000	1	15	AU991098         	2	19990929	G	8520		CRANKCASE       								CONT  	O520  	IO520M      	17032	SO  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 							277540R			(AUS) LEFT CRANKCASE HALF CRACKED IN THE AREA OF NR 2 AND NR 3 MAIN BEARING SADDLES.											3	O			E5CE				 
2000011500384	20000115	00384	CE  	2000	1	15	AU991099         	1	19990226	G	2731	MS24665134	SPLIT PIN       			CESSNA	402   	402C        	207590R	CE  	CONT  	O520  	TSIO520VB   	17040	SO  	MCAULY	3AF32C	3AF32C*     	GL  	ELEVATOR TAB	FAILED          	W				O				OTHER                   				F			FLT CONT AFFECTED         			DE	DESCENT        	1			AU	S 										(AUS) ELEVATOR TRIM TAB DISCONNECTED FROM TRIM JACK.  INVESTIGATION FOUND THAT THE SPLIT PIN HAD SEPARATED ALLOWING THE 	NUT, WASHER AND BOLT TO VIBRATE FREE SEPARATING THE ACTUATING ROD FROM THE TRIM JACK.					1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22EA	 
2000011500385	20000115	00385	CE  	2000	1	15	AU991100         	1	19991013	G	3222	04425061	TORQUE LINK     			CESSNA	150   	150G        	2071816	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A101	1A101DCM    	GL  	NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 										(AUS) NOSE LANDING GEAR UPPER TORQUE LINK CRACKED IN THREE PLACES IN THE LOWER WEB AREA.  CRACK LENGTHS APPROXIMATELY 6.	35MM (0.25 INCH).					1	H	7	1 	3O	3	O		3A19    	E252	5	N	P918	 
2000011500386	20000115	00386	NE  	2000	1	15	AU991101         	3	19990903	G	6111	7823011	BEARING         	HAMSTD      	7827014     	DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	PROPELLER BLADE	SPALLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 					880811			88811		(AUS) PROPELLER NR 1 BLADE RETAINING BEARING RACE BADLY SPALLED.  FURTHER INVESTIGATION FOUND THE RACE WAS ALSO CRACKED.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
2000011500387	20000115	00387	NM  	2000	1	15	AU991102         	1	19991008	G	3234	57420SA	SELECTOR VALVE  			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	MLG	FAULTY          	W				K				NONE                    				O			OTHER                     			LD	LANDING        	1			AU	S 					458					(AUS) LANDING GEAR SELECTOR VALVE FAULTY.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
2000011500388	20000115	00388	GL  	2000	1	15	AU991103         	1	19991013	G	2750		SWITCH          			PAC   	CT4   	CT4A        	05623UC	GL  	CONT  	O360  	IO360HB     	17025	SO  	HARTZL	HCC2Y	BHCC2YF1    	GL  	TE FLAP	FAULTY          	W				O				OTHER                   				F			FLT CONT AFFECTED         			LD	LANDING        	1			AU	S 										(AUS) FLAP MICROSWITCH SUSPECT FAULTY.						1	Q	7	1 	3I	3	O	RT	A9PC    	E1CE	5	C	P920	 
2000011500389	20000115	00389	EU  	2000	1	15	AU991104         	1	19990201	G	6400	360A33109000	FAIRING         			AEROSP	SA365 	SA365C      	8680667	EU  	TMECA 	ARRIEL	ARRIEL1A    	60030	NE  					TAIL ROTOR	CRACKED         	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AU	S 					M180					(AUS) FENESTRON ROTATING FAIRING CRACKED.						1	G	7	2 	3U	3	U		H10EU   	E19EU				 
2000011500390	20000115	00390	CE  	2000	1	15	AU991105         	1	19991005	G	3233	R12ZZ	BEARING         			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	NLG	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AU	S 			17633							(AUS) NOSE LANDING GEAR ACTUATOR DRIVE SHAFT SUPPORT BEARING DISINTEGRATED.						1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15EA	 
1999082000447	19990820	00447	SW  	1999	8	20	BAQA062725       	1	19990711	G	6230	222040002115	MAST            			BELL  	230   	230         	1182149	SW  										MAST MOMENT	GOUGED          	H			BAQA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	03	231UM	1332 				23012				MAST HAD 1 INCH LONG GOUGE ON MATING AREA UNDER SPLIT CONES.  GOUGE DEPTH STARTED AT .001 INCH.						1	G	7	2 	3U			NC	H9SW    					 
1999102900771	19991029	00771	EU  	1999	10	29	BTVR101299       	1	19991012	G	2711	258CW4939A	TRIM ACTUATOR   			BRAERO	DH125 	BAE125800A  	1500285	EU  										LT AILERON	SEIZED          	B			BTVR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			GL	23	611BA	2745 			CHHG188	258178				DURING A ROUTINE SCHEDULED INSPECTION OF THE AILERON TRIM SYSTEM, THE AILERON TRIM SYSTEM FROZE BEFORE FINISHING ONE FUL	L CYCLE.  SUBSEQUENT INVESTIGATION REVEALED THE AILERON TRIM JACK WAS COMPLETELY SEIZED.  THE UNIT IS REGULARLY LUBED AN	D INSPECTED.  IT IS UNKNOWN WHAT CAUSED THE PROBLEM AT THIS TIME, BUT TKS FLUID IS SUSPECTED.  (X)				2	L	7	2 	4F			RT	A3EU    					 
2001032800223	20010328	00223	EU  	2001	3	28	CA000110003      	1	19991012	G	6420	369D25418	BEARING         		369D25400   	HUGHES	369   	369FF       	       	EU  										GEARBOX	MAKING METAL    	W				A	 	 	 	UNSCHED LANDING         				J	 	 	WARNING INDICATION        			CR	CRUISE         	1			CA			1502 			1076					(CAN) INPUT ALIGNMENT BEARING MAKING METAL (CHIP LITE IN CRUISE. GEARBOX STRIPPEDTO DETERMINE CAUSE OF METAL GENERATION.						1	G	7	1 	3U			 	H3WE    					 
2001032800334	20010328	00334	NE  	2001	3	28	CA000110024      	1	19991101	G	6320	S613723050001	GEAR            			SKRSKY	S61   	S61N        	8142104	NE  	GE    	CT58  	CT581401    	30011	NE  					MAIN ROTOR	FAILED          	W				K	 	 	 	NONE                    				W	 	 	INADEQUATE Q C            			IN	INSP/MAINT     	1			CA											(CAN) HELICAL GEARS SENT OUT FOR NICKEL-SULFAMATE REPAIR OF PILOT BORES I.A.W. SIKORSKY S61 OVERHAUL MANUAL. HOWEVER, IT	 WAS LATER DETERMINED THAT THE REQUIRED MPI CRACK CHECKS AFTER GRINDING WERE NOT CARRIED OUT BY THE COMPANY THAT DID THE	 REPAIR PROCESS.				2	G	7	2 	4U	4	U	 	1H15    	1E3				 
2001032800335	20010328	00335	SW  	2001	3	28	CA000110025      	1	19991215	G	3213	369H600151	STRUT           			HUGHES	500N  	500N        	3027374	SW  										LT MLG	CRACKED         	W				O	 	 	 	OTHER                   				J	 	 	WARNING INDICATION        			CL	CLIMB          	1			CA			5019 								(CAN) LEFT REAR LANDING GEAR STRUT STRUCTURALLY FAILED. IT APPEARS THAT THE CRACK BEGAN AT RIVET HOLE FOR STRUT FAIRING 	ATTACHMENT BRACKET.					1	G	7	1 	3U			NC	H3WE    					 
2001032800340	20010328	00340	SW  	2001	3	28	CA000110033      	1	19991222	G	2435	230321823	STATOR          			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					STARTER GEN	FAILED          	W				K		 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA				96   							(CAN) STARTER GENERATOR SENT TO OVERHAUL AFTER ONLY 96 HOURS. STATOR COWLING OUTLET SCREEN FOUND TO BE CLOGGED WITH SOME	 FOREIGN INSULATION WHICH HAD OCCURRED DURING THE PREVIOUS REWIND. STATOR IS NOW QUARANTINED UNTIL FURTHER INVESTIGATION	 IS COMPLETED AS TO WHY PROPER CHECKS WERE NOT CARRIED OUT PREVIOUSLY THAT WOULD HAVE PRVENTED THIS FROM HAPPENING. SENT	 TO AARPE ON 8 FEB 00FOR INVESTIAGATION.			1	G	7	1 	3U	3	U	 	H2SW    	E4CE				 
2001032800345	20010328	00345	WP  	2001	3	28	CA000110040      	2	19991228	G	7210	358348	BEARING         								GARRTT	TPE331	TPE33110UA  	01514	WP  					GEARBOX	MAKING METAL    	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			1491 								(CAN) M50 MATERIAL FOUND IN OIL. BEARING P/N 358348 IN RGB FOUND FRETTING AND SPALLED.											4	T			E4WE				 
2001032800347	20010328	00347	EA  	2001	3	28	CA000110043      	1	19990602	G	5320	75310263101	BRACKET         			DHAV  	DHC7  	DHC7*       	       	EA  	PWA   	120   	PW120A      	 	NE  					HAND PUMP	CRACKED         	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			20467								(CAN) HAND PUMP BRACKET FOUND CORRODED ON INSPECTION. CRACK WAS DETECTED AFTER CORROSSION WAS BLENDED AWAY. PART EXPERIE	NCED APPROX 5 INCH CRACK TRAVERSING APPROX 6 RIVETS. FINDINGS SHOW EVIDENCE OF EXFOLIATIONAND STRESS CORROSION.					2	H	7	4 	4T	4	T	RT	A20EA   	E20NE				 
2001032800348	20010328	00348	CE  	2001	3	28	CA000110044      	1	19991219	G	5320	030A388245	BRACKET         			MTSBSI	MU2   	MU2B36A     	5780413	CE  	GARRTT	TPE331	TPE3315     	01514	WP  					MLG	CRACKED         	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) DURING 100 HOUR INSPECTION THE SUBJECT LANDING GEAR FORWARD DOOR RETRACTION MECHANISM SUPPORT BRACKET WAS FOUND CR	ACKED AT THE OUTER MOST AFT HOLE.					1	H	7	2 	3T	4	T	 	A10SW   	E4WE				 
2000081000038	20000810	00038	SO  	2000	8	10	CA000110051      	1	19991229	G	3242	16775003	CONTROL CABLE   			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					PARKING BRAKE	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								RL443161A			(CAN) NO TEXT						1	L	7	2 	3O	3	O	 	A20SO   	E14EA				 
2000081000039	20000810	00039	CE  	2000	8	10	CA000110058      	1	19991231	G	2810	1003810051	FUEL CAP        			BEECH 	99    	99          	1154002	CE  	PWA   	PT6   	PT6A28      	 	EA  					SEAL	LEAKING         	W				O	 	 	 	OTHER                   				O	 	 	OTHER                     			CL	CLIMB          	1			CA								PCE50747			(CAN) NO TEXT						1	L	7	2 	3T	4	T	 	A14CE   	E4EA				 
2000020500964	20000205	00964	SO  	2000	2	5	CA000118045      	1	19991207	G	5751	2102001	SUPPORT         			PIPER 	PA28  	PA28140     	7102802	SO  	LYC   	O320  	O320E3D     	41508	EA  	SNSNCH	74D	74DM        	EA  	AILERON	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4434 					L4086727A	A46908		(CAN) DURING AN ANNUAL INSPECTION, A 1 INCH CRACK WAS DETECTED IN THE FORWARD RADIUS.						1	L	7	1 	3O	3	O		2A13    	E274	5	N	P88614	 
2000020500967	20000205	00967	SO  	2000	2	5	CA000118054      	1	19991231	G	2140	WZ1V013	BRUSHES         	JANITROL    	B2030       	PIPER 	PA30  	PA30        	7103002	SO  	LYC   	O320  	IO320B1A    	41508	EA  	HARTZL	HCE2Y	HCE2YL2     	GL  	BLOWER MOTOR	FAILED          	W				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			CL	CLIMB          	1			CA								L175755A	BG285		(CAN) DURING CLIMB, SMOKE AND SPARKS WERE NOTICED COMING FROM THE VENTILATION DUCTS AND FROM THE NOSE ACCESS PANEL.  FOU	ND VENT BLOWER MOTOR AND RELATED WIRING BURNT, INSPECTION OF MOTOR FOUND BRUSHES COMPLETELY WORN OUT ALLOWING TENSION SP	RINGS TO CONTACT COMMUTATOR.  BLOWER MOTOR AND RELATED WIRING REPLACED.				1	L	7	2 	3O	3	O		A1EA    	1E12	5	C	P9EA	 
2000020500972	20000205	00972	NE  	2000	2	5	CA000118060      	2	19991206	G	7200	3036212	LP DISK         			AEROSP	ATR42 	ATR42*      	8680900	EU  	PWA   	120   	PW120       		NE  					OUTER RIM	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								120727			(CAN) COMPRESSOR ROTOR FOUND CRACKED ON OUTBOARD EDGE.  P&W SB 21555.						2	H	7	2 	4T	4	T	RT	A53EU   	E20NE				 
2001032800299	20010328	00299	SO  	2001	3	28	CA000128043      	2	19991218	G	7510	628122	ARM             			CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A102	1A102OCM    	GL  	CARB HEAT BOX	DAMAGED         	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) CARB HEAT BOX ACTUATOR ARM HAD BROKEN OFF AT RIVETS THAT SECURE SPRING STEEL STRIP TO ARM.						1	H	7	1 	3O	3	O	 	3A19    	E252	5	N	P918	 
2001032800300	20010328	00300	EA  	2001	3	28	CA000128044      	1	19991222	G	3210	TBC6U114033	BLOCK           			DHAV  	DHC6  	DHC6        	2802606	EA  										MLG	MISMANUFACTURED 	W				K	 	 	 	NONE                    				W	 	 	INADEQUATE Q C            			IN	INSP/MAINT     	1			CA											(CAN) ONE OF OUR NEWLY MNUFACTURED COMPRESSION BLOCKS SAGGED WHEN INSTALLED DURING REGULAR MAINTENENACE. BLOCK REMOVED A	ND NEW ONES INSTALLED WITHOUT PROBLEM. BLOCKS SENT FOR TESTING & CHEMICAL ANALYSIS. HAVE ISOLATED BLOCKS TO WHAT BATCH A	ND POUR.				1	H	7	2 	3T			RT	A9EA    					 
2001032900010	20010329	00010	NE  	2001	3	29	CA000201013      	2	19991223	G	7321	311717503	FUEL CONTROL    			DHAV  	DHC8  	DHC8311     	1386006	EA  	PWA   	PW120 	PW123       	 	NE  					NR 1 ENGINE	FAILED          	W				L	E	 	 	ABORTED APPROACH        	ENGINE SHUTDOWN         			E	 	 	VIBRATION/BUFFET          			AP	APPROACH       	1			CA											(CAN) ENGINE WENT TO AN UNCOMMANDED MAX POWER SETTING. MFC REPLACED.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
2000081000040	20000810	00040	CE  	2000	8	10	CA000209025      	1	19991123	G	2510	AN24	BOLT            			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  	MCAULY	1A103	1A103TCM    	GL  	CREW SEATS	CRACKED         	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			47430					L2324115	RBF091		(CAN) SEAT BACK PIVOT BOLTS ARE REMOVED FOR INSPECTION AND CRACKS ARE FOUND AT THE FILLET BETWEEN THE BOLT HEAD AND SHAN	K.  THESE BOLTS ARE FOUND ON THE VERTICALLY ADJUSTABLE SEATS FITTED TO 150 AND 152 AIRCRAFT.					1	H	7	1 	3O	3	O	NT	3A19    	E223	5	N	P50GL	 
2000071800178	20000718	00178	NE  	2000	7	18	CA000404013      	2	19991203	G	7532	9560137030	BLEED VALVE     			SNIAS 	350   	AS350BA     	8680817	EU  	TMECA 	ARRIEL	ARRIEL1B    	6OO30	NE  					INTERNAL	FAILED          	W				A	 	 	 	UNSCHED LANDING         				O	 	 	OTHER                     			HO	HOVERING       	1			CA			40441	2454 		1434		879			(CAN) BLEED VALVE INTERMITANT OPS.                                                                                      	                                                                                                                        	                                                                                                                        	                                                                                                                        	                                                                                                                        	                                                                                                                       	1	G	7	1 	3U	3	U	NC	H9EU    	E19EU				 
2000071800182	20000718	00182	EA  	2000	7	18	CA000404029      	2	19991124	G	7322	HA610301	CARBURETOR      			HUGHES	269   	269C1       	8059504	SW  	LYC   	O360  	HO360C1A    	41514	EA  					INTERNAL	LEAKING         	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			1500 			75048908		L3486936A			CARBURETOR  LEAKING INTERNALLY.						1	G	7	1 	3O	3	O	O	4H12    	E286				 
2000083000139	20000830	00139	SO  	2000	8	30	CA000404044      	1	19991220	G	3297	AMP3205590	WIRE            			PIPER 	PA34  	PA34200     	7103405	SO  	LYC   	O360  	IO360C1E6   	41514	EA  					DWN LOCK SW	CORRODED        	W				O				OTHER                   				J			WARNING INDICATION        			LD	LANDING        	1			CA								L902551A			(CAN) WITH GEAR SELECTED DOWN, RIGHT MAIN LANDING GEAR FAILED TO INDICATE DOWN AND LOCKED.  INSPECTION REVEALED A CORROD	ED AND BROKEN WIRE AT A SPLICE APPROXIMATELY 1 FOOT FROM THE RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH.  WIRING REPAIRED B	Y REPLACING SUBJECT SPLICE AND OTHER SPLICES IN THAT LOCATION WITH RAYCHEM ENVIRONMENTAL SPLICES (P/N D436).				1	L	7	2 	3O	3	O	 	A7SO    	1E10				 
2000083000162	20000830	00162	SO  	2000	8	30	CA000427014      	1	19990821	G	2497		WIRE            			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					INSTRUMENT PANEL	BROKEN          	W				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			CL	CLIMB          	1			CA								L377361A			(CAN) SMOKE OBSERVED COMING FROM BEHIND THE INSTRUMENT PANEL.  AIRCRAFT RETURNED TO AIRPORT.  A BROKEN WIRE WAS FOUND TO	 BE THE PROBLEM.					1	L	7	2 	3O	3	O	 	A20SO   	E14EA				 
2001030900026	20010309	00026	SO  	2001	3	9	CA000501010      	1	19990602	G	2750	12020001	MOTOR           			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	LTIO540J2BD 	41533	EA  					TE FLAPS	FAILED          	W				O				OTHER                   				F			FLT CONT AFFECTED         			AP	APPROACH       	1			CA								L206368A			(CAN) FLAPS STUCK DOWN ON APPROACH.  C/B WOULD NOT RESET.  FLAP MOTOR REPLACED.  SYSTEM SERVICEABLE.						1	L	7	2 	3O	3	O	 	A20SO   	E14EA				 
2001030900027	20010309	00027	SO  	2001	3	9	CA000501011      	1	19991002	G	2823	757257	O-RING          			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	LTIO540J2BD 	41533	EA  					SHUTOFF VALVE	NICKED          	W				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			CA											(CAN) BOTH L/H & R/H FIREWALL SHUTOFF VALVES WOULD NOT COMPLETELY SHUTOFF FUEL TO ENGINE.  ON TEARDOWN OF VALVE O-RINGS 	WERE FOUND TO BE NICKED.THE O-RINGS ARE NICKED EVERYTIME THE VALVE IS OPERATED.  THE VALVES ARE OPERATED AS PART OF RUN-	UP CHECKS.THE DESIGN OF THE VALVES IS SUCH THAT AS O-RING LUBRICATION IS WASHED AWAY BY REGULAR FLOW OF FUEL THE RING IS	 NICKED.			1	L	7	2 	3O	3	O	 	A20SO   	E14EA				 
2000072600244	20000726	00244	EU  	2000	7	26	CA000518006      	1	19991028	G	6410		BLADE           			SNIAS 	350   	AS350B      	8680801	EU  	TMECA 	ARRIEL	ARRIEL1B    	6OO30	NE  					TAIL ROTOR	DAMAGED         	W				O	 	 	 	OTHER                   				O	 	 	OTHER                     			CR	CRUISE         	1			CA				92900				451			(CAN) SLING MIRROR CAME LOOSE AND WENT THROUGH THE TAIL ROTOR ASSEMBLY.   (THE GLASS).						1	G	7	1 	3U	3	U	 	H9EU    	E19EU				 
2000062800212	20000628	00212	SW  	2000	6	28	CA000518008      	1	19991017	G	6510	206040328101	SPLINE ADAPTER  		206040328101	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					T/R DRIVESHAFT	CHAFED          	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			18600					CAE822258			(CAN) SPLINED ADAPTER AT THE AFT END OF SHORT T/R DRIVE SHAFT RUBBING ON ENGINE OIL TANK COOLER COWLING.  CHAFING THROUG	H THE COWLING HONEYCOMB.  COWLING WAS REPAIRED TO ALLOW CLEARANCE FOR THE COUPLING ADAPTER.					1	G	7	1 	3U	3	U	 	H2SW    	E4CE				 
2001031200427	20010312	00427	SW  	2001	3	12	CA000519017      	1	19991217	G	3233		O-RING          	AEROCD      	500S        	GULSTM	500   	500S        	0141107	SW  	LYC   	O540  	IO540E1B5   	41532	EA  					STRUT	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				80590		3118		RL31348			(CAN) EXCESSIVE WEAR OF O-RING INSIDE CYLINDER ASSEMBLY CAUSED BY CORRODED CHROME ACTUATOR.						1	H	7	2 	3O	3	O	 	6A1     	1E4				 
2000092100010	20000921	00010	SW  	2000	9	21	CA000706032      	1	19991223	G	2810		FUEL CELL       	LYC         		MOONEY	M20   	M20D        	5870210	SW  	LYC   	O360  	O360A1D     	41514	EA  					LT FUEL CELL	LEAKING         	W				O	 	 	 	OTHER                   				K	 	 	FLUID LOSS                			IN	INSP/MAINT     	1			CA								L551636			(CAN) LEFT FUEL CELL WAS FOUND LEAKING ON NOVEMBER 1999.  LEAK WAS REPAIRED ON NOV 28, 1999.  LEAK WAS THEN NOTICED AGAI	N SHORTLY THEREAFTER.  LEAK APPEARED TO COME FROM FORWARD WALL OF CELL.  LOWERED FUEL LEVEL UNTIL FUEL SHOWED DRYING IN 	AREA.  AT THIS LEVEL AT THE FORWARD TOP EDGE OF CELL THE SEALANT WAS FOUND LOOSE (EASY TO PEEL OFF).  AREA WAS PROBABLY 	NOT CLEANED BEFORE APPLICATION.  REMOVED SEALANT ON WHOLE UPPER EDGE OF FORWARD WALL AND RESEALED.  NOW DOES NOT LEAK.  	(X)		1	L	7	1 	3O	3	O	 	2A3     	E286				 
2001032700166	20010327	00166	EA  	2001	3	27	CA000824016      	2	19990908	G	8550		OIL FILTER      			MOONEY	M20   	M20         	5870202	SW  	LYC   	O360  	IO360A1A    	41514	EA  	MCAULY	2D34C	B2D34C53    	GL  	ENGINE	MISINSTALLED    	W				K	 	 	 	NONE                    				W	 	 	INADEQUATE Q C            			IN	INSP/MAINT     	1			CA											(CAN)  FOUND OIL FILTER HOUSING INSTALLED ON AIRCRAFT, 180 OUT. CAUSED AIRCRAFT ENGINEOIL TO OVER HEAT. THIS IS THE SECO	ND TIMEI I HAVE FOUND THIS PROBLEM. THERMO VALVE DOES NOT LINE UP WITH OIL COOLER PASSAGE. NO COOLING FOR OIL.					1	L	7	1 	3O	3	O	 	2A3     	1E10	5	C	P7AE	 
2000113000022	20001130	00022	CE  	2000	11	30	CA000927002      	1	19991229	G	3230	504501033	TORQUE TUBE     			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520MB     	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	TORQUE TUBE	BROKEN          	W				O	 	 	 	OTHER                   				J	 	 	WARNING INDICATION        			AP	APPROACH       	1			CA											(CAN) PILOT COULD NOT GET A GREEN LIGHT INDICATION ON THE LEFT MAIN GEAR.  PILOT MADE A SUCCESSFUL LANDING WITHOUT ANY D	AMAGE TO THE AIRCRAFT.   AIRCRAFT WAS PUT ON JACKS IN THE HANGAR AND TORQUE TUBE WAS FOUND TO BE BROKEN.  NEW TORQUE TUB	E WAS INSTALLED AND GEAR SWING WAS COMPLETED.  COULD NOT DETERMINE WHY THE PART HAD BROKEN AS EVERYTHING WAS WORKING COR	RECTLY.  (X)			1	L	7	2 	3O	3	O	 	3A10    	E5CE	5	C	P22EA	 
2000112900329	20001129	00329	EA  	2000	11	29	CA001107014      	2	19990430	G	8530	05SR21228	CYLINDER        	LYC         		BELL  	47    	47G4A       	1181031	SW  	LYC   	O540  	VO540B1B3   	41532	EA  					ENGINE	FAILED          	W				O	 	 	 	OTHER                   				O	 	 	OTHER                     			NR	NOT REPORTED   	1			CA			825  			L225943					(CAN) CYLINDER HAD LOW COMPRESSION.  (X)						1	G	7	1 	3O	3	O	 	2H3     	E304				 
2001040400035	20010404	00035	SO  	2001	4	4	CA010223013      	1	19991005	G	7721	05K21262	CYLINDER        			PIPER 	PA46  	PA46350P    	       	SO  	LYC   	O540  	TIO540AE2A  	41532	EA  					ENGINE	BROKEN          	W				O	 	 	 	OTHER                   				J	 	 	WARNING INDICATION        			CR	CRUISE         	1			CA			326  								(CAN) OPERATOR EXPERIENCED HIGH ON CONSUMPTION. NR 5 CYLINDER REMOVED AND FOUND BROKEN ON CONTROL RING. CYLINDER/PISTON 	AND RING ASSEMBLY REPLACED.					1	L	7	1 	3O	3	O	RT	A25SO   	E14EA				 
2001100200033	20011002	00033	SW  	2001	10	2	CA010921003      	1	19990926	G	2910	700607000230	HOSE            			BELL  	214   	214B        	1182100	SW  	LYC   	T55   	T5508D      	41555	NE  					HYD SYSTEM	DETERIORATED    	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			12261	12261							(CAN) OIL SOAKED HOSE CLAMP CAUSED RUBBER TO DETERIORATE ON THE HOSE CLAMP WHICH CAUSED THE STEEL BRADING AROUND THE HOS	E TO ERODE, THUS CAUSING THE HOSE TO LEAK.					2	G	7	1 	4U	4	U	 	H6SW    	E4NE				 
2002011500032	20020115	00032	EA  	2002	1	15	CA011005006      	1	19991204	G	3213	17064104	STRUT           			CNDAIR	CL600 	CL6002B19   	1900309	EA  	GE    	CF34  	CF343B1     	 	NE  					RT MLG	FAILED          	W				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			CA											(CAN) INCIDENT IN TIMISUARA, ROMENIA, THE 30 NOV 99 AT 14:20 (UTC). UPON TOUCHDOWN, THE RIGHT WING DROPPED TO THE GROUND	 WHILE THE CAPTAIN USED LEFT BRAKING TO KEEP THE AIRCRAFT ON THE RUNWAY CENTERLINE. INITIAL REPORT REVEALED THAT THE RT 	GEAR BROKE NEAR THE TOP OF THE MLG CYLINDER. NO INJURIES TO THE PASSENGERS AND CREWS.				2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
2002050300028	20020503	00028	GL  	2002	5	3	CA020405004      	2	19990317	G	7230	2305742	CASE            	ALLSN       	6890550     	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						37655					(CAN) LOSS OF POWER REPORTED DUE TO WORN VANES AND LIFTED PLASTIC.						1	G	7	1 	3U	3	U	 	H2SW    	E4CE				 
2003050700114	20030507	00114	EA  	2003	5	7	CA030417004      	1	19991004	G	5740		BUSHING         			CNDAIR	CL600 	CL6002B19   	1900309	EA  	GE    	CF34  	CF343A1     	30015	NE  					WING ATTACHMENT	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.						2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999061000013	19990610	00013	EU  	1999	6	10	CA961007014      	1	19990609	G	3250	CA248003	VALVE           	CASA        		CASA  	C212  	C212CC      	2410204	EU  										NLG STEERING	LEAKING         	W				O				OTHER                   				K			FLUID LOSS                			TX	TAXI/GRND HDL  	1			CA			171  								(CAN) NOSE WHEEL STEERING OBSERVED TO BE OPERATING 45 DEGREES RIGHT AND 30 DEGREES LEFT.  WHERE PILOT VALVE GOES THROUGH	 THE PRE-SELECTOR VALVE CASING THERE WAS GREASE COMING OUT.  VALVE REPLACED.					2	H	7	2 	4T				A43EU   					 
1999021200274	19990212	00274	GL  	1999	2	12	CA990115002      	2	19990110	G	7230	6890550	COMPRESSOR      								ALLSN 	250C  	250C20B     	03013	GL  					NR 1 ENGINE	MALFUNCTIONED   	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4353 	860  				CAE835808			(CAN) PILOT REPORTED THERE WAS NO NOTICEABLE RISE IN TEMPERATURE ON NR 1 ENGINE DURING ANTI-ICE SYSTEM ACTIVATION.  INVE	STIGATION FOUND LINE (P/N 6876333) HAD FAILED.  THIS IS THE SECOND FAILURE OF THAT LINE IN 55 HOURS OF OPERATION.  THE F	AULT WAS FOUND TO BE EXCESSIVE VIBRATION OF THE COMPRESSOR.  THE COMPRESSOR WAS REPLACED AND THE AIRCRAFT RETURNED TO SE	RVICE.   PART TC:  5,063.								3	U			E4CE				 
1999021200282	19990212	00282	GL  	1999	2	12	CA990115010      	3	19990104	G	6111	T10282	BLADE           													HARTZL	HCB3T	HCB3TN3     	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			10260	1526 					BU16865		(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.  IT WAS FOUND THE PROPELLER BLADES HAD NOT BEEN ANODIZED AT THE LAST 	OVERHAUL.															6	C	P15EA	 
1999021200283	19990212	00283	EA  	1999	2	12	CA990115015      	2	19990104	G	8520	SL15628	SEAL            			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2B   	41532	EA  					CRANKSHAFT	LEAKING         	W				A				UNSCHED LANDING         				K			FLUID LOSS                			CR	CRUISE         	1			CA				1748 				L286061A			(CAN) OIL LEAK REPORTED BY PILOT.  INSPECTION FOUND THE FRONT CRANKSHAFT SEAL LEAKING.  IT HAD SLIPPED OUT APPROXIMATELY	 .0625 INCH AND WAS LOOSE.  THE POSSIBLE CAUSE WAS A COLD START AND THE ENGINE RPM TOO HIGH DURING ENGINE WARM UP CAUSIN	G HIGH OIL PRESSURE.  NEW SEAL INSTALLED.				1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999052800013	19990528	00013	SO  	1999	5	28	CA990115016      	1	19990105	G	3710	442CW6	DRIVE COUPLE    			PIPER 	PA31  	PA31350     	7103110	SO  										VACUUM PUMP	SHEARED         	W				E				ENGINE SHUTDOWN         				J			WARNING INDICATION        			CR	CRUISE         	1			CA				669  		9J1378					(CAN) RIGHT VACUUM INOP LIGHT ON IN CRUISE.  AT ENGINE SHUTDOWN CONFIRMED NO VACCUUM AIR PRESSURE FROM RIGHT SIDE.  AVER	AGE RUNNING TIME OF THIS PUMP 445 TO 670 HOURS.  THIS IS 3RD PUMP IN TWO YEARS.					1	L	7	2 	3O				A20SO   					 
1999021200289	19990212	00289	SO  	1999	2	12	CA990115029      	2	19990107	G	8530	SA10200	VALVE           			CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A102	1A102OCM    	GL  	CYLINDER	STICKING        	W				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			CA			952  					667437A	615921		(CAN) INTAKE VALVE STICKING OPEN CAUSING LOSS OF POWER.						1	H	7	1 	3O	3	O		3A19    	E252	5	N	P918	 
1999021200292	19990212	00292	NE  	1999	2	12	CA990115033      	2	19990105	G	7240	311237901	COMBUSTION LINER			AEROSP	ATR72 	ATR72       		EU  	PWA   	PW120 	PW127       		NE  					ENGINE	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			10619	3927 				127018			(CAN) THE ENGINE WAS REMOVED FROM WING AFTER THE OPERATOR FOUND DAMAGE TO THE OUTER COMBUSTION LINER AND THE HP SHROUD S	EGMENTS.  DISASSEMBLY OF THE ENGINE FOUND THE OUTER COMBUSTION LINER HAD SEVERAL SECTIONS OF THE CENTER COOLING RING MIS	SING AND CLEAR EVIDENCE THAT THE BALANCE RING WAS POORLY ATTACHED TO THE BASIC OUTER LINER.  THIS LINER WAS INSTALLED NE	W AT THE LAST OVERHAUL.  UNFORTUNATELY, THE DAMAGE TO THE LINER WAS SO SEVERE IT WAS NO LONGER REPAIRABLE.  PART TC:  11	,748.		2	H	7	2 	4T	4	T	RT		E20NE				 
1999030500181	19990305	00181	NE  	1999	3	5	CA990119004      	1	19990111	G	6320	S613522017003	GEAR            		S61252060004	SKRSKY	S61   	S61N        	8142104	NE  										M/R GEARBOX	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				619  		A1401675994					(CAN) RING GEAR WAS REMOVED TO REPAIR A STUD IN THE LOWER HOUSING.  ON INSPECTION, A CRACK WAS FOUND IN THE LOWER FLANGE	 OF THE RING GEAR.  THE RING GEAR WAS REPLACED.					2	G	7	2 	4U				1H15    					 
1999021200294	19990212	00294	EA  	1999	2	12	CA990119005      	1	19990119	G	3040	P321B95B	TRANSFORMER     			FRCHLD	F27   	F27F        	3373008	EA  	RROYCE	DART  	DART5297E   	54507	EU  					COCKPIT	FAILED          	W				H	D			DEACTIVATE SYST/CIRCUITS	RETURN TO BLOCK         			B			SMOKE/FUMES/ODORS/SPARKS  			TX	TAXI/GRND HDL  	1			CA				290  				13603			(CAN) RESISTANCE ON WINDSHIELD HAD INCREASED.  NEW WINDOW ORDERED.  NEXT APPLICATION OF WINDSHIELD HEAT, THE TRANSFORMER	 OVERHEATED AND FILLED THE COCKPIT WITH SMOKE.  REPLACED.					2	H	7	2 	4T	4	T		7A1     	E297				 
1999052800015	19990528	00015	CE  	1999	5	28	CA990119006      	1	19990101	G	2731	50524047	GUARD           		1015248771  	BEECH 	200   	B200C       	1152924	CE  	PWA   	PT6   	PT6A42      	52043	NE  					ELEVATOR CONTROL	MISSING         	W				O				OTHER                   				W	F		INADEQUATE Q C            	FLT CONT AFFECTED         		CR	CRUISE         	1			CA								PCE93224			(CAN) AIRCRAFT IN-FLIGHT WHEN ELEVATOR TRIM JAMMED.  NO DIFFICULTIES ENCOUNTERED.  INVESTIGATION REVEALED THAT THE ELEVA	TOR TRIM CABLE HAD JUMPED OFF THE DRUM OF THE COCKPIT CONTROL QUADRANT.  ICE MAY HAVE BEEN A FACTOR CAUSING TRIM TO BE S	TIFF.  WHEN OPERATED THIS WAY, ONE CABLE TIGHTENS WHILE THE OTHER LOOSENS.  CABLE GUARD NOT INSTALLED PER IPC.				1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999021900422	19990219	00422	EA  	1999	2	19	CA990119007      	1	19990107	G	3231	555405	VALVE           			CNDAIR	CL600 	CL6001A11   	1900302	EA  										NLG DOOR	FAILED          	W				H				DEACTIVATE SYST/CIRCUITS				O			OTHER                     			AP	APPROACH       	1			CA						059A					(CAN) NOSE GEAR DOORS FAILED TO OPEN WHEN GEAR SELECTED DOWN.   PROBLEM INTERMITTENT AFTER COLD SOAK AT ALTITUDE.						2	L	7	2 	4F			RT	A21EA   					 
1999021200295	19990212	00295	SW  	1999	2	12	CA990119008      	1	19990108	G	2750	2781032135	LINE            			SWRNGN	SA227 	SA227AC     	8780603	SW  										TE FLAP	CRACKED         	W				A				UNSCHED LANDING         				K			FLUID LOSS                			CL	CLIMB          	1			CA											(CAN) PILOT REPORTED BOTH HYDRAULIC PRESSURE ANNUNCIATORS CAME ON AND HYDRAULIC PRESSURE INDICATOR HAD DROPPED TO 100 PS	I SHORTLY AFTER TAKEOFF AND AFTER GEAR AND FLAPS WERE SELECTED UP.  INSPECTION FOUND THE FLAP UP LINE CRACKED NEAR THE H	YDRAULIC POWER PACK.  CRACK RUNNING PARALLEL WITH TUBE, ABOUT .75 INCH LONG.				2	L	7	2 	4T			RT	A8SW    					 
1999052800016	19990528	00016		1999	5	28	CA990119010      	4	19990104	G	2562	MN1300	BATTERY         	AMERIKING   	AK450       	CHRIS 	HUSKY 	A1          	221020X	NM  										ELT	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						354026					(CAN) AT RE-CERTIFICATION WHEN ELT OPENED THERE WERE TRACES OF ABRASION ON THE BATTERY JACKETS WHERE BATTERIES CONTACT E	ACH OTHER.  SOME OF THE 'D' CELLS WERE DAMAGED TO THE POINT THAT THE NEGATIVE OR 'CAN' WAS EXPOSED AND COULD HAVE TOUCHE	D THE ADJACENT CELL CAUSING A SHORT.  THE SUBMITTER INDICATES THE INSIDE DIMENSION OF THE BATTERY BOX ALLOWS THE BATTERI	ES TO RATTLE AROUND.			1	H	7	1 	3O			NC	A22NM   					 
1999052800017	19990528	00017	CE  	1999	5	28	CA990119012      	1	19990108	G	7120	04511201	MOUNT           			CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A102	1A102OCM    	GL  	ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			3000 					2047929AS0	G14848		(CAN) LEFT TUBE MEMBER AT THE LOWER NOSE GEAR STRUT ATTACH POINT FOUND CRACKED.  WHEN REPAIRING, THE TUBE WAS FOUND CORR	ODED.					1	H	7	1 	3O	3	O		3A19    	E252	5	N	P918	 
1999021200947	19990212	00947	EU  	1999	2	12	CA990119013      	1	19990112	G	2611	CG7PD1	SMOKE DETECTOR  			AIRBUS	300   	A300B4203   	3930306	EU  	GE    	CF6   	CF650C2     	30018	NE  					CARGO BAY	FAILED          	W				A				UNSCHED LANDING         				N			FALSE WARNING             			CR	CRUISE         	1			CA								455827			(CAN) SMOKE WARNING INDICATION FROM AFT CARGO COMPARTMENT ON OUTBOUND DEPARTURE.  CARGO HOLE AND SYSTEM CHECKED, SECURED	 IAW MEL.  SMOKE DETECTOR REPLACED.  AIRCRAFT RETURNED TO SERVICE.					2	L	7	2 	4F	4	F		A35EU   	E23EA				 
1999021200948	19990212	00948	GL  	1999	2	12	CA990119014      	3	19990111	G	6114	B3414	LINK PINS       			CESSNA	172   	172RG       	2072438	CE  	LYC   	O360  	O360F1A6    	41514	EA  	MCAULY	2D34C	B2D34C220   	GL  	PROPELLER	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4426 	1464 				L2930536A	860511		(CAN) PROPELLER RECEIVED FOR TBO OVERHAUL.  UPON DISMANTLE TOLERANCE INSPECTION, THE LINK PINS WERE FOUND WORN BELOW THE	 MANUFACTURER'S MINIMUM TOLERANCES.  THE LINK PINS WERE REPLACED.					1	H	7	1 	3O	3	O		3A17    	E286	5	C	P7EA	 
1999021200949	19990212	00949	GL  	1999	2	12	CA990119015      	3	19990111	G	6111	C5270	BEARING         			CESSNA	172   	172RG       	2072438	CE  	LYC   	O360  	O360F1A6    	41514	EA  	MCAULY	2D34C	B2D34C220   	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4426 	1464 				L2930536A	860511		(CAN) PROPELLER RECEIVED FOR TBO OVERHAUL.  UPON DISMANTLE INSPECTION, THE BLADE THRUST BEARINGS WERE FOUND CORRODED.  T	HE BEARINGS WERE REPLACED WITH NEW BEARINGS.					1	H	7	1 	3O	3	O		3A17    	E286	5	C	P7EA	 
1999021200950	19990212	00950	EA  	1999	2	12	CA990119016      	2	19990104	G	8520		CRANKCASE       			BEECH 	76    	76          	1153005	CE  	LYC   	O360  	O360A1G     	41514	EA  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2431 					L2528236A			(CAN) ON A SCHEDULED ON CONDITION INSPECTION, A CRACK WAS FOUND AT THE NR 2 CYLINDER HOLD DOWN STUD.						1	L	7	2 	3O	3	O		A29CE   	E286				 
1999021200951	19990212	00951	GL  	1999	2	12	CA990119017      	3	19990111	G	6111	10151C5	BLADE           													HARTZL	HCB3Z	HCB3Z201    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA									AF532		(CAN) PROPELLER RECEIVED FOR 5 YEAR CORROSION INSPECTION.  INSPECTION FOUND LIGHT SURFACE CORROSION ON THE BLADES BORE R	ADII.  CORROSION CLEANED PER MANUFACTURER'S INSTRUCTIONS AND BLADES RETURNED TO SERVICE.															5	C	P907	 
1999021200952	19990212	00952	GL  	1999	2	12	CA990119018      	3	19990111	G	6111	57A1851	BEARING         													HARTZL	HCB3Z	HCB3Z201    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA									AF532		(CAN) PROPELLER RECEIVED FOR TBO OVERHAUL.  UPON DISMANTLE, FOUND THE BLADE THRUST BEARINGS TO BE CORRODED.  THE THRUST 	BEARINGS WERE REPLACED WITH NEW.															5	C	P907	 
1999052800018	19990528	00018	CE  	1999	5	28	CA990119019      	1	19990113	G	6120	A20107	IDLE GEAR       		DCFS290D7BT4	CESSNA	421   	421B        	2076014	CE  	CONT  	O520  	GTSIO520H   	17032	SO  	MCAULY	3AF34C	3AF34C92    	GL  	PROPELLER ASSY	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						781543		607002	751005		(CAN) DURING NDT INSPECTION, A CRACK WAS FOUND IN THE IDLE GEAR.						1	L	7	2 	3O	3	O		A7CE    	E7CE	5	C	P22E	 
1999052800019	19990528	00019		1999	5	28	CA990119020      	4	19990113	G	6122	B20258	FLYWEIGHT DISC  		DCFS290D7BT4	CESSNA	421   	421B        	2076014	CE  	CONT  	O520  	GTSIO520H   	17032	SO  	MCAULY	3AF34C	3AF34C92    	GL  	PROP GOVERNOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						781543		607002	751005		(CAN) DURING NDT INSPECTION, A CRACK WAS FOUND IN THE FLYWEIGHT DISC, CRACK GOING FROM OUTER EDGE TO INBOARD EDGE.						1	L	7	2 	3O	3	O		A7CE    	E7CE	5	C	P22E	 
1999021200953	19990212	00953	GL  	1999	2	12	CA990119021      	3	19990113	G	6114	57A203632	BOLT            													HARTZL	HCB3Z	HCB3Z201    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA									AF10		(CAN) PROPELLER RECEIVED FOR 5 YEAR CORROSION INSPECTION.  DISMANTLE INSPECTION FOUND TWO COUNTERWEIGHT BOLTS CORRODED. 	 THE BOLTS WERE REPLACED WITH NEW.															5	C	P907	 
1999021200954	19990212	00954	GL  	1999	2	12	CA990119022      	3	19990113	G	6111	57A1851	BEARING         													HARTZL	HCB3Z	HCB3Z201    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA									AF10		(CAN) PROPELLER RECEIVED FOR TBO OVERHAUL.  DISMANTLE INSPECTION FOUND THE BLADE THRUST BEARINGS TO BE CORRODED.  THE BL	ADE THRUST BEARINGS WERE REPLACED.															5	C	P907	 
1999021200955	19990212	00955	EA  	1999	2	12	CA990119023      	3	19990113	G	6111		BLADE           			BEECH 	23    	A23         	1151204	CE  	CONT  	O346  	IO346A      	17033	SO  	SNSNCH	74DC	M74DC       	EA  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2284 	953  				1004706A	B642		(CAN) DUE TO CORROSION OF THE PROPELLER BLADES, CAMBER AND FACE GRINDING IN ACCORDANCE WITH THE SENSENICH MAINTENANCE MA	NUAL WAS CARRIED OUT.					1	L	7	1 	3O	3	O		A1CE    	E3CE	5	N	P88614	 
1999021200956	19990212	00956	GL  	1999	2	12	CA990119024      	3	19990113	G	6111		BLADE           			CESSNA	172   	172H        	2072424	CE  	CONT  	O300  	O300D       	17022	SO  	MCAULY	1C172	1C172EM     	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2217 	477  				35923D7D	E14501		(CAN) DURING THE GRINDING PROCESS CORROSION APPEARED.  EXTRA GRINDING IN ACCORDANCE WITH THE MCCAULEY MAINTENANCE MANUAL	 WAS REQUIRED TO REMOVE THE CORROSION PITS FROM THE BLADE(S) CAMBER AND FACES.					1	H	7	1 	3O	3	O	NT	3A12    	E253	5	N	P910	 
1999021900423	19990219	00423	NE  	1999	2	19	CA990119028      	2	19990101	G	7200		ENGINE          								GE    	CF6   	CF680C2B2   	30025	NE  					NR 1	LEAKING         	W				A				UNSCHED LANDING         				K			FLUID LOSS                			CL	CLIMB          	1			CA			28492	5832 				695269			(CAN) NR 1 ENGINE OIL QUANTITY DECREASED RAPIDLY IN CLIMB, 15 MINUTES AFTER TAKEOFF.  THE FLIGHT WAS DIVERTED. POST -FLI	GHT INSPECTION FOUND AN OIL LEAK AT THE 6 O'CLOCK POSITION.  THE SCAVENGE O-RING WAS REPLACED AND A GROUND RUN INDICATED	 THE OIL LEAK WAS STILL A PROBLEM.  IN CONSULTATION WITH THE MANUFACTURER, IT WAS DETERMINED THE OIL LEAK WAS INTERNAL, 	SO THE ENGINE WAS REPLACED.  TOTAL CYCLES:  8,707.								4	F			E13NE				 
1999021900424	19990219	00424	CE  	1999	2	19	CA990119030      	1	19990112	G	5210	04120201819	SKIN            			CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A102	1A102OCM    	GL  	PASSENGER DOOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			13196					900428OH	QH004		(CAN) DOOR SKIN FOUND CRACKED IN TWO PLACES AT THE TOP.						1	H	7	1 	3O	3	O		3A19    	E252	5	N	P918	 
1999021900433	19990219	00433	SO  	1999	2	19	CA990119044      	2	19990105	G	8530	537750	BOLT            			PIPER 	PA46  	PA46310P    	7104605	SO  	CONT  	O520  	TSIO520BE   	17040	SO  					NR 2 CYLINDER	FRACTURED       	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			165  					273726R			(CAN) THE NR 2 CYLINDER ROCKER COVER HOLD-DOWN BOLTS BROKE, SENDING INTAKE BOLT UPPER BROKEN HALF THROUGH THE ROCKER COV	ER. THE CYLINDER WAS REMOVED AND SENT FOR REPAIR.  NO OTHER DAMAGE WAS FOUND TO THE CYLINDER OR THE PISTON.  ALL OTHER H	OLD-DOWN BOLTS WERE CHECKED.				1	L	7	1 	3O	3	O	RT	A25SO   	E8CE				 
1999021900434	19990219	00434	NE  	1999	2	19	CA990119046      	2	19990107	G	7210	31073301	BEARING         								PWA   	120   	PW120       		NE  					GEARBOX	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			20687	10194				120530			(CAN) INSPECTION FOUND M50 METAL IN THE REDUCTION GEARBOX DURING ROUTINE INSPECTION, AND WAS SENT FOR OVERHAUL.  DISASSE	MBLY OF THE RGB FOUND THE METAL CONTAMINATION WAS FROM A SEVERELY WORN NR 15 BEARING, WITH MATERIAL LOSS FROM THE OUTER 	RACE AND THE ROLLERS.									4	T			E20NE				 
1999021900435	19990219	00435	NE  	1999	2	19	CA990119047      	2	19990106	G	7210	31073301	BEARING         			DHAV  	DHC8  	DHC8*       		NM  	PWA   	120   	PW120A      		NE  					GEARBOX	SPALLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			20347	14902				120874			(CAN) REDUCTION GEARBOX SENT FOR REFURBISHING.  ON ARRIVAL, A LARGE ACCUMULATION OF METAL FOUND IN RGB CHIP DETECTOR.  S	OURCE OF METAL CONTAMINATION FROM SPALLING OF NR 15 BEARING WITH MATERIAL LOSS FROM OUTER RACE.  CAUSE OF SPALLING COULD	 BE RESULT OF BRG DISTORTION RESULTING FROM EXCESS FRETTING OF BRG LOCATION DIAMETER, OR, RESULT OF LIGHTNING STRIKE, BU	T RESIDUAL MAGNETISM FOUND UNLIKE THAT FOUND ON A TYPICAL LIGHTNING STRIKE AND NO EVIDENCE OF ELECT ARCING NOTED.  SIGNI	FICANT BUILD ERRORS, USED WRONG (SHORTER) BOLTS TO SECURE NR 15 BRG WHICH MAY HAVE LOOSENED AND EXACERBATED FRETTING CON	DITION WHICH WAS POSSIBLE CAUSE OF BRG FAILURE:  NR 12 AND NR 14 BRG HAVE MISMATCHED S/N'S ON INNER AND OUTER RACES.	2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999021900436	19990219	00436	NE  	1999	2	19	CA990119048      	2	19990112	G	7210	311657901	PINION GEAR     								PWA   	PW120 	PW123       		NE  					GEARBOX	SPALLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1571 					123209			(CAN) THE REDUCTION GEARBOX WAS SENT FOR INVESTIGATION AFTER METAL CONTAMINATION WAS FOUND.  THE SOURCE OF THE METAL CON	TAMINATION WAS A SPALLED 2ND STAGE PINION GEAR (RT).  ALSO, EXHIBITING SIGNS OF DAMAGE IN SIMILAR LOCATIONS WAS THE OTHE	R 2ND STAGE PINION AND THE BULL GEAR.  IT APPEARED THE TEETH OF THE 2ND STAGE GEARS DEVELOPED PITS ALONG THE LINES OF MA	XIMUM FORCE AND THAT THIS PITTING DEVELOPED INTO FULL SPALL ON SOME TEETH.  WHY THE GEARS FAILED AT SUCH A LOW TIME WAS 	NOT APPARENT.  IT IS POSSIBLE THAT THE TOOTH HARDENING WAS NOT ADEQUATE.							4	T			E20NE				 
1999052800022	19990528	00022		1999	5	28	CA990125001      	4	19990111	G	2562	11268	CIRCUIT BOARD   	NARCO       	ELT10       															ELT	SHORTED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						11268					(CAN) ELT CIRCUIT BOARD FOUND SHORTED.  THE TRANSMITTER WAS U/S.																			 
1999021900437	19990219	00437	NE  	1999	2	19	CA990125002      	3	19990106	G	6114	B442	RETAINER        			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	PROPELLER HUB	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			3903 						HJ669		(CAN) SPRING RETAINER FOUND CRACKED DURING ROUTINE OVERHAUL.						2	L	7	2 	4T			RT	A24CE   		5	C	P10NE	 
1999021900438	19990219	00438	NE  	1999	2	19	CA990125003      	3	19990105	G	6111	A32042	SET SCREW       			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  	HARTZL	HCE4A	HCE4A3I     	NE  	PROPELLER BLADE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2537 					PCEPS0156	HJ851		(CAN) PROPELLER BLADE (S/N 2879J) HAD END PLAY OF 1.  SET SCREW FOUND TO BE WORN 0.030 INCH BELOW MINIMUM LENGTH.						2	L	7	2 	4T	4	T	RT	A24CE   	E26NE	5	C	P10NE	 
1999021900440	19990219	00440	GL  	1999	2	19	CA990125006      	3	19990114	G	6111	F84686R	BLADE           			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2B   	41532	EA  	HARTZL	HCE3Y	HCE3YR2A    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				1488 				RL223861L	DJ9714A		(CAN) DURING OVERHAUL, CORROSION WAS FOUND IN THE BLADE BALANCE HOLES.  INSPECTED AND CORROSION WAS REMOVED PER HARTZELL	 SB 136.					1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
1999021900441	19990219	00441	GL  	1999	2	19	CA990125007      	3	19990114	G	6111	582NC4	BLADE           													MCAULY	3AF32C	3AF32C87    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				1039 					713450		(CAN) DURING OVERHAUL, CORROSION WAS FOUND ON PROPELLER BLADE SURFACE AND IN THE COUNTERWEIGHT GROOVE.																5	C	P22EA	 
1999052800024	19990528	00024	CE  	1999	5	28	CA990125010      	1	19990115	G	2720		CLEVIS          		2660001104  	CESSNA	208   	208         	2073702	CE  	PWA   	PT6   	PT6A114     	52043	NE  					RUDDER CABLE	BENT            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			3895 					PCE17333			(CAN) RIGHT AFT RUDDER CONTROL CABLE SWAGED CLEVIS BENT AND BUCKLED.  THIS HAD CAUSED CABLE STRAND SEPARATION AND FRAYIN	G.  FURTHER INSPECTION  FOUND THE RIGHT CABLE CLAMP P/N 2613397-2 LOOSE ON THE CABLE, LEADING TO A NO-LOCK CONDITION ON 	THE RIGHT RUDDER CONTROL CABLE WHEN THE CONTROL LOCK WAS DEPLOYED.  THE AIRCRAFT HAD BEEN PARKED OUTSIDE DURING STRONG W	IND CONDITIONS.  THIS ALLOWED WIND TO MOVE RUDDER AGAINST ITS MECH STOP IN THE RIGHT HAND DIRECTION ONLY.  THIS UNLOADED	 THE RIGHT RUDDER CABLE TENSION ALLOWING CABLE END CLEVIS TO SWING ABOUT ITS BOLTED CENTER; THUS, THE CLEVIS FORWARD END	 FOULED THE CABLE CUT-OUT ON BULKHEAD ASSY P/N 2612059-1 AT STA 427.88 AND BENDING THE CLEVIS.	1	H	7	1 	3T	3	T	NT	A37CE   	E4EA				 
1999012900958	19990129	00958	NE  	1999	1	29	CA990125014      	2	19990112	G	7260	39600205	GEARBOX         								RROYCE	BR700 	BR700710A220		NE  					ENGINE	CRACKED         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			16   					12120			(CAN) ENGINE OIL WAS VISIBLE ON HI-POWER RUN-UP.  INSPECTION FOUND OIL COMING FROM A 0.400 INCH LONG LINE ON THE ACCESSO	RY GEARBOX .  NO VISIBLE CRACK DETECTED.  FURTHER REPORT TO FOLLOW.  PART TC:  9.										4	F			E00057EN				 
1999012900959	19990129	00959	GL  	1999	1	29	CA990125017      	2	19990106	G	7240	23055521	SEAL            								ALLSN 	AE300 	AE3007A     		GL  					ENGINE	WORN            	W				E				ENGINE SHUTDOWN         				A			FLAME/FIRE                			IN	INSP/MAINT     	1			CA			1785 					310065			(CAN) ENGINE WAS HARD TO START, WITH A BALL OF FIRE OUT OF THE TAILPIPE AND RAPID RISE IN ITT.  BORESCOPE INSPECTION REV	EALED HP TURBINE BLADE DAMAGE AT THE TIPS.  DURING DISASSEMBLY, THE COMBUSTION OUTER SEAL RING ASSEMBLY REAR FLANGE WAS 	FOUND SEPARATED FROM THE REMAINDER OF THE SEAL AND WAS IN TWO HALVES APPROXIMATELY 180 DEGREES EACH.  A 0.157 INCH DIAME	TER BALL BEARING LIKE ASSEMBLY WAS ALSO FOUND DURING REMOVAL OF THE HP TURBINE 1ST STAGE VANE AND SUPPORT ASSEMBLY.  THI	S PIECE WAS FOUND RESTING ON THE FRONT LIP OF THE COMBUSTION LINER OUTER SEAL RING.  THE BALL BEARING LIKE PART APPEARS 	FOREIGN TO THE ENG.  THE INVESTIGATION CONTINUES AND A FURTHER REPORT WILL FOLLOW.  PART TC:  1,417.						4	F			TE6CH				 
1999021900444	19990219	00444	EU  	1999	2	19	CA990125018      	1	19990107	G	6520	4619003003	GEARBOX         			BOLKMS	105   	BO105C      	5626005	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TAIL ROTOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			3743 			1148		CAE836045			(CAN) FOUND THREE AREAS OF DEEP CORROSION IN THE MAGNESIUM CASE NEAR THE UPPER GEARBOX MOUNTS.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999021900446	19990219	00446	SW  	1999	2	19	CA990129007      	1	19990115	G	2910	2781006641	LINE            			SWRNGN	SA226 	SA226TC     	8780404	SW  	GARRTT	TPE331	TPE3313UW   	01514	WP  					HYDRAULIC SYS	CHAFED          	W				O				OTHER                   				J			WARNING INDICATION        			LD	LANDING        	1			CA								P03450			(CAN) .75 INCH STAINLESS HYDRAULIC LINE FOUND CHAFED IN THE RIGHT HAND NACELLE INBOARD.  ACCESSIBLE THROUGH THE WHEELWEL	L PANELS.  LINE HAD BEEN RUBBING ON A STRINGER.					2	L	7	2 	4T	4	T	RT	A8SW    	E4WE				 
1999052800028	19990528	00028	GL  	1999	5	28	CA990129008      	3	19990115	G	6114	C4645	CYLINDER        			CESSNA	177   	177B        	2073708	CE  	LYC   	O360  	O360A1F6    	41514	EA  	MCAULY	2D34C	B2D34C211   	GL  	PROPELLER HUB	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				829  				L1536536A	773957		(CAN) PROPELLER CYLINDER WORN BEYOND MANUFACTURER'S LIMITS.						1	H	7	1 	3O	3	O		A13CE   	E286	5	C	P7EA	 
1999052800029	19990528	00029	NE  	1999	5	28	CA990129009      	3	19990119	G	6111	90LNA2	BLADE           			CESSNA	441   	441         	2076020	CE  						MCAULY	4HFR34	4HFR34C660  	NE  	PROPELLER	OUT OF TRACK    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						OD027			950848		(CAN) PROPELLER BLADE OUT OF TRACK, BLADE REPAIRED MAY 1996.  SEPTEMBER 1998 REMOVED FROM SERVICE FOR HARDNESS TESTING.						1	L	7	2 	3T			RT	A28CE   		5	C	3PNE	 
1999052800030	19990528	00030	GL  	1999	5	28	CA990129010      	3	19990120	G	6114	57A18032	CYLINDER        			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	PROPELLER HUB	LEAKING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				2453 				PCE85171	BUA20038		(CAN) OIL LEAK OBSERVED RUNNING DOWN NR 3 PROPELLER BLADE.   INVESTIGATION DISASSEMBLY FOUND PROPELLER CYLINDER TO BE WO	RN BELOW MANUFACTURER'S LIMITS.					1	L	7	2 	4T	4	T		A24CE   	E4EA	6	C	P15E	 
1999052800031	19990528	00031	EU  	1999	5	28	CA990129013      	1	19990111	G	3260	622800200	SWITCH          			BAG   	JETSTM	JETSTM3212  	1500217	EU  										NLG	FAILED          	W				L				ABORTED APPROACH        				N			FALSE WARNING             			AP	APPROACH       	1			CA											(CAN) ON APPROACH, GEAR SELECTED DOWN, THE NOSE GEAR WAS STILL SHOWING RED INDICATING INTRANSIT.  GEAR CYCLED WITH NO EF	FECT.  APPROACH ABORTED.  EMERGENCY EXTENSION ALSO TRIED TO NO AVAIL.  OVER TOWER RUN CARRIED OUT, GEAR APPEARED DOWN. A	IRCRAFT LANDED, ENGINES SHUT OFF AT TOUCHDOWN AND NOSE WHEEL HELD UP, BUT LANDING WAS OK.  NOSE GEAR DOWNLOCK SWITCH HAD	 FAILED.  OAT WAS AT MINUS 40 DEGREES AND MAY HAVE BEEN THE REASON FOR INTERMITTENT OPERATION.			2	L	7	2 	4T			RT	BA15CAA 					 
1999052800032	19990528	00032	GL  	1999	5	28	CA990129014      	3	19990111	G	6111	V8833N	BLADE           			CESSNA	180   	180         	2072602	CE  						HARTZL	HCA2V	BHCA2VF3    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				104  					HUBCU39		(CAN) DURING THE 6-YEAR CORROSION INSPECTION, CORROSION WAS FOUND IN THE BLADE BALANCE LEAD HOLE, THE CORROSION WAS REMO	VED IAW MANUFACTURER'S INSTRUCTIONS.  THE SUBMITTER SUGGESTS THAT PROPELLERS SHOULD BE OVERHAULED EVERY 5 YEARS PER THE 	MANUFACTURER'S RECOMMENDATIONS.				1	H	7	1 	3O			NC	5A6     		5	C	P24E	 
1999021900447	19990219	00447	SW  	1999	2	19	CA990129015      	1	19990113	G	2160	BYLB504371	MIXING VALVE    			SWRNGN	SA226 	SA226TC     	8780404	SW  	GARRTT	TPE331	TPE33110UA  	01514	WP  					BLEED AIR SYS	FAILED          	W				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			DE	DESCENT        	1			CA						253E		P54151			(CAN) ON DESCENT, SMOKE NOTED IN AFT CABIN FOLLOWED BY AIR CONDITIONER CIRCUIT BREAKER TRIPPING.  INSPECTION SHOWED THAT	 THE LEFT MIXING VALVE HAD INTERNALLY SHORTED ITSELF TO GROUND DAMAGING THE PRINTED CIRCUIT BOARD ON CABIN TEMPERATURE C	ONTROLLER.  THIS WAS CAUSE OF SMOKE.				2	L	7	2 	4T	4	T	RT	A8SW    	E4WE				 
1999052800033	19990528	00033	EA  	1999	5	28	CA990129016      	3	19990121	G	6111		BLADE           			PIPER 	PA18  	PA18A150    	7101837	SO  						SNSNCH	74DM	M74DM       	EA  	PROPELLER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				594  					K4080		(CAN) DURING INSPECTION LPI, FOUND .1250 INCH CRACK ON THE BLADE TIP TRAILING EDGE (TE), OF NR 1 BLADE, THE CRACK WAS RU	NNING DOWN THE CORD OF THE BLADE.  CORROSION WAS FOUND ON THE ENTIRE SURFACE OF THE PROPELLER.  THE CRACK WAS FILED OUT,	 THE CORROSION WAS REMOVED AND THE PROPELLER WAS RETURNED TO SERVICE.  THE SUBMITER SUGGESTS REGULAR INSPECTIONS BE CARR	IED OUT PER THE MANUFACTURER'S RECOMMENDATIONS.			1	H	7	1 	3O				1A2     		5	N	P886	 
1999052800034	19990528	00034	SO  	1999	5	28	CA990129017      	2	19990118	G	8520		CRANKCASE       			CESSNA	414   	414         	2075908	CE  	CONT  	O520  	TSIO520J    	17040	SO  	MCAULY	3AF32C	3AF32C93    	GL  	ENGINE	CRACKED         	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		CR	CRUISE         	1			CA				1200 				21753271K	779585		(CAN) DURING CRUISE ,THE PILOT NOTICED FLUCTUATING MANIFOLD PRESSURE ON NR 1 ENGINE.  THE ENGINE THEN LOST POWER AND BEG	AN TO LOSE OIL PRESSURE.  THE ENGINE WAS SECURED AND THE AIRCRAFT MADE AN UNEVENTFUL EMERGENCY LANDING.  POST-FLIGHT INS	PECTION FOUND TWO HOLES IN THE RIGHT SIDE OF THE CRANKCASE.				1	L	7	2 	3O	3	O	RT	A7CE    	E8CE	5	C	P22E	 
1999052800035	19990528	00035	GL  	1999	5	28	CA990129018      	3	19990121	G	6111	F84774	BLADE           			PIPER 	PA32  	PA32RT300T  	7103216	SO  						HARTZL	HCE2Y	HCE2YR1BF   	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			9413 	1433 					DK1211		(CAN) PROPELLER RECEIVED FOR 6 YEAR CORROSION INSPECTION.  THE PAINT WAS REMOVED FROM THE BLADES AND INSPECTION FOUND CO	RROSION ON THE CAMBER AND THRUST FACE OF THE BLADES.  EXTRA WORK WAS REQUIRED TO REMOVE THE CORROSION.					1	L	7	1 	3O				A3SO    		5	C	P9EA	 
1999021900448	19990219	00448	EU  	1999	2	19	CA990129019      	1	19990123	G	5244		ACCESS DOOR     			AMD   	FALC50	FALCON50MYST	2730106	EU  	GARRTT	TFE731	TFE7313     	01518	WP  					FUSELAGE	MISMANUFACTURED 	W				O				OTHER                   				E	W		VIBRATION/BUFFET          	INADEQUATE Q C            		CR	CRUISE         	1			CA											(CAN) ACCESS DOOR OPENED IN-FLIGHT.  VIBRATION NOTED IN CRUISE.  FURTHER INVESTIGATION FOUND THAT THE NUMBER OF FASTENER	S AND THE SAFETY IS INADQUATE.  THE FASTENERS WERE REMOVED FROM THE DOOR AND INSTALLED IN THE RECEPTACLES AND THE FIT WA	S OK.  ONCE THE FASTENERS WERE INSTALLED IN THE DOOR, THE SAFETY WAS UNSATISFACTORY.  INVESTIGATOR SUSPECTS THAT THE FAS	TENERS ARE TOO SHORT.  IN ADDITION, HE NOTES THAT IF THE FORWARD EDGE CAMLOC WERE TO FAIL OR BE IMPROPERLY ATTACHED, THE	RE WOULD BE A LENGTH OF 21 INCHES ON THE FORWARD EDGE IN THE AIRFLOW NOT SAFTIED.		2	L	7	3 	4F	4	F		A46EU   	E6WE				 
1999052800036	19990528	00036		1999	5	28	CA990129020      	1	19990120	G	6120	CPW311835404	TSCU            								PWA   	PW120 	PW123       		NE  					ENGINE	FAULTY          	W				D				RETURN TO BLOCK         				L			NO TEST                   			TX	TAXI/GRND HDL  	1			CA			84   					AG0042			(CAN) AUTOFEATHER SYSTEM ARM LIGHT ILLUMINATES AT 90 PERCENT TORQUE, WITH NO SELECTION ON OF THE AUTOFEATHER SYSTEM.  TO	RQUE SIGNAL CONDITIONING UNIT (TSCU) REPLACED.										4	T			E20NE				 
1999021900449	19990219	00449	EU  	1999	2	19	CA990129021      	1	19990120	G	2420	224W4710513	CONNECTOR       			AIRBUS	310   	A310304     		EU  										IDG HARNESS	FAILED          	W				H				DEACTIVATE SYST/CIRCUITS				O			OTHER                     			TX	TAXI/GRND HDL  	1			CA											(CAN) IDG HARNESS CONNECTOR IN ENGINE PYLON SEVERELY ARCED ON 3 RECEPTACLE CONNECTORS.  REPAIRED/REPLACED.						2	L	7	2 	4F			RT	A35EU   					 
1999021900450	19990219	00450	EA  	1999	2	19	CA990129022      	1	19990126	G	2760	601R106002	LINK            			CNDAIR	CL600 	CL6002B19   		EA  										RT SPOILER	DAMAGED         	W				D				RETURN TO BLOCK         				J			WARNING INDICATION        			TX	TAXI/GRND HDL  	1			CA						55					(CAN) WITH AIRCRAFT ON STANDBY AT AIRPORT, AN UNCOMMANDED DEPLOYMENT OF THE RIGHT FLIGHT SPOILER OCCURRED.  STATUS MESSA	GE 'FLT SPOILERS' ON EICAS AND ON THE SYNOPTIC PAGE, RT SPOILER SHOWED TO BE AT 26 DEGREES.  COMFIRMED VISUALLY.  RIGHT 	HAND SPOILER LINK TO PCU FOUND DAMAGED.  UNDER INVESTIGATION.				2	L	7	2 	4F			RT	A21EA   					 
1999052800037	19990528	00037	NE  	1999	5	28	CA990129023      	2	19990127	G	7260	4018T16P04	SEAL            		5018T48P01  	CNDAIR	CL600 	CL6002B19   		EA  	GE    	CF34  	CF343A1     	30015	NE  					NR 2 ENGINE	RUPTURED        	W				E				ENGINE SHUTDOWN         				K	W		FLUID LOSS                	INADEQUATE Q C            		AP	APPROACH       	1			CA								807272			(CAN) ON FINAL,THE NR 2 ENGINE OIL PRESSURE SHOWED ON THE ECAIS.  FOLLOWING THE CHECK LIST, THE NR 2 ENGINE WAS SHUTDOWN	.  POST-FLIGHT INSPECTION FOUND A RUPTURED RING MATING SEAL ON THE AXIS BETWEEN THE IDG AND THE ACCESSORY GEARBOX, WHICH	 CAUSED THE LOSS OF THE OIL PRESSURE.  IT WAS FOUND THE SEAL HAD BEEN REPLACED AND WAS INSTALLED IMPROPERLY.				2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999021900451	19990219	00451	SW  	1999	2	19	CA990129024      	1	19990127	G	5302	206033004003	SKIN            			BELL  	206   	206L        	1181522	SW  										TAIL BOOM	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			11050								(CAN) TAIL BOOM INSPECTED PER AD CF-98-42, ASB-206L-98-114 FOUND A 1.5 INCH CRACK LT SIDE OF TAIL BOOM FORWARD AND BELOW	 HORIZONTAL STABILIZER CUT-OUT REPAIRED.					1	G	7	1 	3U				H2SW    					 
1999021900452	19990219	00452	SW  	1999	2	19	CA990129025      	1	19990113	G	6730	2120760057	SERVO           			BELL  	212   	212         	1181420	SW  	PWA   	PT6T  	PT6T3       	52045	EA  					CYCLIC	STICKING        	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA				583  				CPPS60495			(CAN) SERVO STICKING DURING CONTROL INPUTS UNDER HYDRAULIC SYSTEM PRESSURE.						1	G	7	1 	4U	4	U		H4SW    	E22EA				 
1999021900453	19990219	00453	SW  	1999	2	19	CA990129026      	1	19990113	G	6330	2120403631	SEAL            		212040001127	BELL  	212   	212         	1181420	SW  	PWA   	PT6T  	PT6T3       	52045	EA  					TRANSMISSION	LEAKING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				707  		ABW40007		CPPS60495			(CAN) MAIN INPUT SEAL LEAKING.  REPLACED.						1	G	7	1 	4U	4	U		H4SW    	E22EA				 
1999022600207	19990226	00207	SO  	1999	2	26	CA990202002      	1	19990119	G	2140	14E001	VIBRATOR        	JANITROL    	B3040       	PIPER 	PA34  	PA34200T    	7103406	SO  	CONT  	O360  	TSIO360EB   	17025	SO  	MCAULY	3AF34C	3AF34C503   	GL  	HEATER	FAILED          	W				A	B	H		UNSCHED LANDING         	EMER. DESCENT           	DEACTIVATE SYST/CIRCUITS		B			SMOKE/FUMES/ODORS/SPARKS  			CR	CRUISE         	1			CA						1791788		307182	951433		(CAN) CABIN HEATER STARTED BACKFIRING AND PILOT SMELLED ODOR.  HEATER TURNED OFF.  BANGING AND ODOR STOPPED.  HEATER REM	OVED AND IGNITION FOUND INTERMITTENT.  VIBRATOR REPLACED.					1	L	7	2 	3O	3	O		A7SO    	E9CE	5	C	P22EA	 
1999031200281	19990312	00281	GL  	1999	3	12	CA990202003      	3	19990121	G	6114	B1901	ARM             			PIPER 	PA31T 	PA31T       	7103124	SO  	PWA   	PT6   	PT6A28      		EA  	HARTZL	HCB3T	HCB3TN3     	GL  	PROP HUB	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				2980 				PCE41649	BU5276		(CAN) INSPECTION FOUND LINK ARMS, IN BUSHINGS, WORN BEYONDS LIMITS.  REPLACED WITH NEW LINK ARMS (P/N B4016).  BETA RING	 WAS ALSO FOUND WORN AND WAS REPLACED.					1	L	7	2 	3T	4	T		A8EA    	E4EA	6	C	P15EA	 
1999022600209	19990226	00209		1999	2	26	CA990202007      	4	19990112	G	3421	5223120004	AMPLIFIER       			CVAC  	340   	340CVAC     	242270A	WP  	ALLSN 	501D  	501D13      	03004	GL  					E/E BAY	MALFUNCTIONED   	W				A	G			UNSCHED LANDING         	O2 MASK DEPLOYED        			B			SMOKE/FUMES/ODORS/SPARKS  			CR	CRUISE         	1			CA								501041			(CAN) DURING CRUISE, CREW OBSERVED VERY STRONG TOXIC ODOR WITH LOSS OF CAPT FDI/CDI.  DEPLOYED 02 MASK, LANDED.  DETERMI	NED INST AMP BURNED, NR 1 FDI FUSE BLOWN.  REPLACED, SERVICEABLE.					2	L	7	2 	4R	4	T		6A6     	E282				 
1999031200283	19990312	00283	GL  	1999	3	12	CA990202008      	3	19990128	G	6111	F8475D4	BLADE           			PIPER 	PA32  	PA32300     	7103212	SO  	LYC   	O540  	IO540K1A5   	41532	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	PROPELLER	MISMANUFACTURED 	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA			2375 	762  				L1346548A	CH15866		(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.  BLADES WERE FOUND TO BE BELOW MINIMUM ACCEPTABLE WIDTH.						1	L	7	1 	3O	3	O		A3SO    	1E4	5	C	P920	 
1999052800038	19990528	00038	EA  	1999	5	28	CA990202009      	1	19990128	G	5312	C2FS533	BULKHEAD        			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					BS 228	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			16334					MM2145			(CAN) INSPECTION PER AD CF-98-38 FOUND THE BULKHEAD AT STA 228 CRACKED.						1	H	7	1 	3R	3	R		A806    	5E1				 
1999052800039	19990528	00039	CE  	1999	5	28	CA990202010      	1	19990124	G	3260		BULB            			BEECH 	B300  	B300        	1159232	CE  	PWA   	PT6   	PT6A60A     	52043	NE  					MLG INDICATOR	FAILED          	W				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			CA								PCE95687			(CAN) LEFT MAIN LANDING GEAR GREEN LIGHT NOT ILLUMINATING.  BULB REPLACED WITH BURNT ONE AND OBVIOUS RESULT.  AIRCRAFT L	ANDED OK.  BULB REPLACED AGAIN OK.					2	L	7	2 	4T	4	T	RT	A24CE   	E4EA				 
1999052800040	19990528	00040	EA  	1999	5	28	CA990202011      	2	19990122	G	8530	72877	LIFTER          			PIPER 	PA34  	PA34200     	7103405	SO  	LYC   	O360  	IO360C1E6   	41514	EA  					LT & RT ENGINE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			824  					L1656151A			(CAN) DURING INSPECTION, METAL WAS DETECTED IN BOTH ENGINE OIL FILTERS.  THE METAL WAS SENT TO LYCOMING FOR ANALYSIS.  I	T WAS DETERMINED THE METAL CAME FROM THE HYDRAULIC LIFTER HOUSING.  THE TWO ENGINES WERE TAKEN OUT OF SERVICE AND SENT F	OR REPAIR.				1	L	7	2 	3O	3	O		A7SO    	1E10				 
1999052800041	19990528	00041	SO  	1999	5	28	CA990202013      	1	19990120	G	5280	4752932	HINGE           		4752931     	PIPER 	PA31  	PA31350     	7103110	SO  										MLG DOOR	CRACKED         	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			CA			15045								(CAN) AFTER TAKEOFF THE GEAR INTRANSIT LIGHT REMAINED ON.  AIRCRAFT RETURNED.  RIGHT HAND INBOARD FORWARD DOOR HINGE FOU	ND BROKEN.  THUS, DOOR WOULD NOT CLOSE PROPERLY.					1	L	7	2 	3O				A20SO   					 
1999030500182	19990305	00182	SO  	1999	3	5	CA990203001      	2	19990115	G	8520	628488	LIFTER          			CESSNA	182   	182M        	2072728	CE  	CONT  	O470  	O470R       	17026	SO  	MCAULY	2A34C	2A34C201    	GL  	NR 4 CYLINDER	BROKEN          	W				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CL	CLIMB          	1			CA				800  				200166R	687635		(CAN) AFTER DEPARTURE DURING CLIMB-OUT, THE ENGINE BEGAN TO LOSE POWER.  THE PILOT TURNED BACK TO THE POINT OF DEPARTURE	, THE AIRCRAFT MADE A FORCED LANDING 38 MILES EAST OF THE BASE.  THE AIRCRAFT WAS RECOVERED AND THE CAUSE OF THE POWER L	OSS WAS DETERMINED TO BE THE FAILURE OF NR 4 CYLINDER HYDRAULIC LIFTER, WHICH PREVENTED THE EXHAUST VALVE FROM OPENING.				1	H	7	1 	3O	3	O	NT	3A13    	E273	5	C	P3EA	 
1999030500183	19990305	00183	NE  	1999	3	5	CA990203003      	3	19990126	G	6111	R7447AO	BLADE           													HAMSTD	23E	23E50       	NE  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				1654 					RRE4948		(CAN) PROPELLER RECEIVED FOR OVERHAUL AND CORROSION WAS FOUND IN ALL THREE BLADES, IN THE FILLET AND THE BORES.  CORROSI	ON IN THE FILLETS WAS REMOVED BY MACHINING, WHILE THE BLADE BORE CORROSION WAS REMOVED BY REAMING.  THE BLADES WERE LIQU	ID PENETRANT INSPECTED AND NO OTHER DEFECTS WERE FOUND.														6	C	P603	 
1999022600210	19990226	00210	SW  	1999	2	26	CA990203004      	1	19990128	G	7120	205060106001	MOUNT           			BELL  	205   	205A1       	1181414	SW  	LYC   	T53   	T5313B      	41549	NE  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								LE07641			(CAN) ENGINE MOUNT CRACKED ALONG WELD BEAD.  REPLACED.						1	G	7	1 	4U	4	U		H1SW    	E17EA				 
1999022600211	19990226	00211	NM  	1999	2	26	CA990203005      	1	19990123	G	8012	10309	SWITCH          	GARRTT      	97907821    	BOEING	727   	727277      	138408S	NM  	PWA   	JT8   	JT8D15      	52051	NE  					NR 2 ENGINE	STUCK           	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			J			WARNING INDICATION        			CR	CRUISE         	1			CA						P335		695337			(CAN) NR 2 ENGINE START VALVE LIGHT ILLUMINATED IN-FLIGHT.  START VALVE REPLACED, LIGHT STILL ON.  PRESSURE SWITCH REPLA	CED, CHECKED SERVICEABLE.					2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
1999052800043	19990528	00043	NM  	1999	5	28	CA990203008      	1	19990127	G	3260	864202	SWITCH          			DHAV  	DHC8  	DHC8301     		NM  										NLG	OUT OF ADJUST   	W				O				OTHER                   				N			FALSE WARNING             			AP	APPROACH       	1			CA											(CAN) ON APPROACH ,THE NOSE GEAR GREEN ADVISORY DOWN AND LOCKED LIGHTS CYCLED.  GEAR CYCLED SEVERAL TIMES.  NOSE LIGHT S	TAYED AT DOWN AND LOCKED.   AIRCRAFT LANDED OK.  DRAG STRUT PROXIMITY SENSOR AND NOSE FORWARD DOOR MECHANISM PROXIMITY S	ENSOR WERE OUT OF ADJUSTMENT.				2	H	7	2 	4T			RT	A13NM   					 
1999031200284	19990312	00284	NE  	1999	3	12	CA990203025      	2	19990103	G	7230	MS16555622	PIN             			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					COMPRESSOR	LOOSE           	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			3513 					PCEPS0103			(CAN) INERTIAL VANE CONTROL (IVC) LINKAGE DOWEL PIN WORKED ITSELF LOOSE, LINKAGE CAME APART.  SPRING FOUND LYING ON TOP 	OF THE AIR INLET SCREEN, REST OF LINKAGE FOUND IN BOTTOM OF THE ENGINE COWLING.  DOWEL PIN WAS NOT FOUND.  FOD DAMAGE ON	 1ST STAGE COMPRESSOR BLADES.  DAMAGE FOUND WITHIN LIMITS AND WAS DRESSED OUT.  CT BLADE INSPECTION CARRIED OUT, NO DAMA	GE FOUND.  SUSPECT DOWEL PIN WAS INJESTED AND REJECTED BY THE 1ST STAGE COMPRESSOR BLADES.  INDICATIONS ON THE ENGINE IN	LET SCREEN THAT AN OBJECT WAS REJECTED.		2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999030500195	19990305	00195	NE  	1999	3	5	CA990209001      	2	19990102	G	7310	O301007710	LINE            			SNIAS 	350   	AS350B2     	8680813	EU  	TMECA 	ARRIEL	ARRIEL1D    		NE  					FUEL SYSTEM	CRACKED         	W				O				OTHER                   				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			1153 					9481			(CAN) FUEL LEAK DURING START.  INSPECTION FOUND LEFT HAND FUEL INJECTOR LINE CRACKED.  THIS LINE HAD NOT BEEN REMOVED SI	NCE INITIAL INSTALLATION AND THE ALIGNMENT WAS CORRECT.					1	G	7	1 	3U	3	U		H9EU    	E19EU				 
1999052800046	19990528	00046	EA  	1999	5	28	CA990209002      	1	19990202	G	5312	C2FS533	BULKHEAD        			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					BS 228	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								JP211421			(CAN) AD CF-98-38 INSPECTION FOUND THE BULKHEAD AT STA 228 CRACKED AT THE BOTTOM LEFT.						1	H	7	1 	3R	3	R		A806    	5E1				 
1999052800047	19990528	00047	EA  	1999	5	28	CA990209003      	1	19990202	G	5312	C2FS533	BULKHEAD        			DHAV  	DHC2  	DHC2*       	2800108	EA  	PWA   	R985  	R985AN14B   	52008	NE  					BS 228	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								19554			(CAN) BULKHEAD STA 228 FOUND CRACKED PER AD CF-98-38.  CRACKS RUNNING ALONG THE LOWER LEFT CORNER AND MID-WAY UP THE RIG	HT SIDE.  BOTH CRACKS WERE RUNNING ALONG THE BEND AND STARTED AT THE CUT-OUTS.					1	H	7	1 	3R	3	R		A806    	5E1				 
1999052800048	19990528	00048		1999	5	28	CA990209004      	4	19990130	G	3454	1980	SCREWS          			CNDAIR	CL600 	CL6002B19   		EA  										COCKPIT	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						1980					(CAN) FIVE SCREWS AND WASHERS FOUND INSIDE THE NAV RECEIVER DURING MODIFICATION.  SCREWS BELIEVED TO BE FROM THE METAL C	OVER ON ONE OF THE CIRCUIT BOARDS.					2	L	7	2 	4F			RT	A21EA   					 
1999052800049	19990528	00049	EU  	1999	5	28	CA990209005      	1	19990204	G	2520	85615RH3	ACTUATOR        		5000        	AMD   	FALC50	FALCON900   	2700160	EU  										FOOTREST	SHORTED         	W				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			LD	LANDING        	1			CA			437  			S4391					(CAN) ON PREP FOR LANDING, ELECTRIC FOOTRESTS WERE RETRACTED TO STOWED POSITIONS AND NR 1 SEAT RIGHT SIDE HAD AN ODOR OF	 BURNING WIRES.  AIRCRAFT LANDED OK.  SEAT WAS DISMANTLED AND NEGATIVE WIRE FOUND BURNED OFF OF TERMINAL BLOCK WHICH IS 	ATTACHED TO ACTUATOR.   ACTUATOR IS IN CLOSE PROXIMITY TO CABLE THAT OPERATES RECLINE/SWIVEL FEATURE OF SEAT ASSY.  THIS	 MAY HAVE BEEN IN CONTACT W ITH FOOTREST ACTUATOR WIRING AND LED TO IT BREAKING OFF.   MANUFACTURER OF SEAT INFORMED.  M	FG STATES THAT WITH CAPS FACING UP, MAY SNAG ON RECLINE/SWIVEL CABLES.   IN FUTURE, MFG SAYS ALL ACTUATORS WILL BE CONNE	CTED FACE DOWN OR AWAY FROM POSSIBLE INTERFERENCE.  INSTALLERS ALSO CAUTIONED TO TRACK SEAT AFTER INSTALL.	2	L	7	3 	4F			RT	A46EU   					 
1999052800050	19990528	00050	GL  	1999	5	28	CA990209008      	1	19990125	G	5540	GS2680001	SEAL            			BOMBDR	BD700 	BD7001A10   	1390006	GL  										RUDDER	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			5    								(CAN) ON POST-FLIGHT INSPECTION, THE UPPER LEFT RUDDER GAP SEAL P/N GD245-9701-1 WAS FOUND DAMAGED, AS WELL AS THE MID L	EFT RUDDER GAP SEAL P/N GD245-9700-1 AND THE RUDDER.  THE UPPER RUDDER SEAL ENTERED THE LEADING EDGE OF THE RUDDER DURIN	G FULL NOSE RIGHT RUDDER POSITION.  ALL THE PARTS WERE DAMAGED WHEN THE RUDDER WAS RETURNED TO NEUTRAL POSITION.				2	L	7	2 	4F			RT	T00003NY					 
1999052800051	19990528	00051	EA  	1999	5	28	CA990209009      	1	19990128	G	5312	C2FS533	BULKHEAD        			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN1     	52008	NE  					BS 228	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			10977					2648			(CAN) INSPECTION PER CR-98-38 FOUND THE BULKHEAD AND CHANNEL ASSEMBLY CRACKED.						1	H	7	1 	3R	3	R		A806    	5E1				 
1999052800052	19990528	00052	EU  	1999	5	28	CA990209011      	1	19990121	G	3250	Z4242170001	SPRING          			ZLIN  	242   	Z242L       	9970204	EU  										NLG STEERING	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2291 								(CAN) DURING GROUND RUN, PLAY WAS NOTICED IN THE NOSE WHEEL STEERING SYSTEM.  THE STEERING SPRING WAS FOUND BROKEN.  USE	RS WERE REMINDED OF PROPER TAXI TECHNIQUES.					1	L	7	1 	3O			0	A76EU   					 
1999030500197	19990305	00197	EA  	1999	3	5	CA990209012      	2	19990128	G	8520	LW18840	CAMSHAFT        								LYC   	O360  	AEIO360A1B6 	41514	EA  					ENGINE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2291 					L2662551A			(CAN) DURING INSPECTION, A SMALL AMOUNT OF METAL PARTICLES WAS FOUND IN THE ENGINE OIL FILTER.  INVESTIGATION REVEALED T	HE ABNORMAL WEAR TO THE CAMSHAFT AND THE CAM FOLLOWER WAS BADLY SPALLED.  THE ENGINE WAS REMOVED AND SENT FOR REPAIR.										3	O			1E10				 
1999030500198	19990305	00198		1999	3	5	CA990209013      	1	19990128	G	7820	L24266710000	SILENCER        								LYC   	O360  	AEIO360A1B6 	41514	EA  					EXHAUST	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2291 					L2662551A			(CAN) DURING INSPECTION OF THE ENGINE EXHAUST SYSTEM, THE NR 1 SILENCER WAS FOUND BROKEN WITH A PIECE MISSING.  THE NR 1	 SILENCER WAS REPLACED.										3	O			1E10				 
1999030500199	19990305	00199		1999	3	5	CA990209014      	1	19990120	G	7820	L24266710000	SILENCER        								LYC   	O360  	AEIO360A1B6 	41514	EA  					EXHAUST	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2602 					L2652551A			(CAN) DURING INSPECTION OF THE ENGINE EXHAUST SYSTEM, THE NR 1 SILENCER WAS FOUND BROKEN WITH A PIECE MISSING.  THE NR 1	 SILENCER WAS REPLACED.										3	O			1E10				 
1999052800053	19990528	00053	SW  	1999	5	28	CA990209015      	1	19990119	G	3246	5200025012	SPINDLE         			MOONEY	M20   	M20E        	5870212	SW  	LYC   	O360  	IO360A1A    	41514	EA  					MLG WHEEL	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1879 					L1407251A			(CAN) UPON REMOVAL OF WHEEL ASSY, THE WELD WHICH ATTACHES THE GUSSET ON BOTH LEFT AND RIGHT ASSY WERE FOUND CRACKED.  MO	ONEY INFORMED, AND SUGGESTED THEY HAD NEVER HEARD OF IT BEFORE.  SUBMITTER SUGGESTS THAT TO FIND BOTH LEGS CRACKED INDIC	ATES A POSSIBLE HARD LANDING.				1	L	7	1 	3O	3	O		2A3     	1E10				 
1999052800054	19990528	00054	NM  	1999	5	28	CA990209016      	1	19990203	G	3260		SWITCH          			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					MLG DOOR	CONTAMINATED    	W				C				ABORTED TAKEOFF         				N			FALSE WARNING             			TO	TAKEOFF        	1			CA								120063			(CAN) WHEN GEAR RETRACTED, LEFT MAIN GEAR DOOR OPEN WARNING ON.  GEAR RECYCLED AND FAULT THE SAME.  WITH GEAR DOWN, DOOR	 POSITION INDICATION WAS NORMAL.  INSPECTION LEAD TO CLEANING OF PROXIMITY SWITCHES.  SUBMITTER SUSPECTS EITHER DEBRIS O	R COLD WEATHER CAUSED THE PROBLEM.				2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999052800055	19990528	00055	SO  	1999	5	28	CA990209020      	1	19990128	G	7810	282793	STACK           			PIPER 	PA23  	PA23250     	7102308	SO  	LYC   	O540  	IO540C4B5   	41532	EA  					EXHAUST	SEPARATED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				102  				L372748			(CAN) BLACK SOOT NOTED ON RIGHT HAND OUTBOARD LANDING GEAR DOOR AND OUTBOARD COWL FLAP.  EXHAUST STACK FOUND SEPARATED. 	  NO OTHER LOOSE AREAS NOTED.   SUBMITTER SUGGESTS THAT THE REAR STACK WAS TOO SHORT AND THE SPRING ACTION OF REAR SUPPO	RT CAUSED THE SEPARATION OR VIBRATION OR BACK FIRE ON PREVIOUS START.				1	L	7	2 	3O	3	O		1A10    	1E4				 
1999030500200	19990305	00200	SO  	1999	3	5	CA990209025      	1	19990128	G	7721	756307	THERMOCOUPLE    			PIPER 	PA23  	PA23250     	7102308	SO  	LYC   	O540  	IO540C4B5   	41532	EA  					ENGINE	MISINSTALLED    	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA				500  				L372748			(CAN) AIRCRAFT WAS RECENTLY PURCHASED WITH HIGH TIME ENGINES. AFTER 102.3 HOURS OF OPERATION THERE HAVE BEEN MANY MISCEL	LANEOUS EGT PROBLEMS.  INVESTIGATION FOUND THE EGT (THERMOCOUPLE) PROBES INSTALLED IN WHAT APPEARS TO BE RANDOM POSITION	S.  PIPER WAS CONTACTED TO OBTAIN THE CORRECT DRAWING OF THE INSTALLATION INSTRUCTIONS.  THE PROBES WERE REPLACED AND TH	E OVERLEAN AND OVERRICH PROBLEMS WENT AWAY.			1	L	7	2 	3O	3	O		1A10    	1E4				 
1999052800059	19990528	00059	CE  	1999	5	28	CA990210001      	1	19990202	G	2435	06123042	DATA PLATE      	LEARSIEGLER 	23048018    	BEECH 	99    	99          	1154002	CE  	PWA   	PT6   	PT6A20      	52043	EA  					START/GENERATOR	MISMARKED       	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA				677  		6979		PCE22144			(CAN) STARTER/GENERATOR REMOVED FOR OVERHAUL.   THE DATA PLATE WAS STAMPED AS A 23048-006, HOWEVER, IT IS ACTUALLY A-018	 (BEECH EQUIVALENT IS 100-389005-11).   WHEN PHYSICALLY INSPECTED, IT HAD THE WRONG BRUSHES INSTALLED. THE DASH 006 IS A	 200 AMP GENERATOR WHILE THE  DASH 018 IS A 250 AMP GENERATOR.  THERE ARE ALSO NUMEROUS OTHER DIFFERENCES.  RESEARCH CAR	RIED OUT ON THIS PROBLEM.  GENERATOR HAD BEEN THROUGH 2 OVERHAULS AND PROBLEM NOT NOTED.  UNABLE TO DETERMINE WHEN MOD H	APPENED.  S/G WAS ON VARIOUS AIRCRAFT OVER THE YEARS.  SUBMITTER STATED GENERATOR MODIFIED IN AN UNAPPROVED MANNER.		1	L	7	2 	3T	3	T		A14CE   	E4EA				 
1999030500201	19990305	00201	GL  	1999	3	5	CA990210002      	3	19990203	G	6111	T10282	BLADES          			DHAV  	DHC6  	DHC6300     	2802606	EA  						HARTZL	HCB3T	HCB3TN3     	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				2753 					BUA32698		(CAN) DURING OVERHAUL, CORROSION WAS FOUND ON ALL BLADE BUTTS.  CORROSIION WAS REMOVED AND THE BLADES WERE RETURNED TO S	ERVICE PER HARTZELL MANUAL NR 133C.					1	H	7	2 	3T			RT	A9EA    		6	C	P15EA	 
1999030500202	19990305	00202	GL  	1999	3	5	CA990210003      	3	19990129	G	6114	H4716	HUB             			CESSNA	188   	188CESSNA   	2073002	CE  						MCAULY	2A34C	D2A34C58    	GL  	PROPELLER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				807  					871433		(CAN) PROPELLER WAS SENT FOR CORROSION INSPECTION AND AFTER TEARDOWN, THE PROPELLER HUB AND TWO NUTS WERE FOUND CRACKED.	  PROPELLER ASSEMBLY WAS OVERHAULED.					1	L	7	1 	3O				A9CE    		5	C	P3EA	 
1999052800060	19990528	00060	CE  	1999	5	28	CA990210005      	1	19990128	G	5753	122101015	BRACKET         			CESSNA	185   	A185F       	2072821	CE  						MCAULY	D3A34	D3A34C403   	GL  	TE FLAP	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			5068 						920355		(CAN) INBOARD FLAP TRACK BRACKET IN THE LEFT AND RIGHT WINGS FOUND CRACKED.						1	H	7	1 	3O				3A24    		5	C	P47G	 
1999052800071	19990528	00071	EA  	1999	5	28	CA990210016      	2	19990210	G	7414	10382681	CONDENSER       	BENDIX      	IO68291018  	PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					MAGNETO	MALFUNCTIONED   	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				572  		F2892026R		L836461A			(CAN) DURING RUN-UP, THE RIGHT MAGNETO DID NOT CUT OUT.  THE CAPACITOR WAS REPLACED AND THE ENGINE RETURNED TO NORMAL.						1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999052800072	19990528	00072	EA  	1999	5	28	CA990210017      	1	19990125	G	5711	2151003268	CAP             			CNDAIR	CL215 	CL2151A10   		EA  										WING SPAR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2663 								(CAN) INSPECTION PER SB 215-A454 FOUND A HAIR LINE CRACK AT THE LOWER SPAR CAP AT WS 51-650 LT.  INSPECTION PERFORMED BY	 NDT USING ULTRASONIC, EDDY CURRENT AND DYE PENETRANT.  REPAIR WILL BE IAW PSP 297 CH. 57-15-06.					2	H	7	2 	4R				A14EA   					 
1999030500204	19990305	00204	CE  	1999	3	5	CA990210018      	1	19990125	G	6120	C2995150101	CONTROL ASSY    			CESSNA	208   	208B        	2073701	CE  	PWA   	PT6   	PT6A114     	52043	NE  	MCAULY	3AF34C	3GFR34C703  	GL  	CSU	DISCONNECTED    	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			18000					PCE17268	922064		(CAN) PROPELLER CONSTANT SPEED UNIT FAILED WHEN SHEAF FAILED AND LET GO AT SWEDGED JOINT.  SUBMITTER SUGGESTS THAT THIS 	PART, WHICH IS ON CONDITION, BE MADE A LIFE LIMITED PART.  IT IS STATED THAT THERE IS NO INSPECTION METHOD THAT CAN BE U	SED TO DETECT WEAR WHEN THE UNIT IS IN SERVICE.  THERE IS AN IMPROVED PART, BUT IT IS ONLY RECOMMENDED AFTER FAILURE, IT	 IS NOT A MANDATORY REQUIREMENT.			1	H	7	1 	3T	3	T		A37CE   	E4EA	5	C	P60GL	 
1999052800073	19990528	00073	EU  	1999	5	28	CA990219001      	1	19990107	G	3260		SWITCH          			BAG   	JETSTM	JETSTM3212  	1500217	EU  						ROTOL	R333	R333482F12  	GL  	DOWNLOCK	CORRODED        	W				O				OTHER                   				N			FALSE WARNING             			DE	DESCENT        	1			CA			15348								(CAN) GEAR REQUIRED SEVERAL CYCLES TO GET DOWN AND LOCK INDICATION.  WIRE CONNECTION AT DOWNLOCK SWITCH FOUND CORRODED.						2	L	7	2 	4T			RT	BA15CAA 		6	C	P61G	 
1999052800074	19990528	00074	SO  	1999	5	28	CA990219002      	1	19990129	G	7714	574AW	INDICATOR       			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					DUAL TACH	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			4927 			1714		L589461A			(CAN) LEFT TACH INDICATION FAILURE IN-FLIGHT.  TACH DRIVE SPRING FAILED POSSIBLY BECAUSE IT HAD NOT BEEN LUBED PROPERLY 	AT ANGLE DRIVE ADAPTER.					1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999052800075	19990528	00075	CE  	1999	5	28	CA990219003      	1	19990203	G	7410	MS3106A1093S	CONNECTOR       			BEECH 	100   	A100        	1152915	CE  	PWA   	PT6   	PT6A28      		EA  					IGNITIION INPUT	MISINSTALLED    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								PCE51273			(CAN) CREW OBSERVED A DELAY IN THE ENGINE START TIME.  MAINTENANCE INSPECTION FOUND POOR SOLDER CONNECTIONS AT THE IGNIT	ION REGULATOR POWER INPUT CANNON PLUG.  CONNECTIONS WERE REPAIRED AND IGNITION TIME GROUND CHECKED SERVICEABLE.					1	L	7	2 	3T	4	T		A14CE   	E4EA				 
1999052800076	19990528	00076	GL  	1999	5	28	CA990219005      	3	19990209	G	6111	590AT4	BLADE           			CESSNA	185   	A185E       	2072818	CE  						MCAULY	2A34C	D2A34C58    	GL  	PROPELLER	CORRODED        	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			3869 	177  					755335		(CAN) DURING OVERHAUL, BOTH PROPELLER BLADE FERRULES AND THREADS WERE FOUND CORRODED.  THE FERRULES WERE SCRAPPED.  THE 	BLADE THREADS WERE DRESSED PER THE MCCAULEY MANUAL.					1	H	7	1 	3O				3A24    		5	C	P3EA	 
1999052800077	19990528	00077	CE  	1999	5	28	CA990219007      	1	19990203	G	5610	1013840257	WINDSHIELD      			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  					COCKPIT	CRACKED         	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			3543 			91297H9933		PCE85415			(CAN) WINDSHIELD CRACKED AND DELAMINATED ON LOWER INSIDE CORNER.						1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999052800079	19990528	00079	SO  	1999	5	28	CA990219012      	1	19990207	G	3232	762550	O-RING          			PIPER 	PA31T 	PA31T2      	7103127	SO  	PWA   	PT6   	PT6A135     	52043	NE  					MLG DOOR	FAILED          	W				O				OTHER                   				O			OTHER                     			AP	APPROACH       	1			CA								PCE92363			(CAN) LEFT INBOARD GEAR DOOR ACTUATOR BOTTOM GT RING.  THE O-RING AND BACK-UP FAILED.  THIS CAUSED THE ALL HYDRAULIC FLU	ID LOSS.   EMERGENCY GEAR EXTENSION USED.  CAUSE OF O-RING FAILURE WAS A PAINT CHIP ON INSIDE OF THE O-RING AND BACK-UP 	RING.				1	L	7	2 	3T	4	T	RT	A8EA    	E4EA				 
1999060900007	19990609	00007		1999	6	9	CA990219013      	1	19990205	G	7820	L24266710000	SILENCER        								LYC   	O360  	AEIO360A1A  	41514	EA  					EXHAUST	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2093 					L2514551A			(CAN) DURING INSPECTION,  A PIECE WAS FOUND BROKEN FROM THE NR 1 EXHAUST SYSTEM SILENCER.  INSPECTION OF THE NR 2 EXHAUS	T SILENCER ASSEMBLY WAS FOUND FREE OF DEBRIS.  THE NR 1 SILENCER WAS REPLACED.										3	O			1E10				 
1999052800080	19990528	00080	EA  	1999	5	28	CA990219014      	2	19990216	G	7250	3012000	TURBINE WHEEL   			BEECH 	90    	65A90       	1152908	CE  	PWA   	PT6   	PT6A20      	52043	EA  					NR 2 ENGINE	SPALLED         	W				C	E			ABORTED TAKEOFF         	ENGINE SHUTDOWN         			J			WARNING INDICATION        			TO	TAKEOFF        	1			CA			17338	3157 				PCE22402			(CAN) DURING TAKEOFF, THE PILOT NOTICED A TEMPORARY TORQUE INCREASE FROM NR 2 ENGINE.  THE THROTTLE WAS REDUCED TO IDLE 	AND THE FLIGHT WAS ABORTED.  DURING ENGINE RUN DOWN, THE NR 2 PROPELLER WAS SLOWING DOWN IN AN ERRATIC MANNER.  POST-FLI	GHT INSPECTION FOUND THE OIL DISCOLORED DARKER.  THERE WAS METAL DEBRIS IN THE OIL FILTER AND THE FRONT GEARCASE FINGER 	SCREEN.  THE PROPELLER, WHEN ROTATED, WAS BINDING AND RUBBING AT SPOTS. INSPECTION OF THE POWER SECTION THROUGH THE EXHA	UST DUCTS REVEALED THE TURBINE WHEEL HAD DROPPED, SO THERE WAS NO CLEARANCE AT THE BOTTOM AND 0.030 INCH  - 0.040 INCH A	T THE TOP.  THE ENGINE WAS MAINTENANCE FREE FOR THE LAST 300 HOURS.	1	L	7	2 	3T	3	T		3A20    	E4EA				 
1999052800081	19990528	00081		1999	5	28	CA990219015      	4	19990211	G	6122	D20271	GOVERNOR        			CESSNA	172   	172RG       	2072438	CE  	LYC   	O360  	O360F1A6    	41514	EA  	MCAULY	2D34C	B2D34C220   	GL  	PROPELLER	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								RL2697236A	800966		(CAN) PROPELLER GOVERNOR BODY WAS FOUND WORN OVERSIZE, AT THE POINT WHERE THE IDLER GEAR STUD IS PRESS FITTED TO THE GOV	ERNOR BODY.  NO REPAIRS ARE PERMITTED, SO THE GOVERNOR WAS REPLACED.					1	H	7	1 	3O	3	O		3A17    	E286	5	C	P7EA	 
1999052800082	19990528	00082	EA  	1999	5	28	CA990219016      	1	19990210	G	5210		WARNING LIGHT   			CNDAIR	CL600 	CL6002B19   		EA  										PASSENGER DOOR	ILLUMINATED     	W				G	I			O2 MASK DEPLOYED        	CABIN DEPRESSURIZATION  			N			FALSE WARNING             			CR	CRUISE         	1			CA											(CAN) IN CRUSIE, A PASSENGER DOOR WARNING ON EMERGENGY DEPRESS AND OXYGEN MASKS DEPLOYED.   AIRCRAFT DESCENDED, EMERGENC	Y LANDING TURNED OUT TO BE A FALSE WARNING.					2	L	7	2 	4F			RT	A21EA   					 
1999052800086	19990528	00086	SO  	1999	5	28	CA990219025      	2	19990108	G	8530	654654	SEAL            			CESSNA	404   	404CESSNA   	2075901	CE  	CONT  	O520  	GTSIO520M   	17032	SO  	MCAULY	3FF32	3FF32C501   	GL  	INTAKE VALVE	LEAKING         	W				O				OTHER                   				A			FLAME/FIRE                			NR	NOT REPORTED   	1			CA			798  					810566R	804566		(CAN) INTAKE VALVE ON NR 3 CYLINDER LEAKING CAUSING ACCUMULATION OF FUEL IN EXHAUST, RESULTING IN VISUAL FLAME.						1	L	7	2 	3O	3	O		A25CE   	E7CE	5	C	P45G	 
1999052800087	19990528	00087	EU  	1999	5	28	CA990219026      	1	19990208	G	2820	0164248820	REGULATOR       			SNIAS 	350   	AS350B2     	8680813	EU  	TMECA 	ARRIEL	ARRIEL1D    		NE  					FUEL SYSTEM	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			206  					9558			(CAN) A FUEL LEAK WAS NOTICED UNDER AN ENGINE.  CLOSER INSPECTION FOUND THAT WITH THE FUEL BOOSTER PUMPS ON, THERE WAS A	 FUEL LEAK FROM THE REGULATOR UNIT WHICH IS CONNECTED DIRECTLY TO A DRAIN ASSEMBLY.  THIS FUEL LEAK IS NOT NORMAL.  TURB	OMECA ADVISED THE PART BE SENT FOR REPAIRS.				1	G	7	1 	3U	3	U		H9EU    	E19EU				 
1999052800088	19990528	00088	NE  	1999	5	28	CA990219027      	2	19990130	G	7261	UL12942	PUMP            		M06626AA    	BOEING	757   	757236      		NM  	RROYCE	RB211 	RB211535E4  	54555	NE  					ENGINE OIL	FAILED          	W				C				ABORTED TAKEOFF         				W	J		INADEQUATE Q C            	WARNING INDICATION        		TO	TAKEOFF        	1			CA			23504	621  		DM3672		30649			(CAN) ON TAKEOFF ROLL, ENGINE OIL PRESSURE LIGHT AND ECAIS OIL PRESSURE LIGHT CAME ON.  TAKEOFF WAS ABORTED.  INVESTIGAT	ION FOUND OIL PUMP SCAVENGE PUMP DRIVE SHAFT SLIPPED OUT OF THE SPLINES DUE TO IMPROPER INSTALLATION.  SERVICEABLE PUMP 	AND DRIVE SHAFT INSTALLED.				2	L	7	2 	4F	4	F	RT	A2NM    	E12EU				 
1999081200327	19990812	00327	NM  	1999	8	12	CA990219028      	1	19990201	G	2750	NAS16128	O-RING          		65516022    	BOEING	737   	737242C     	1384478	NM  	PWA   	JT8   	JT8D9A      	52048	NE  					TE FLAP	WORN            	W				O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		CR	CRUISE         	1			CA								674277			(CAN) LOSS OF A-SYSTEM HYDRAULIC QUANTITY.   LEAK IN FLAP SELECTOR FLOW REGULATOR, SEAL REPLACED.						2	L	7	2 	4F	4	F		A16WE   	E2EA				 
1999052800089	19990528	00089	NE  	1999	5	28	CA990219029      	2	19990201	G	7310	AS430B120	O-RING          			BOEING	757   	757236      		NM  	RROYCE	RB211 	RB211535E4  	54555	NE  					FUEL SYSTEM	DAMAGED         	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			K	J		FLUID LOSS                	WARNING INDICATION        		CR	CRUISE         	1			CA								30649			(CAN) PILOT NOTICED DISCREPANCY OF 800 KG BETWEEN CALCULATED AND TOTALIZER FUEL, ABOUT 30 SECONDS LATER GOT FUEL CONFIGU	RATION ECIAS MESSAGE.  PRECAUTIONARY ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO POINT OF DEPARTURE.  POST- FLIGHT INSPECTI	ON FOUND FUEL LEAK BETWEEN FUEL FLOW GOVERNOR AND FUEL PRESSURE PUMP.  O-RING FOUND DAMAGED.  NEW O-RING INSTALLED.  LEA	K CHECK CARRIED OUT SERVICEABLE AND AIRCRAFT RETURNED TO SERVICE.			2	L	7	2 	4F	4	F	RT	A2NM    	E12EU				 
1999081200328	19990812	00328	NE  	1999	8	12	CA990219030      	2	19990203	G	7397		WIRE            	WHITTAKER   	320115      	BOEING	737   	737242C     	1384478	NM  	PWA   	JT8   	JT8D9A      	52048	NE  					FUEL HEAT VALVE	BROKEN          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			CA						9660		674277			(CAN) FUEL HEAT VALVE OPEN LIGHT ON NR 2 ENGINE REMAINED BRIGHT BLUE AFTER ENGINE START.  AFTER CONSULTING MAINTENANCE, 	IT WAS DECIDED THAT THE VALVE HAD FAILED IN THE CLOSED POSITION.   A/C OPERATED ON MEL FOR CLOSED VALVE.  AFTER TAKEOFF,	 THE OIL TEMPERATURE WAS CLIMBIMG INTO YELLOW ARC.  A/C R AIRCRAFT RETURNED.  BROKEN WIRES ON FUEL HEAT VALVE CANON PLUG	.			2	L	7	2 	4F	4	F	 	A16WE   	E2EA				 
1999081200329	19990812	00329	NM  	1999	8	12	CA990219033      	1	19990210	G	2612	LK86072	FIRE DETECTOR   			BOEING	757   	75728A      	1384976	NM  	RROYCE	RB211 	RB211535E4  	54555	NE  					NR 2 ENGINE	FAILED          	W				E	F	A		ENGINE SHUTDOWN         	ACTIVATE FIRE EXT.      	UNSCHED LANDING         		A	J		FLAME/FIRE                	WARNING INDICATION        		CR	CRUISE         	1			CA								30604			(CAN) NR 2 ENGINE FIRE LOOP 1 FAULT ON STATUS PAGE.    DEFERRED TO MEL.   PRIOR TO DESCENT AT 310 FEET, HAD AURAL AND VI	SUAL INDICATION OF RIGHT ENGINE FIRE.  ENGINE SHUT DOWN, WARNING EXTINGUISHED AFTER ONE BOTTLE DISCHARGED.   AIRCRAFT LA	NDED SAFELY.  ENGINE FIRE SENSOR REPLACED.  NR 2 FIRE BOTTLE REPLACED.				2	L	7	2 	4F	4	F	RT	A2NM    	E12EU				 
1999052800090	19990528	00090	NE  	1999	5	28	CA990219034      	2	19990208	G	7210	31073301	BEARING         								PWA   	120   	PW120A      		NE  					GEARBOX	SPALLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			21418	5083 				120228			(CAN) THE ENGINE WAS SENT FOR ROUTINE MAINTENANCE AFTER METAL WAS FOUND IN THE REDUCTION GEARBOX (RGB) SCAVENGE FILTER. 	  INVESTIGATION FOUND THE EXTENT OF THE DAMAGE MADE AN RGB OVERHAUL THE APPROPRIATE WORKSCOPE.  THE SOURCE OF THE METAL 	CONTAMINATION WAS A SPALLED NR 15 BEARING OUTER RACE, WITH SUBSTANTIAL MATERIAL LOSS.  THE FAILURE OF THE NR 15 BEARING 	IS NOT UNCOMMON IN PW120 RGB'S.  THE MORE COMMON CAUSES ARE LIGHTNING STRIKES AND ELECTRICAL EROSION CHAIN PITTING AROUN	D THE OUTER RACES AND/OR ROLLING ELEMENTS OF THE PROPELLER SHAFT BEARINGS.							4	T			E20NE				 
1999052800091	19990528	00091	CE  	1999	5	28	CA990223002      	1	19990209	G	3230	NAS464P5A42	BOLT            		12436001    	CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  					MLG	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			197  					247559			(CAN) AFT DRAG LINK BOLT FOUND WITH THE BOLT HEAD SHEARED OFF.  SUBMITTER STATED THIS IS THE SECOND ONE FOUND IN 200 HOU	RS ON THE SAME AIRCRAFT.					1	H	7	1 	3O	3	O		A4CE    	E5CE				 
1999091700404	19990917	00404	SW  	1999	9	17	CA990223003      	1	19990210	G	6220	204011144003	NUT             		204011140005	BELL  	205   	205A1       	1181414	SW  	LYC   	T53   	T5313B      	41549	NE  					MAIN ROTOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1987 	799  		708471		LEO7654			(CAN) DURING ROUTINE INSPECTION OF THE MAIN ROTOR HEAD, THE DRAG BRACE NUT WAS FOUND CRACKED.  NUT WAS REPLACED.						1	G	7	1 	4U	4	U		H1SW    	E17EA				 
1999060400315	19990604	00315	GL  	1999	6	4	CA990223005      	3	19990216	G	6111	A1851	BEARING         			GRUMAV	G21   	G21A        	3951204	SO  	PWA   	R985  	R985AN14B   	52008	NE  	HARTZL	HCB3R	HCB3R302    	GL  	PROPELLER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				1883 				202281	BB454		(CAN) ROUTINE INSPECTION AT OVERHAUL FOUND THE PROPELLER BLADE BEARING CRACKED AND THE BLADE CORRODED AROUND THE SHANK. 	 THE BEARING WAS REPLACED AND THE PROP BLADE SHANK WAS REWORKED.					1	H	7	2 	3R	3	R		TC654   	5E1	5	C	P28E	 
1999060400316	19990604	00316	CE  	1999	6	4	CA990223006      	1	19990203	G	8120	63272910	TURBOCHARGER    			CESSNA	402   	402CESSNA   	207590K	CE  	CONT  	O520  	TSIO520E    	17040	SO  	MCAULY	3AF32C	3AF32C87    	GL  	NR 2 ENGINE	SEIZED          	W				C	D			ABORTED TAKEOFF         	RETURN TO BLOCK         			R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			CA				932  				L2081249J	7522360		(CAN) ON TAKEOFF ROLL, THE NR 2 ENGINE RPM AND MANIFOLD PRESSURE WERE LIMITED TO 2200 RPM AND 26.  THE TAKEOFF WAS ABORT	ED.   INVESTIGATION FOUND A PIECE OF EXHAUST JAMMED IN THE TURBOCHARGER VANES.   AFTER INSPECTION OF THE EXHAUST SYSTEM,	 AN EXHAUST COUPLING (BELLOWS STYLE) WAS FOUND SHEDDING MATERIAL INTO THE EXHAUST SYSTEM.				1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22E	 
1999060400317	19990604	00317	GL  	1999	6	4	CA990223007      	3	19990209	G	6111	C4902	NUT             													MCAULY	2A34C	D2A34C58    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				529  					811219		(CAN) DURING INSPECTION  FOR AN OIL LEAK, THE PROPELLER BLADE RETENTION NUT WAS FOUND SEVERELY CORRODED.  THE NUT WAS RE	PLACED PER THE MCCAULEY MAINTENANCE MANUAL.															5	C	P3EA	 
1999081200330	19990812	00330	SW  	1999	8	12	CA990223008      	1	19990211	G	7921	H33C32	BEARING         		204062540001	BELL  	205   	205A1       	1181414	SW  	LYC   	T53   	T5313B      	41549	NE  					OIL COOLER	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4    			346		LE07253X			(CAN) HAND TURNING OF ENGINE OIL COOLER DURING INSPECTION REVEALED SOMETHING LOOSE AND NOISEY.   BEARINGS REPLACED THERE	BY RECTIFYING PROBLEM.					1	G	7	1 	4U	4	U		H1SW    	E17EA				 
1999081200331	19990812	00331	WP  	1999	8	12	CA990223009      	1	19990208	G	2510	7260111453	SEAT BELT       			ROBSIN	R44   	R44         	7640120	WP  	LYC   	O540  	O540F1B5    	41532	EA  					CABIN	DETERIORATED    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1276 					L2476640A			(CAN) UPON TRYING TO FASTEN THE AFT LEFT SEAT BELT, THE WEB STITCHING BECAME UNDONE ALLOWING THE WEBBING TO SEPARATE FRO	M THE LOWER ATTACH POINT.  INVESTIGATION INDICATES EITHER IMPROPER STITCHING OR THREAD DETERIORATION.  TOTAL CALENDAR TI	ME IN SERVICE IS APPROX 19 MONTHS.				1	G	7	1 	3O	3	O		H11NM   	E295				 
1999060400318	19990604	00318	EA  	1999	6	4	CA990223010      	2	19990209	G	7322	229550	TUBE            	PRECISION   	MA4SPA      						LYC   	O320  	O320D2A     	41508	EA  					CARBURETOR	MISINSTALLED    	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			W			INADEQUATE Q C            			CR	CRUISE         	1			CA				52   		75026911		RL770339A			(CAN) DURING FLIGHT, THE PILOT NOTICED THROTTLE MOVEMENT WAS OBSTRUCTED.  THE AIRCRAFT LANDED SAFELY.  ON THE GROUND, TH	E THROTTLE OPERATION WAS NORMAL.  ON REMOVAL OF THE AIR INTAKE, MAINTENANCE PERSONNEL FOUND THE PUMP DISCHARGE TUBE ASSE	MBLY SITTING ON THE CARBURETOR AIR BOX.  IT APPEARED TO BE A MANUFACTURER'S DEFECT, WHERE THE TUBE WAS NOT SECURED PROPE	RLY.   AFTER COMING ADRIFT,THE TUBE MUST HAVE FLOATED UP AND RESTRICTED THE CARBURETOR OPERATION.  THIS CAME ON A RE-MAN	UFACTURED ENGINE FROM LYCOMING AND WAS IN OPERATION FOR ONLY 52 HOURS.							3	O			E274				 
1999060400319	19990604	00319	CE  	1999	6	4	CA990223011      	1	19990210	G	2913	66003013	PUMP            			LEAR  	35    	35A         	5170602	CE  										HYDRAULIC SYSTEM	FAILED          	W				A				UNSCHED LANDING         				F	J		FLT CONT AFFECTED         	WARNING INDICATION        		AP	APPROACH       	1			CA			8234 			165387B					(CAN) ON FINAL WITH FULL FLAPS, THE LEFT SPOILER ON REMAINED EXTENDED WHEN CONTROLS WERE RETURNED TO NEUTRAL.   AIRCRAFT	 LANDED OK.  NR 2 HYDRAULIC PUMP HAD FAILED AND CONTAMINATED SYSTEM WITH DEBRIS WHICH CLOGGEDTHE SPOILER FILTER.  THIS C	AUSED SPOILER TO FREEZE IN POSITION.  INVESTIGATION OF PUMP SHOWED THAT ONE OF THE PISTON RETAINER SCREWS WAS MISSING. T	HE SCREW FOUND IN PUMP CAVITY.  IT APPEARS THIS SCREW HAD BACKED OUT OF POSITION AS IT WAS NOT SHEARED AND THREADS IN PL	ATE WERE NOT DAMAGED.  THIS BEING THE CASE, IT WOULD BE CAUSE FOR PUMP FAILURE AS IT WOULD END UP IN PISTON CAVITY.  THE	RE WAS NO EVIDENCE OF A SCREW BEING SAFETY WIRED AS OTHER 3 SCREWS WERE, BUT THIS COULD NOT BE CONFIRMED.	2	L	7	2 	4F				A10CE   					 
1999060400321	19990604	00321	SO  	1999	6	4	CA990223015      	1	19990202	G	3210		BOLTS           		6531902     	PIPER 	PA28  	PA28140     	7102802	SO  	LYC   	O320  	O320E3D     	41508	EA  					LT MLG	SHEARED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			9907 					RL4572227A			(CAN) LEFT MAIN LANDING GEAR CYLINDER MOUNT, 2 BOLTS OF P/N AN525-416-20 AND P/N AN4-11A WERE SHEARED OFF.  THERE WAS NO	 DAMAGE TO THE CYLINDER, BUT THE REMAINING 3 BOLTS WERE FOUND LOOSE.   SUBMITTER SUGGESTED THESE BOLTS BE TORQUE CHECKED	 EVERY 100 HOURS.				1	L	7	1 	3O	3	O		2A13    	E274				 
1999081200333	19990812	00333	NM  	1999	8	12	CA990223016      	1	19990203	G	5753		BRACKET         		652678664   	BOEING	727   	72782       	1384029	NM  	PWA   	JT8   	JT8D7B      	52053	NE  					TE FLAP	BROKEN          	W				O				OTHER                   				F			FLT CONT AFFECTED         			NR	NOT REPORTED   	1			CA								649672			(CAN) INBOARD FLAPS WOULD NOT RETRACT TO LESS THAN 1.5 DEGREES.  FOUND RIGHT INBOARD FLAP FAIRING  FORWARD BEARING SUPPO	RT BRACKET BROKEN.					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999060400323	19990604	00323	EA  	1999	6	4	CA990223018      	2	19990212	G	7421	AGF26	GLOW PLUG       	CHAMPION    		DHAV  	DHC6  	DHC6300     	2802606	EA  	PWA   	PT6   	PT6A27      	52043	EA  					ENGINE	MISSING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			255  					PCE42181			(CAN) DURING ROUTINE INSPECTION, THE ELEMENT WAS FOUND MISSING ON THE LEFT HAND GLOW PLUG.  THE ENGINE WAS INSPECTED FOR	 DAMAGE.   A NEW GLOW PLUG WAS INSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVICE.					1	H	7	2 	3T	4	T	RT	A9EA    	E4EA				 
1999060400325	19990604	00325	GL  	1999	6	4	CA990223020      	2	19990216	G	7210	6899239G	BEARING         								ALLSN 	250C  	250C20B     	03013	GL  					GEARBOX	FAILED          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			CA								CAE835653			(CAN) DURING FLIGHT NR 2, ENGINE HAD A CHIP DETECTOR LIGHT.  RESET WAS CARRIED OUT, BUT THE LIGHT CAME BACK ON.  THE AIR	CRAFT RETURNED TO BASE.   ALL ENGINE PARAMETERS WERE NORMAL.  POST-FLIGHT BOTH THE UPPER AN LOWER CHIP DETECTORS WERE RE	MOVED AND METAL CONTAMINATION WAS PRESENT ON BOTH PLUGS.  THE ENGINE WAS REMOVED FROM THE AIRCRAFT AND INSPECTION REVEAL	ED THE NR 2.5 BEARING WAS DAMAGED ALONG WITH THE SPUR GEAR ADAPTER SHAFT AND THE COUPLING TURBINE TO COMPRESSOR SHAFT, W	HICH WERE DAMAGED FROM BEARING MATERIAL COMING IN CONTACT.							3	U			E4CE				 
1999081200336	19990812	00336	WP  	1999	8	12	CA990224001      	1	19990210	G	6320	369D2512711	RING GEAR       		369D25100901	HUGHES	369   	369D        	4470706	WP  										M/R TRANSMISSION	BROKEN          	W				O				OTHER                   				J			WARNING INDICATION        			LD	LANDING        	1			CA			803  			1810					(CAN) M/R TRANSMISSION NOISE.  CHIP DETECTOR LIGHT WAS NOTICED AND SUBSEQUENT INSPECTION OF CHIP DETECTOR PLUG REVEALED 	SEVERAL METAL FLAKES.  TRANSMISSION WAS REMOVED, DISASSEMBLED AND OUTPUT RING GEAR TOOTH WAS FOUND TO BE COMPLETELY BROK	EN OFF.  TOOTH AND LARGE AMOUNTS OF METAL FOUND AT BOTTOM OF CASE.				1	G	7	1 	3U				H3WE    					 
1999081200337	19990812	00337	EA  	1999	8	12	CA990224002      	1	19990714	G	6310		CLUTCH          		107D2003515 	BOEING	107   	1072        	9420604	EA  	GE    	CT58  	CT581401    	30011	NE  					FREEWHEEL	FAILED          	W				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CL	CLIMB          	1			CA						TA1127		280244L			(CAN) HELICOPTER DROPPED LOGS OFF AT LANDING THEN HEADED UP HILL AT 70 PERCENT TORQUE.   PILOT NOTICED NR 1 ENGINE HAD L	OW POWER OUTPUT, LOW TORQUE, LOW N1, LOW FUEL PRESSURE.   FAN SPEED ON NR 1 ENGINE WAS 107 PERCENT AND NR 2 ENGINE WAS A	T 100 PERCENT.  AIRCRAFT RETURNED.  NR 1 CLUTCH FAILURE SUSPECTED.  AIRCRAFT SHUTDOWN.  TRANSMISSION REPLACED.				2	G	7	2 	4U	4	U		1H16    	1E3				 
1999031200285	19990312	00285	NE  	1999	3	12	CA990224004      	2	19990214	G	7200		ENGINE          			BOEING	727   	72722       	1384002	NM  	PWA   	JT8   	JT8D7B      	52053	NE  					NR 3	FAILED          	W				D				RETURN TO BLOCK         				E			VIBRATION/BUFFET          			TX	TAXI/GRND HDL  	1			CA			55580	201  				653920			(CAN) AS NR 3 ENGINE POWER WAS ADVANCED FOR TAKE-OFF, A VIBRATION WAS NOTICED AT 1.5 EPR, VIBRATION BEGAN AT 45 PERCENT 	N1 WITH THE GREATEST VIBRATION AT 73 PERCENT N1, VIBRATION DECREASED AT 90 PERCENT N1 AND THERE WAS CONTINUOUS EPR FLUCT	UATIONS.  THE AIRCRAFT RETURNED TO BLOCKS.  DURING SUBSEQUENT TROUBLESHOOTING, THE ENGINE OPERATING PERFORMANCE DETERIOR	ATED.  THE AIRCRAFT WAS FERRIED TO THE MAINTENANCE BASE WHERE THE NR 3 ENGINE WAS REPLACED.   PART TC:  43,835.			2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999031200286	19990312	00286	GL  	1999	3	12	CA990224005      	3	19990217	G	6114	C0840126	SPIDER          			CESSNA	180   	180         	2072602	CE  	CONT  	O470  	O470A       	17026	SO  	HARTZL	HC82V	HC82V*      	GL  	PROP HUB	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								401453A	8552N		(CAN) DURING ROUTINE SIX-YEAR CORROSION INSPECTION, USING LIQUID PENETRATIVE INSPECTION METHOD, BOTH LUGS ON THE SIDE OF	 THE PROPELLER HUB WERE FOUND CRACKED.					1	H	7	1 	3O	3	O	NC	5A6     	E273	5	C	P23EA	 
1999031200287	19990312	00287	NE  	1999	3	12	CA990224006      	2	19990215	G	7230	116050004	GEARBOX         			BELL  	205   	205A1       	1181414	SW  	LYC   	T53   	T5313B      	41549	NE  					ENGINE	MALFUNCTIONED   	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				1367 				LE07560A			(CAN) ENGINE VIBRATION AROUND N2 GEARBOX AREA.  THE GEARBOX WAS REPLACED AND THE PROBLEM WAS CURED.						1	G	7	1 	4U	4	U		H1SW    	E17EA				 
1999081200339	19990812	00339		1999	8	12	CA990224007      	1	19990216	G	8200	SPE16549	COVER           	PLESSEY     	SPM18RSMK1  															OUTER CASING	CRACKED         	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						8669					(CAN) ON INSPECTION, MOTOR COVER FOUND NOT TO BE IN CONFORMANCE WITH TATC.  SUP.																			 
1999081200340	19990812	00340		1999	8	12	CA990224008      	1	19990204	G	2421	11053092	ROTOR           	BENDIX      	28B14117B   															ALTERNATOR	OVERMAGNETIZED  	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA				110  		R59					(CAN) AC GENERATOR VOLTAGE WAS 39.2 V, TOLERENCE IS 23 TO 25 V.  BEARINGS NOT MANUFACTURED BY RECOMMENDED MANUFACTURER.																			 
1999081200341	19990812	00341	CE  	1999	8	12	CA990224009      	1	19990210	G	6120	993800075	CONTROL CABLE   			BEECH 	100   	A100        	1152915	CE  	PWA   	PT6   	PT6A28      	 	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	PROP CONTROL	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			10711					PCE50218	BUA21617		(CAN) RIGHT HAND PROPELLER CONTROL CABLE FOUND BROKEN APPROXIMATELY 14 INCHES FROM THE ROD END UNDER THE PEDESTAL.						1	L	7	2 	3T	4	T	 	A14CE   	E4EA	6	C	P15EA	 
1999081200342	19990812	00342	CE  	1999	8	12	CA990224010      	1	19990128	G	3310	RC20GF151K	RESISTOR        			CESSNA	401   	401B        	207590E	CE  	CONT  	O520  	TSIO520EB   	17040	SO  					LIGHT	BURNT           	W				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			CR	CRUISE         	1			CA			9327 					183525H			(CAN) IN CRUISE, A SMALL AMOUNT OF SMOKE NOTICED FOLLOWED BY BURNT SMELL.  SMOKE COMING FROM CENTER INSTRUMENT PANEL.  S	MOKE QUIT AND ALL  SYSTEMS SEEMED OK.  ON GROUND, FOUND THE COPILOT'S POST LIGHTS NOT WORKING.  RESISTOR MOUNTED ON THE 	BACK OF CIRCUIT RHEOSTAT FOUND BURNT.				1	L	7	2 	3O	3	O		A7CE    	E8CE				 
1999081200343	19990812	00343	CE  	1999	8	12	CA990224011      	1	19990216	G	5610	5042006931	WINDSHIELD      			BEECH 	100   	100BEECH    	1152916	CE  	PWA   	PT6   	PT6A28      		EA  					COCKPIT	CRACKED         	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			CA			3140 					PCE50045			(CAN) IN CRUISE AT 22,000 FEET, A LOUD SNAP HEARD COMING FROM PILOT'S WINDSHIELD.   INNER PANE FOUND CRACKED.						1	L	7	2 	3T	4	T		A14CE   	E4EA				 
1999081200344	19990812	00344	NM  	1999	8	12	CA990224012      	1	19990210	G	2750	745581A	CONTROL CABLE   			DHAV  	DHC8  	DHC8102     	2809003	NM  										TE FLAP	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						3173					(CAN) OPERATOR REPORTED FLAPS JAMMED AT 4 DEGREES.  FOUND THE LEFT SECONDARY CABLE TWISTED WITH ONE STRAND LOOSE JAMMING	 THE CABLE IN THE SLEEVE.					2	H	7	2 	4T			RT	A13NM   					 
1999031200288	19990312	00288	GL  	1999	3	12	CA990224013      	3	19990217	G	6111		BLADE           			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	PROPELLER	MISMANUFACTURED 	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				6478 				L134676	729740		(CAN) PROPELLER BLADE WAS MEASURED AND FOUND TO BE BELOW MINIMUM WIDTH.   PROPELLER WAS REMOVED FROM SERVICE.						1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
1999031200289	19990312	00289	GL  	1999	3	12	CA990224014      	3	19990218	G	6110	57C083842	CLAMP           													HARTZL	HCB3Z	HCB3Z201    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA									AF534		(CAN) PROPELLER DISMANTLED FOR CORROSION INSPECTION, FOUND CLAMPS PITTED INTERNALLY BEYOND REPAIRABLE LIMITS, CLAMPS REP	LACED.															5	C	P907	 
1999031200290	19990312	00290	GL  	1999	3	12	CA990224015      	3	19990218	G	6114	57A1851	BEARING         													HARTZL	HCB3Z	HCB3Z201    	GL  	PROP HUB	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA									AF534		(CAN) PROPELLER DISMANTLED FOR INSPECTION, BLADE BEARINGS WERE FOUND CORRODED.  THE BEARINGS WERE REPLACED.																5	C	P907	 
1999081200345	19990812	00345	SO  	1999	8	12	CA990224016      	1	19990217	G	3231	AN3H10A	BOLT            		4438600     	PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  					MLG	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L31461			(CAN) THREE LANDING GEAR BOLTS FOUND BROKEN AND 2 OTHERS FOUND LOOSE ON THE DIRECTION ARM.						1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999031200291	19990312	00291	NE  	1999	3	12	CA990224017      	2	19990211	G	7200		ENGINE          								GE    	CF6   	CF680C2A5   		NE  					NR 2	FAILED          	W				C				ABORTED TAKEOFF         				E	X	J	VIBRATION/BUFFET          	ENGINE FLAMEOUT           	WARNING INDICATION        	TO	TAKEOFF        	1			CA			19590					705102			(CAN) NR 2 ENGINE FAILED ON ROTATION.  NO THROTTLE RESPONSE.  SOME METAL PARTICLES FOUND IN THE EXHAUST.  ENGINE REMOVED	.  WAITING FOR SHOP REPORT.   PART TC:  8,624.										4	F			E13NE				 
1999031200292	19990312	00292		1999	3	12	CA990224018      	4	19990224	G	3425		PFD             			CNDAIR	CL600 	CL6002B19   		EA  										RT & LT COCKPIT	FAILED          	W				L				ABORTED APPROACH        				O			OTHER                     			AP	APPROACH       	1			CA											(CAN) FOLLOWING A GO-AROUND FOR A WIND SHEAR WARNING, THE AIRCRAFT WAS STRUCK BY LIGHTNING.  AIRCRAFT AT 4,500 FEET.  BO	TH PFD'S WENT BLANK AND THE STANDBY AIRSPEED INDICATOR WAS REPORTED AS SPINNING.  PILOT REPORTED 'MILLIONS OF MESSAGES',	 BUT COULD NOT RECALL ANY OF THEM.  EMERGENCY LIGHTS CAME ON IN CABIN.  PILOT DECLARED EMERGENCY.   APPROXIMATELY 45 SEC	ONDS AFTER LIGHTNING STRIKE, THE PFD'S CAME BACK ON AND SHORTLY AFTER OR POSSIBLY AT SAME TIME (PILOT UNSURE), THE ASI S	TOPPED SPINNING.  AIRCRAFT LANDED OK 2 TO 3 MINUTES AFTER STRIKE.  ON THE GROUND, ALL SYSTEMS FUNCTIONED NORMALLY.		2	L	7	2 	4F			RT	A21EA   					 
1999081200346	19990812	00346	CE  	1999	8	12	CA990224019      	1	19990209	G	7120	075100331	MOUNT           			CESSNA	185   	A185F       	2072821	CE  	CONT  	O520  	IO520D      	17032	SO  	MCAULY	2A34C	D2A34C58    	GL  	ENGINE	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2421 					566127	761037		(CAN) AFTER REMOVING THE ENGINE COWLING, THE ENGINE SUPPORT WAS FOUND BROKEN.						1	H	7	1 	3O	3	O		3A24    	E5CE	5	C	P3EA	 
1999081200347	19990812	00347	SO  	1999	8	12	CA990224020      	1	19990207	G	3246	LM501310	BEARING         		45504005    	PIPER 	PA31  	PA31350     	7103110	SO  										MLG WHEEL	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			257  								(CAN) GEAR BEARING SEIZED.  SUSPECT THE UNIT WAS OVERTORQUED.  AUTO BEARING FAILURE LED TO DAMAGE TO WHEEL ASSEMBLY.						1	L	7	2 	3O				A20SO   					 
1999081200348	19990812	00348	NE  	1999	8	12	CA990226001      	3	19990219	G	6111	57A32042	SET SCREW       			BEECH 	1900  	1900D       	1154162	CE  						HARTZL	HCE4A	HCE4A3I     	NE  	PROPELLER BLADE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1788 						MJ801		(CAN) THE PROPELLER BLADE SET SCREW HAD WORN ENOUGH TO ALLOW BLADE MOVEMENT IN EXCESS OF .8750 INCH.						2	L	7	2 	4T			RT	A24CE   		5	C	P10NE	 
1999081200352	19990812	00352	CE  	1999	8	12	CA990226005      	1	19990221	G	5280	11581006052	DOOR            			BEECH 	100   	A100        	1152915	CE  	PWA   	PT6   	PT6A28      		EA  					MLG	DAMAGED         	W				O				OTHER                   				O			OTHER                     			CL	CLIMB          	1			CA			7387 					PCE50673			(CAN) DURING GEAR RETRACTION, THE GEAR INTRANSIT WARNING LIGHTS STAYED ON.  GEAR CYCLED WITH NO RESPONSE.   EMERGENCY EX	TENSION USED.  GEAR DOOR LEFT HAND MAIN INBOARD FOUND DAMAGED BY WHEEL ASSY.  WHEN GEAR RETRACTED, MOTOR CIRCUIT BREAKER	 HAD ALSO TRIPPED.  INVESTIGATION FOUND THE LEFT MAIN ATTACH LINE BRACKET INSTALLED AND IMPROPERLY ALIGNED FROM MANUFACT	URER.			1	L	7	2 	3T	4	T		A14CE   	E4EA				 
1999081200353	19990812	00353	NE  	1999	8	12	CA990226006      	2	19990202	G	7261	4022T27G22	PUMP            			CNDAIR	CL600 	CL6002A12   	1900304	EA  	GE    	CF34  	CF341A      		NE  					NR 2 ENGINE	MALFUNCTIONED   	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			CA			9827 					350146			(CAN) NR 2 ENGINE LOW OIL PRESSURE LIGHT IN-FLIGHT.  POST-FLIGHT INSPECTION FOUND THE NR 2 ENGINE OIL PUMP WAS INOPERATI	VE.					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999081200354	19990812	00354	EU  	1999	8	12	CA990226007      	1	19990222	G	2611	CG7G01	SMOKE DETECTOR  			AIRBUS	300   	A300B4203   	3930306	EU  	GE    	CF6   	CF650C2     	30018	NE  					CABIN	FAILED          	W				A				UNSCHED LANDING         				N			FALSE WARNING             			CL	CLIMB          	1			CA								455827			(CAN) AFT BULKHEAD SMOKE WARNING ILLUMINATED, AIRCRAFT SAFELY LANDED.   INVESTIGATION REVEALED CONDENSATION IN SMOKE DET	ECTOR DUCT LEADING TO FAILURE OF UNIT.					2	L	7	2 	4F	4	F	RT	A35EU   	E23EA				 
1999081200356	19990812	00356	SO  	1999	8	12	CA990226010      	2	19990218	G	8530	530348	PISTON          		SA10200A20P 	CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  					ENGINE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1088 			J9819220		670607A			(CAN) DURING INSPECTION THE COMPRESSION ON NR 1 CYLINDER WAS 67/80 AND THERE WERE NON-MAGNETIC PARTICLES IN THE OIL FILT	ER.  CYLINDER NR 1 WAS REMOVED AND MANY PARTS OF THE PISTON HAD DISINTEGRATED AT THE TOP COMPRESSION RING.  THE RING WAS	 BROKEN.  THE TOLERANCE OF 0.010 INCH WAS FAR EXCEEDED, MAYBE IT WAS FRETTING BY THE TOP RING THAT CAUSED THE INCIDENT. 	 THE CYLINDER AND PISTON WERE REPLACED.			1	H	7	1 	3O	3	O		3A19    	E252				 
1999081200357	19990812	00357	EA  	1999	8	12	CA990301001      	1	19990208	G	3246	9543077	WHEEL           		9543051     	DHAV  	DHC6  	DHC6100     		EA  	PWA   	PT6   	PT6A20A     	52043	EA  					MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						77599		21991			(CAN) WHEEL FOUND CRACKED.  CRACK 20 CM LONG HAD OPENED ABOUT 6 MM.  THE CRACK HAD PASSED THROUGH TWO FINS AND WAS PROGR	ESSING TOWARDS THE OUTSIDE OF THE RIM.  TIRE DID NOT DEFLATE.  NO MECHANICAL DAMAGE IN AREA OF CRACK.					1	H	7	2 	3T	4	T		A9EA    	E4EA				 
1999081200358	19990812	00358	EU  	1999	8	12	CA990301002      	1	19990203	G	4920	T62T40C1	BEARING         	SOLAR       	160180201   	BRAERO	DH125 	HS125700A   	4230170	EU  	GARRTT	TFE731	TFE7313R    	01518	WP  					TURBINE	SEIZED          	W				E	F			ENGINE SHUTDOWN         	ACTIVATE FIRE EXT.      			P			NO WARNING INDICATION     			TX	TAXI/GRND HDL  	1			CA			316  			785501		P84322			(CAN) APU SHUT DOWN DUE TO ROTOR GROUP SEIZURE.   THE BEARING WAS A CORRECT ONE, AND FAILED MUCH TOO EARLY.						2	L	7	2 	4F	4	F		A3EU    	E6WE				 
1999081200359	19990812	00359	EA  	1999	8	12	CA990301003      	1	19990225	G	7732	079316	SCREW           		6015091013  	CNDAIR	CL600 	CL6002B19   		EA  										VIBRATE ANALYZER	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						079316					(CAN) ENGINE VIBRATION SIGNAL CONDITIONING UNIT REMOVED TO DO SB'S SCREWS FOUND ROLLING AROUND LOOSE INSIDE SEVERAL ELEC	TRONIC COMPONENTS, CAPACITORS, TRANSISTORS, ETC., WERE FOUND BURNED ON ONE CIRCUIT BOARD.  LIKELY THE RESULT OF THE LOOS	E SCREW.				2	L	7	2 	4F			RT	A21EA   					 
1999081200362	19990812	00362	EA  	1999	8	12	CA990301007      	1	19990301	G	3320	BB100200337	LIGHT           			CNDAIR	CL600 	CL6002B19   		EA  										ROW 8	FAILED          	W				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			CL	CLIMB          	1			CA											(CAN) SHORTLY AFTER DEPARTURE, A PASSENGER NOTED SMELL OF SMOKE.  SMOKE SEEN BY CABIN ATTENDANT COMING FROM AROUND PASSE	NGER SERVICE UNIT. EMERGENCY DECLARED AND AIRCRAFT LANDED OK.  FIRE CREWS MET AIRCRAFT AND IDENTIFIED SMOKE AS COMING FR	OM SIDEWALL LIGHTING IMMEDIATELY ABOVE THE RIGHT HAND PASSENGER DOOR.  NO EXTINGUISHER REQUIRED.  INSPECTION FOUND ONE W	IRE BURNED AT LIGHTING FIXTURE.			2	L	7	2 	4F			RT	A21EA   					 
1999081200366	19990812	00366	CE  	1999	8	12	CA990301012      	1	19990216	G	2750	0523920	BEARING         		052390135   	CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	TE FLAP	BROKEN          	W				A				UNSCHED LANDING         				F			FLT CONT AFFECTED         			CL	CLIMB          	1			CA			2718 					RL11076	IA016		(CAN) ONE FLAP ROLLER SEIZED, EVEN THOUGH IT WAS COVERED IN GREASE.  THE NEEDLES WERE MESSED UP AND THE BEARING WENT FLA	T AS A RESULT.					1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
1999081200367	19990812	00367	WP  	1999	8	12	CA990303001      	1	19990210	G	6320	369D2512513	BEARING         	WESTERNGEAR 	369D25100901	HUGHES	369   	369D        	4470706	WP  										M/R TRANSMISSION	TIGHT           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1250 			1810					(CAN) DURING REPAIR ON MAIN ROTOR TRANSMISSION, IT WAS NOTICED THAT THE ROLLER BEARING 309025146 INNER RACE HAD MOVED BA	CK FROM ITS ORIGINAL PRESSED ON POSITION.  IT WAS FOUND TO BE TIGHT AGAINST THE T/R OUTPUT PINION RETAINING RING.					1	G	7	1 	3U				H3WE    					 
1999070900370	19990709	00370	GL  	1999	7	9	CA990303002      	2	19990215	G	7200		ENGINE          			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE BAY	FAILED          	W				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			CA								CAE833603			(CAN) THE PILOT WAS IN SLOW CRUISE WHEN THE ENGINE OUT LIGHT ACTIVATED.  THE ENGINE HAD DECELLERATED TO FLIGHT IDLE.  SI	NCE THE HELICOPTER WAS ONLY 300 FEET ABOVE GROUND, IT SUSTAINED BELLY DAMAGE ON THE ENSUING HARD LANDING.					1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999081200368	19990812	00368	GL  	1999	8	12	CA990303003      	3	19990219	G	6114	A2202	HUB             			PIPER 	PA34  	PA34200T    	7103406	SO  	CONT  	O360  	TSIO360EB   	17025	SO  	HARTZL	HCC2Y	BHCC2YF2    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				2097 				234636R	AN5582E		(CAN) INSPECTION FOUND CORROSION ON THE HUB TO ENGINE MOUNTING FLANGE.  THE BEARING RACES WERE ALSO DENTED BY THE BALLBE	ARINGS.  THE HUB WAS OVERHAULED AND THE BEARINGS WERE REPLACED.					1	L	7	2 	3O	3	O		A7SO    	E9CE	5	C	P920	 
1999081200369	19990812	00369	NE  	1999	8	12	CA990303004      	2	19990129	G	7240	311565201	CASE            			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					GAS GENERATOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			5978 					PCE114064			(CAN) ON INSPECTION, SEVERE CORROSION WAS FOUND AT THE 6 O'CLOCK POSITION ON THE GAS GENERATOR CASE. THE CORROSION WAS S	O SEVERE THAT IT RESULTED IN PIN HOLES IN THE GAS GENERATOR CASE.					2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999081200370	19990812	00370	EA  	1999	8	12	CA990303005      	1	19990303	G	5711	S6628	SPAR            			CNDAIR	CL215 	CL2151A10   		EA  										WS 51	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2532 								(CAN) RIGHT HAND LOWER SPAR CAP FOUND CRACKED PER AD CF-92-26 AND SB 215-A454.  CRACK FOUND BY ULTRASONIC INSPECTION.						2	H	7	2 	4R				A14EA   					 
1999081200371	19990812	00371	EA  	1999	8	12	CA990303006      	2	19990219	G	8520	72877	TAPPET          								LYC   	O360  	AEIO360A1B6 	41514	EA  					ENGINE	SPALLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2496 					L2662451A			(CAN) DURING SCHEDULED INSPECTION, MODERATE AMOUNT OF METAL WAS FOUND IN THE OIL FILTER.  NR 2 AND NR 4 CYLINDERS WERE R	EMOVED FOR INVESTIGATION AND IT WAS OBSERVED NR 1 AND NR 2 CYLINDERS INTAKE CAMSHAFT LOBES WERE ABNORMALLY WORN AND THE 	CAM FOLLOWERS WERE BADLY SPALLED.  THE ENGINE WAS REMOVED FOR REPAIR.									3	O			1E10				 
1999081200372	19990812	00372	EA  	1999	8	12	CA990303007      	2	19990219	G	8520	LW18840	CAMSHAFT        								LYC   	O360  	AEIO360A1B6 	41514	EA  					ENGINE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2496 					L2662451A			(CAN) DURING SCHEDULED INSPECTION, MODERATE AMOUNT OF METAL WAS FOUND IN THE OIL FILTER.  NR 2 AND NR 4 CYLINDERS WERE R	EMOVED FOR INVESTIGATION AND IT WAS OBSERVED NR 1  NR 2 CYLINDERS INTAKE CAMSHAFT LOBES WERE ABNORMALLY WORN AND THE CAM	 FOLLOWERS WERE BADLY SPALLED.  THE ENGINE WAS REMOVED FOR REPAIR.									3	O			1E10				 
1999081200373	19990812	00373	EU  	1999	8	12	CA990303008      	1	19990219	G	2750	ONL312014	BOLT            	MORAVN      	Z4243430000 	ZLIN  	242   	Z242L       	9970204	EU  										TE FLAP	BENT            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			946  								(CAN) AS A RESULT OF PREVIOUS DISCOVERY OF A BENT FLAP BELLCRANK BOLT, A REPEAT INSPECTION WAS IMPLEMENTED.   IT WAS THE	N REVEALED THAT THE LEFT FLAP BOLT WAS SLIGHTLY BENT.  STUDENTS WERE REMINDED ABOUT THE SPEED LIMITATION FOR FLAP EXTENS	ION.				1	L	7	1 	3O			0	A76EU   					 
1999081200374	19990812	00374	SO  	1999	8	12	CA990303009      	1	19990219	G	3260	89291003	SWITCH          			PIPER 	PA44  	PA44180     	7104402	SO  										MLG	INTERMITTENT    	W				L				ABORTED APPROACH        				N			FALSE WARNING             			AP	APPROACH       	1			CA			536  								(CAN) AFTER UNDERCARRIAGE SELECTED DOWN, THE LEFT MAIN GEAR SAFE LIGHT DID NOT COME ON, BUT THE GEAR UNSAFE LIGHT DID GO	 OUT.  GEAR CYCLED AND THE SAFE LIGHT ON EVENTUALLY.   INVESTIGATION DETERMINED THAT THE CONTACTS FOR THE GEAR SAFE LIGH	T WERE DEFECTIVE.  THIS SWITCH HAS THREE SETS OF CONTACTS, ONE FOR THE HYDRAULIC PUMP, ONE FOR GEAR UNSAFE, AND ONE FOR 	GEAR SAFE LIGHT.			1	L	7	2 	3O				A19S0   					 
1999081200376	19990812	00376	NM  	1999	8	12	CA990303011      	1	19990210	G	2782	2145011	ACTUATOR        		2145011     	BOEING	727   	727260      		NM  	PWA   	JT8   	JT8D17      	52049	NE  					LE FLAP	JAMMED          	W				O				OTHER                   				F			FLT CONT AFFECTED         			LD	LANDING        	1			CA						5088		689961			(CAN) AFTER LANDING, NR 7 RIGHT SPOILER STAYED UP.  ACTUATOR REPLACED.						2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
1999082100046	19990821	00046	SW  	1999	8	21	CA990303012      	1	19990224	G	5302	714771	FRAME           			BBAVIA	8     	8GCBC       	1220803	SW  	LYC   	O360  	O360C2E     	41514	EA  					TAILBOOM	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L2487836A			(CAN) THE FRAME  FOUND CRACKED ALL THE WAY AROUND APPROXIMATELY 2 INCHES UP FROM THE BOTTOM.						1	H	7	1 	3O	3	O		A21CE   	E286				 
1999081200377	19990812	00377	SW  	1999	8	12	CA990303013      	1	19990224	G	5302	7146061	FRAME           			BBAVIA	8     	8GCBC       	1220803	SW  	LYC   	O360  	O360C2E     	41514	EA  					TAILBOOM	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L1937436A			(CAN) CRACK FOUND AT WELD AROUND FRAME.  THIS IS THE TAILWHEEL SPRING FORWARD ATTACH POINT.  ALSO P/N 7-1470-36.						1	H	7	1 	3O	3	O		A21CE   	E286				 
1999081200378	19990812	00378		1999	8	12	CA990303014      	1	19990226	G	3500	503201	DIAPHRAGM       	SCOTT       	5500C1ABF23A															OXYGEN REGULATOR	BURNT           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						69172					(CAN) THE RUBBER DIAPHRAGM INSIDE THE OXYGEN CYLINDER REGULATOR WAS FOUND REDUCED TO ASH.  SUBMITTER SUSPECTS THAT LAST 	TIME THE REGULATOR HAD BEEN OVERHAULED, THE DIAPHRAGM WAS CONTAMINATED WITH SOME COMBUSTIBLE MATERIAL, OIL OR GREASE FOR	 EXAMPLE, AND WHEN EXPOSED TO SOME PRESSURIZED OXYGEN,THERE WAS AN INSTANCE OF SPONTANEOUS COMBUSTION INSIDE THE REGULAT	OR.  SUBMITTER STATED THIS COULD BE A VERY SERIOUS PROBLEM.																 
1999081200383	19990812	00383	CE  	1999	8	12	CA990303019      	1	19990226	G	5412		FIREWALL        			CESSNA	172   	172R        	2072401	CE  										FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			405  								(CAN) A CRACK FOUND ON THE FIRWALL RADIATING FROM THE RIVETS UNDERNEATH THE RIGHT HAND COWL MOUNT BRACKET.						1	H	7	1 	3O			NT	3A12    					 
1999081200384	19990812	00384	SW  	1999	8	12	CA990308002      	1	19990225	G	6240	206076373001	TACH GENERATOR  			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C30      	03013	GL  					ROTOR	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								CAE890139			(CAN) WHEN HYDRAULIC PUMP AND TACHOMETER GENERATOR WERE REMOVED TO REPLACE TRANSMISSION OIL PUMP SEAL, THE TACH GENERATO	R HAD TO BE PRIED OFF.  THE DRIVE SPLINES ON THE TACH WERE WORN RAZOR SHARP, FURTHER WEAR WOULD HAVE RESULTED IN TACH GE	NERATOR PROBLEM.  INVESTIGATION FOUND THE WRONG LUBRICANT WAS USED TO LUBRICATE THE SPLINES.  BELL 204-040-755-005 WAS U	SED INSTEAD OF ANTI-CORROSION COMPOUND MIL-A-907.			1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999081200386	19990812	00386	SO  	1999	8	12	CA990308004      	2	19990220	G	8530		PISTON          			CESSNA	421   	421C        	2076016	CE  	CONT  	O520  	GTSIO520L   	17032	SO  	MCAULY	3FF32	3FF32C501   	GL  	ENGINE	FAILED          	W				E	B	A		ENGINE SHUTDOWN         	EMER. DESCENT           	UNSCHED LANDING         		E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CL	CLIMB          	1			CA				1400 				604412	802942		(CAN) PILOT REPORTED VIBRATION FOLLOWED BY LOSS OF OIL PRESSURE.  IN-FLIGHT SHUTDOWN CARRIED OUT. POST-FLIGHT INVESTIGAT	ION INDICATED PISTON FAILURE DUE TO DETONATION.  FURTHER REPORT TO FOLLOW.					1	L	7	2 	3O	3	O		A7CE    	E7CE	5	C	P45GL	 
1999081200387	19990812	00387	EA  	1999	8	12	CA990308005      	2	19990210	G	8530		CYLINDER        			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					NR 2 ENGINE	SEPARATED       	W				E	D			ENGINE SHUTDOWN         	RETURN TO BLOCK         			E			VIBRATION/BUFFET          			TX	TAXI/GRND HDL  	1			CA				837  				L206368A			(CAN) PILOT REPORTED ENGINE BACKFIRING ON START/TAXI, ENGINE WAS RUN FOR 30 MINUTES.  AFTER ENGINE SHUTDOWN, INSPECTION 	FOUND THE NR 6 CYLINDER HEAD, ON THE NR 2 ENGINE WAS SEPARATED FROM THE BARREL.					1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999081200388	19990812	00388	SW  	1999	8	12	CA990308006      	1	19990228	G	7921	J33C32	BEARING         		204062540001	BELL  	205   	205A1       	1181414	SW  	LYC   	T53   	T5313B      	41549	NE  					COOLER BLOWER	LACK OF LUBE    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			420  			130		LE07560A			(CAN) NOTICEABLE NOISE COMING FROM ENGINE OIL COOLER BLOWER.  BEARINGS INSPECTED AND FOUND DRY.  INSTALLATION OF NEW BEA	RINGS ELIMINATED EXCESS NOISE.					1	G	7	1 	4U	4	U		H1SW    	E17EA				 
1999081200389	19990812	00389		1999	8	12	CA990308007      	4	19990114	G	2297		WIRE            			CESSNA	172   	172R        	2072401	CE  										AUTOPILOT	CHAFED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) AUTOPILOT WOULD NOT ENGAGE.  FOUND THE A/P DISCONNECT WIRING OPEN FROM THE DISCONNECT SWITCH TO THE A/P COMPUTER. 	 BROKEN WIRE BEHIND INSTRUMENT PANEL.  WIRING BUNDLE CHAFING BEHIND PILOT'S PANEL.					1	H	7	1 	3O			NT	3A12    					 
1999081200390	19990812	00390	EA  	1999	8	12	CA990308008      	2	19990203	G	8540	LW10292	IDLER GEAR      			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					NR 2 ENGINE	BROKEN          	W				A				UNSCHED LANDING         				R	A	E	PARTIAL RPM/PWR LOSS      	FLAME/FIRE                	VIBRATION/BUFFET          	CR	CRUISE         	1			CA			1312 					L15868A			(CAN) DURING FLIGHT, THE NR 2 ENGINE BEGAN TO LOSE POWER.   AFTER AN UNSCHEDULED LANDING, THE ENGINE QUIT ON GROUND.  IN	SPECTION FOUND DAMAGED GEARS IN THE REAR GEARBOX, TEETH MISSING ON THE DAMAGED GEARS CAUSED THE CAMSHAFT TO STOP TURNING	, THIS LED TO ENGINE FAILURE.  REASON FOR GEAR FAILURE IS UNKNOWN.  THE ENGINE WAS SENT FOR REPAIR.				1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999081200391	19990812	00391	CE  	1999	8	12	CA990308009      	1	19990225	G	3397	L45B22	WIRE            			BEECH 	100   	A100        	1152915	CE  	PWA   	PT6   	PT6A28      	 	EA  					COCKPIT	FAILED          	W				H				DEACTIVATE SYST/CIRCUITS				B			SMOKE/FUMES/ODORS/SPARKS  			NR	NOT REPORTED   	1			CA								PCE51524			(CAN) WHEN STARTING THE AIRCRAFT, SMOKE NOTED IN THE CABIN.  AIRCRAFT SHUTDOWN.  INSPECTION FOUND A BURNT WIRE FROM THE 	THRESHOLD LIGHT FUSE TO SWITCH; AND TO BAGGAGE COMPARTMENT LIGHT SWITCH TO AFT DOME LIGHT.  AFT DOME LIGHT SOCKET WAS BR	OKEN, POSSIBLY FROM LOADING BAGGAGE.  THE POSITIVE POST WAS OFF AND GROUNDED. HOWEVER, THE FUSE DID NOT BLOW RIGHT AWAY 	CAUSING THE WIRE TO MELT.  FUSE TO BE SENT TO MANUFACTURER FOR ANALYSIS.			1	L	7	2 	3T	4	T	 	A14CE   	E4EA				 
1999081200392	19990812	00392	NE  	1999	8	12	CA990308010      	2	19990219	G	7260	602070001	GEARBOX         			BRAERO	748   	HS7482B     	1500248	EU  	RROYCE	DART  	DART5352    	54509	NE  					ENGINE	MAKING METAL    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				3316 				15114			(CAN) DURING REMOVAL OF THE ALTERNATOR, FERROUS METAL WAS FOUND IN THE ALTERNATOR AREA.  THE GEARBOX WAS REPLACED.						2	L	7	2 	3T	4	T		A24EU   	E297				 
1999081200393	19990812	00393	EA  	1999	8	12	CA990308012      	2	19990225	G	7240	3023779	DIFFUSER        								PWA   	PT6   	PT6A50      	52043	EA  					ENGINE	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) DURING AN HSI, A DIFFUSER TUBE WAS FOUND BROKEN.  THE ENGINE WAS SENT FOR REPAIR.											4	T			E4EA				 
1999081200394	19990812	00394	SO  	1999	8	12	CA990308013      	1	19990301	G	2913	3058687	CENTER PLATE    	LFE         	1213HBG310  	PIPER 	PA31  	PA31310     	7103103	SO  										HYDRAULIC PUMP	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						OE91071					(CAN) AFTER PREMATURE FAILURE OF HYDRAULIC PUMP, INSPECTION FOUND THE CENTER PLATE CRACKED.						1	L	7	1 	3O			RT	A20SO   					 
1999032600143	19990326	00143	EA  	1999	3	26	CA990308014      	1	19990217	G	5530	C2FS4045A	CHANNEL         		C2FS535     	DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					BS 228	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			11438					17429			(CAN) CHANNEL RIVETED TO BULKHEAD STA 228 TO REINFORCE THE PICK-UP OF FOUR BOLTS FOR RUDDER POST WAS FOUND CRACKED.  NEW	 PART INSTALLED. AREA ADDRESSED BY CF-98-38.					1	H	7	1 	3R	3	R		A806    	5E1				 
1999081200396	19990812	00396	NM  	1999	8	12	CA990308017      	1	19990215	G	3233	651783012	ACTUATOR        		651783012   	BOEING	727   	727277      	138408S	NM  	PWA   	JT8   	JT8D17      	52049	NE  					LT MLG	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA						DA2437					(CAN) LEFT MAIN GEAR ACTUATOR LEAKING,  REPLACED.						2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
1999081200399	19990812	00399	EU  	1999	8	12	CA990308021      	1	19990225	G	7712		TSCU            	BFGOODRICH  		AEROSP	ATR42 	ATR42300    	8680920	EU  	PWA   	120   	PW120       		NE  	HAMSTD	14SF	14SF5       	NE  	NR 2 ENGINE	ERRATIC         	W				C				ABORTED TAKEOFF         				N			FALSE WARNING             			TO	TAKEOFF        	1			CA								120503	MFG870702		(CAN) ON TAKEOFF, NR 2 ENGINE BECAME UNCONTROLLABLE.  TAKEOFF WAS REJECTED AND THE AIRCRAFT RETURNED TO BLOCKS.  THE TOR	QUE SIGNAL CONDITIONING UNIT (TSCU) WAS REPLACED AND THE SYSTEM WAS CHECKED SERVICEABLE.					2	H	7	2 	4T	4	T	RT	A53EU   	E20NE	6	C	P7NE	 
1999081200400	19990812	00400	CE  	1999	8	12	CA990308022      	1	19990225	G	3230		SPACER          			CESSNA	402   	402B        	207590P	CE  										LT MLG	MISSING         	W				O				OTHER                   				W			INADEQUATE Q C            			LD	LANDING        	1			CA											(CAN) PILOT APPARENTLY HAVING A BRAKE PROBLEM AFTER LANDING.  IT TURNED OUT THAT THE LEFT HAND GEAR LINKS OR SCISSORS HA	D SEPARATED AS IF DISCONNECTED.  THE OVERSIZE RETAINING WASHER WAS MISSING.					1	L	7	2 	3O				A7CE    					 
1999082700101	19990827	00101	EA  	1999	8	27	CA990308023      	2	19990218	G	7530		BOLT            		B1741       	ROBSIN	R22   	R22BETA     		NM  	LYC   	O320  	O320B2C     	41508	EA  					COMPRESSOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				1686 				L1445639A			(CAN) CRACKS FOUND AT BOLT HOLES ON FAN HUB.						1	G	7	1 	3O	3	O		H10WE   	E274				 
1999081200411	19990812	00411	EA  	1999	8	12	CA990308040      	1	19990217	G	5320	C2FS535	CHANNEL         			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					BS 228	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			15801					42111907			(CAN) THE CHANNEL, RIVETED TO BULKHEAD STA 228 TO REINFORCE PICKUP OF FOUR BOLTS FOR RUDDER POST, FOUND CRACKED.  NEW ST	YLE CHANNEL ASSY INSTALLED. NEW P/N C2 FS4045A WHICH HAS DOUBLERS RIVETED TO OUTER EDGES.					1	H	7	1 	3R	3	R		A806    	5E1				 
1999081200442	19990812	00442	SO  	1999	8	12	CA990310034      	1	19990118	G	7810	LW120935	CLAMP           			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					EXHAUST	MISSING         	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		CL	CLIMB          	1			CA								L11568			(CAN) DURING CLIMB-OUT,THE NR 2 ENGINE SUDDENLY LOST ABOUT 12 OF MANIFOLD PRESSURE. THE ENGINE WAS FEATHERED AND THE AIR	CRAFT RETURNED TO ITS POINT OF DEPARTURE.  INSPECTION REVEALED THE EXHAUST CLAMP, ON THE LEFT CYLINDER BANK EXHAUST TUBE	/TURBO TRANSITION ASSEMBLY, MISSING. THE MISSING CLAMP CAUSED LOSS OF EXHAUST GAS PRESSURE TO THE TURBOCHARGER; AND HENC	E, THE ENGINE TO GO TO NORMALLY ASPIRATED.  ALL PARTS WERE ACCOUNTED FOR EXCEPT FOR THE CLAMP WHICH WAS REPLACED. THE EN	GINE WAS GROUND RUN SERVICEABLE AND THE AIRCRAFT WAS RETURNED TO SERVICE.		1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999081200444	19990812	00444	SO  	1999	8	12	CA990310036      	1	19990222	G	8120	4066109020	TURBOCHARGER    			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  					NR 2 ENGINE	SEIZED          	W				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			CA				283  				L726561A			(CAN) DURING CLIMB-OUT, THE NR 2 ENGINE BEGAN TO LOSE POWER AND WENT NORMALLY ASPIRATED. THE AIRCRAFT DIVERTED AND LANDE	D WITHOUT INCIDENT. POST-FLIGHT INSPECTION REVEALED THE TURBOCHARGER HAD FAILED.  THE TURBOCHARGER WAS REPLACED AND THE 	AIRCRAFT RETURNED TO SERVICE.				1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999081200482	19990812	00482		1999	8	12	CA990310079      	1	19990204	G	2435	11102715	BEARINGS        	BENDIX      	28B14117B   															START/GENERATOR	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						R59					(CAN) BENDIX (ALLIED SIGNAL) USES BEARINGS MANUFACTURED BY TORRINGTON FAFNIR AIRCRAFT BEARING DIVISION AND ARE IDENTIFIE	D BY BENDIX PART NUMBER AND LOT NUMBER ON THE BEARING.  THE TWO BEARINGS THAT WERE REMOVED WERE MANUFACTURED BY RHP AND 	ARE A LOWER QUALITY BEARING.  SUBMITTER STATED THIS IS AN UNAPPROVED PART.																	 
1999081200492	19990812	00492	NE  	1999	8	12	CA990310092      	2	19990108	G	7250		HP TURBINE      			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					NR 2 ENGINE	DAMAGED         	W				E	B			ENGINE SHUTDOWN         	EMER. DESCENT           			A			FLAME/FIRE                			AP	APPROACH       	1			CA			21734					120279			(CAN) NR 2 ENGINE HAD A TORQUE SURGE OF 107 PERCENT ON APPROACH.  THE TORQUE SURGE SUBSIDED AFTER A FEW SECONDS. THEN A 	LOUD BANG WAS HEARD AND THERE WAS SMOKE IN THE COCKPIT AND CABIN.  THE AIRCRAFT DECLARED AN EMERGENCY AND LANDED WITHOUT	 INCIDENT.  POST-FLIGHT INSPECTION FOUND WHEN THE HP TURBINE WAS TURNED A WEIRD SOUND WAS HEARD.  THE ENGINE WAS REPLACE	D.  THE REMOVED ENGINE WAS SENT TO P&W FOR INVESTIGATION.			2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999081200493	19990812	00493	EU  	1999	8	12	CA990310093      	1	19990115	G	2913	40052	PUMP            			FOKKER	F28   	F28MK1000   	4990808	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					NR 2 ENGINE	FAILED          	W				A				UNSCHED LANDING         				K	J		FLUID LOSS                	WARNING INDICATION        		CR	CRUISE         	1			CA								9153			(CAN) THERE WAS SIGNIFICANT DROP IN HYDRAULIC QUANTITY FROM THE UTILITY SYSTEM IN-FLIGHT.  PER THE CHECK LIST THE PUMPS 	WERE OFF LOADED.  RE-ENGAGING THE PUMPS PRIOR TO LANDING, THE NR 2 UTILITY SYSTEM DID NOT COME BACK ON LINE.  LOSS OF AL	L HYDRAULIC SYSTEMS.  NR 1 PRESSURE DURING LANDING ROLL RESULTED IN LOSS OF NOSE WHEEL STEERING.  MAINTENANCE WAS CALLED	 AND THE AIRCRAFT WAS TOWED TO THE GATE.  INSPECTION FOUND NR 2 UTILITY PUMP LEAKING BADLY FROM THE SHAFT SEAL.  THE PUM	P WAS REPLACED.  THE SYSTEM REPLENISHED, CHECKED SERVICEABLE, AND THE AIRCRAFT RETURNED TO SERVICE.		2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999081200494	19990812	00494	NM  	1999	8	12	CA990310094      	1	19990119	G	7931	8D1437	SWITCH          			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					NR 2 ENGINE	INTERMITTENT    	W				C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			CA								120189			(CAN) TAKEOFF REJECTED DUE TO LOW OIL PRESSURE WARNING LIGHT ON NR 2 ENGINE.  AIRCRAFT RETURNED TO GATE AND OIL WAS ADDE	D TO NR 2 ENGINE.  MAINTENANCE TROUBLESHOT ENGINE AND THE FOLLOWING WAS ACCOMPLISHED:  P2.5/P3 SWITCHING VALVE CLEANED, 	CENTRIFUGAL BREATHER OIL SEAL REPLACED, OIL PRESSURE CHECK VALVE ASSEMBLY, AND OIL PRESSURE REGULATING VALVE REPLACED, A	ND OIL PRESSURE SWITCH REPLACED.  SYSTEM CHECKED SERVICEABLE AND THE AIRCRAFT RETURNED TO SERVICE.			2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999052800092	19990528	00092	EU  	1999	5	28	CA990310095      	2	19990201	G	7200		ENGINE          			FOKKER	F28   	F28MK1000   	4990808	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					NR 2	FAILED          	W				E	F	A		ENGINE SHUTDOWN         	ACTIVATE FIRE EXT.      	UNSCHED LANDING         		E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CL	CLIMB          	1			CA								9292			(CAN) NR 2 ENGINE FAILED ON CLIMB-OUT, A SEVERE VIBRATION WAS FELT THROUGHOUT THE AIRCRAFT.  THE ENGINE WAS SHUTDOWN, TH	E FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT DIVERTED.  THE AIRCRAFT LANDED SAFELY.  INITIAL INSPECTION FOUND THE OIL	 TANK COMPLETELY EMPTY.  OIL WAS FOUND IN THE TAILPIPE.  THERE WAS NO APPARENT BLADE DAMAGE VISIBLE FROM AN EXTERNAL INS	PECTION.  THE ENGINE WAS REPLACED.  A FURTHER REPORT WILL FOLLOW.			2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999081200495	19990812	00495	NM  	1999	8	12	CA990310097      	1	19990226	G	6120	78249047	PCU             			DHAV  	DHC8  	DHC8301     		NM  	PWA   	PW120 	PW123       		NE  	HAMSTD	14SF	14SF15      	NE  	NR 1 ENGINE	MISINSTALLED    	W				C				ABORTED TAKEOFF         				W			INADEQUATE Q C            			TO	TAKEOFF        	1			CA								123125	881224		(CAN) TAKEOFF WAS REJECTED DUE TO NR 1 ENGINE ONLY PRODUCING 89 PERCENT TORQUE AT THE FIREWALL.  THE AIRCRAFT RETURNED T	O GATE WHERE MAINTENANCE INSPECTION REVEALED A BOLT INSTALLED BACKWARDS ON THE PROPELLER CONTROL UNIT, WHICH HAD BEEN RE	PLACED THE NIGHT BEFORE.  THE BOLT WAS INSTALLED CORRECTLY AND THE AIRCRAFT GROUND CHECKED SERVICEABLE.				2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
1999081200496	19990812	00496	NM  	1999	8	12	CA990310098      	1	19990301	G	2421	31708001A	GENERATOR       			DHAV  	DHC8  	DHC8301     		NM  	PWA   	PW120 	PW123       		NE  					NR 2 ENGINE	FAILED          	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			K	J		FLUID LOSS                	WARNING INDICATION        		CL	CLIMB          	1			CA				2509 				123036			(CAN) NR 2 ENGINE WAS SHUTDOWN SHORTLY AFTER TAKEOFF DUE TO OIL PRESSURE DROPPING.   AIRCRAFT RETURNED TO ITS DEPARTURE 	POINT.  POST-FLIGHT INSPECTION FOUND THE OIL TANK VERY LOW AND THE REDUCTION GEARBOX AND AC GENERATOR FLAGS DISPLAYED. F	URTHER INSPECTION REVEALED THE AC GENERATOR HAD SUFFERED A CATASTROPHIC FAILURE.  MAINTENANCE FLUSHED THE ENGINE OIL SYS	TEM, REPLACED THE NECESSARY FILTERS, COMPLETED SEVERAL GROUND RUNS, AND DEEMED THE ENGINE FIT FOR FERRY FLIGHT TO HOME B	ASE. AT HOME BASE,  AC GENERATOR WAS REPLACED, GROUND RUNS COMPLETED, AND SYSTEMS CHECKED SERVICEABLE.  THE AIRCRAFT WAS	 RETURNED TO SERVICE.	2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999081200505	19990812	00505	CE  	1999	8	12	CA990311011      	1	19990112	G	2435	X13041	BEARING         		643259A18R  	BEECH 	95    	95B55       	1152729	CE  	CONT  	O470  	IO470L      	17026	SO  					NR 2 ENGINE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				1199 				297744R			(CAN) DURING INSPECTION, WHEN PROP WAS TURNED, GRINDING NOISES COULD BE HEARD COMING FROM THE STARTER OR STARTER ADAPTER	.  IT WAS CONCLUDED STARTER ADAPTER WAS NOT DISENGAGING. THE STARTER AND STARTER ADAPTER WERE REPLACED,TESTED SERVICEABL	E AND AIRCRAFT RETURNED TO SERVICE.  A SUBSEQUENT TEARDOWN REPORT OF THE STARTER ADAPTER READ IN PART THE PREMATURE FAIL	URE WAS A RESULT OF BEARING WEAR DUE TO CORROSION.  THIS BEARING FITS INTO A WORMSHAFT DRIVE.  THE WORMSHAFT DRIVE MESHE	S WITH GEAR STARTER WORM WHEEL AND, AS A RESULT OF THE WORN OUT BEARING, THE WORMSHAFT DRIVE HAD EXCESSIVE SIDE AND END 	PLAY.  WHEN THE STARTER WAS ENGAGED, THE STARTER WORM WHEEL AND SPRING WOULD NOT DISENGAGE DUE TO MISALIGNMENT.	1	L	7	2 	3O	3	O	RT	3A16    	3E1				 
1999081200512	19990812	00512	EU  	1999	8	12	CA990311019      	1	19990118	G	2750	9787320002	POWER DRIVE UNIT			PILATS	PC12  	PC12        	7090550	EU  										TE FLAP	SLOW            	W				K				NONE                    				J			WARNING INDICATION        			IN	INSP/MAINT     	1			CA			58   			0349					(CAN) POWER DRIVE UNIT VERY SLOW TO OPERATE WHEN COLD SOAKED.  FLAP SYSTEM TRIPPED OFF LINE.						1	L	7	1 	3T			RT	A78EU   					 
1999081200513	19990812	00513	EU  	1999	8	12	CA990311020      	1	19990203	G	2752	951D1009	ACTUATOR        			PILATS	PC12  	PC12        	7090550	EU  						HARTZL	HCE4A	HCE4A3A     	NE  	TE FLAP	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			91   	91   		0798A			HV1031		(CAN) FAILED BACKLASH TEST IN ACCORDANCE WITH HB98-460.						1	L	7	1 	3T			RT	A78EU   		5	C	P10NE	 
1999081200529	19990812	00529	CE  	1999	8	12	CA990311036      	1	19990113	G	3020	727725	CIRCUIT BREAKER 			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					COCKPIT	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			201  								(CAN) CIRCUIT BREAKER FOR ANTI-ICE ACTUATOR WOULD OPEN DURING FLIGHT.  CIRCUIT BREAKER WAS REPLACED WITH NEW.						2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999081200534	19990812	00534	CE  	1999	8	12	CA990311041      	1	19990104	G	3260	444EN496	SWITCH          			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					RT MLG	FAILED          	W				O				OTHER                   				F			FLT CONT AFFECTED         			LD	LANDING        	1			CA			350  					PSO242			(CAN) CREW REPORTED DURING FLARE, AIRCRAFT PROPS WOULD GO TO IDLE POSITION BEFORE TOUCHDOWN.  FOUND RIGHT SQUAT SWITCH W	AS SHORTED BETWEEN PINS A AND B CAUSING INTERMITTENT SELECT SIGNALS.   SWITCH REPLACED.					2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999081200535	19990812	00535	CE  	1999	8	12	CA990311042      	1	19990121	G	3234		LIGHT           			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					MLG HANDLE	FAILED          	W				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			CA								PSO242			(CAN) CREW REPORTED DURING LANDING PHASE, THE GEAR HANDLE LIGHTS WOULD NOT EXTINGUISH.  NO ACTION WOULD CLEAR THESE LIGH	TS.  MAINTENANCE FOUND A FLAP SENSE WIRE AT W.S. 45.00, RT WING, HAD CHAFED THROUGH, SHORTING OUT WIRE NR W50A22.  WIRE 	WAS REPAIRED.   SUBMITTER STATED A FLEET-WIDE CAMPAIGN FOR THE REMAINING AIRCRAFT HAS BEEN INITIATED.				2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999081200537	19990812	00537		1999	8	12	CA990311044      	4	19990208	G	3416	280040102	INDICATOR       	MEGGITT     		BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					ALTIMETER	FAILED          	W				O				OTHER                   				J			WARNING INDICATION        			CR	CRUISE         	1			CA			670  					PCEPS0191			(CAN) FLIGHT CREW REPORTED THE DIGITAL DISPLAY OF RIGHT ALTIMETER WENT BLANK DISPLAYING THE FAILED FLAG.   MAINTENANCE R	EPLACED THE UNIT WITH ANOTHER UNIT. THIS IS THE ELEVENTH UNIT REPLACED IN LESS THAN 6 MONTHS.  MANUFACTURED BY MEGGITT E	LECTRONICS.				2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999081200540	19990812	00540		1999	8	12	CA990311047      	4	19990224	G	3416	280040102	INDICATOR       	MEGGITT     		BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					ALTIMETER	FAILED          	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			CA			325  								(CAN) DURING CRUISE FLIGHT, THE CREW NOTED THE RIGHT DIGITAL DISPLAY ON THE RIGHT ALTIMETER WAS DARK AND SHOWED FAILED. 	 PRESENT RELIABILITY FOR THIS PART NUMBER UNIT IS 1.89 FAILURES PER 1,000 FLIGHT HOURS.  MANUFACTURED BY MEGGITT AVIONIC	S.				2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999081200549	19990812	00549		1999	8	12	CA990311056      	4	19990208	G	3416	280040102	INDICATOR       	MEGGITT     		BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					ALTIMETER	FAILED          	W				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			CA			214  					PCEPSO197			(CAN) CREW REPORTED FLICKERING ON DIGITAL DISPLAY.  UNIT THEN FLAGGED FAILED.  REMOVED AND REPLACED WITH YET ANOTHER REP	LACEMENT.  MANUFACTURER OF ALTIMETER, MEGGITT AVIONICS.					2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999081200557	19990812	00557	EA  	1999	8	12	CA990311064      	1	19990112	G	3211	C3U547	FITTING         		C3U1004     	DHAV  	DHC3  	DHC3        	2800202	EA  	PWA   	PT6   	PT6A135     	52043	NE  					MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								PCE35094			(CAN) CRACKS FOUND IN LANDING GEAR FITTING ON INNER SURFACE EDGE OF FITTING.  PARTS REPLACED.						1	H	7	1 	3R	4	T		A815    	E4EA				 
1999081200558	19990812	00558	CE  	1999	8	12	CA990311065      	1	19990119	G	2760		SPEED BRAKE     			CESSNA	500   	560CESSNA   	2076750	CE  										LT&RT WING	FAILED          	W				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			CA			2508 								(CAN) SPEED BRAKES WOULD NOT RETRACT AFTER LANDING.  LEFT WING TRAILING EDGE WIRE FROM P63 PIN F TO J239 PIN 6 FOUND WIR	E BROKEN FOR DOWNLIMIT SWITCH.  INSULATION ALSO MISSING FROM 2 OTHER WIRES.  FRETTING OCCURRED FROM TYE-WRAP ATTACHMENT 	AT WS 78 ON RIGHT WING FROM P62 PIN L TO J240 PIN 3.  ALSO, A BROKEN WIRE FOR DOWNLIMIT SWITCH.   FRETTING OCCURRED ON L	OWER SKIN AT WS 90.			2	L	7	2 	4F			RT	A22CE   					 
1999081200575	19990812	00575	CE  	1999	8	12	CA990318004      	1	19990218	G	7920	3030150	LINE            			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  					RT ENGINE OIL	BENT            	W				E				ENGINE SHUTDOWN         				K	J		FLUID LOSS                	WARNING INDICATION        		NR	NOT REPORTED   	1			CA				1829 				PCE85170			(CAN) ON A COLD START (APPROX -37 CELSIUS), HIGH OIL PRESSURE (>200 PSI) WAS OBSERVED ON RIGHT ENGINE.  ENGINE START WAS	 ABORTED.  COPILOT OBSERVED OIL FLOWING FROM ENGINE.  FURTHER INVESTIGATION FOUND THIS TUBE HAD (WAS) BENT SEVERELY AT B	OTH BEND RADII AND HAD ALLOWED THE AFT END OF THE TUBE TO BECOME DISCONNECTED.  THIS ALLOWED THE OIL TO LEAK FROM THE EN	GINE.  TUBE WAS CHANGED WITH NEW STYLE (REF P&W SB 3173).  OIL FILTER WAS FOUND TO BE DAMAGED.  SOME MATERIAL WAS FOUND 	IN FILTER AND CHECKS I.A.W. PT6A-41 MM CH 79-20-04(3) WERE C/W AND AIRCRAFT RETURNED TO SERVICE.		1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999081200576	19990812	00576	GL  	1999	8	12	CA990318006      	3	19990302	G	6114		HUB             													MCAULY	2D34C	B2D34C211   	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				389  					777204		(CAN) DURING INSPECTION OF THE PROPELLER, USING LPI, LIGHT CORROSION WAS FOUND ON THE PROPELLER HUB.  THE HUB WAS GLASS 	BEAD BLASTED AND THE PROPELLER RETURNED TO SERVICE.															5	C	P7EA	 
1999081200577	19990812	00577	GL  	1999	8	12	CA990318007      	3	19990303	G	6111		LINK            													HARTZL	HCB3T	HCB3TN3     	GL  	PROPELLER PITCH	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				1251 					BU12290		(CAN) PROPELLER WAS SENT FOR PROPELLER STRIKE INSPECTION/REPAIR.  DURING INSPECTION,THE LINK ARMS AND THE BETA RING WERE	 FOUND WORN BEYOND LIMITS.															6	C	P15EA	 
1999081200578	19990812	00578	GL  	1999	8	12	CA990318008      	3	19990304	G	6111		BLADE           			CESSNA	172   	172N        	2072434	CE  						MCAULY	1C160	1C160DTM    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				5562 					734808		(CAN) DURING INSPECTION ,CORROSION WAS FOUND ON BOTH PROPELLER BLADES.  THE CORROSION WAS REMOVED AND LPI INSPECTION FOU	ND NO FURTHER TRACES OF CORROSION.					1	H	7	1 	3O			NT	3A12    		5	N	P910	 
1999090200001	19990902	00001	GL  	1999	9	2	CA990318009      	3	19990304	G	6114	C040121	HUB             			BEECH 	35    	B35         	1151506	CE  	CONT  	E185  	E1858       	17014	SO  	HARTZL	HCA2V	HCA2V204    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				172  				20283008	AK1314		(CAN) INSPECTION FOUND LIGHT CORROSION ON THE EXTERNAL SURFACES OF THE PROPELLER HUB SPIDER.  THE CORROSION WAS DRESSED 	OUT AND THE HUB WAS CADIUM PLATED.					1	L	7	1 	3O	3	O		A777    	E246	5	C	P24EA	 
1999081200579	19990812	00579	GL  	1999	8	12	CA990318010      	3	19990311	G	6111	D843310	BLADE           													HARTZL	HCA2V	HCA2VK2     	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				317  					H1735		(CAN) INSPECTION FOUND CORROSION ON THE FACE SIDE OF THE PROPELLER BLADES.  THE CORROSION WAS REMOVED WITH LIGHT GRINDIN	G.															5	C	P24EA	 
1999081200580	19990812	00580	SW  	1999	8	12	CA990318011      	1	19990301	G	2910	2781032075	LINE            			SWRNGN	SA227 	SA227AC     	8780603	SW  						ROTOL	R321	R321482F8   	GL  	HYDRAULIC SYSTEM	CRACKED         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			24675						DRG134584		(CAN) SUPPLY LINE TO UPSIDE OF NLG ACTUATOR FOUND CRACKED.  FLUID IN FLAMMABLE BAG.						2	L	7	2 	4T			RT	A8SW    		6	C	P61GL	 
1999081200582	19990812	00582	SO  	1999	8	12	CA990318014      	1	19990308	G	3710	8313	GASKET          	AIRBORNE    	441CW       	PIPER 	PA31  	PA31350     	7103110	SO  										VACUUM PUMP	FAILED          	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			K	J		FLUID LOSS                	WARNING INDICATION        		CR	CRUISE         	1			CA			550  								(CAN) VACUUM PUMP GASKET FAILED IN-FLIGHT CAUSED OIL LOSS FROM NR 1 ENGINE.  THE ENGINE WAS SHUT DOWN.  AIRCRAFT RETURNE	D TO ITS DEPARTURE POINT.  POST-FLIGHT INSPECTION CONFIRMED FAILURE.  NEW VACUUM PUMP GASKET WAS INSTALLED AND THE AIRCR	AFT RETURNED TO SERVICE.				1	L	7	2 	3O				A20SO   					 
1999081200584	19990812	00584	SW  	1999	8	12	CA990318016      	1	19990309	G	7921	H33C32	LINER           		204062540001	BELL  	205   	205A1       	1181414	SW  	LYC   	T53   	T5313B      	41549	NE  					BLOWER	LOOSE           	W				O				OTHER                   				E			VIBRATION/BUFFET          			IN	INSP/MAINT     	1			CA				435  		346		LEO7253X			(CAN) AFTER REPLACING THE OIL COOLER BLOWER BEARING, THE BLOWER ASSEMBLY CAUSED HIGH FREQUENCY VIBRATION WHEN GROUND RUN	.  TROUBLESHOOTING REVEALED BEARING LINER, WHICH IS PRESSURE FITTED INTO THE BLOWER HOUSING, WAS LOOSE AND TURNING.  THI	S CAUSED MISALIGNMENT OF THE BLOWER SHAFT.				1	G	7	1 	4U	4	U		H1SW    	E17EA				 
1999081200589	19990812	00589	CE  	1999	8	12	CA990318021      	1	19990101	G	2730	12601491	JACKSCREW       			CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  					ELEVATOR	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								812418R			(CAN) EXCESSIVE PLAY FOUND IN ELEVATOR TRIM JACK WORM GEAR.						1	H	7	1 	3O	3	O		A4CE    	E5CE				 
1999081200590	19990812	00590	SO  	1999	8	12	CA990318022      	1	19990115	G	3221	4027300	TRUNNION        			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  					NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L770861A			(CAN) NOSE GEAR WAS OVER-STEERED WITH SCISSORS HOOKED TOGETHER.						1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999081200591	19990812	00591	SO  	1999	8	12	CA990318023      	1	19990224	G	2841	994992	GAUGE           			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  					FUEL QUANTITY	MALFUNCTIONED   	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			12834					L770861A			(CAN) WHEN FULL, THE FUEL GAUGE WOULD READ 3/4.						1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999081200592	19990812	00592		1999	8	12	CA990318024      	4	19990224	G	3418	450742	DETECTOR        			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  					STALL SYSTEM	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L770861A			(CAN) WHEN FLYING THROUGH MOISTURE, THE STALL WARNING WOULD CHIRP POSSIBLY SHORTING OUT.						1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999081200593	19990812	00593		1999	8	12	CA990318025      	4	19990224	G	6113	4393304	BULKHEAD        			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  	HARTZL	HCE3Y	HCE3YR2A    	GL  	SPINNER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L770861A	DJ8612A		(CAN) LIP OF BACK PLATE CRACKED.						1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P33EA	 
1999081200594	19990812	00594	CE  	1999	8	12	CA990318026      	1	19990108	G	5230	12170692	HANDLE          			CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	CARGO DOOR	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								564814	840808		(CAN) OUTSIDE LEVER ON CARGO DOOR BROKEN.						1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47GL	 
1999060400326	19990604	00326	CE  	1999	6	4	CA990318027      	1	19990201	G	3211	NAS14740	BOLT            			CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	RT MLG	SHEARED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			11506					564814	840808		(CAN) ON INSPECTION OF THE MLG, THE FRONT RIGHT HAND BOLT ATTACHING THE GEAR LEG  WAS FOUND TO BE SHEARED.  OTHER BOLTS 	WERE INVESTIGATED WITH NO FAILURES.					1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P47G	 
1999081200595	19990812	00595	CE  	1999	8	12	CA990318028      	1	19990210	G	3020	50389028	BOOT            			BEECH 	100   	100BEECH    	1152916	CE  	PWA   	PT6   	PT6A28      		EA  					COWL	SHORTED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								51421			(CAN) LIP BOOT HEAT SHORTED OUT.						1	L	7	2 	3T	4	T		A14CE   	E4EA				 
1999081200596	19990812	00596	SO  	1999	8	12	CA990318029      	1	19990218	G	3242	763233	CALIPER         			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  					BRAKE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L442561A			(CAN) WALLS INSIDE CALIPERS CORRODED BEYOND LIMITS.						1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999081200597	19990812	00597	EA  	1999	8	12	CA990318031      	1	19990205	G	5743	215150622	SKIN            		21515061    	CNDAIR	CL215 	CL2151A10   		EA  										RUDDER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2532 								(CAN) SKIN CRACKED BENEATH MOUNTING FOOT PAD OF COUNTER BALANCE ARM.  POSSIBLE CAUSE BY VIBRATION AND/OR IN-FLIGHT STRES	SES OF WEIGHTS SUSPENDED ON SUBSTANTIAL MOMENT ARM WITH INSUFFICIENT STRUCTURAL SUPPORT AT MOUNTING POINT.					2	H	7	2 	4R				A14EA   					 
1999061800011	19990618	00011	EA  	1999	6	18	CA990318032      	1	19990208	G	5711	S6638	SPAR CAP        			CNDAIR	CL215 	CL2151A10   		EA  										WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2532 								(CAN) WHILE C/W AD CF 92-26, A CRACK WAS DISCOVERED VISUALLY IN THE LOWER FORWARD SPAR CAP.   A SECOND CRACK APPROXIMATE	LY 1.1250 INCH WAS FOUND IN THE RADIUS OF SHEAR ANGLE.   INSPECTION WAS C/W PRE AD REQUIREMENT.  AD CALLS FOR ULTRASONIC	 TESTING.				2	H	7	2 	4R				A14EA   					 
1999052800093	19990528	00093	EU  	1999	5	28	CA990318033      	1	19990301	G	3242	9595601511	BRAKE           	GOODRICH    	9595601511  	PILATS	PC12  	PC12        	7090550	EU  										MLG	FAILED          	W				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			CA											(CAN) PIC - UPON LANDING , EXPERIENCED BRAKE DRAGGING CAUSING DIFFICULTY IN MAINTAINING DIRECTIONAL CONTROL.  DEICING OF	 THE BRAKE WAS CARRIED OUT WITHOUT FURTHER REPORTED FLIGHT INCIDENT.  THE DIRECTOR, MAINTENANCE IN DISCUSSION WITH THE P	ILAUTS REPRESENTATIVE, SPECIFIED, RECURRING DEFECTS OF SIMILAR NATURE ARE BEING EXPERIENCED BY OTHER OPERATORS OF THE PI	LATUS PCI2 UTILITING THE GOODRICH BRAKING SYSTEM 9595601511.  CARBON DUST BUILD-UP COUPLED WITH THE ADDED CHARACTERISTIC	S ASSOCIATED WITH ICING ARE SPECIFIED AS THE ROOT CAUSES.  THE PILATUS REPRESENTATIVE SUGGESTED THE OPERATOR APPLY A RED	UCTION TO THE CURRENT APPROVED MAINTENANCE SCHEDULE ASSOCIATED WITH BRAKE ASSEMBLY CLEANING FROM 200 HRS TO 100 HRS.	1	L	7	1 	3T			RT	A78EU   					 
1999081200598	19990812	00598	EA  	1999	8	12	CA990318034      	2	19990226	G	7321	25244405	BEARING         			BEECH 	100   	A100        	1152915	CE  	PWA   	PT6   	PT6A28      		EA  					FCU HOUSING	FAILED          	W				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			NR	NOT REPORTED   	1			CA				707  				PCE50295			(CAN) CREW REPORTED TORQUE FLUCTUATIONS, GROUND RUN CONFIRMED TORQUE FLUCTUATIONS ALONG WITH FUEL FLOW, PROPELLER SPEED 	AND ENGINE RPM FLUCTUATIONS.  OIL PRESSURE AND TEMPERATURES WERE NORMAL.  THE FCU WAS REMOVED TO INSPECT FCU DRIVE AND T	HE NG FLYWEIGHT BEARINGS HAD FAILED. THE FCU AND FUEL PUMP WERE REPLACED.  THE ENGINE WAS GROUND RUN SERVICEABLE.				1	L	7	2 	3T	4	T		A14CE   	E4EA				 
1999081200599	19990812	00599	EA  	1999	8	12	CA990318035      	2	19990225	G	7414	M3984	CONDENSER       	SLICK       	4353        						LYC   	O360  	AEIO360A1B6 	41514	EA  					MAGNETO	FAILED          	W				D				RETURN TO BLOCK         				O			OTHER                     			TX	TAXI/GRND HDL  	1			CA			606  			96040424		L2514551A			(CAN) DURING A PRE-FLIGHT MAGNETO CHECK, THE RIGHT HAND MAGNETO WAS FOUND LIVE WITH THE MAG SWITCH SELECTED OFF.  INSPEC	TION FOUND THE CONDENSER WOULD CREATE AN OPEN CIRCUIT WHEN SLIGHT PRESSURE APPLIED TO THE TERMINAL WIRE ATTACHMENT. THE 	MAGNETO WAS REPLACED, CHECKED SERVICEABLE ,AND THE AIRCRAFT RETURNED TO SERVICE.									3	O			1E10				 
1999081200600	19990812	00600	EU  	1999	8	12	CA990318036      	1	19990225	G	3251	Z4242170001	SPRING          	MORAVN      	L24242370000	ZLIN  	242   	Z242L       	9970204	EU  										NLG STEERING	BROKEN          	W				D				RETURN TO BLOCK         				J			WARNING INDICATION        			TX	TAXI/GRND HDL  	1			CA			26   								(CAN) DURING GROUND RUN, THE NOSE WHEEL STEERING SYSTEM OPERATED WITH EXCESSIVE FREE PLAY.  IT WAS FOUND THAT THE RIGHT 	SPRING WAS BROKEN.					1	L	7	1 	3O			0	A76EU   					 
1999081200601	19990812	00601	SO  	1999	8	12	CA990318037      	1	19990225	G	3260		CONTACTS        		89291003    	PIPER 	PA44  	PA44180     	7104402	SO  										MLG	DEFECTIVE       	W				L				ABORTED APPROACH        				N			FALSE WARNING             			AP	APPROACH       	1			CA			716  								(CAN) AFTER THE UNDERCARRIAGE WAS SELECTED DOWN ON APPROACH, THE LT MAIN GEAR AND THE NOSE GEAR SAFE LIGHTS ILLUMINATED,	 THE GEAR UNSAFE INDICATION LIGHT EXTINGUISHED AND THEN APPROXIMATELY 20 SECONDS LATER, THE RIGHT MAIN GEAR SAFE LIGHT I	LLUMINATED.  IT WAS DETERMINED THE CONTACTS FOR THE GEAR UNSAFE LIGHT WERE DEFECTIVE.  THIS UNDERCARRIAGE DOWNLOCK SWITC	H CONTAINS THREE SETS OF CONTACTS; ONE FOR HYDRAULICS, ONE FOR THE LANDING GEAR UNSAFE LIGHT, AND ONE FOR THE GEAR SAFE 	LIGHT.  THE SWITCH WAS REPAIRED BY SWITCHING THE GEAR SAFE CIRCUIT TO A SERVICEABLE SPARE SET OF CONTACTS IN THE SWITCH.		1	L	7	2 	3O				A19S0   					 
1999060400327	19990604	00327	CE  	1999	6	4	CA990318038      	1	19990223	G	5220	08110401	WINDOW          			CESSNA	310   	310J        	2074226	CE  	CONT  	O470  	IO470U      	17026	SO  	MCAULY	2AF34C	D2AF34C81   	GL  	EMERGENCY EXIT	SEPARATED       	W				A				UNSCHED LANDING         				D			INFLIGHT SEPARATION       			CL	CLIMB          	1			CA			9933 					CS931802U	741107		(CAN) AFTER T/F EMERGENCY WINDOW DEPARTED AIRCRAFT.  UPON FURTHER INVESTIGATION, THE WINDOW SEPARATED FROM THE FRONT AND	 PROCEEDED TO PEEL BACKWARDS.  THE EMERGENCY CABLE WAS NOT PULLED.  THE REAR LOCKING PINS WERE BENT AND THE WINDOW TABS 	WERE RIPPED FROM THE WINDOW BEING ATTACHED TO THE REAR LOCKING PIN.   ALL INSPECTION CRITERIA WAS COMPLIED WITH PRIOR TO	 INCIDENT.			1	L	7	2 	3O	3	O		3A10    	3E1	5	C	P5EA	 
1999081200602	19990812	00602	CE  	1999	8	12	CA990318039      	1	19990226	G	5610	08136591	WINDSHIELD      			CESSNA	310   	310L        	2074230	CE  	LYC   	O540  	TIO540A2B   	41532	EA  					COCKPIT	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			9128 					RL112661A			(CAN) CRACKED AND CRAZED WINDSHIELD REPLACED.  NO INCIDENTS IN FLIGHT HISTORY REPORTED.						1	L	7	2 	3O	3	O		3A10    	E14EA				 
1999081200603	19990812	00603	SW  	1999	8	12	CA990318040      	1	19990305	G	2752	DW4K2	BEARING         			SWRNGN	SA226 	SA226T      	8780122	SW  										FLAP ACTUATOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			6559 								(CAN) LEFT FLAP ACTUATOR CENTER WALKING BEAM BEARING OUTER RACE CRACKED.						2	L	7	2 	4T			RT	A5SW    					 
1999070900371	19990709	00371	SW  	1999	7	9	CA990318041      	1	19990302	G	6710	MS3569129	NUT             		206010355001	BELL  	206   	206L        	1181522	SW  										M/R PITCH LINK	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) AFTER READING ISSUE 3&4/98- FEEDBACK PUBLICATION, A VISUAL INSPECTION WAS CARRIED OUT (USING 10X MAG).   A CRACK W	AS FOUND IN M/R PITCH LINK NUT.					1	G	7	1 	3U				H2SW    					 
1999060400328	19990604	00328	CE  	1999	6	4	CA990318044      	1	19990310	G	2497		WIRE            			CESSNA	500   	550         	2076604	CE  	PWA   	JT15  	JT15D4      	52112	NE  					GLARESHIELD	CHAFED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								71714			(CAN) INSTRUMENT PANEL WIRING AFFECTED BY VARIOUS MANUFACTURE HARDWARE INSTALLATION.  CESSCOM SERVICE CONDITION REPORT F	ILED 180729 WITH CESSNA ENGINEERING.  OTHER SDRS NOTED.					1	L	7	2 	4F	4	F	 	A22CE   	E1NE				 
1999060400329	19990604	00329	CE  	1999	6	4	CA990318045      	1	19990310	G	2497		WIRE            			CESSNA	500   	550         	2076604	CE  	PWA   	JT15  	JT15D4      	52112	NE  					GLARESHIELD	CHAFED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								71718			(CAN) INSTRUMENT PANEL WIRING AFFECTED BY VARIOUS MANUFACTURE HARDWARE INSTALLATIONS.  CESSCOM SERVICE CONDITION REPORT 	FILED 180729 WITH CESSNA ENGINEERING.  OTHER SDRS NOTED.					1	L	7	2 	4F	4	F	 	A22CE   	E1NE				 
1999081200604	19990812	00604	EA  	1999	8	12	CA990318046      	3	19990308	G	6111		BLADE           			PIPER 	PA20  	PA20        	7102002	SO  						SNSNCH	74D	74DM        	EA  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			746  						A49773		(CAN) DEEP CORROSION ON PROPELLER THRUST FACE.  EXTRA WORK WAS REQUIRED TO REMOVE CORROSION IAW SENSENICH MANUAL SPRM 59	0.					1	H	7	1 	3O				1A4     		5	N	P88614	 
1999081200605	19990812	00605	EA  	1999	8	12	CA990318047      	1	19990304	G	2810		FUEL CELL       			DHAV  	DHC7  	DHC7102     	2802708	EA  	PWA   	PT6   	PT6A50      	52043	EA  	HAMSTD	24PF	24PF305     	GL  	FUSELAGE	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			20465								(CAN) WHILE PERFORMING AD'S CF-86-14 AND CF 87-04, A FUEL LEAK IN THIS AREA WAS NOTED.  LEAK WAS FROM THE END OF THE FUE	L TANK AND FOUND LEAKING THROUGH THE CORRECTIVE SEALANT USED IN THE AD'S.					2	H	7	4 	4T	4	T		A20EA   	E4EA	6	C	P1NE	 
1999081200606	19990812	00606	EA  	1999	8	12	CA990318048      	1	19990308	G	2435	1253	SPRING          	LUCAS       	BC09101     	DHAV  	DHC7  	DHC7102     	2802708	EA  	PWA   	PT6   	PT6A50      	52043	EA  	HAMSTD	24PF	24PF305     	GL  	START/GENERATOR	BROKEN          	W				E				ENGINE SHUTDOWN         				E			VIBRATION/BUFFET          			IN	INSP/MAINT     	1			CA				307  		1253		PCE86302	237483		(CAN) NR 1 ENG VIBS DURING RUN-UP.  FINDINGS:   BROKEN BRUSH RETAINING CLIP IN STARTER/GENERATOR.  COMPONENT REPLACED.						2	H	7	4 	4T	4	T		A20EA   	E4EA	6	C	P1NE	 
1999081200607	19990812	00607	SO  	1999	8	12	CA990318049      	2	19990218	G	7414	107902018	FLYWEIGHT       			PIPER 	PA28  	PA28RT201T  	7102817	SO  	CONT  	O360  	TSIO360F    	17025	SO  					MAGNETO	LOOSE           	W				O				OTHER                   				E			VIBRATION/BUFFET          			IN	INSP/MAINT     	1			CA				1200 				232766R			(CAN) PILOT REPORTED ROUGH RUNNING ENGINE ON RUN-UP.  INSPECTION FOUND RIGHT HAND MAGNETO DEAD.  DURING REMOVAL OF THE M	AGNETO, THE IMPULSE COUPLING FLYWEIGHT FELL OUT.  THE AXLE/RIVET HEAD FOUND MISSING.  ALL CYLINDERS, OIL SUMP AND ACCESS	ORY SECTION, WERE INSPECTED.  HALF THE RIVET HEAD WAS FOUND IN THE ACCESSORY COVER, THE OTHER HALF WAS NOT LOCATED.  POS	SIBLY VACATED THROUGH THE OIL DRAIN.  NO METAL CONTAMINATION WAS FOUND IN THE OIL SCREENS OR THE OIL FILTER.			1	L	7	1 	3O	3	O		2A13    	E9CE				 
1999081200608	19990812	00608	SO  	1999	8	12	CA990318050      	2	19990218	G	8530	641916	CYLINDER        			FLEET 	80    	FLEET80     		EA  	CONT  	O200  	O200A       	17020	SO  					ENGINE	FRACTURED       	W				O				OTHER                   				E			VIBRATION/BUFFET          			IN	INSP/MAINT     	1			CA				577  		C79814		698628A			(CAN) PILOT REPORTED ROUGH RUNNING ENGINE AT HIGH RPM.  RUN-UP FOUND NR 4 CYLINDER WAS COLD.  THE ROCKER COVER WAS REMOV	ED AND THE ROCKER SHAFT, ROCKERS AND BOSSES BROKEN.   ALL FOUR CYLINDERS WERE REPLACED.					1	H	7	1 	3O	3	O		788     	E252				 
1999081200611	19990812	00611		1999	8	12	CA990318053      	1	19990308	G	7603		CABLE           								ROTAX 	912   	ROTAX912    	55555	EU  					THROTTLE	SEVERED         	W				A				UNSCHED LANDING         				E	D		VIBRATION/BUFFET          	INFLIGHT SEPARATION       		CR	CRUISE         	1			CA			2945 					4380626			(CAN) WHEN PILOT ATTEMPTED TO REDUCE POWER DURING FLIGHT, THE ENGINE RAN ROUGH.  WHEN THROTTLE WAS RETURNED TO CRUISE PO	SITION, ENGINE WAS SMOOTH.  FOUND THAT LEFT SIDE THROTTLE CABLE WAS SEVERED, AND, AS A RESULT, POWER COULD NOT BE REDUCE	D ON BOTH CARBURETORS SIMULTANEOUSLY.   ENGINE WAS TURNED OFF ON VERY SHORT FINAL TO FACILITATE LANDING.									3	I			EXPE3I				 
1999081200618	19990812	00618	SW  	1999	8	12	CA990318060      	1	19990224	G	3260	MS243314	SWITCH          			SWRNGN	SA226 	SA226AT     	8780405	SW  										MLG	FAILED          	W				A				UNSCHED LANDING         				O			OTHER                     			CL	CLIMB          	1			CA											(CAN) AFTER TAKEOFF, GEAR SELECTED UP, BUT DID NOT RETRACT, AIRCRAFT LANDED WITHOUT INCIDENT.  MICROSWITCH FOUND ICED UP	.  REPLACED.					2	L	7	2 	4T			RT	A5SW    					 
1999081200619	19990812	00619	NE  	1999	8	12	CA990318061      	2	19990310	G	7230	NM1026190200	CLAMP           		601800001001	CNDAIR	CL600 	CL6002B19   		EA  	GE    	CF34  	CF343B1     		NE  					COMPRESSOR	LOOSE           	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			J			WARNING INDICATION        			CR	CRUISE         	1			CA											(CAN) IN CRUISE, THE FLIGHT CREW GOT A WARNING 'R 14TH DUCT' ON EICAS.  EMERGENCY PROCEDURES CARRIED OUT.  AIRCRAFT LAND	ED OK.  THE 14TH STAGE BLEED AIR LEAK 'C' CLAMP FOUND LOOSE.					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999081200621	19990812	00621	WP  	1999	8	12	CA990318064      	1	19990302	G	4920	99F12428	NUT             		CTCP8590F   	CVAC  	340   	340CVAC     	242270A	WP  	ALLSN 	501D  	501D13D     	03004	GL  					TURBINE SECTION	MISSING         	W				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			CA			473  			P35224		501379			(CAN) WHEN STARTING APU, A SURGE SOUND COMING FROM THE UNIT.  THE COMPLETE UNIT REPLACED.  ON TEARDOWN OF THE HOT SECTIO	N, TWO NUTS WERE MISSING.  THE LOSS OF THESE NUTS POSSIBLY CAUSED DAMAGE TO THE TURBINE WHEEL AND NOZZLES.					2	L	7	2 	4R	4	T		6A6     	E282				 
1999081200622	19990812	00622	SO  	1999	8	12	CA990318065      	1	19990308	G	2140	25T6411	BRUSH           		90E83       	PIPER 	PA31  	PA31350     	7103110	SO  										HEATER BLOWER	WORN            	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			CA			291  			BR09PJ134470					(CAN) FRONT HEATER QUIT IN-FLIGHT AND RE-LIGHTED.  FLIGHT CONTINUED WITH NO FURTHER PROBLEM.  NEXT FLIGHT, HEATER DID NO	T START.  JANITROL TROUBLESHOOTING LED TO COMBUSTION MOTOR FAILURE - STARTED IF TAPPED UPON.  INSIDE MOTOR FOUND ONE BRU	SH COMPLETELY WORN.  MOTOR WAS REPLACED ALMOST A YEAR AGO USING REPLACEMENT KIT NR 90E96-2 WHICH REPLACES ORIGINAL (NOW 	UNAVAILABLE) MOTOR P/N YZ14042.  NOTED NEW MOTOR IS SMALLER IN DIAMETER AND LENGTH SO A KIT SUPPLIED ADAPTER IS NECESSAR	Y.  RECOMMENDATION:  MOTOR SHOULD HAVE A BRUSH INSPECTION TIME LIMIT.		1	L	7	2 	3O				A20SO   					 
1999081200623	19990812	00623	SO  	1999	8	12	CA990318066      	1	19990308	G	3397	L120EC	WIRE            			PIPER 	PA31  	PA31350     	7103110	SO  										TAXI LIGHT	CORRODED        	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			11605								(CAN) ROTTEN CORRODED WIRE CORE, ALTHOUGH COVERED WITH HELICORD, WAS EXPOSED TO WEATHER WHEN NOSE GEAR IS DOWN.  LOCATED	 IN SPACE BETWEEN NOSE OLEO AND FRONT NOSE WHEELWELL WALL.  WIRE WAS ROTTEN INSIDE.  ITS INSULATION COVERING WAS NOT TOO	 GOOD ITSELF.  DISCOVERED BY ACCIDENT DURING TROUBLESHOOTING.  DURING REMOVAL OF HELI-PROTECTIVE WRAP AROUND TWO WIRES, 	PIECE JUST FELL OFF.   CAUSE: OLD AGE AND EXPOSED WIRING.			1	L	7	2 	3O			 	A20SO   					 
1999042100079	19990421	00079	EU  	1999	4	21	CA990318068      	2	19990101	G	7250	JR22422	BLADE           			FOKKER	F28   	F28MK1000   	4990808	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					NR 1 ENGINE	FAILED          	W				E				ENGINE SHUTDOWN         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA								9539			(CAN) DURING CRUISE AT FL 300, NR 1 ENGINE FLAMED OUT.  PILOT REPORTED NR 1 ENGINE HP FUEL LEVER MOVING UNCOMMANDED TO S	HUT-OFF POSITION.  FLIGHT CREW ATTEMPTED RE-START, BUT VIBRATIONS WERE EXCESSIVE SO ENGINE WAS SHUT DOWN.  POST- FLIGHT 	INSPECTION AT DESTINATION FOUND LP TURBINE BLADE DAMAGE.  LP TURBINE BLADES AND DISKS ROUTED TO ROLLS ROYCE FOR INVESTIG	ATION.  FURTHER REPORT TO FOLLOW.			2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999061000007	19990610	00007	NE  	1999	6	10	CA990318069      	2	19990114	G	7250	UL29272	SEAL            		M05623AA    	BOEING	757   	757200      	1384950	NM  	RROYCE	RB211 	RB211535E437	54555	NE  					TURBINE	DEBONDED        	W				E				ENGINE SHUTDOWN         				M			OVER TEMP                 			NR	NOT REPORTED   	1			CA			2239 			DM4043		31213			(CAN) PILOT ATTEMPTED THREE STARTS, BUT ENGINE OVERTEMPTED AND WITH NO N2 INDICATION.  DURING EACH ATTEMPT, THE EGT WENT	 TO 576 DEGREES CELSIUS FOR LESS THAN ONE MINUTE.  WALK-AROUND FOUND NO ABNORMALITIES OR LOOSE MATERIALS IN THE EXHAUST.	  IP COMPRESSOR WOULD NOT TURN.  ENGINE WAS REMOVED AND INSPECTION FOUND THE IP TURBINE HONEYCOMB SEAL MATERIAL HAD COME	 DEBONDED FROM ITS PARENT MATERIAL PART.  INVESTIGATION IS ONGOING.  FURTHER REPORT TO FOLLOW.			2	L	7	2 	4F	4	F	RT	A2NM    	E12EU				 
1999042100080	19990421	00080	EU  	1999	4	21	CA990318070      	2	19990307	G	7250		TURBINE BLADE   			FOKKER	F28   	F28MK3000   	4990809	EU  	RROYCE	SPEY  	SPEY55515P  	54521	EU  					LP TURBINE	FAILED          	W				E				ENGINE SHUTDOWN         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA								9241			(CAN) NR 1 ENGINE SHUTDOWN IN-FLIGHT, REPORTED LP TURBINE BLADE FAILURE.  NO OTHER INFO AVAILABLE.  FURTHER REPORT TO FO	LLOW.					2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999081200624	19990812	00624	SW  	1999	8	12	CA990318071      	1	19990308	G	5302	206023119151	SKIN            		206023119151	BELL  	206   	206L        	1181522	SW  										TAILBOOM	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) EXCESSIVE CORROSION FOUND ON LE ON UPPER SURFACE AT JUNCTION OF DOUBLER.  CORROSION WAS PROTRUDING THROUGH SKIN AN	D WAS LOCATED UNDERNEATH PAINT AND SEALANT.  CORROSION WAS LOCATED IN LINE WITH THE ATTACHMENT C/T TAILBOOM DOUBLERS.  S	TABILIZER REMOVED FROM SERVICE AND REPLACED.				1	G	7	1 	3U				H2SW    					 
1999081200626	19990812	00626	SO  	1999	8	12	CA990318073      	1	19990312	G	5620		WINDOW          			EMB   	110   	EMB110P1    	3260122	SO  	PWA   	PT6   	PT6A34      	52043	EA  					CABIN	LEAKING         	W				K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			CA								PCG57486			(CAN) GLYCOL PENATRATED CABIN WINDOW SOAKING INSULATION.  WHEN HEATER APPLIED, VAPORS VISIBLE ON INTERIOR.  WINDOW RESEA	LED AND INSULATION REPLACED.					1	L	7	2 	4T	4	T		A21SO   	E4EA				 
1999081200627	19990812	00627	SW  	1999	8	12	CA990318074      	1	19990310	G	6230	430310450101	BEARING         			BELL  	430   	430         	1182150	SW  										SWASHPLATE	MAKING METAL    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			782  								(CAN) SWASHPLATE INSPECTED IAW UPCOMING ASB(430-99-XX - NOT YET ISSUED).  FINDINGS ARE AS FOLLOWS:  METAL FLAKES FOUND I	N GREASE COMING FROM INNER AND OUTER RACE CAGES OF BEARING.  BALL BEARING HAD EVIDENCE OF FLAT SPOT OR MARKS.					1	G	7	2 	3U			RT	H9SW    					 
1999081200628	19990812	00628	NE  	1999	8	12	CA990318075      	2	19990308	G	7210	311193101	BEARING         								PWA   	PW120 	PW127       		NE  					GEARBOX	PITTED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			10222					127101			(CAN) THE ENGINE WAS SENT FOR INSPECTION AND REPAIR AFTER THE OPERATOR SUSTAINED A SEVERE LIGHTNING STRIKE.  INSPECTION 	FOUND EXTENSIVE MAGNETIZATION OF THE STEEL COMPONENTS AND ELECTRICAL DISCHARGE PITTING DAMAGE TO THE NR 15 AND NR 18 BEA	RINGS THAT CLEARLY CONFIRMS THE WISDOM OF ENGINE REMOVAL AT THIS TIME.  THERE WAS ALSO CONSIDERABLE FRETTING OF THE RGB 	BEARING BORES NECESSITATING A NUMBER OF REPAIRS TO RESTORE ALIGNMENT AND BEARING LOCATION DIAMETER ROUNDNESS.								4	T			E20NE				 
1999081200630	19990812	00630	SW  	1999	8	12	CA990323002      	1	19990308	G	5330	206031100281	SKIN            			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					FUSELAGE	DEBONDED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			12521					CAE822906F			(CAN) DURING ROUTINE INSPECTION, SOME DEBONDING WAS NOTICED ON UNDERSIDE OF FUSELAGE BELLY.  FURTHER INSPECTION REVEALED	 THAT DEBONDING WAS SLIGHTLY BEYOND REPAIRABLE LIMITS.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999081200631	19990812	00631	SW  	1999	8	12	CA990323003      	1	19990308	G	5320	206031301023	SUPPORT         			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					GEAR ATTACH	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			12521					CAE822906F			(CAN) DURING SCHEDULED INSPECTION, 2 CRACKS WERE FOUND AT CROSSTUBE SUPPORT AREA.  CROSSTUBE SUPPORT WILL BE REPLACED WI	TH NEW BELL PART NUMBER WHICH IS MANUFACTURED WITH THICKER MATERIAL AND MANUFACTURED THROUGH A DIFFERENT PROCESS.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999081200632	19990812	00632	SO  	1999	8	12	CA990323005      	2	19990220	G	8530		CYLINDER        			CESSNA	421   	421C        	2076016	CE  	CONT  	O520  	GTSIO520L   	17032	SO  					ENGINE	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA								604412			(CAN) DETONATION OF NR 4 CYLINDER CAUSED SEVERE MELTING AND DETERIORATION OF NR 4 PISTON RING AND AREA, PRODUCING AN OPE	NING INTO THE BOTTOM OF THE PISTON.  METAL CONTAMINATION FROM NR 4 CYLINDER DETONATION CAUSED OIL STARVATION TO THE BEAR	ING SURFACES OF NR 2 CONNECTING ROD AND CRANK PIN JOURNAL. THE SEVERE OVERHEATING AND METAL TRANSFER CAUSED NR 2 CONNECT	ING ROD AND CAP TO SEPARATE CAUSING FURTHER INTERNAL DAMAGE TO THE INNER SURFACES OF THE CRANKCASE AND THE CYLINDER BARR	ELS OF NR 1 AND NR 2 CYLINDERS.  THIS DAMAGE HAS PREVENTED THE REMOVAL OF NR 1  NR 2 CYLINDERS FROM THEIR BORES.  THE CA	USE OF THIS DETONATION DAMAGE HAS NOT BEEN DETERMINED.	1	L	7	2 	3O	3	O		A7CE    	E7CE				 
1999081200634	19990812	00634	EA  	1999	8	12	CA990323007      	1	19990308	G	5711	S6638	CAP             			CNDAIR	CL215 	CL2151A10   		EA  										SPAR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2947 								(CAN) LEFT LOWER FORWARD SPAR CAP FOUND CRACKED.  IT WAS FOUND VISUALLY WHERE THE RADIUS OF THE SPAR CAP WAS POORLY CUT 	OUT.  RADIUS LESS THAN .25 INCH.  AREA WILL BE INSPECTED BY ULTRASOUND.					2	H	7	2 	4R				A14EA   					 
1999081200635	19990812	00635	NE  	1999	8	12	CA990323008      	2	19990308	G	8520	272230	REARCASE        			CNDAIR	CL215 	CL2151A10   		EA  	PWA   	R2800 	CA3         	52026	NE  					ENGINE	CRACKED         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA				246  				P33442			(CAN) OIL WAS OBSERVED ON THE ENGINE GEARCASE.  AFTER CLEANING AND INSPECTION, A CRACK WAS FOUND AT A STUD HOLE.  THE SU	BMITTER STATES THAT A ZERO TIME ENGINE WAS ALSO INSPECTED AND A HAIRLINE CRACK WAS FOUND ON THAT ENGINE.  BOTH ENGINES A	RE BEING RETURNED TO THE OVERHAUL SHOP FOR REPLACEMENT.				2	H	7	2 	4R	4	R		A14EA   	E231				 
1999081200637	19990812	00637	CE  	1999	8	12	CA990323010      	1	19990309	G	5740	8178414	BOLT            			BEECH 	100   	A100        	1152915	CE  	PWA   	PT6   	PT6A28      		EA  					WING	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			10179					PCE50256			(CAN) WHILE COMPLETING AD CF-81-25R5, WING BOLT INSPECTION, THE RIGHT FORWARD LOWER BOLT WAS FOUND TO BE VERY TIGHT.  AF	TER REMOVAL OF THE BOLT, DISCOVERED THE BOLT AND NUT WERE DAMAGED WHICH MADE THE BOLT VERY DIFFICULT TO REMOVE.  UPON FU	RTHER INVESTIGATION, AGREED THE BOLT AND NUT WERE ASSEMBLED WITH LITTLE PIECES OF DIRT ON THE THREADS.  THE BOLT AND NUT	 WERE REPLACED.			1	L	7	2 	3T	4	T		A14CE   	E4EA				 
1999081200638	19990812	00638	NM  	1999	8	12	CA990323012      	1	19990312	G	2780		SWITCH          			BOEING	727   	727277      	138408S	NM  	PWA   	JT8   	JT8D15      	52051	NE  					LE FLAP	OUT OF ADJUST   	W				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			CA								695337			(CAN) WHEN FLAPS SELECTED TO FIVE DEGREES FORWARD FLAP ANNUNCIATOR PANEL ILLUMINATED TO GREEN, NORMAL, THEN INDICATED AM	BER AND FLICKERED - GREEN - AMBER WHILE NR 6 LE FLAP INDICATED NEITHER.   AFTER SOME TIME ALL INDICATED RETURNED TO NORM	AL. NR 6 LE FLAP POSITION SWITCH LINKAGE OUT OF ADJUSTMENT.  ADJUSTED SERVICEABLE.				2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
1999081200639	19990812	00639	NM  	1999	8	12	CA990323014      	1	19990308	G	5730		RIVETS          			BOEING	727   	727221      	1384071	NM  										WS 750	MISSING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) DURING POST-FLIGHT, MAINTENANCE NOTICED 3 MISSING RIVETS ON LT WING LOWER SKIN AT FORWARD SPAR STA 750.  REPAIRED 	IN ACCORDANCE WITH BOEING REPAIR.					2	L	7	3 	4F				A3WE    					 
1999081200640	19990812	00640	NM  	1999	8	12	CA990323015      	1	19990308	G	5730		RIVETS          			BOEING	727   	727221      	1384071	NM  										WS 750	MISSING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) DURING POST-FLIGHT, MAINTENANCE NOTICED 3 MISSING RIVETS ON LT WING LOWER SKIN AT FORWARD SPAR STA 750.  REPAIRED 	IN ACCORDANCE WITH BOEING REPAIR.					2	L	7	3 	4F				A3WE    					 
1999081200642	19990812	00642	NM  	1999	8	12	CA990323017      	1	19990310	G	2420		GCU             			BOEING	727   	72782       	1384029	NM  	PWA   	JT8   	JT8D7B      	52053	NE  					COCKPIT	ARCING          	W				O				OTHER                   				J			WARNING INDICATION        			CR	CRUISE         	1			CA								649672			(CAN)  NR 1 GENERATOR'S CIRCUIT BREAKER TRIPPED, GCU RECEPTACLE ARCING.  RECEPTACLE AND GCU REPLACED.						2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999081200643	19990812	00643	NM  	1999	8	12	CA990323018      	1	19990312	G	2780		SWITCH          			BOEING	727   	72782       	1384029	NM  	PWA   	JT8   	JT8D7B      	52053	NE  					LE SLAT	FAILED          	W				K				NONE                    				N			FALSE WARNING             			IN	INSP/MAINT     	1			CA								649672			(CAN) LEADING EDGE POSITION ANNUNCIATOR, INDICATOR NO LIGHTS ON SLAT NR 7 WITH NR 7 EXTENDED.  PILOTS LE GREEN AND AMBER	 INDICATION SERVICEABLE.  DEFERRED FOR PARTS, OPERATED PER MEL.  NR 7 SLAT POSITION SWITCH REPLACED.					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999081200646	19990812	00646	EA  	1999	8	12	CA990323021      	2	19990317	G	8520	LW18840	CAMSHAFT        								LYC   	O360  	AEIO360A1B6 	41514	EA  					ENGINE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2600 					L2640851A			(CAN) DURING THE REMOVAL OF NR 1 AND NR 3 CYLINDERS TO INVESTIATE AN INCREASE IN OIL CONSUMPTION, FOUND THE NR 3 AND NR 	4 CYLINDER INTAKE CAM LOBES WERE WORN ABNORMALLY.  THE CORRESPONDING LIFTERS WERE NOT DAMAGED.  THE ENGINE WAS REMOVED A	ND SENT FOR REPAIR.									3	O			1E10				 
1999081200647	19990812	00647		1999	8	12	CA990323022      	1	19990317	G	7820	L24266710000	SILENCER        								LYC   	O360  	AEIO360A1B6 	41514	EA  					EXHAUST	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				600  				L2663251A			(CAN) INSPECTION FOUND THE EXHAUST NR 1 SILENCER CRACKED.  THE SILENCER WAS REPLACED.											3	O			1E10				 
1999081200648	19990812	00648	NE  	1999	8	12	CA990323023      	1	19990221	G	7921	7630807902104	BLOWER          			SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					OIL COOLER	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				558  				CAE890238S			(CAN) INSPECTION FOUND BEARING FAILURE CAUSING INTERNAL WEAR OF THE FAN BLADES.						1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999081200649	19990812	00649	EU  	1999	8	12	CA990323024      	1	19990303	G	5320	350A38101832	BEAM            			SNIAS 	350   	AS350BA     	8680817	EU  	TMECA 	ARRIEL	ARRIEL1B    	6OO30	NE  					FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						4X38A		4404			(CAN) FPI REVEALED A CRACK ON THE THIN WEB OF CROSSBEAM (X-BEAM).  MGB X-BEAM CHANGED.  REF:  SB 05.00.28, AD 96.156.071	(B)R1.					1	G	7	1 	3U	3	U	NC	H9EU    	E19EU				 
1999081200650	19990812	00650	EU  	1999	8	12	CA990323025      	1	19990127	G	5350	350A210024XX	COWL            			SNIAS 	350   	AS350D      	8680803	EU  	LYC   	LTS101	LTS101600A2 	41560	NE  					FUSELAGE	SEPARATED       	W				A				UNSCHED LANDING         				D			INFLIGHT SEPARATION       			CR	CRUISE         	1			CA								LE43458E			(CAN) DURING FLIGHT, THE FORWARD BELLY COWLING SEPARATED FROM THE AIRCRAFT AND LANDED IN A FIELD.  THE AIRCRAFT LANDED W	ITHOUT INCIDENT.  SUBSEQUENT INVESTIGATION REVEALED THAT 4 LATCHES WERE WORN AND MAY NOT HAVE BEEN POSITIVELY ENGAGED. T	HE LATCHES AND COWLING WERE REPLACED.				1	G	7	1 	3U	3	U		H9EU    	E5NE				 
1999081200651	19990812	00651	CE  	1999	8	12	CA990323026      	1	19990316	G	2841	05160061	GROUND STRAP    			CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A102	1A102OCM    	GL  	FUEL GAUGE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			7290 					255350A48	G13920		(CAN) AIRCRAFT FUEL GAUGES INOPERATIVE/MISREADING.  INSPECTION CARRIED OUT AND GROUND WIRES FOUND CORRODED/BROKEN.  PART	S REPLACED.					1	H	7	1 	3O	3	O		3A19    	E252	5	N	P918	 
1999081200652	19990812	00652	NE  	1999	8	12	CA990323027      	2	19990318	G	7230		WHEEL           			CNDAIR	CL600 	CL6002B19   		EA  	GE    	CF34  	CF343B1     		NE  					COMPRESSOR	DAMAGED         	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		CL	CLIMB          	1			CA								807223			(CAN) NR 1 ENGINE ITT WAS 100 DEGREES CELSIUS HIGHER THAN NR 2 ENGINE DURING CLIMB.  MAXIMUM CONTINUOUS 860 DEGREES CELS	IUS REACHED WITH N1 5 PERCENT BELOW MAXIMUM.  DURING THRUST REDUCTION ON TURN- AROUND, AN UNUSUAL NOISE WAS HEARD FROM N	R 1 ENGINE AND ITT WENT TO 999 DEGREES CELSIUS.  THE ENGINE WAS SHUT DOWN.  POST-FLIGHT BORESCOPE INSPECTION CARRIED OUT	 AND SIGNIFICANT DAMAGE FOUND AT THE 7TH STAGE COMPRESSOR.  THE ENGINE WAS REPLACED.			2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999081200653	19990812	00653	EA  	1999	8	12	CA990323028      	1	19990322	G	2421		GENERATOR       			CNDAIR	CL600 	CL6002B19   		EA  										NR 2	FAILED          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			CA											(CAN) LOSS OF GENERATOR NR 2 DURING FLIGHT.  DAMAGED ELECTRICAL HARNESS AND DAMAGED FCU.  BLUE IDG WIRE RUBBING AND ARCI	NG MELTED FCU PB FITTING ALLOWING FUEL TO LEAK OUT.  AD CF-99-09 ISSUED.					2	L	7	2 	4F			RT	A21EA   					 
1999081200656	19990812	00656	EA  	1999	8	12	CA990323031      	1	19990301	G	5342	M2054901	FITTING         			GRUMAV	TBM   	TBM3EAIRTRD 	3950310	EA  	WRIGHT	R2600 	R260020     	67050	EA  	HAMSTD	23E	23E50       	NE  	HORIZONTAL STAB	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			3888 					78486	FA8853		(CAN) THE DEFECT WAS DETECTED DURING AN ANNUAL INSPECTION.  CORROSION WAS EXTENSIVE ENOUGH TO REQUIRE REPLACEMENT OF THE	 FIN ATTACH FITTING.  ALL AIRCRAFT IN FLEET TO BE SUBJECTED TO SPECIAL INSPECTION IN THE AFFECTED AREA.					1	L	7	1 	4R	4	R		L82     	TC176	6	C	P603	 
1999081200657	19990812	00657	EA  	1999	8	12	CA990323032      	1	19990310	G	5553	M2054901	FITTING         			GRUMAV	TBM   	TBM3AIRTRD  	3950308	EA  	WRIGHT	R2600 	R260020     	67050	EA  	HAMSTD	23E	23E50       	NE  	VERTICAL STAB	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			3282 					W445102	P86995		(CAN) THE DEFECT WAS DETECTED DURING AN ANNUAL INSPECTION.  CORROSION WAS EXTENSIVE ENOUGH TO REQUIRE REPLACEMENT OF THE	 ATTACH FITTING.  ALL AIRCRAFT IN FLEET WILL BE SUBJECTED TO SPECIAL INSPECTION OF THE AFFECTED AREA.					1	L	7	1 	4R	4	R		L82     	TC176	6	C	P603	 
1999081200658	19990812	00658	EA  	1999	8	12	CA990323033      	1	19990310	G	5553	M2054901	FITTING         			GRUMAV	TBM   	TBM3EAIRTRD 	3950310	EA  	WRIGHT	R2600 	R260020     	67050	EA  	HAMSTD	23E	23E50       	NE  	VERTICAL STAB	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			3690 					447247	P56062		(CAN) THE DEFECT WAS DETECTED DURING AN ANNUAL INSPECTION.  CORROSION WAS EXTENSIVE ENOUGH TO REQUIRE REPLACEMENT OF THE	 ATTACH FITTING.  ALL AIRCRAFT IN FLEET WILL BE SUBJECTED TO SPECIAL INSPECTION IN THE AFFECTED AREA.					1	L	7	1 	4R	4	R		L82     	TC176	6	C	P603	 
1999081200674	19990812	00674	SO  	1999	8	12	CA990330017      	2	19990211	G	8530		PISTON          			CESSNA	337   	337D        	2075717	CE  	CONT  	O360  	IO360C      	17025	SO  	MCAULY	2AF34C	D2AF34C302  	GL  	ENGINE	CRACKED         	W				E				ENGINE SHUTDOWN         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			CA				542  				352764	7911029		(CAN) IN CRUISE, THE ENGINE BEGAN TO RUN ROUGH.  ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED.  POST-FLIGHT INSPECTION FOUND	 A CYLINDER PISTON CRACKED.					1	H	7	2 	3O	3	O		A6CE    	E1CE	5	C	P5EA	 
1999070900373	19990709	00373	SW  	1999	7	9	CA990330018      	1	19990317	G	2435	230322711	DAMPENER        			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					START/GENERATOR	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA				412  				CAE832010			(CAN) SEVERAL UNAPPROVED PARTS WERE FOUND DURING DISASSEMBLY AT OVERHAUL OF STARTER/GENERATOR.  A LUCAS BACKPLATE AND FR	ICTION RING WERE FOUND IN PLACE OF THE APC PARTS, BUT THERE WAS NO EVIDENCE OF FAILURE.  CORRECT PARTS WERE PROCURED AND	 INSTALLED.  IN ADDITION, AN EXTRA BEARING RAFFLE DISK P/N 150SG1  017 WAS FOUND BETWEEN THE FAN P/N 150SG1107 AND THE 2	 BELLEVILLE SPRINGS P/N 150SG1093.  ONE BELLEVILLE SPRING WAS INSTALLED BACKWARDS WHICH WAS SUBSEQUENTLY CORRECTED.			1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999081200675	19990812	00675	CE  	1999	8	12	CA990330019      	1	19990317	G	3213	508103237	TORQUE LINK     			BEECH 	100   	A100        	1152915	CE  	PWA   	PT6   	PT6A28      		EA  					MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								PCE51096			(CAN) TORQUE LINK HAS A CRACK AT THE CENTER SINGLE BOLT LUG.  CRACK IS LOCATED ON THE INBOARD RADIUS.						1	L	7	2 	3T	4	T		A14CE   	E4EA				 
1999081200676	19990812	00676	CE  	1999	8	12	CA990330020      	1	19990317	G	2720	03101965	SPRING          			CESSNA	172   	172N        	2072434	CE  	LYC   	O360  	O360A4M     	41514	EA  					RUDDER	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			6852 					L3359036A			(CAN) MAINTENANCE NOTICED A LACK OF TENSION ON RUDDER CABLES DURING INSPECTION.  CAUSE WAS NOTED AS THE FAILURE OF THE R	UDDER RETURN SPRING (LEFT).					1	H	7	1 	3O	3	O	NT	3A12    	E286				 
1999081200677	19990812	00677	NE  	1999	8	12	CA990330021      	2	19990318	G	7260	717000	FILTER          			BOEING	727   	72725       	1384006	NM  	PWA   	JT8   	JT8D7B      	52053	NE  					GEARBOX	LOOSE           	W				C				ABORTED TAKEOFF         				K	J		FLUID LOSS                	WARNING INDICATION        		TO	TAKEOFF        	1			CA			38303	5064 				653765			(CAN) ON TAKEOFF ROLL, NR 2 ENGINE OIL FILTER BYPASS LIGHT CAME ON FOLLOWED BY OIL QUANTITY AND OIL PRESSURE LOSS.  TAKE	OFF REJECTED.  POST-FLIGHT INSPECTION OF THE GEARBOX FOUND ONE OF THE FOUR HELICOILS THAT HOLD THE OIL FILTER COVER ON, 	TO HAVE PULLED OUT OF ITS HOUSING.  THIS CAUSED THE OIL FILTER TO DROP DOWN IN ONE CORNER CAUSING LOSS OF OIL AND OIL PR	ESSURE.  THE GEARBOX WAS REMOVED FOR REPAIR.			2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999081200679	19990812	00679	EA  	1999	8	12	CA990330023      	2	19990310	G	8520	LW10646	ROD             			PIPER 	PA31  	PA31325     	7103105	SO  	LYC   	O540  	TIO540F2BD  	41532	EA  					ENGINE	BROKEN          	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			CA				2144 				L755861A			(CAN) DURING FLIGHT, THE NR 1 ENGINE BEGAN TO LOSE POWER.  THE AIRCRAFT WAS DIVERTED AND LANDED WITHOUT INCIDENT.  POST-	FLIGHT INSPECTION FOUND THE NR 6 CYLINDER PISTON NOT MOVING.  FURTHER INVESTIGATION FOUND THE CONNECTING ROD BROKEN.  TH	E ENGINE WAS REPLACED.				1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999081200680	19990812	00680	NE  	1999	8	12	CA990330024      	3	19990208	G	6111	6101A12	BLADE           													HAMSTD	12D	12D40       	NE  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			271  	231  					AC4113617		(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.  CORROSION FOUND ON THE BLADES.  THE BLADES REQUIRED RE-ANODIZING.																5	C	P257	 
1999082100047	19990821	00047	GL  	1999	8	21	CA990330025      	3	19990203	G	6111	57C0840132	BLADE           													HARTZL	HCA2V	HCA2VK2     	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2394 	805  					J283		(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.  CORROSION WAS FOUND ON THE SPIDER, BEARINGS (P/N 57A0971) AND THE BL	ADES (P/N V8433-7).  THE BLADES WERE CORRODED BEYOND REPAIR.															5	C	P24EA	 
1999081200681	19990812	00681	GL  	1999	8	12	CA990330026      	3	19990330	G	6111		BLADE           													MCAULY	1B90	1B90CM      	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1372 	786  					48895		(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.  CAMBER AND LEADING EDGES OF PROPELLER BLADES REQUIRED OVERHAUL.																5	N	P842	 
1999081200682	19990812	00682	GL  	1999	8	12	CA990330027      	3	19990127	G	6111		BLADE           													MCAULY	1C172	1C172EM     	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA									E17006		(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.  PROPELLER BLADES WERE FOUND CORRODED.																5	N	P910	 
1999081200683	19990812	00683	NE  	1999	8	12	CA990330028      	3	19990225	G	6111	6101A12	BLADE           								PWA   	R1340 	R1340AN1    	52016	NE  	HAMSTD	12D	12D40       	NE  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				367  				4155	7992CPL		(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE BLADE WAS FOUND CORRODED AND INSPECTION FOUND THE TABER BORE WAS 	NOT ANODIZED IAW THE OVERHAUL MANUAL. THE TABER BORE WAS POLISHED AND ANODIZED AND THE FILLETS WERE MACHINED.										3	R			5E2	5	C	P257	 
1999081200684	19990812	00684	GL  	1999	8	12	CA990330029      	3	19990218	G	6111	F8465B7R	BLADE           													HARTZL	HCE2Y	HCE2YR2     	GL  	PROPELLER	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA									BP3956		(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.  THE BLADES WERE FOUND WITH STONE DAMAGE.  THE BLADES WERE TRIMMED.																5	C	P9EA	 
1999081200685	19990812	00685	GL  	1999	8	12	CA990330030      	3	19990218	G	6111	F8465B7R	BLADE           													HARTZL	HCE2Y	HCE2YR2     	GL  	PROPELLER	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA									BP648		(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.  BLADES WERE FOUND WITH STONE DAMAGE.  THE BLADES WERE TRIMMED.																5	C	P9EA	 
1999081200686	19990812	00686	GL  	1999	8	12	CA990330031      	3	19990226	G	6111	G90DCA2	BLADE           			CESSNA	180   	180J        	2072622	CE  	CONT  	O470  	O470R       	17026	SO  	MCAULY	2A34C	2A34C203    	GL  	PROPELLER	DAMAGE          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1893 	1030 				226458R	804542		(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION.  PROPELLER BLADES WERE FOUND WITH STONE DAMAGE. THE BLADES WERE TRIMM	ED.					1	H	7	1 	3O	3	O		5A6     	E273	5	C	P3EA	 
1999081200687	19990812	00687	NE  	1999	8	12	CA990330032      	3	19990303	G	6114	512316	HUB             			DHAV  	DHC3  	DHC3        	2800202	EA  	PWA   	R1340 	S3H1G       	52016	NE  	HAMSTD	23D	23D40       	NE  	PROPELLER	MISREPAIRED     	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA								13008	217049		(CAN) INSPECTION FOUND THE HUB BARREL DOWEL PINS HAD BEEN BRAZED IN PLACE.  IN PLACE OF OVERSIZED DOWELS BEING INSTALLED	.  THEY WERE SCRAPPED AND  REPLACED.  ALSO, THE PROPELLER BLADES WERE FOUND NOT ANODIZED.  THE BLADES WERE ANODIZED AND 	RETURNED TO SERVICE.				1	H	7	1 	3R	3	R		A815    	E142	6	C	P719	 
1999081200688	19990812	00688	GL  	1999	8	12	CA990330033      	3	19990304	G	6111		BLADE           			GULSTM	AA5   	AA5         	0631410	SO  	LYC   	O320  	O320E2G     	41508	EA  	MCAULY	1C172	1C172*      	GL  	PROPELLER	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L4205727A	730056		(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE PROPELLER BLADES WERE FOUND WITH STONE DAMAGE.  THE BLADES WERE T	RIMMED.					1	L	7	1 	3O	3	O		A16EA   	E274	5	N	P910	 
1999081200689	19990812	00689	NM  	1999	8	12	CA990330034      	1	19990309	G	2420		GCU             			BOEING	727   	72782       	1384029	NM  	PWA   	JT8   	JT8D7B      	52053	NE  					ENGINE	FAILED          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			CA								649672			(CAN) NR 1 GENERATOR FIELD BREAKER TRIPPED.  NR 1 GENERATOR AC CONTROL BREAKER TRIPPED. ELECTRICAL FAULT PANEL ALL LIT U	P.  GENERATOR CONTROL UNIT REPLACED.					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999081200690	19990812	00690	SO  	1999	8	12	CA990330037      	2	19990322	G	8520		ROD             			CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  					ENGINE	BROKEN          	W				B	A			EMER. DESCENT           	UNSCHED LANDING         			E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA				1617 				6760R			(CAN) OIL PROBLEM IN-FLIGHT, AIRCRAFT RETURNED TO POINT OF DEPARTURE.  POST-FLIGHT INSPECTION FOUND NO OIL IN THE ENGINE	, BUT OIL WAS FOUND ON THE ENGINE COMPARTMENT.  TEMPERATURE PROBE NUT FOUND LOOSE AND THIS WAS DETERMINED TO BE THE CAUS	E OF THE OIL LEAK.  THE SUBMITTER SUGGESTS THE TEMPERATURE PROBE NUT BE LOCKWIRED.				1	H	7	1 	3O	3	O		3A19    	E252				 
1999081200691	19990812	00691	NE  	1999	8	12	CA990330038      	2	19990322	G	7230	1685MK6	VSV ACTUATOR    			AIRBUS	320   	A320232     	3930326	EU  	IAE   	V2527 	V2527A5     		NE  					NR 2 ENGINE	MALFUNCTIONED   	W				C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			CA			16478					V10080			(CAN) THE AIRCRAFT WAS ON TAKEOFF ROLL WHEN AN ECAM MESSAGE NR 2 COMPRESSOR VANE ILLUMINATED.  THE TAKEOFF WAS ABORTED A	ND THE AIRCRAFT RETURNED TO THE GATE.  THE VARIABLE VANE ACTUATOR AND THE MASTER BLEED ACTUATOR WERE REPLACED, POWER ASS	URANCE RUNS WERE CARRIED OUT SERVICEABLE AND THE AIRCRAFT RETURNED TO SERVICE.				2	L	7	2 	4F	4	F	RT	A28NM   	E40NE				 
1999081200692	19990812	00692	NM  	1999	8	12	CA990330039      	1	19990311	G	2910	AN8144D	PLUG            		AEB215101   	DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					HYDRAULIC SYSTEM	LEAKING         	W				A				UNSCHED LANDING         				K	J		FLUID LOSS                	WARNING INDICATION        		CR	CRUISE         	1			CA						0116H		120063			(CAN) IN-FLIGHT, HYDRAULIC LEAK.  RETURNED TO YOW.  PLUG IN NR 2 MANIFOLD FOUND LOOSE AND NOT LOCKWIRED.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999081200694	19990812	00694	CE  	1999	8	12	CA990330041      	1	19990320	G	3242	1769	STATOR DISK     	BFGOODRICH  	215286      	CESSNA	500   	550         	2076604	CE  	PWA   	JT15  	JT15D4      	52112	NE  					BRAKE	CRACKED         	W				D				RETURN TO BLOCK         				O			OTHER                     			TX	TAXI/GRND HDL  	1			CA				702  		1769		71751			(CAN) BRAKE ASSEMBLIES CRACKING AT STATORS CAUSING SEIZING AND EXCESSIVE DRAGGING.  OPERATOR REQUESTED BF GOODRICH TO SU	PPLY TEARDOWN REPORT THROUGH CESSNA MANUFACTURER.					1	L	7	2 	4F	4	F		A22CE   	E1NE				 
1999081200695	19990812	00695	CE  	1999	8	12	CA990330042      	1	19990313	G	3242	0122	STATOR DISK     	BF GOODRICH 	215286      	CESSNA	500   	550         	2076604	CE  	PWA   	JT15  	JT15D4      	52112	NE  					BRAKE	CRACKED         	W				D				RETURN TO BLOCK         				O			OTHER                     			TX	TAXI/GRND HDL  	1			CA				696  		0122		71751			(CAN) BRAKE ASSEMBLIES CRACKING AT STATORS CAUSING SEIZING AND EXCESSIVE DRAGGING.  OPERATOR REQUESTED BF GOODRICH TO SU	PPLY TEARDOWN REPORT THROUGH CESSNA MANUFACTURER.					1	L	7	2 	4F	4	F		A22CE   	E1NE				 
1999081200696	19990812	00696	CE  	1999	8	12	CA990330043      	1	19990318	G	2510	161102103	CABLE           			CESSNA	172   	172R        	2072401	CE  										COCKPIT  SEAT	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			530  								(CAN) FLIGHT CREW SEAT RELEASE CABLES FOUND TO BE BROKEN INTERNALLY, NEAR HANDLES.						1	H	7	1 	3O			NT	3A12    					 
1999061800016	19990618	00016	EU  	1999	6	18	CA990330044      	1	19990317	G	3397		WIRE            			AIRBUS	300   	A300B4203   	3930306	EU  	GE    	CF6   	CF650C2     	30018	NE  					CARGO BAY	FAILED          	W				H				DEACTIVATE SYST/CIRCUITS				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			CA								455827			(CAN) FORWARD LOWER CARGO COMPARTMENT WIRING CHAFED ON CLAMP ABOVE CEILING LINER, LEADING TO ARCING, BURNING AND TRIPPED	 CIRCUIT BREAKER.  WIRING REPAIRED.					2	L	7	2 	4F	4	F	RT	A35EU   	E23EA				 
1999081200697	19990812	00697	EA  	1999	8	12	CA990330045      	1	19990325	G	2760	840504	WIRE            			CNDAIR	CL601 	CL6012A12   	1900303	EA  										PROX SWITCH	CHAFED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) CURVED FORWARD LEADING EDGE OF FLAP COMES INTO CONTACT TO VERTICALLY MOUNTED PROXIMITY SWITCH AND RUBS SURFACE OF 	WIRE BUNDLE.					2	L	7	2 	4F			RT	A21AE   					 
1999060400330	19990604	00330	EU  	1999	6	4	CA990330053      	1	19990311	G	3242	9595601511	BRAKE           	BFGOODRICH  	5324512049  	PILATS	PC12  	PC12        	7090550	EU  										LH MLG	SEIZED          	W				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			CA			260  			0230					(CAN) AFTER LANDING, BRAKES FAILED TO RELEASE CAUSING TIRE TO BLOW.  THE BRAKES WERE FOUND TO BE SEIZED FROM ACCUMULATIO	N OF CARBON DUST.  AN EVALUATION WAS REQUESTED FROM BF GOODRICH OF THE BRAKE ASSEMBLY.					1	L	7	1 	3T			RT	A78EU   					 
1999081200704	19990812	00704		1999	8	12	CA990330057      	4	19990311	G	3416	280040102	ALTIMETER       	MEGGITT     		BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					COCKPIT	FAILED          	W				O				OTHER                   				J			WARNING INDICATION        			CR	CRUISE         	1			CA			266  					PSO242			(CAN) FLIGHT CREW NOTED THAT THE RIGHT DIGITAL ALTIMETER FAILED AND HAD OPENED THE CIRCUIT BREAKER.  THE CIRCUIT BREAKER	 WOULD NOT RESET.   THE ALTIMETER WAS REPLACED WITH ANOTHER MEGGITT UNIT OF LIKELY THE SAME QUALITY.					2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999081200705	19990812	00705	NE  	1999	8	12	CA990330058      	2	19990315	G	7532	312124803	BLEED VALVE     			CESSNA	208   	208B        	2073701	CE  	PWA   	PT6   	PT6A114A    	52043	NE  					COMPRESSOR	FAILED          	W				C				ABORTED TAKEOFF         				O			OTHER                     			TO	TAKEOFF        	1			CA			1691 					PCEPCD550			(CAN) CREW REPORTED ENGINE SURGING THROUGH 1,500 POUNDS OF TORQUE.  SURGE WOULD NOT OCCUR UNLESS THE POWER WAS REDUCED B	ELOW 1,500 POUNDS TORQUE AND THEN ADVANCED THROUGH 1,500 POUNDS TORQUE.  MAINTENANCE FOUND THE COMPRESSOR BLEED VALVE ST	ICKING AT 1,500 POUNDS OF TORQUE.  THE BLEED VALVE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.				1	H	7	1 	3T	3	T		A37CE   	E4EA				 
1999081200706	19990812	00706	CE  	1999	8	12	CA990330059      	1	19990315	G	3244	114800129	WEIGHT          			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					NLG WHEEL	LOOSE           	W				C				ABORTED TAKEOFF         				E			VIBRATION/BUFFET          			TO	TAKEOFF        	1			CA			548  								(CAN) DURING ROTATION,THE FLIGHT CREW REPORTED A SEVERE SHIMMY AND VIBRATION THAT CONTINUED THROUGH THE CLIMB, EVENTUALL	Y SUBSIDING.  THE WHEEL WAS DISASSEMBLED AND THE WEIGHT PATCH WAS FOUND TO HAVE COME UNGLUED.					2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999081200707	19990812	00707	CE  	1999	8	12	CA990330060      	1	19990318	G	3234		HARNESS         			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					MLG	CHAFED          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			CA								PCEPS0163			(CAN) UPON GEAR SELECTION AFTER TAKEOFF, THE CREW COULD NOT RETRACT THE LANDING GEAR.  MAINTENANCE FOUND THE MAIN WIRE B	UNDLE ASSOCIATED WITH THE HANDLE CONTROL ASSY TO BE CHAFED.					2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999081200724	19990812	00724	GL  	1999	8	12	CA990330079      	3	19990312	G	6110		PROPELLER ASSY  			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2B   	41532	EA  	HARTZL	HCE2Y	HCE2YR2     	GL  	FORWARD	MISOVERHAULED   	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA			4707 	1800 				L161761	CJ505		(CAN) THE SUBMITTER SCRAPPED THIS PROPELLER AND A NEW PROPELLER WAS TAKEN INTO SERVICE. THE SUBMITTER REPORTS THAT THE P	REVIOUS OVERHAUL WAS LOW COST AND QUESTIONABLE PARTS WERE REINSTALLED.  SINCE THAT OVERHAUL, ROTATIONAL PLAY IN THE BLAD	ES WAS REPORTED AND VIBRATIONS WERE EVIDENT.  THE LOW COST OVERHAUL WAS NOT DONE BY THE SHOP THAT HAS SUBMITTED THIS SDR	.			1	L	7	2 	3O	3	O		A20SO   	E14EA	5	C	P9EA	 
1999081200725	19990812	00725	EU  	1999	8	12	CA990330080      	1	19990318	G	3297		WIRE            			AEROSP	ATR42 	ATR42300    	8680920	EU  	PWA   	120   	PW120       	 	NE  	HAMSTD	14SF	14SF5       	NE  	MLG	DAMAGED         	W				C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			CA											(CAN) UNABLE TO RETRACT LANDING GEAR. INVESTIGATION REVEALED BROKEN WIRE BETWEEN PSEU AND THE LANDING GEAR SELECTOR VALV	E.  WIRE REPAIRED.					2	H	7	2 	4T	4	T	RT	A53EU   	E20NE	6	C	P7NE	 
1999081200726	19990812	00726	SO  	1999	8	12	CA990330081      	1	19990319	G	3230	41949003	UPLOCK          	PIPER       		PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2B   	41532	EA  					LT MLG	DIRTY & RUSTY   	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			CA			11734					L98161			(CAN) LEFT HAND LANDING GEAR HOOK FAILED TO MOVE INTO POSITION ON RETRACTION AFTER TAKEOFF.  INVESTIGATION FOUND ACCUMUL	ATED DIRT AND RUST ON THE UPLOCK ROD, TELESCOPIC END, UNDER THE DUST BOOT, CAUSING SLUGGISH OPERATION OF UPLOCK HOOK.  I	T IS TO BE NOTED THAT CLEANING AND LUBRICATION IS REQUIRED AFTER EACH LANDING GEAR AND WHEELWELL WASHING.				1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999081200729	19990812	00729	CE  	1999	8	12	CA990330084      	1	19990315	G	2731	656500757CR	CONTROL CABLE   			CESSNA	500   	550         	2076604	CE  	PWA   	JT15  	JT15D4      	52112	NE  					ELEVATOR TRIM	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			3318 					71769			(CAN) CABLE FRAYED UNDER NOSE DOWN STOP BLOCK, STOP BLOCKS UTILIZE A CLAMPING PRESSURE DIRECTLY TO THE CABLE.  OVERTIGHT	ENING WILL CAUSE THE DEFORMATION AND STRESS THE CABLE STRANDS.  NEW CABLE INSTALLED.					1	L	7	2 	4F	4	F	 	A22CE   	E1NE				 
1999081200730	19990812	00730	CE  	1999	8	12	CA990330085      	1	19990316	G	5540	12124095	BULKHEAD        			CESSNA	210   	210J        	2073439	CE  	CONT  	O520  	IO520J      	17032	SO  					RUDDER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2598 					553574			(CAN) WHILE COMPLYING WITH AD 72-07-09, THE INSPECTOR DETECTED A CRACK AT THE LOWER INBOARD CORNER OF THE RIGHT RUDDER C	ABLE CUT-OUT OF THE AFT BULKHEAD.  CRACK RUNS AT A 45 DEGREE ANGLE BELOW THE BOLT HOLE CUT-OUT.					1	H	7	1 	3O	3	O		3A21    	E5CE				 
1999082000993	19990820	00993	NE  	1999	8	20	CA990401001      	2	19990304	G	8530		CYLINDER        	GBZH        		DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					ENGINE	SEPARATED       	W				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CL	CLIMB          	1			CA				353  		JP206670		JP206670			(CAN) ON CLIMB-OUT, PILOT REPORTED THE ENGINE STARTED TO LOOSE POWER.  PILOT RETURNED TO POINT OF DEPARTURE.  POST-FLIGH	T INSPECTION REVEALED THE NR 9 CYLINDER HAD SEPARATED.  THE NR 9 CYLINDER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERV	ICE.				1	H	7	1 	3R	3	R		A806    	5E1				 
1999043000102	19990430	00102	NE  	1999	4	30	CA990401002      	2	19990316	G	7230		BEARING         			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					NR 1 ENGINE	FAILED          	W				E	G			ENGINE SHUTDOWN         	O2 MASK DEPLOYED        			B	K		SMOKE/FUMES/ODORS/SPARKS  	FLUID LOSS                		DE	DESCENT        	1			CA			3012 					PCEPS0144			(CAN) ON APPROACH, THE CREW REPORTED FLASHES OF LIGHT COMING FROM NR 1 ENGINE EXHAUST.  THIS WAS FOLLOWED IMMEDIATELY BY	 A SLIGHT YAWING OF THE AIRCRAFT.  TORQUE FLUCTUATIONS AND AN INCREASE IN ITT ON THE NR 1 ENGINE.  THE ENGINE WAS SHUT D	OWN.  THERE WAS MILD TO MEDIUM SMOKE CONTAMINATION IN THE CABIN, THE OXYGEN MASKS WERE DEPLOYED, AND THE SMOKE EVACUATED	.  THE LANDING WAS UNEVENTFUL.  POST-FLIGHT INSPECTION FOUND THE 1ST STAGE COMPRESSOR DIFFICULT TO TURN BY HAND AND OIL 	COMING FROM THE AIR INLET INDICATING A FAILURE OF NR 1 BEARING, BUT THIS IS NOT CONFIRMED.  FURTHER REPORT TO FOLLOW.		2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999082000995	19990820	00995		1999	8	20	CA990401005      	1	19990305	G	2434	15881703	BEARING         	BENDIX      	30B10711A   															GENERATOR	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						1056					(CAN) ANTI-DRIVE END BEARING FAILURE CAUSING MAJOR DAMAGE TO ROTOR, EXCITER STATOR, AND MAIN STATOR.  ALSO NOTED UNAPPRO	VED INSULATORS WERE INSTALLED (COMMERCIAL SLEEVING) INSTEAD OF THE CORRECT 5 INSULATORS P/N 22-200-026.																		 
1999082000996	19990820	00996	SW  	1999	8	20	CA990401006      	1	19990325	G	6510	204040623005	BEARING         		212040600009	BELL  	205   	205A1       	1181414	SW  	LYC   	T53   	T5313B      	41549	NE  					T/R DRIVE SHAFT	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			467  			A2003389		LE07560A			(CAN) DURING INSPECTION, GREASE SHIELD WAS FOUND MOVED/TURNED BY THE SLIP MARK.  BEARING REPLACED.						1	G	7	1 	4U	4	U		H1SW    	E17EA				 
1999082000997	19990820	00997	NE  	1999	8	20	CA990401007      	3	19990318	G	6111	6101A18	BLADE           													HAMSTD	2D	2D30        	NE  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						T23514			T23514		(CAN) DURING OVERHAUL, CORROSION WAS FOUND ON THE PROPELLER BLADES SHANK AND IN THE BLADE TAPER BORES. THE BLADES WERE M	ACHINED TO THE OVERHAUL SPECIFICATIONS AND RETURNED TO SERVICE.															5	C	P206	 
1999082000998	19990820	00998		1999	8	20	CA990401008      	4	19990323	G	3417	ARP4000622981910	CONNECTOR       			CNDAIR	CL600 	CL6002B19   		EA  										AIR DATA	MISMANUFACTURED 	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						216					(CAN) COMPONENT FOUND WITH PIN E SHEARED OFF UPON RECEIPT FROM MANUFACTURE.						2	L	7	2 	4F			RT	A21EA   					 
1999082000999	19990820	00999	CE  	1999	8	20	CA990401009      	1	19990325	G	5711		SPAR            			CESSNA	188   	A188        	2073004	CE  										WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			3500 								(CAN) REAR SPAR CRACK IN RADIUS AT ROOT ATTACH POINT.  ALSO A FRONT SPAR CRACK IN RADIUS AT ROOT ATTACH POINT.						1	L	7	1 	3O				A9CE    					 
1999082001000	19990820	01000	CE  	1999	8	20	CA990401010      	1	19990325	G	5711		SPAR            			CESSNA	188   	A188        	2073004	CE  										WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) REAR SPAR CRACK IN THE RADIUS AT THE ROOT ATTACH POINT.						1	L	7	1 	3O				A9CE    					 
1999082001001	19990820	01001	SO  	1999	8	20	CA990401011      	1	19990318	G	8120	LW12689	TURBOCHARGER    			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540F2BD  	41532	EA  					ENGINE	LEAKING         	W				E	F			ENGINE SHUTDOWN         	ACTIVATE FIRE EXT.      			A			FLAME/FIRE                			TX	TAXI/GRND HDL  	1			CA				1175 		AR158		RL78268A			(CAN) ON LANDING OIL SEAL LEAK FROM TURBOCHARGER IGNITED.  WHEN THE ENGINE WAS RETARDED TO IDLE, THERE WAS NO DAMAGE TO 	THE AIRCRAFT OR ENGINE COMPONENTS.					1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999082700102	19990827	00102	EU  	1999	8	27	CA990401012      	1	19990313	G	2435	4435	BEARING         	LUCAS       	23080005    	BRAERO	DH125 	BAE125800A  	1500285	EU  										STARTER/GEN	DAMAGED         	W				O				OTHER                   				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			CA				938  		4435					(CAN) PILOTS REPORTED THE NR 2 GENERATOR FELL OFF-LINE AND WOULD NOT RESET.  STARTER /GENERATOR SHAFT SHEARED BECAUSE TH	E BEARINGS HAD FAILED.					2	L	7	2 	4F			RT	A3EU    					 
1999090200002	19990902	00002	EA  	1999	9	2	CA990401013      	2	19990317	G	7322		FCU             			PIPER 	PA32  	PA32RT300T  	7103216	SO  	LYC   	O540  	TIO540S1AD  	41532	EA  	HARTZL	HCE2Y	HCE2YR1     	GL  	ENGINE	MALFUNCTIONED   	W				A				UNSCHED LANDING         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CR	CRUISE         	1			CA								L567267A	DK1293		(CAN) THE ENGINE WAS RUNNING ROUGH, IN CRUISE, WITH MOMENTARY LOSS OF POWER. THIS  ENGINE HAD BEEN RUNNING INTERMITTENTL	Y FOR SOME TIME.  THE REPLACEMENT OF THE ELECTRIC FUEL PUMP AND THE FUEL CONTROL UNIT SEEMED TO HAVE SOLVED THIS PROBLEM	.				1	L	7	1 	3O	3	O		A3SO    	E14EA	5	C	P9EA	 
1999082700906	19990827	00906	SO  	1999	8	27	CA990401015      	1	19990322	G	5712		RIB             			PIPER 	PA34  	PA34200     	7103405	SO  	LYC   	O360  	IO360C1E6   	41514	EA  					BS 69	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4383 					L1656151A			(CAN) AT 1,000-HOUR INSPECTION, FOUND TWO CRACKS (FORWARD TOP CORNER AND TOP MIDDLE) ON DOUBLE RIB STA 69.24 ON RT WING 	IN GEAR WHEELWELL.					1	L	7	2 	3O	3	O		A7SO    	1E10				 
1999082700104	19990827	00104		1999	8	27	CA990401016      	4	19990314	G	2562	AV12NSN	ANTENNA         			PIPER 	PA23  	PA23250     	7102308	SO  	LYC   	O540  	IO540C4B5   	41532	EA  					ELT	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L372748			(CAN) TECHNICIAN FOUND ELT ANTENNA COMPLETELY BROKEN OFF.  IT WAS OK AT PILOT WALK-AROUND AT DEPARTURE.  VOR ANTENNA APP	EARED TO BE PARTLY SHEARED OFF.  AIRCRAFT HAD RECENTLY FLOWN INTO ICING CONDITIONS.  ALSO HAD PRE-FLIGHT DE-ICING.					1	L	7	2 	3O	3	O		1A10    	1E4				 
1999082700108	19990827	00108	CE  	1999	8	27	CA990401023      	1	19990317	G	7920	130F00612D022	FITTING         			BEECH 	99    	99          	1154002	CE  	PWA   	PT6   	PT6A28      		EA  	HARTZL	HCB3T	HCB3TN3     	GL  	ENGINE OIL	LOOSE           	W				E				ENGINE SHUTDOWN         				K	J		FLUID LOSS                	WARNING INDICATION        		CR	CRUISE         	1			CA			1801 					PCE51811	BU4989		(CAN) DECREASING OIL PRESSURE WITH SLIGHT FLUCTUATIONS ON NR 1 ENGINE.  PRECAUTIONARY ENGINE SHUTDOWN CARRIED OUT - UNEV	ENTFUL LANDING.  INBOARD LINE FROM OIL COOLER FOUND TO BECAUSE OF OIL LEAK.  NO PREVIOUS RECORDED ACTIVITY PACK TO ORIGI	NAL INSTALLATION RELATED TO CAUSING THE LOOSENING OF THE FLARED FITTING.				1	L	7	2 	3T	4	T		A14CE   	E4EA	6	C	P15EA	 
1999082700109	19990827	00109		1999	8	27	CA990412001      	4	19990325	G	2562	400010	SWITCH          			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ELT	FAILED          	W				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			CA								CAE823364			(CAN) ELT G-SWITCH FOUND TO BE U/S DURING ANNUAL RECERTIFICATION.   ELT UNIT RETURNED TO MANUFACTURER FOR REPAIR.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999082700110	19990827	00110	NE  	1999	8	27	CA990412002      	2	19990320	G	7261	59500342	LINE            			CESSNA	208   	208B        	2073701	CE  	PWA   	PT6   	PT6A114     	52043	NE  					OIL SEPARATOR	CRACKED         	W				O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			CA			6955 			PCE19183		PCE19183			(CAN) PILOT REPORTED AN OIL LEAK AT THE FRONT OF THE ENGINE.  THE ENGINE WAS CLEANED AND RUN-UP. INSPECTION REVEALED A C	IRCUMFERENTIAL CRACK APPROXIMATELY ONE-HALF WAY AROUND THE OIL SEPARATOR REFERENCE LINE, WHERE IT IS WELDED TO THE BODY.	  A NEW PART HAS BEEN ORDERED FOR INSTALLATION.				1	H	7	1 	3T	3	T		A37CE   	E4EA				 
1999082700111	19990827	00111	EA  	1999	8	27	CA990412003      	2	19990329	G	7321	32447452	FCU             			BEECH 	90    	C90         	1152913	CE  	PWA   	PT6   	PT6A21      	52043	EA  					NR 2 ENGINE	FAILED          	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CR	CRUISE         	1			CA				4131 				PCE24338			(CAN) DURING CRUISE, THE NR 2 ENGINE BEGAN TO SURGE AND RUN ROUGH, THE T5 AND TORQUE BEGAN TO FLUCTUATE AND THE PILOT HA	D NO CONTROL OF POWER.  THE ENGINE WAS SHUT DOWN AND AN UNEVENTFUL LANDING WAS CARRIED OUT.  POST-FLIGHT INSPECTION FOUN	D THE FUEL CONTROL UNIT DRIVE SHAFT SHEARED.  NO OTHER ABNORMALITIES WERE FOUND.  THE FCU AND THE FUEL PUMP WERE REPLACE	D AND THE AIRCRAFT WAS RETURNED TO SERVICE.			1	L	7	2 	3T	4	T		3A20    	E4EA				 
1999082700112	19990827	00112	NE  	1999	8	27	CA990412004      	2	19990324	G	7532	672905001	BLEED VALVE     	JANITROL    		BOEING	737   	7372H4      	138448C	NM  	PWA   	JT8   	JT8D9A      	52048	NE  					NR 2 ENGINE	FAILED          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			CA						5720900		P678078			(CAN) AFTER TAKEOFF, THE FLIGHT CREW WAS UNABLE TO OPEN THE NR 2 ENGINE BLEED SHUT-OFF VALVE.  THE AIRCRAFT RETURNED TO 	ITS POINT OF DEPARTURE AND MADE AN UNEVENTFUL LANDING.  MAINTENANCE REPLACED THE VALVE AND THE AIRCRAFT RETURNED TO SERV	ICE.				2	L	7	2 	4F	4	F		A16WE   	E2EA				 
1999082700113	19990827	00113	CE  	1999	8	27	CA990412005      	1	19990327	G	5610	10138402516	WINDSHIELD      	PPG         		BEECH 	200   	B200        	1152922	CE  	PWA   	PT6   	PT6A41      	52043	EA  					COCKPIT	SHATTERED       	W				B	I	A		EMER. DESCENT           	CABIN DEPRESSURIZATION  	UNSCHED LANDING         		D			INFLIGHT SEPARATION       			CR	CRUISE         	1			CA			1474 			92352H2915		PCE80171			(CAN) COPILOT WINDSHIELD INNER PLY SHATTERED.  AIRCRAFT WAS IN CRUISE AT 27,000 FEET AT MAXIMUM CABIN DIFFERENTIAL (6.0 	PSI).  FLIGHT CREW DEPRESSURIZED AIRCRAFT AND DESCENDED TO 12,000 FEET.					1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999082700115	19990827	00115	SO  	1999	8	27	CA990412007      	1	19990322	G	5620	45099013	WINDOW          			PIPER 	PA31T 	PA31T       	7103124	SO  	PWA   	PT6   	PT6A28      		EA  					CABIN	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			15067					PCE50170			(CAN) MAINTENANCE CARRIED OUT A SPECIAL INSPECTION OF THE AIRCRAFT WINDOWS.  WINDOW CRACKS WERE DISCOVERED.   CRACKS WER	E NOT SEVERE TO CAUSE WINDOW SEPARATION, BUT DID EXCEED ALLOWABLE LIMITS FOR PRESSURIZED FLIGHT.   FLEET AIRCRAFT INSPEC	TED (WITH PRISM).  CRACKS WERE DISCOVERED IN VARIOUS WINDOWS (COCKPIT AND CABIN SIDE ACRYLIC).  RECOMMEND REDUCING PIPER	 INTERVAL OF 1,000 HOURS (INSPECTION) TO 500 HOURS.			1	L	7	2 	3T	4	T		A8EA    	E4EA				 
1999082700119	19990827	00119	NM  	1999	8	27	CA990412011      	1	19990325	G	3230	101085	VALVE           			BOEING	727   	727227      	1384078	NM  	PWA   	JT8   	JT8D9A      	52048	NE  					MLG	FAILED          	W				J	A			DUMP FUEL               	UNSCHED LANDING         			K	J		FLUID LOSS                	WARNING INDICATION        		CL	CLIMB          	1			CA						2548A		666036			(CAN) TOTAL 'A' SYSTEM HYDRAULIC SYSTEM LOSS - QUANTITY AND PRESSURE.  MAIN GEAR LOCK OPERATED SEQUENCE VALVE FAILED.  R	EPLACED.					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999082700120	19990827	00120	CE  	1999	8	27	CA990412012      	1	19990331	G	2150	AD1134121246	DUCT            			CESSNA	500   	550         	2076604	CE  	PWA   	JT15  	JT15D4      	52112	NE  					COOLING SYSTEM	SEPARATED       	W				B	A			EMER. DESCENT           	UNSCHED LANDING         			J			WARNING INDICATION        			CR	CRUISE         	1			CA			3582 					71714			(CAN) FLOOD COOLING DUCT CLAMP REQUIRED RE-ATTACHMENT AFTER DUCT FOUND SEPARATED.   AIRCRAFT EXPERIENCED INCREASE IN RAT	E OF CLIMB.  PRESURIZATION UNABLE TO BE MAINTAINED WITH COOLING DUCT SEPARATED.					1	L	7	2 	4F	4	F		A22CE   	E1NE				 
1999082700121	19990827	00121	GL  	1999	8	27	CA990412013      	3	19990326	G	6111	F8475D4	BLADE           	FRZV        		PIPER 	PA32  	PA32300     	7103212	SO  	LYC   	O540  	IO540K1A5   	41532	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			675  	297  				L1003948	CH16707		(CAN) PAINT REMOVED FROM PROPELLER BLADES FOR INSPECTION.  CORROSION WAS FOUND AND EXTRA WORK WAS REQUIRED TO REMOVE THE	 CORROSION PER HARTZELL MANUAL 133C.					1	L	7	1 	3O	3	O		A3SO    	1E4	5	C	P920	 
1999061800018	19990618	00018	NM  	1999	6	18	CA990413013      	1	19990401	G	2497		WIRE            			DHAV  	DHC8  	DHC8301     	       	NM  										CABIN	CHAFED          	W				O				OTHER                   				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			CA			9918 								(CAN) WIRE BUNDLE BEHIND WARDROBE SHELF CHAFING.  OPERATOR FOUND LARGE WIRE HARNESS ON LOWER SHELF, FORWARD OUTBOARDD CO	RNER OF SHELF.  BLACK, ERODED WIRES OVERHEATED AND 5 FUSED TOGETHER.					2	H	7	2 	4T			RT	A13NM   					 
1999060400331	19990604	00331	NM  	1999	6	4	CA990413014      	1	19990322	G	2710	F52036	CONTROL ROD     			UNIVAR	415   	F1A         	0420204	NM  	CONT  	C90   	C9012F      	17009	SO  					AILERON	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1369 					47790			(CAN) INTERNAL CORROSION OF CONTROL RODS WAS FOUND.  THE AILERON CONTROL ROD (RT) WAS CORRODED THROUGH AT ROD-END INBOAR	D TO ATTACHMENT LUG AT AILERON BELLCRANK.  (WING ROOT AREA).  PN F-52036 EXTERNAL CORROSION OF 50 PERCENT OF WALL THICKN	ESS WAS FOUND ON BOTTOM SURFACE OF THE ELEVATOR CONTROL ROD.  PN F-52022.				1	L	7	1 	3O	3	O		A787    	E252				 
1999070900382	19990709	00382	NM  	1999	7	9	CA990420030      	1	19990413	G	6510	B2241	DRIVESHAFT      			ROBSIN	R22   	R22BETA     		NM  	LYC   	O320  	O320B2C     	41508	EA  					TAIL ROTOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1868 			9996		L1624439A			(CAN) DURING INSPECTION OF THE T/R DRIVE SHAFT, IT WAS NOTED THAT THE PAINT WAS PEELING.  PAINT WAS THEN REMOVED AND SUR	FACE CORROSION WAS DETECTED BOTH INSIDE AND OUTSIDE THE TUBE.  THE TUBE IS DEFORMED AND THE NOMINAL DIAMETER IS 0.009 IN	CH UNDER MANUFACTURER'S SPECIFICATION.  THE MAINTENANCE MANUAL ALLOWS 0.002 INCH MAXIMUM REDUCTION.  TUBE B224-1 WILL BE	 REPLACED AND AIRCRAFT RETURNED TO SERVICE.  NO SIGN THAT THE TAILROTOR HAD BEEN IMPACTED WHATSOEVER.			1	G	7	1 	3O	3	O		H10WE   	E274				 
1999061800019	19990618	00019	EA  	1999	6	18	CA990420032      	1	19990420	G	5744	601R130001	LUG             			CNDAIR	CL600 	CL6002B19   		EA  										LT AILERON	CRACKED         	W				O				OTHER                   				F			FLT CONT AFFECTED         			CR	CRUISE         	1			CA			850  			SBRJ312					(CAN) FLIGHT CREW REPORTED .8 DEGREES RIGHT WING DOWN REQUIRED.  INITIAL REWORK OF LE FLAP DID NOT CORRECT PROBLEM.  FUR	THER INVESTIGATION REVEALED EXCESSIVE BACKLASH IN THE LT AILERON.  EXAMINATION OF AILERON ATTACHMENT POINTS REVEALED CRA	CKING AND SEPARATION OF BOTH INBOARD  AND OUTBOARD PCU ATTACHMENT (NARROWER) LUGS.  OPERATOR ALSO REPORTED OBSERVING PLA	Y IN THE FEEDBACK LINKAGE OF THE INBOARD PCU.  THE CENTER MOUNT POINT LOBES WERE SPLIT OPEN AT THE TOP PORTION.  BOTH PC	U'S AND LINK ASSEMBLIES WERE REPLACED.  SEE ORIGINAL FOR MORE DETAILS.		2	L	7	2 	4F			RT	A21EA   					 
1999060400332	19990604	00332	CE  	1999	6	4	CA990423001      	1	19990408	G	5343		SKIN            			CESSNA	401   	401         	207590C	CE  	CONT  	O520  	TSIO520EB   	17040	SO  	MCAULY	3AF32C	3AF32C87    	GL  	NLG WW	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			6294 					271461R	772967		(CAN) NLG DRAG BRACE REVEALED SIDE-TO-SIDE PLAY.  INVESTIGATION REVEALED CRACKS IN THE SKIN SURROUNDING THE LEFT HAND AT	TACHMENT POINT FOR THE DRAG BRACE.  THE BULKHEAD NORMALLY PROVIDING SUPPORT FOR THE SKIN IN THAT AREA WAS NO LONGER ATTA	CHED.  THE RIVETS HAD SHEARED ALLOWING THE MOVEMENT AND SUBSEQUENT CRACKING.   A PREVIOUS TOWING INCIDENT WHICH HAD EXCE	EDED THE TOWING LIMITS IS LIKELY THE CAUSE.   AFTER THE INCIDENT, DAMAGE WAS NOT READILY VISIBLE FROM THE WHEEL WELL.  T	O VIEW THE DAMAGE, IT IS NECESSARY TO REMOVE THE FLOOR OF THE NOSE BAGGAGE COMPARTMENT.  THIS INSPECTION IS RECCOMMENDED	 FOR ANY INCIDENTS EXPERIENCED OF A NOSE STEERING OVER LIMIT CONDITIONS.	1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22E	 
1999082700122	19990827	00122	GL  	1999	8	27	CA990423005      	3	19990412	G	6110	3003999	SHAFT           								PWA   	PT6   	PT6A21      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	PROPELLER ASSY	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				367  		PCE252233		PCE252233			(CAN) DURING RENTAL ENGINE RE-CERTIFICATION INSPECTION, THE PROPELLER SHAFT FLANGE WAS FOUND CRACKED.  THE CRACK WAS 2.5	0 INCHES LONG CIRCUMFERENTIALLY FOLLOWING RADIUS OF SHAFT TO THE FLANGE.  NO PROP STRIKE INCIDENTS WERE RECORDED IN THE 	LOG BOOKS.   PRELIMINARY INDICATIONS WERE THAT THE PROP SHAFT WAS PURCHASED FROM A VENDOR IN AN OVERHAULED CONDITION.  P	&W REQUESTED AN INVESTIGATION  INTO THE OVERHAUL PROCESSES.								4	T			E4EA	6	C	P15EA	 
1999052800097	19990528	00097	NE  	1999	5	28	CA990423012      	2	19990101	G	7200		ENGINE          			SNIAS 	350   	AS350B2     	8680813	EU  	TMECA 	ARRIEL	ARRIEL1D    		NE  					ENGINE BAY	FAILED          	W				C	R			ABORTED TAKEOFF         	AUTOROTATION            			X	A		ENGINE FLAMEOUT           	FLAME/FIRE                		TO	TAKEOFF        	1			CA			597  					9540			(CAN) ENGINE FAILURE ON TAKEOFF AT APPROXIMATELY 50 FEET.  FLAME AND DEBRIS OBSERVED COMING FROM TAILPIPE, BY GROUND PER	SONNEL.   SUCCESSFUL AUTOROTATION EXECUTED.  NO FURTHER DAMAGE.   FAILURE APPEARS TO BE IN THE GAS PRODUCER SECTION.  NO	 FURTHER INFO AT THIS TIME.				1	G	7	1 	3U	3	U		H9EU    	E19EU				 
1999061800020	19990618	00020	EA  	1999	6	18	CA990423016      	1	19990422	G	4920	GTCP36150RJ	APU             			CNDAIR	CL600 	CL6002B19   		EA  										APU BAY	FAILED          	W				F				ACTIVATE FIRE EXT.      				A			FLAME/FIRE                			TX	TAXI/GRND HDL  	1			CA						304					(CAN) AFTER APU START AND BLEEDS TRANSFERRED TO APU, THE RPM DROPPED AND EGT VENT WENT HIGH WITH NO WARINING IN THE COCK	PIT.  APU SHUTDOWN MANUALLY.  APU STARTED AGAIN ON GROUND,  EGT WENT TO 580 DEGREES CELSIUS AT 50 PERCENT RPM, FOLLOWED 	BY A 2 METER LONG FIRE FROM THE EXHAUST WITHOUT FIRE WARNING.   AWAITING INFO.				2	L	7	2 	4F			RT	A21EA   					 
1999052800098	19990528	00098	EA  	1999	5	28	CA990430007      	2	19990409	G	7200		ENGINE          			ROBSIN	R44   	R44         	7640120	WP  	LYC   	O540  	O540F1B5    	41532	EA  					ENGINE BAY	FAILED          	W				R	A			AUTOROTATION            	UNSCHED LANDING         			E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CL	CLIMB          	1			CA			1007 					L2499940A			(CAN) THE ENGINE STARTED TO SURGE AND VIBRATE IN CLIMB.  THE PILOT ATTEMPTED TO RETURN TO BASE, WHEN THE ENGINE QUIT.  T	HE AIRCRAFT AUTOROTATED TO THE GROUND.   FURTHER REPORT TO FOLLOW.					1	G	7	1 	3O	3	O		H11NM   	E295				 
1999070900387	19990709	00387	EU  	1999	7	9	CA990430009      	1	19990423	G	6330	10510157	SUPPORT         			BOLKMS	105   	BO105C      	5626005	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TRANSMISSION	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								CAE800130			(CAN) DURING INSPECTION OF TRANSMISSION SUPPORTS AND UPON REMOVAL OF CLEAR ADHESIVE TAPE, MINOR SURFACE CORROSION WAS FO	UND ON FORWARD STRUT OF LT SUPPORT ASSY.  CORROSION WAS IN AREA WHERE PAINT HAD FLAKED OFF.  CORROSION REMOVED, AREA TRE	ATED AND RE-PAINTED.				1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999052800099	19990528	00099	EA  	1999	5	28	CA990430023      	2	19990414	G	7200		ENGINE          			PIPER 	PA42  	PA42720     	7104212	SO  	PWA   	PT6   	PT6A61      	52043	EA  					NR 2	FAILED          	W				O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			CA			3268 					PCE99130			(CAN) NR 2 ENGINE WOULD NOT START.  INVESTIGATION DETERMINED THE COMPRESSOR SECTION WOULD NOT ROTATE.  ENGINE REMOVED FO	R OVERHAUL, FURTHER REPORT TO FOLLOW.					1	L	7	2 	4T	4	T		A23SO   	E4EA				 
1999060400333	19990604	00333	CE  	1999	6	4	CA990430035      	1	19990428	G	2497		WIRE            			CESSNA	500   	550         	2076604	CE  	PWA   	JT15  	JT15D4      	52112	NE  					GLARESHIELD	CHAFED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								71751			(CAN) INSTRUMENT PANEL WIRING AFFECTED BY VARIOUS MANUFACTURE HARDWARE INSTALLATIONS.  CESSCOM SERVICE CONDITION REPORT 	FILED 180729 WITH CESSNA ENGINEERING.  OTHER SDRS NOTED.					1	L	7	2 	4F	4	F	 	A22CE   	E1NE				 
1999060400334	19990604	00334	EU  	1999	6	4	CA990430036      	1	19990409	G	5531	D33000001	SPAR            			WSK   	M18   	M18DROMADER 	9810102	EU  										VERT STABILIZER	FRACTURED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1107 								(CAN) THE VERTICAL FIN REAR MAIN SPAR WEB BELOW THE UPPER RUDDER HINGE FOUND TO BE CRACKED IN SEVERAL PLACES.  DISCUSSIO	NS WITH THE MANUFACTURER REVEALED THAT THE LATEST MODELS OF THIS AIRCRAFT HAVE A STRONGER REAR SPAR IN THE FIN.					1	L	7	1 	3O				A47EU   					 
1999052800102	19990528	00102	NE  	1999	5	28	CA990430053      	2	19990302	G	7230	UL16208	ANNULUS FILLER  		M01623AA    	BOEING	757   	757*        		NM  	RROYCE	RB211 	RB211535E4  	54555	NE  					NR 2 ENGINE	FAILED          	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			E	M		VIBRATION/BUFFET          	OVER TEMP                 		CL	CLIMB          	1			CA			23892			DM3999		30557			(CAN) NR 2 ENGINE SURGED AT CONSTANT POWER AT 3000.  ENGINE WAS SHUTDOWN.  WINDMILL RPM WAS ABNORMAL, N1 SPOOLED DOWN AS	 ENGINE EGT EXCEEDED RED LINE.  EGT PEAKED AT 953 DEGREES FOR 5 SECONDS.  FAILED ANNULUS FILLER BITS RECOVERED AND WERE 	SENT TO ROLLS ROYCE FOR INVESTIGATION.  ENGINE STRIP REVEALED FAN CASE HOLED AND TWO FAN BLADES DAMAGED, SOME DAMAGE FOU	ND IN IP TURBINE AND HP COMPRESSOR.			2	L	7	2 	4F	4	F	RT	A2NM    	E12EU				 
1999052800104	19990528	00104	GL  	1999	5	28	CA990430056      	2	19990303	G	7532		PIN             		A70152      	EMB   	145   	EMB145      		SO  	ALLSN 	AE300 	AE3007A     		GL  					BLEED VALVE	LOOSE           	W				E				ENGINE SHUTDOWN         				F	E	M	FLT CONT AFFECTED         	VIBRATION/BUFFET          	OVER TEMP                 	LD	LANDING        	1			CA			1950 	249  				310067			(CAN) DURING LANDING ROLLOUT, WHILE IN REVERSE, THE NR 1 ENGINE FLAMED OUT.   ATTEMPTS TO RESTART THE ENGINE AT THE GATE	 RESULTED IN A HUNG START.  BORESCOPE OF THE ENGINE REVEALED SEVERE HP TURBINE DAMAGE, BLADES REDUCED TO STUBS.   ENGINE	 STRIP CONFIRMED HP1 BLADES FAILED THROUGH AEROFOIL, LEAVING FRACTURE SURFACES JAGGED, WITH 2ND STAGE VANES EXHIBITING S	EVERE DISTRESS.  14 STAGE BLEED VALVE OVERTRAVEL PIN WAS FOUND IN THE BOTTOM OF THE INNER BYPASS DUCT.  THIS IS AN AIRFR	AME PART.		2	L	7	2 	4F	4	F	RT	T00011AT	TE6CH				 
1999052800105	19990528	00105	EU  	1999	5	28	CA990505004      	2	19990427	G	7220	JR21756A	DUCT            			FOKKER	F28   	F28MK1000   	4990808	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					NR 2 ENGINE	FAILED          	W				O				OTHER                   				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CR	CRUISE         	1			CA			42932					9158			(CAN) IN CLIMB, NR 2 ENG REQD 5 PERCENT HIGHER RPM TO MAINTAIN SAME THRUST AS NR 1 ENG.  ON LEVELING OFF, CREW DECIDED T	O TREND BOTH ENGS TO ASSIST MAINT IN T/S OF LOWER POWER PROBLEM.  100 MILES OUT, A THUD FOLLOWED BY A CONTINUOUS SHUDDER	 FELT ACCOMPANIED BY 20-30 PERCENT LOSS OF THRUST ON NR 2 ENG.  ALL OTHER NR 2 ENG PARAMETERS UNCHANGED, BUT A SLIGHT VI	BRATION FELT AT NR 2 HP FUEL LEVER.  WITH POWER REDUCTION ON NR 2 ENG, SHUDDER DECREASED, BUT ENG DID NOT SOUND NORMAL. 	 ENG SHUT DOWN.  POST-FLIGHT INSP REVEALED 2 EACH NR 2 ENG COWLINGS MISSING AND FRONT BYPASS DUCT FOUND RUPTURED AT FWD 	FLANGE ALONG UPPER CIRCUMFERENCE.  NO SECONDARY DAMAGE NOTED.  ENG REPLACED.  FURTHER REPORT WILL FOLLOW.	2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999070900390	19990709	00390	EU  	1999	7	9	CA990505057      	1	19990427	G	2910	704A33690004	BELT            	AEROSP      	350A35013004	SNIAS 	350   	AS350BA     	8680817	EU  	TMECA 	ARRIEL	ARRIEL1B    	6OO30	NE  					HYDRAULIC PUMP	DEBONDED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			80   					4550			(CAN) DURING MAINTENANCE, THE HYDRAULIC PUMP DRIVE ASSY BELT WAS FOUND DEBONDED AT THE JOINT AREA AFTER ONLY 80 HOURS TS	N.   NEW BELT INSTALLED.					1	G	7	1 	3U	3	U	NC	H9EU    	E19EU				 
1999091700405	19990917	00405	EU  	1999	9	17	CA990510017      	1	19990504	G	2730	28BF02047	PUSHROD         			BRASOV	IS28  	IS28B2      	4490102	EU  										ELEVATOR	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1600 								(CAN) WEAR MARKS FOUND ON CENTER OF 6 PUSHROD (AT TOP OF VERTICAL STABILIZER).  DEPTH OF MARK APPROXIMATELY 50 PERCENT O	F WALL THICKNESS.  THE POSSIBLE CAUSE IS THOUGHT TO HAVE HAPPENED WHILE TOWING THIS GLIDER OVER SEVERAL TRIPS AND THE EL	EVATOR CONTROL PUSHROD WAS BOUNCING AND MAKING CONTACT WITH THE FIBERGLASS FAIRING AND WEARING INTO PUSHROD.  THE PUSHRO	D WAS SECURED IN A MANNER WHICH WOULD PREVENT A RECURRENCE.			1	K	0	0 					G40EU   					 
1999070900391	19990709	00391	EA  	1999	7	9	CA990510026      	1	19990401	G	7722	P260	CONNECTOR PIN   			CNDAIR	CL600 	CL6002B16   	1900305	EA  	GE    	CF34  	CF343B1     		NE  					NR 2 ENGINE	UNLOCKED        	W				E				ENGINE SHUTDOWN         				J	M		WARNING INDICATION        	OVER TEMP                 		TO	TAKEOFF        	1			CA								872509			(CAN) SHORTLY AFTER TAKEOFF ON PRODUCTION FLIGHT 1, THE NR 2 ENGINE ITT CLIMBED TO 998 DEGREES CELSIUS AND REMAINED STEA	DY FOR ABOUT 3 SECONDS.  FLUCTUATIONS WERE NEXT OBSERVED BETWEEN 650 AND 998 DEGREES.   ALL OTHER ENGINE PARAMETERS WERE	 NORMAL.  ACCOMPANYING THE 998 DEGREES CELSIUS WAS AN ENGINE MASTER WARNING AND HOT IN THE ITT GAUGE.  NR 2 ENGINE WAS S	HUTDOWN, BUT THE WARNINGS AND FLUCTUATIONS CONTINUED UNTIL SHORT FINAL.  THE SINGLE ENGINE LANDING WAS UNEVENTFUL.  INSP	ECTION REVEALED A CONNECTING PIN ON THE GAUGE/SENSOR WAS UNLOCKED.  FURTHER INVESTIGATION ATTRIBUTED THE FAULT TO WRONG 	WIRE CRIMPING ON THE CONNECTOR.  PIN WAS REPLACED.	2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999052800106	19990528	00106	GL  	1999	5	28	CA990510029      	2	19990429	G	7322		CARBURETOR      			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	MALFUNCTIONED   	W				R	A			AUTOROTATION            	UNSCHED LANDING         			R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			CA								CAT24579			(CAN) IN CRUISE AT 5,000 FEET, THE RPM OF THE TURBINE AND ROTOR WAS INCREASING.  THE MAIN ROTOR BLADE PITCH WAS INCREASE	D AND THE TORQUEMETER SHOWED AN EXCEEDANCE OF 105 PERCENT.  REDUCTION OF THE POWER LEVER MAINTAINED THE ROTOR AND ENGINE	 SPEEDS.  AN AUTOROTATION WAS CARRIED OUT.  POST-FLIGHT THE TURBINE, FUEL CONTROL UNIT, AND THE GOVERNOR WERE SENT TO A 	REPAIR SHOP FOR EVALUATION.  A FURTHER REPORT WILL FOLLOW.			1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999052800107	19990528	00107	EA  	1999	5	28	CA990510030      	2	19990501	G	8500		ENGINE          			GRUMAV	TBM   	TBM3EAIRTRD 	3950310	EA  	WRIGHT	R2600 	R260020     	67050	EA  	HAMSTD	23E	23E50       	NE  	ENGINE BAY	FAILED          	W				A				UNSCHED LANDING         				Y			ENGINE STOPPAGE           			CR	CRUISE         	1			CA				219  				437707	P55111		(CAN) DURING A FERRY FLIGHT AT 2,000 FEET, THE ENGINE FAILED.   A FORCED LANDING WAS CARRIED OUT WITH EXTENSIVE DAMAGE T	O THE AIRCRAFT.  THE ENGINE WILL BE DISASSEMBLED TO DETERMINE THE CAUSE OF THE ENGINE FAILURE.  FURTHER REPORT TO FOLLOW	.				1	L	7	1 	4R	4	R		L82     	TC176	6	C	P603	 
1999070900392	19990709	00392	SW  	1999	7	9	CA990513001      	1	19990428	G	2910	214076146001	SERVO           			BELL  	214   	214B1       	1182105	SW  	LYC   	T55   	T5508D      	41555	NE  					HYDRAULIC SYSTEM	DEFECTIVE       	W				O				OTHER                   				W			INADEQUATE Q C            			NR	NOT REPORTED   	1			CA				2534 				LE31927			(CAN) MAIN HYDRAULIC SERVO'S RETURNED FROM REPAIR FACILITY.  MANY DEFECTS WERE NOTED WHICH AFFECT AIRWORTHINESS.  SERVO'	S REPAIRED AND RETURNED TO SERVICEABLE STATUS.					2	G	7	1 	4U	4	U		H6SW    	E4NE				 
1999060400335	19990604	00335	CE  	1999	6	4	CA990513003      	1	19990211	G	7810	08507311	BELLOWS         			CESSNA	401   	401         	207590C	CE  	CONT  	O520  	TSIO520EB   	17040	SO  	MCAULY	3AF32C	3AF32C87    	GL  	TURBOCHARGER	BUCKLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								271461R	772967		(CAN) A FAULTY BELLOWS ASSEMBLY CAN CAUSE THE SEIZURE OF THE TURBOCHARGER.  INTERNAL METAL BUCKLING AND PEELING OF THE E	XHAUST CAN CAUSE PIECES TO DEPART INTO THE EXHAUST STREAM EVENTUALLY CAUSING THE SEIZURE OF THE TURBOCHARGER.  THE MAINT	ENANCE SCHEDULE INVESTIGATES THIS PORTION OF THE EXHAUST SYSTEM BUT DOES NOT CALL FOR DISASSEMBLY OF THIS PART UNLESS TH	ERE IS BULGING OR CRACKING VISIBLE ON THE OUTSIDE OF THE PART.  THERE IS ALSO AN FAA AD 75-23-08 ADDRESSING THE SIMILAR 	EXTERNAL INSPECTION.  THIS CONDITION IS NOT VISIBLE FROM THE OUTSIDE.  CESSNA HAS AN ALTERNATE PART AVAILABLE, OPERATOR 	REPORTS THAT NO PROBLEMS OF A SIMILAR NATURE HAVE BEEN NOTED TO-DATE.	1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22E	 
1999070900393	19990709	00393	SW  	1999	7	9	CA990513006      	1	19990430	G	2435	150SG1064	ARMATURE        	LEARSIEGLER 	23032018    	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					START/GENERATOR	MISREPAIRED     	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA				910  		3911		822972			(CAN) DURING OVERHAUL, LUCAS STARTER /GENERATOR WAS FOUND WITH AN APC ARMATURE INSTALLED P/N 150SG1064.  THE APPROVED PA	RT IS LUCAS P/N 23032-1920.  CORRECT ARMATURE WAS SUBSEQUENTLY INSTALLED AND O/H COMPLETED.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999082001004	19990820	01004	SW  	1999	8	20	CA990513007      	1	19990430	G	2435	230321920	ARMATURE        		150SG118Q   	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20J     	03013	GL  					STARTER/GEN	MISOVERHAULED   	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA			6330 	957  		1165		CAE270334			(CAN) FOLLOWING OVERHAUL, IT WAS FOUND THAT THE STARTER/GENERATOR CONTAINED NUMEROUS PARTS THAT ARE NOT APPROVED.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999061800026	19990618	00026	SO  	1999	6	18	CA990521008      	2	19990503	G	8530	630046	PISTON PIN      			CESSNA	206   	206CESSNA   	2073302	CE  	CONT  	O520  	IO520A      	17032	SO  	MCAULY	2A34C	D2A34C58    	GL  	ENGINE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			21   					970943	771604		(CAN) AIRCRAFT ENGINE WAS BROUGHT IN TO CARRY OUT CSB-99-3.  WHEN PREPARING TO REINSTALL THE PISTON PINS, THE PINS WERE 	FOUND WITH SUBSTANTIAL CORROSION FOR THE TIME IN SERVICE.  THE PARTS WILL BE SENT TO CONTINENTAL FOR EVALUATION.					1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P3EA	 
1999081200731	19990812	00731	CE  	1999	8	12	CA990521022      	1	19990507	G	7810	BI3002241	EXHAUST TUBE    	BUTTERFIELD 	STCSA2905NM 	BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2524 			KITSN1549		PCE85170			(CAN) ORIGINAL SNAG WAS CHAFING AT TUBE WHERE IT ATTACHES TO EXHAUST STACK.  A WEEK LATER FOLLOWING INSTALLATION OF NEW 	PART, TUBES WERE FOUND TO BE CRACKED INBETWEEN PLEATS OF FLEX TUBE.  ON ONE TUBE, MATERIAL WAS MISSING AND SIGNIFICANT A	MOUNT OF EXHAUST WAS LEAKING INTO COWL AREA.  NO SIGN OF OVERHEATING.  REPLACED TUBES WITH NEW GASKETS.  SUBMITTER STATE	D COMMUTER AIR TRANSPORT REPORTS THIS IS COMMON.			1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999061800028	19990618	00028	CE  	1999	6	18	CA990521030      	1	19990423	G	2121		BEARINGS        	ELECTROMECH 	EM608       	LEAR  	35    	35LEAR      	5170600	CE  										BLOWER	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						1043					(CAN) BEARINGS FOUND WITHIN BLOWER ASSY WERE NOT OF THE MANUFACTURER'S TYPE.  BEARING WAS SEIZING WHICH, IN TURN, CAUSED	 ABNORMAL CURRENT DRAW AND BURNING BRUSHES (ARCING).  PREVIOUS CERTIFICATION WAS CANADIAN AERO ACCESSORIES.					2	L	7	2 	4F				A10CE   					 
1999061800029	19990618	00029	EU  	1999	6	18	CA990521031      	1	19990423	G	2121	AE004244	BEARINGS        		AE4540MK1   	BRAERO	748   	HS7482B     	1500248	EU  										BLOWER	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						1530					(CAN) SPILL VALVE IN FOR OVERHAUL.  BEARINGS ON ARMATURE FOUND TO DIFFER FROM ONES LISTED IN IPL. BEARINGS WILL BE REPLA	CED.					2	L	7	2 	3T				A24EU   					 
1999061800030	19990618	00030	EU  	1999	6	18	CA990521032      	1	19990427	G	2822	SPE1002021	BEARINGS        	PLESSEY     	BP1RSMK6    	BRAERO	748   	HS7482A     	4231001	EU  										BOOST PUMP	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						43723					(CAN) FUEL BOOST PUMP IN FOR OVERHAUL.  BEARINGS ON ARMATURE FOUND TO BE DIFFERENT FROM ONES IN IPL.  BEARINGS WILL BE R	EPLACED.					2	L	7	2 	3T				A24EU   					 
1999061800031	19990618	00031	EU  	1999	6	18	CA990521033      	1	19990429	G	8200	SPE10002023	BEARINGS        	PLESSEY     	SPM8RSMK1   	BRAERO	748   	HS7482A     	4231001	EU  	RROYCE	DART  	DART5342    		EU  					PUMP	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						8992R		16375			(CAN) WATER/METH PUMP IN FOR OVERHAUL.  BEARINGS ON ARMATURE FOUND TO DIFFER FROM ONES LISTED IN IPL.  BEARINGS WILL BE 	REPLACED.					2	L	7	2 	3T	4	T		A24EU   	A196				 
1999061800032	19990618	00032	SW  	1999	6	18	CA990521038      	1	19990505	G	5302	206031004115B	SKIN            			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20B     	03013	GL  					TAILBOOM	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			10502			BCJN08660		CAE831160			(CAN) DURING INSPECTION, FOUR SMALL CREASES WERE DISCOVERED ON TAILBOOM BETWEEN STATIONS 69.0 AND 72.0.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999061800033	19990618	00033	NE  	1999	6	18	CA990521046      	2	19990513	G	7200		ENGINE          			CNDAIR	CL600 	CL6002A12   	1900304	EA  	GE    	CF34  	CF341A      		NE  					NR 2	MAKING METAL    	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			D	J		INFLIGHT SEPARATION       	WARNING INDICATION        		CR	CRUISE         	1			CA				2063 				350139			(CAN) AT 7,000 FEET, A SHEARING NOISE WAS HEARD FROM NR 2 ENGINE.  THE ENGINE WAS SHUT DOWN.  POST-FLIGHT INSPECTION FOU	ND METAL IN THE MAIN OIL FILTER AND CHIP DETECTOR. THE ENGINE WAS REMOVED AND SENT FOR INVESTIGAITON.					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999061800035	19990618	00035		1999	6	18	CA990521050      	1	19990506	G	7930	9717517103	WIRE            		800508105   						PWA   	PT6   	PT6A67B     	52043	NE  					OIL QUANTITY	SEVERED         	W				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			CA			566  					PCEPR0090			(CAN) OIL QUANTITY LIGHT CAME ON UPON LANDING.   BROKEN WIRE FOUND, OIL WAS AT RECOMMENDED LEVEL.   THE OIL LIGHT WILL N	OT COME ON UNLESS THE AIRCRAFT IS ON THE GROUND.  IF THIS HAPPENS IN THE AIR, THE PILOT WILL NOT BE AWARE OF THE SITUATI	ON UNTIL AIRCRAFT ON GROUND.  SECOND INCIDENT WHERE INDICATIONS WERE ONLY DISCOVERED AFTER SYSTEM ENERGIZED BY SQUAT SWI	TCH.  THE SYSTEM IS DEFAULTED TO PUT THE LIGHT ON INSTEAD OF OFF IF THE CIRCUIT IS BROKEN.  RESEARCHING THIS ITEM.								4	T			E26NE				 
1999061800036	19990618	00036	EU  	1999	6	18	CA990521053      	2	19990313	G	7310	JR30861A	LINE            			GULSTM	G1159 	GIV         	3980115	SO  	RROYCE	TAY   	TAY6118     		EU  					FUEL SYSTEM	LEAKING         	W				E	A	F		ENGINE SHUTDOWN         	UNSCHED LANDING         	ACTIVATE FIRE EXT.      		J	F	E	WARNING INDICATION        	FLT CONT AFFECTED         	VIBRATION/BUFFET          	CR	CRUISE         	1			CA			5055 					16349			(CAN) DURING FLIGHT, CREW NOTICED THE GENERATOR CAME OFF-LINE TWICE, ALSO, AUTO THROTTLE KEPT DISCONNECTING UNTIL FINALL	Y THEY WOULD NOT RE-ENGAGE.  ENGINE POWER THEN ROLLED BACK WITH HP RPM REMAINING CONSTANT.  SECONDS LATER, CREW HAD AN E	NGINE FIRE WARNING.  THEY RETARDED THE THROTTLES AND PULLED THE T-HANDLES AND THE FIRE LIGHT WENT OUT, SO THE FIRE BOTTL	ES WERE NOT DISCHARGED.  AIRCRAFT DIVERTED.  POST-FLIGHT INSPECTION FOUND THE ELECTRICAL HARNESS BURNT AND THE ENGINE CO	NTROL RODS IMMOVABLE.  THE FUEL LINE TO APPROACH IDLE SOLENOID WAS FOUND HOLED.  SHOP CONFIRMED THE PIPE CONDITIION AND 	SURMISED THE ELECTRICAL HARNESS WAS ROUTED AND CLAMPED IMPROPERLY CAUSING FRETTING OF THE PIPE.	2	L	7	2 	4F	4	F	RT	A12EA   	E25NE				 
1999070900394	19990709	00394	WP  	1999	7	9	CA990531001      	1	19990429	G	6720	369H75319	TORQUE TUBE     		369D297500  	HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					TAIL ROTOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								CAE833902			(CAN) T/R PEDAL ASSY REMOVED FOR 0/H.  UPON DISASSEMBLY INSPECTION, A CRACK WAS FOUND IN THE TORQUE TUBE.  THE CRACK PRO	PAGATED FROM BOTH SIDES OF THE CENTER HOLE WHERE THE CONTROL ROD BELLCRANK ATTACHES.					1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999061800038	19990618	00038	GL  	1999	6	18	CA990531004      	2	19990513	G	7230	23038126	COMPRESSOR      			BELL  	206   	206L        	1181522	SW  	ALLSN 	250C  	250C20R2    		GL  					ENGINE	FAILED          	W				B	A			EMER. DESCENT           	UNSCHED LANDING         			Y	J		ENGINE STOPPAGE           	WARNING INDICATION        		CR	CRUISE         	1			CA			1907 	34   				CAE836522			(CAN) IN CRUISE AT 5,300 FEET, WITH AUTO-LIGHT AND ANTI-ICE SELECTED ON, A LOUD EXPLOSION WAS HEARD FOLLOWED BY AN IMMED	IATE YAW TO THE LEFT.  THE ENGINE HORN ALSO BECAME AUDIBLE, SO AN AUTO ROTATION WAS CARRIED OUT.  ON DESCENT, THE TAIL R	OTOR CONTACTED THE TREES.   AFTER LANDING ,THE ENGINE INTAKE AREA WAS FOUND TO HAVE COMPRESSOR PIECES LAYING ON THE FORW	ARD SIDE OF THE BELLMOUTH. THE TAIL ROTOR DRIVE WAS ALSO FOUND FAILED AFTER TOUCHDOWN.  THE TURBINE TEMPERATURE WAS NOTI	CED TO BE ABOVE 900 CELSIUS DURING AUTO-ROTATION.		1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999070900397	19990709	00397	SW  	1999	7	9	CA990531007      	1	19990503	G	2434	230640098	GENERATOR       			BELL  	205   	205A1       	1181414	SW  	LYC   	T53   	T5313B      	41549	NE  					DC SYSTEM	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						2824		LEO7592			(CAN) GENERATOR WARNING LIGHT FLASHED SEVERAL TIMES AND WOULD NOT PRODUCE ANY OUTPUT.  GENERATOR REPLACED, BUT PROBLEM R	EMAINED.  VOLTAGE REGULATOR CHANGED AND SYSTEM IS NOW SERVICEABLE.					1	G	7	1 	4U	4	U		H1SW    	E17EA				 
1999061800039	19990618	00039	SO  	1999	6	18	CA990531009      	2	19990511	G	8520		CONNECTING ROD  			CESSNA	210   	T210N       	2073456	CE  	CONT  	O520  	TSIO520M    	17040	SO  	MCAULY	D3A34	D3A34C402   	GL  	NR 2 CYLINDER	FRACTURED       	W				A				UNSCHED LANDING         				E	K		VIBRATION/BUFFET          	FLUID LOSS                		CR	CRUISE         	1			CA				968  				520009	7911076		(CAN) INITIAL INVESTIGATION REVEALED A 2 INCH HOLE THROUGH THE TOP OF THE RIGHT ENGINE BLOCK.  THE RIGHT MAGNETO BROKE A	ND VIEWING THROUGH THE HOLE OF THE CRANKSHAFT, THE CONNECTING ROD WAS FOUND DESTROYED.					1	H	7	1 	3O	3	O		3A21    	E8CE	5	C	P47G	 
1999070900398	19990709	00398	EU  	1999	7	9	CA990531026      	1	19990527	G	6330	10510056	FRAME           			BOLKMS	105   	BO105C      	5626005	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TRANSMISSION	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4753 					CAE835686			(CAN) DURING A PAST MAJOR INSPECTION, THE TRANSMISSION A-FRAME WAS COVERED WITH HEAT SHRINK FOR PROTECTION.  AT THE NEXT	 MAJOR INSPECTION, HEAT SHRINK WAS REMOVED.  RT AND LT FRAMES WERE CORRODED BEYOND LIMITS (80 PERCENT) AND WERE SUBSEQUE	NTLY SCRAPPED.				1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999070900399	19990709	00399	CE  	1999	7	9	CA990531042      	1	19990526	G	5320	05130351	SUPPORT         			CESSNA	172   	172         	2072402	CE  	CONT  	O300  	O300A       	17022	SO  					COCKPIT	BROKEN          	W				O				OTHER                   				F			FLT CONT AFFECTED         			DE	DESCENT        	1			CA								13663D8A			(CAN) RIGHT HAND CONTROL COLUMN OPPERATION BECAME BLOCKED CAUSING LOSS OF AIRCRAFT DURING LANDING APPROACH.  THE INSTRUM	ENT PANEL BRACE BECAME BROKEN AS STATED IN TC SYSTEM SAFETY, DORVAL ACCOMPANYING PHOTO.  TSB REPORT TO FOLLOW FILE A99Q0	075-2 CADORS 99Q0262.				1	H	7	1 	3O	3	O	NT	3A12    	E253				 
1999070900400	19990709	00400		1999	7	9	CA990603003      	4	19990516	G	2312	KY196	RADIO           			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					VHF	INTERMITTENT    	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			CA								CAE834272			(CAN) WHILE DISPLAYING FREQUENCY ON STANDBY, THE COMM DISPLAY DISAPPEARS LEAVING ONE DIGIT INTERMITTENT AND RETURNS TO N	ORMAL AFTER TUNING KNOB IS MOVED ANOTHER CLICK.					1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999090300237	19990903	00237	NM  	1999	9	3	CA990603005      	1	19990525	G	2432	25582003	BATTERY         			BOEING	737   	737217      	1384464	NM  	PWA   	JT8   	JT8D9A      	52048	NE  					E/E BAY	OVERHEATED      	W				H				DEACTIVATE SYST/CIRCUITS				B	M		SMOKE/FUMES/ODORS/SPARKS  	OVER TEMP                 		TX	TAXI/GRND HDL  	1			CA						9200715		674200			(CAN) DURING BOARDING, CREW NOTICED AN ELECTRICAL SMELL IN THE CABIN AND INITIATED FAULT ISOLATION PROCEDURES.  THE BATT	ERY CHARGER CIRCUIT BREAKER TRIPPED AND THE MAIN AIRCRAFT BATTERY OVERHEATED.  BATTERY AND CHARGER REPLACED.  BATTERY HA	D NOT BEEN MODIFIED PER BOEING SL.				2	L	7	2 	4F	4	F		A16WE   	E2EA				 
1999070900401	19990709	00401	SW  	1999	7	9	CA990603006      	1	19990521	G	2913	2120760111	PUMP            			BELL  	205   	205A1       	1181414	SW  	LYC   	T53   	T5313B      	41549	NE  					HYDRAULIC SYSTEM	FAILED          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			CA				52   		143020CF		LEO7592			(CAN) PILOT HEARD NOISE FROM PYLON AREA,THEN NR 2 HYDRAULIC PRESSURE WARNING LIGHT ILLUMINATED.  PILOT RESET CIRCUIT BRE	AKER, BUT PROBLEM STILL PRESENT.  DEFECTIVE HYDRAULIC PUMP REPLACED AND AIRCRAFT RETURNED TO SERVICE.					1	G	7	1 	4U	4	U		H1SW    	E17EA				 
1999090300238	19990903	00238	NM  	1999	9	3	CA990603008      	1	19990511	G	7830	MJ4512W	CONTROL ROD     			BOEING	737   	737281      	138448P	NM  	PWA   	JT8   	JT8D17      	52049	NE  					THRUST REVERSER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) DURING INSPECTION, THE THRUST REVERSER FOLLOW-UP CONTROL ROD FORWARD ROD END BEARING WAS FOUND ADRIFT, FURTHER INS	PECTION FOUND THE ROD END WAS CRACKED AND SPLITTING APART.  REPLACED.					2	L	7	2 	4F	4	F		A16WE   	E2EA				 
1999081200733	19990812	00733	SO  	1999	8	12	CA990603011      	1	19990603	G	2731	71056003	SPRING          			PIPER 	PA31  	PA31350     	7103110	SO  										ELEVATOR TRIM	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			421  								(CAN) PILOT REPORTED NO BACK PRESSURE ON ELEVATOR SYSTEM IN-FLIGHT.  AIRCRAFT REQUIRED MORE ELEVATOR TRIM THAN USUAL.  N	OTE:  THESE ELEVATOR RETURN SPRINGS WERE REPLACED IN 1998 TO COMPLY WITH AD 98-08-18 AND PIPEX S/B 626C.  THE AD ALSO PL	ACED A 1,000 HOUR LIFE-LIMIT ON SPRING.  THE PREVIOUS SUCCEEDING SPRINGS HAD NO LIFE-LIMIT AND SUBMITTER HAD EXPERIENCED	 NO PROBLEMS WITH THEM.			1	L	7	2 	3O				A20SO   					 
2000081000034	20000810	00034	CE  	2000	8	10	CA990603018      	1	19990527	G	3260	1003810061	DOWNLOCK SWITCH 			BEECH 	100   	100BEECH    	1152916	CE  	PWA   	PT6   	PT6A28      	 	EA  					DRAG BRACE	INTERMITTENT    	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			AP	APPROACH       	1			CA								PCE50339			(CAN) AIRCRAFT WAS ON APPROACH WHEN THE GEAR WAS SELECTED DOWN AND ONLY THE NOSE AND LEFT MAIN GEAR DOWN LIGHT ILLUMINAT	ED.  AS THE AIRCRAFT ENTERED A RIGHT TURN, THE RIGHT GEAR DOWN LIGHT ILLUMINATED.  THE DOWNLOCK SWITCH WAS REPLACED.					1	L	7	2 	3T	4	T	 	A14CE   	E4EA				 
1999090300247	19990903	00247	NM  	1999	9	3	CA990614022      	1	19990531	G	2780		BEARING         			BOEING	727   	72725       	1384006	NM  	PWA   	JT8   	JT8D7B      	52053	NE  					LE FLAP	MISALIGNED      	W				A				UNSCHED LANDING         				F	J		FLT CONT AFFECTED         	WARNING INDICATION        		CR	CRUISE         	1			CA								649100			(CAN) ON TEST FLIGHT, NR 7 SLAT DID NOT EXTEND CORRECTLY CAUSING IT TO JAM.  IN COMPLETING MOD, SLAT BOLT WAS NOT LINED 	UP TO BEARING AND NOT INSTALLED IN THE PROPER PLACE.   REPAIRED.					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
2000083000039	20000830	00039	NE  	2000	8	30	CA990614024      	3	19990601	G	6111	AG1002	BLADE           	HAMSTD      		AYRES 	S2    	S2RNORMAL   	7630202	SO  	PWA   	R1340 	R1340AN1    	52016	NE  	HAMSTD	12D	12D40       	NE  	42 STATION	CRACKED         	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA						780711		39416	74236		(CAN) NOT AN SDR - PROPELLER WAS IN FOR OVERHAUL DUE TO IMPACT DAMAGE FROM GRAVEL. PROPELLER WAS OVERHAULED AND RETURNED	 TO SERVICE.					1	L	7	1 	3R	3	R	NC	A3SW    	5E2	5	C	P257	 
1999090300249	19990903	00249	NM  	1999	9	3	CA990614062      	1	19990521	G	2752		ACTUATOR        			BOEING	727   	727277      	138408S	NM  	PWA   	JT8   	JT8D15      	52051	NE  					TE FLAP	SLOW            	W				O				OTHER                   				I			FLT. ATTITUDE INST.       			CL	CLIMB          	1			CA								695337			(CAN) FLAPS SLOW TO RETRACT FROM 5 TO 2 DEGREES.  FLAP UP CABLE TENSION LOW.						2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
1999090300251	19990903	00251	NM  	1999	9	3	CA990614064      	1	19990518	G	5280		SEAL            			BOEING	727   	72727C      	138400J	NM  	PWA   	JT8   	JT8D7B      	52053	NE  					NLG DOOR	LOOSE           	W				A				UNSCHED LANDING         				O			OTHER                     			CR	CRUISE         	1			CA								653499			(CAN) NOSE GEAR LIGHT COMES ON IN-FLIGHT, NOSE GEAR AREA BANGING ABOVE 320 KNOTS.   FOU  FOUND DOOR FRONT SEAL LOOSE AND	 BLOCKING DOOR REPAIRED.					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999090300252	19990903	00252		1999	9	3	CA990614065      	4	19990320	G	2350	65528041	AUDIO UNIT      			BOEING	727   	727277      	138408S	NM  	PWA   	JT8   	JT8D15      	52051	NE  					COCKPIT	FAILED          	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			CA								695337			(CAN) RADIO NAV FAILURES, IDENT STRENGTHS LOW FOR CAPT, FO AND SO.  REPLACED AUDIO ACCESSORY UNIT.						2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
1999090300253	19990903	00253	NM  	1999	9	3	CA990614066      	1	19990523	G	2612		FIRE LOOP       			BOEING	727   	727277      	138408S	NM  	PWA   	JT8   	JT8D15      	52051	NE  					NR 1 ENGINE	CHAFED          	W				A				UNSCHED LANDING         				N			FALSE WARNING             			CR	CRUISE         	1			CA								695337			(CAN) NR 1 ENGINE GROUND FAULT DETECTOR LIGHT ON, NR 1 FIRE PROTECTION LIGHT ON IN-FLIGHT, EXTINGUISHED ON GROUND.  FOUN	D FIRE LOOP CHAFING ON COWLING, REPAIRED.					2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
2000081000035	20000810	00035	EU  	2000	8	10	CA990614071      	1	19990604	G	5530	D33000001T	STABILIZER      	WSK         		WSK   	M18   	M18DROMADER 	9810102	EU  	WSK   	ASZ62 	ASZ62IRM18  	 	NE  					LT LWR FWD SKIN	CRACKED         	W				O	 	 	 	OTHER                   				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			14480					KAA6406104			(CAN) SEE SKETCH						1	L	7	1 	3O	3	R	 	A47EU   	E10NE				 
1999090300256	19990903	00256		1999	9	3	CA990614073      	4	19990608	G	3160	066302305	FACE PLATE      	KING        	KAP315      															DATA RECORDER	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						1222					(CAN) FACEPLATE RECEIVED NOT AS INDICATED ON MANUFACTURER'S DRAWING.																			 
1999082001007	19990820	01007	SW  	1999	8	20	CA990630010      	1	19990604	G	6210	369D21100517	BLADE           			HUGHES	500N  	500N        	3027374	SW  	ALLSN 	250C  	250C20B     	03013	GL  					MAIN ROTOR	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2220 			9999J142		CAE833836			(CAN) UPON INSPECTION, A VOID WAS DETECTED IN THE GRIP PLATE THAT IS BEYOND THE MANUFACTURER'S SET FORTH REPAIRABLE LIMI	TS AND ALSO OUTSIDE THE PARAMETERS OFADS AND SBS THAT CALL FOR INSPECTION FOR THESE PROBLEMS.					1	G	7	1 	3U	3	U	NC	H3WE    	E4CE				 
1999082000212	19990820	00212	EU  	1999	8	20	CA990630026      	1	19990614	G	2435	203S22C	BEARING         		GA1308      	SNIAS 	350   	AS350B1     	8680811	EU  										START/GEN	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA			1026 			19594					(CAN) BOTH ARMATURE BEARINGS FOUND ARE UNAPPROVED PARTS.  BEARINGS ARE MARKED:   203S22C 11401 JAPAN MRC.  THE APPROVED 	BEARINGS ARE LUCAS P/N 03-6009-23.  UNAPPROVED BEARINGS HELD IN QUARANTINE.  CORRECT, APPROVED BEARINGS INSTALLED DURING	 OVERHAUL.				1	G	7	1 	3U				H9EU    					 
1999090300266	19990903	00266	NM  	1999	9	3	CA990630049      	1	19990606	G	5320		FASTENER        			BOEING	727   	72727C      	138400J	NM  	PWA   	JT8   	JT8D7B      	52053	NE  					BS 480-620	MISSING         	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA								653499			(CAN) WHILE COMPLYING WITH PEMCO SB 727-53-003-001R1 FOR AMC FOR AD 98-23-51 MISSING FASTENERS BETWEEN STA 480 TO 620 WH	ERE STR 3L WAS REMOVED DUE TO A/C MOD FROM PAX TO CARGO.   ALSO SAME FOUND WHERE SECTION OF FRAMES WERE REMOVED DUE TO M	OD PER SB.  ALL ORIGINAL FASTENER HOLES WERE TO BE PICKED UP WHEN INSTALLING FUSE DOUBLERS.  ALSO, FUSE DOUBLER/TRIPLER 	INTERNAL SPLICE PLATES WERE MISSING.   MISSING PARTS INSTALLED.			2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999090300269	19990903	00269	NM  	1999	9	3	CA990630053      	1	19990612	G	3510	280001	REGULATOR       			BOEING	727   	72727C      	138400J	NM  	PWA   	JT8   	JT8D7B      	52053	NE  					OXYGEN SYSTEM	MALFUNCTIONED   	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						644		653499			(CAN) CAPTAIN'S OXYGEN REGULATOR WILL NOT FUNCTION CORRECTLY IN EMERGENCY POSITION ON.  OXYGEN REGULATOR REMOVED AND REP	LACED IAW MM.					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999090300270	19990903	00270	NM  	1999	9	3	CA990630054      	1	19990615	G	5270		SWITCH          			BOEING	727   	727260      		NM  	PWA   	JT8   	JT8D17      	52049	NE  					CARGO DOOR	OUT OF ADJUST   	W				O				OTHER                   				N			FALSE WARNING             			CR	CRUISE         	1			CA								689961			(CAN) CARGO DOOR LIGHT ON S/O PANEL IN-FLIGHT WHEN DIFF EXCEEDS 7 PSI.   NO OTHER LIGHT ON.   CARGO DOOR SWITCH S7 ON LO	CKS ADJUSTED PER MM.					2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
1999090300271	19990903	00271	NM  	1999	9	3	CA990630055      	1	19990617	G	2612		CLAMP           			BOEING	727   	72727C      	138400J	NM  	PWA   	JT8   	JT8D7B      	52053	NE  					FIRE LOOP	MISINSTALLED    	W				A				UNSCHED LANDING         				N	W		FALSE WARNING             	INADEQUATE Q C            		CR	CRUISE         	1			CA								653499			(CAN) NR 2 FIRE DETECTION CIRCUIT GROUND LIGHT ON REAR CIRCUIT PANEL.   REPOSITIONED TWO FIRE LOOP CLAMP GROMMETS ON THE	 NR 2 ENGINE CHECK.					2	L	7	3 	4F	4	F		A3WE    	E2EA				 
2000073100150	20000731	00150	CE  	2000	7	31	CA990630056      	1	19990610	G	2720	1006000121	BELLCRANK       	BEECH       	9763000060  	BEECH 	100   	A100        	1152915	CE  	PWA   	PT6   	PT6A28      	 	EA  					RUDDER BELLCRANK	CORRODED        	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			18144					PCE50256			(CAN) THE RUDDER BELLCRANK WAS REMOVED AND CORROSION WAS FOUND ON THE SURFACE WHERE THE TORQUE TUBE CONNECTS.  THERE WAS	 ALSO CORROSION FOUND ON THE BOLT HOLES.  THE BELLCRANK AND BOLTS WERE REPLACED.  SUBMITTER STATED THAT THIS AREA IS HAR	D TO INSPECT BECAUSE THE TORQUE TUBE COVERS THE BELLCRANK.  THE SUBMITTER ALSO STATED THAT IT IS NOTEWORTHY THAT THIS AR	EA GETS EXPOSED TO THE ELEMENTS BECAUSE OF HOLES WHERE THE ELEVATOR TORQUE TUBES GO THROUGH THE TAIL CONE.  THERE IS NO 	SCHEDULED MAINTENANCE TO REMOVE THIS BELLCRANK FOR INSPECTION.		1	L	7	2 	3T	4	T	 	A14CE   	E4EA				 
2000081000036	20000810	00036	CE  	2000	8	10	CA990630057      	1	19990611	G	5541	9763000023	SPAR            	BEECH       	9763000601  	BEECH 	100   	A100        	1152915	CE  	PWA   	PT6   	PT6A28      	 	EA  					CENTRE ATTCH PNT	CRACKED         	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			12474					PCE50250			(CAN) THE RUDDER WAS REMOVED TO REPAIR SOME LOOSE RIVETS ON THE TORQUE TUBE, BUT A CRACK ABOUT 1 CENTIMETER LONG WAS DIS	COVERED ON THE RUDDER SPAR (P/N 96-630000-307).  THE SPAR WAS ALSO FOUND TO BE CRACKED IN BEHIND.  THE CRACKS ORIGINATED	 FROM THE NUTPLATE INSIDE THE RUDDER SPAR ON THE CENTER ATTACH POINT AT STATION 22.5.  THE SPAR AND DOUBLER WERE REPLACE	D.  TWO OTHER KING AIRS IN FLEET WERE DISCOVERED TO HAVE THE SAME CRACKS IN THIS AREA.  THE SUBMITTER NOTED THAT IT IS V	ERY DIFFICULT TO SEE THE CRACKS WITH THE RUDDER ON THE AIRCRAFT AS THE HINGE BRACKET (P/N 97-630012-1) IS COVERING THIS 	AREA.	1	L	7	2 	3T	4	T	 	A14CE   	E4EA				 
1999101300022	19991013	00022	EU  	1999	10	13	CA990630059      	1	19990610	G	6230	4619305032	MAST            	ZENITH      	4638001001  	BOLKMS	105   	BO105CBS    	5626008	EU  										MAIN ROTOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4987 	1432 		208					(CAN) CRACKS VISIBLE ON FLANGE SURFACE EMANATING FROM ROTOR HEAD ATTACHMENT BORES.						1	G	7	2 	3U			NC	H3EU    					 
1999090300272	19990903	00272	NM  	1999	9	3	CA990630060      	1	19990615	G	5270		SWITCH          			BOEING	727   	727260      		NM  	PWA   	JT8   	JT8D17      	52049	NE  					CARGO DOOR	OUT OF ADJUST   	W				A				UNSCHED LANDING         				N			FALSE WARNING             			CL	CLIMB          	1			CA								689961			(CAN) CARGO DOOR CAME ON IN-FLIGHT.   ADJUSTED DOOR CLOSE SWITCH TESTED OK.  SAME SNAG AT 7 PSI, ADJUSTED LOCK ROD SWITC	HES, WIRING INSPECTED, SYSTEM TESTED OK.					2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
1999082000214	19990820	00214	EU  	1999	8	20	CA990630077      	1	19990521	G	6320	4638305028	BEARING         			BOLKMS	105   	BO105CBS    	5626008	EU  										M/R GEARBOX	SPALLED         	W				O				OTHER                   				J			WARNING INDICATION        			CR	CRUISE         	1			CA			906  								(CAN) INNER RACE OF ROLLER BEARING WAS FOUND HEAVILY SPALLED.						1	G	7	2 	3U			NC	H3EU    					 
1999082000215	19990820	00215	EU  	1999	8	20	CA990630078      	1	19990610	G	6320	4638302023	BEARING         		4638001001  	BOLKMS	105   	BO105CBS    	5626008	EU  										M/R GEARBOX	DISINTEGRATED   	W				K				NONE                    				J			WARNING INDICATION        			IN	INSP/MAINT     	1			CA			1432 			208					(CAN) EXCESSIVE DEBRIS FOUND IN FILTER ASSEMBLY.						1	G	7	2 	3U			NC	H3EU    					 
1999081200734	19990812	00734		1999	8	12	CA990630079      	4	19990609	G	6122	441827	GOVERNOR        			CNDAIR	CL215 	CL2151A10   		EA  						HAMSTD	43E	43E60       	NE  	PROPELLER	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						WH51999			174052		(CAN) P.C.U. FAILURE CAUSED AN OVERSPEED CONDITION.  P.C.U REPLACED ALONG WITH ENGINE PER P&W SB.1413 REV B.						2	H	7	2 	4R				A14EA   		6	C	P871	 
1999081200735	19990812	00735	NE  	1999	8	12	CA990630080      	2	19990531	G	8520	39785	LINK PIN        			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					CRANKCASE	DISPLACED       	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA				839  				4223663			(CAN) NR 7 LINK PIN ASSY FOUND DISPLACED REARWARD JAMMING AGAINST INTERNAL CRANKCASE STRUCTURE.  THE LOCK PLATE SCREW FA	ILED ALLOWING PIN TO MIGRATE.  QUALITY CONTROL IS SUSPECTED AT OVERHAUL,  LOCKWIRE RETAINING SCREW COULD NOT BE FOUND DU	RING INTERNAL INSPECTION.				1	H	7	1 	3R	3	R		A806    	5E1				 
1999081200736	19990812	00736	EA  	1999	8	12	CA990630089      	1	19990610	G	2821		FILTER          			CNDAIR	CL215 	CL2156B11415		EA  										FUEL SYSTEM	CONTAMINATED    	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			CA											(CAN) FUEL CONTAMINATION WAS CAUSING ENGINE FUEL FILTER ANNUNCIATION NO ENGINE PARAMETERS AFFECTED.  FIBER LIKE FUZZ FOU	ND IN FILTER ELEMENTS.  NOTE:  LINE MAINTENANCE CLEAN UP OF FUEL CELLS INTRODUCED THE CONTAMINATION CHANGES TO THE CLEAN	-UP PROCEDURE HAS RECTIFIED THE FAULT.				2	H	7	2 	4T			RT	A14EA   					 
1999090300273	19990903	00273	NM  	1999	9	3	CA990630091      	1	19990526	G	2782	65449617	ACTUATOR        	BOEING      	65449617    	BOEING	737   	7372A9C     	1384495	NM  	PWA   	JT8   	JT8D9A      	52048	NE  					LE FLAP	SPLIT           	W				H				DEACTIVATE SYST/CIRCUITS				K			FLUID LOSS                			LD	LANDING        	1			CA						354		674382			(CAN) LOSS OF HYDRAULIC FLUID ON LANDING.  NR 8 GROUND SPOILER CYLINDER SPLIT IN TWO AT PISTON SIDE.  REPLACED.						2	L	7	2 	4F	4	F		A16WE   	E2EA				 
1999082700908	19990827	00908	CE  	1999	8	27	CA990630095      	1	19990609	G	3233	MCB15ASI	CONTROL  UNIT   			BEECH 	100   	B100        	1152919	CE  	GARRTT	TPE331	TPE3316252B 	01514	WP  					MLG	MALFUNCTIONED   	W				O				OTHER                   				J			WARNING INDICATION        			LD	LANDING        	1			CA								P27079			(CAN) INTERMITTANT PROBLEM ON THE LANDING GEAR RETRACTION SYSTEM IN THE UP POSITION ONLY.   SOMETIMES THE 'GEAR IN TRANS	ITION' LIGHT STAYED LIT AND, ON ONE OCCASION, THE GEAR DOWN SELECTION COULD NOT BE DONE OTHER THAN BY THE MANUAL SYSTEM.	  MANY GEAR RETRACTIONS WERE DONE ON THE GROUND.  DYNAMIC BRAKE RELAY INSPECTED AND FOUND A BAD CONTACT ON THE UP SELECT	ION.  CONTACT CLEANED, FAULT CLEARED.			1	L	7	2 	4T	4	T		A14CE   	E2WE				 
1999081200742	19990812	00742	NE  	1999	8	12	CA990707006      	3	19990608	G	6112	8022523	BOOT            	HAMSTD      	SFA13N1ROA  	DHAV  	DHC8  	DHC8311     	1386006	EA  	PWA   	PW120 	PW123       		NE  	HAMSTD	14SF	14SF15      	NE  	PROP DEICE	SHORTED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4952 			88795423		123113	901009		(CAN) OVERHEATING OF PROPELLER BLADE DEICE BOOT EVIDENT.  BOOT AND RELAY REPLACED FOR THE HEATER CONTROL NR 3061-K4PN KC	-D4N.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
1999081200743	19990812	00743	NE  	1999	8	12	CA990707008      	2	19990627	G	7314	324485318	PUMP            			DHAV  	DHC8  	DHC8311     	1386006	EA  	PWA   	PW120 	PW123       		NE  					FUEL SYSTEM	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			14148	57   		B27028N		123113			(CAN) AN INVESTIGATION INTO A FUEL LEAK INTO THE NR 2 ENGINE DRAIN COLLECTOR BOX RESULTED IN THE REPLACEMENT OF THE MECH	ANICAL FUEL CONTROL AND THE ENGINE DRIVEN FUEL PUMP.  THIS WAS DUE TO A SHAFT SEAL LEAK.  MFC NR 3244853, EDFP NR 500826	9G.				2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999081200747	19990812	00747	NE  	1999	8	12	CA990707014      	2	19990615	G	7321	324485316	FCU             			DHAV  	DHC8  	DHC8311     	1386006	EA  	PWA   	PW120 	PW123       		NE  					NR 2 ENGINE	FAILED          	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		CL	CLIMB          	1			CA			10170					123133			(CAN) NR 2 ENGINE TORQUE DROPPED TO 20 PERCENT INCREASE IN PLA RESULTED IN FURTHER DECREASE  IN TORQUE.  HMFCU REPLACED.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999081200748	19990812	00748	NE  	1999	8	12	CA990707016      	2	19990618	G	7250	214117037	RIVET           								LYC   	ALF502	ALF502R5    	41580	NE  					TURBINE WHEEL	MISSING         	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA			10475					LF05567A			(CAN) A RETENTION RIVET ON THE FOURTH TURBINE WHEEL IS MISSING.											4	F			E6NE				 
1999081200750	19990812	00750	EA  	1999	8	12	CA990707019      	1	19990623	G	2435	23088002A	GENERATOR       			DHAV  	DHC8  	DHC8311     	1386006	EA  	PWA   	PW120 	PW123       		NE  					START/GENERATOR	VIBRATING       	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			6638 	219  				123129			(CAN) DURING LOW POWER OPERATION, NR 2 ENGINE WAS FOUND TO HAVE NOTICEABLE VIBRATION EVIDENT THROUGH THE POWER AND CONDI	TION LEVERS.  INVESTIGATION LED TO THE REPLACEMENT OF THE STARTER/GENERATOR UNIT.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999081200754	19990812	00754	NE  	1999	8	12	CA990707026      	2	19990615	G	7200		ENGINE          			BOEING	737   	737217      	1384464	NM  	PWA   	JT8   	JT8D17      	52049	NE  					NR 1	SLOW            	W				C				ABORTED TAKEOFF         				R			PARTIAL RPM/PWR LOSS      			TO	TAKEOFF        	1			CA								708821			(CAN) ON TAKEOFF, NR 1 ENGINE SLOW TO SPOOL UP.   AT TAKEOFF, THRUST, EPR FLUCTUATED.						2	L	7	2 	4F	4	F		A16WE   	E2EA				 
1999081200755	19990812	00755	NE  	1999	8	12	CA990707030      	2	19990505	G	7200	110071006	ENGINE          								LYC   	T53   	T5317A      	41549	NE  					ENGINE BAY	MISOVERHAULED   	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						JTS018806		LE07537C			(CAN) MILITARY PARTS FOUND INSTALLED AT ENGINE OVERHAUL INSPECTION.   NOTE:  HISTORY UNKNOWN. TYPE APPROVAL IE26.											4	U			E17EA				 
1999081200756	19990812	00756	CE  	1999	8	12	CA990707033      	1	19990624	G	2750	0523920	ROLLER          		052390138   	CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	TE FLAP	BROKEN          	W				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			CA				5126 				L415576	733708		(CAN) AFTER LANDING, THE FLAPS WERE SELECTED UP AND WERE SUBSEQUENTLY DAMAGED DUE TO A FAILURE OF THE OUTBOARD ROLLER AS	SY.					1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
1999082000218	19990820	00218	SW  	1999	8	20	CA990707035      	1	19990226	G	2435	PW203PP	BEARING         	LUCAS       	23032027    	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					START/GEN	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA				70   		14035		CAE832457			(CAN) STARTER/GENERATOR BEARINGS WERE FOUND TO NOT COMPLY WITH LUCAS SERVICE BULLETIN FOR MOD B UPGRADE REQUIREMENTS.  I	T IS SUSPECTED THAT THESE BEARINGS ARE NOT AN APPROVED 203PP PART.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999081200757	19990812	00757	GL  	1999	8	12	CA990707036      	2	19990623	G	7314	23003114	PUMP            			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					FUEL SYSTEM	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				502  		PE5105		CAE823401			(CAN) FUEL PUMP DRIVE SHAFT SHIFTING IN HOUSING, COULD POSSIBLY DISENGAGE DRIVE GEAR.  RESULT:  FUEL PUMP SENT FOR TEARD	OWN O-RING AND SIR CLIP FOUND DAMAGED.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999082000220	19990820	00220	SW  	1999	8	20	CA990707040      	1	19990624	G	2435		STARTER         	AIRPRTSCORP 	150SG117Q   	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					START/GEN	MISOVERHAULED   	W				O				OTHER                   				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA				582  		3080		800555			(CAN) UNAPPROVED PARTS FOUND ON APC STARTER/GENERATOR.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999081200759	19990812	00759	EU  	1999	8	12	CA990707049      	1	19990630	G	5532	5553012149	SKIN            	PILATS      	555301203700	PILATS	PC12  	PC12        	7090550	EU  										VERTICAL STAB	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			88   			139					(CAN) TWO CRACKS FOUND IN VERTICAL STABILIZER SKIN AT TOP RT REAR SPAR RIVET.  REPAIR CARRIED OUT PER PILATUS DRAWING.						1	L	7	1 	3T			RT	A78EU   					 
1999081200760	19990812	00760	CE  	1999	8	12	CA990707050      	1	19990608	G	2750	C1450046RX	GEARBOX         			CESSNA	208   	208B        	2073701	CE  	PWA   	PT6   	PT6A114     	52043	NE  					TE FLAP	FAILED          	W				H				DEACTIVATE SYST/CIRCUITS				F	J		FLT CONT AFFECTED         	WARNING INDICATION        		CL	CLIMB          	1			CA								PCE19192			(CAN) FLAP FAILURE WHEN RETRACTED.  FUNCTIONED IN EMERGENCY MODE ONLY WHEN CHECKED BY MAINTENANCE PERSONNEL.  FLAP MOTOR	 AND GEARBOX REPLACED.					1	H	7	1 	3T	3	T		A37CE   	E4EA				 
1999081200761	19990812	00761	NE  	1999	8	12	CA990707051      	2	19990623	G	8530		CYLINDER        			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					ENGINE	SEPARATED       	W				C				ABORTED TAKEOFF         				E			VIBRATION/BUFFET          			TO	TAKEOFF        	1			CA				490  				274956			(CAN) LOSS OF POWER AT TAKEOFF.  INVESTIGATION FOUND NR 6 CYLINDER HAD SEPARATED BETWEEN THE BARREL AND CYLINDER HEAD.						1	H	7	1 	3R	3	R		A806    	5E1				 
1999081200762	19990812	00762	CE  	1999	8	12	CA990707053      	1	19990624	G	2810		FUEL            			CESSNA	150   	152         	2071835	CE  										FUEL CELL	CONTAMINATED    	W				C				ABORTED TAKEOFF         				O			OTHER                     			TO	TAKEOFF        	1			CA											(CAN) FUEL CONTAMINATION, WATER.						1	H	7	1 	3O			NT	3A19    					 
1999081200763	19990812	00763	CE  	1999	8	12	CA990707054      	1	19990624	G	3242	06603300	CALIPER         			CESSNA	208   	208B        	2073701	CE  										BRAKE	CRACKED         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			1131 								(CAN) FLUID WAS OBSERVED AROUND BOLT HEAD WHICH ATTACHES THE BRAKE PAD BACKING PLATE TO THE CALIPER.  CRACK SUSPECTED OT	 BOLT HOLE.					1	H	7	1 	3T				A37CE   					 
1999081200764	19990812	00764	EA  	1999	8	12	CA990707055      	1	19990629	G	2722	2770537109	PCU             			CNDAIR	CL601 	CL6012A12   	1900303	EA  										RUDDER	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						06340					(CAN) DURING BACKLASH CHECK WITH ONLY 10 POUNDS SIDE LOAD, PCU WOULD DEFLECT 1.5 INCHES ONE WAY BYPASSING INTERNALLY ONL	Y 323 HRS, 265 DAYS					2	L	7	2 	4F			RT	A21AE   					 
1999081200765	19990812	00765		1999	8	12	CA990707056      	4	19990602	G	2565		DITCHING DAM    			DHAV  	DHC8  	DHC8311     	1386006	EA  	PWA   	PW120 	PW123       		NE  					EMERGENCY EXIT	DEPLOYED        	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			CA											(CAN) DITCHING DAM DEPLOYED IN-FLIGHT.  AIRSPEED SLOWED TO FLIGHT IN ROUGH AIR SPEED AND RETURNED TO BASE.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999081200766	19990812	00766	NE  	1999	8	12	CA990707057      	3	19990611	G	6110		PROPELLER ASSY  			DHAV  	DHC8  	DHC8311     	1386006	EA  	PWA   	PW120 	PW123       		NE  	HAMSTD	14SF	14SF15      	NE  	FORWARD	MISREPAIRED     	W				C				ABORTED TAKEOFF         				K			FLUID LOSS                			TO	TAKEOFF        	1			CA											(CAN) PROPELLER ASSEMBLY MISREPAIRED.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
1999081200767	19990812	00767	NM  	1999	8	12	CA990707058      	1	19990628	G	2933	3810047105	INDICATOR       			DHAV  	DHC8  	DHC8102     	2809003	NM  										COCKPIT	STUCK           	W				C				ABORTED TAKEOFF         				F	J		FLT CONT AFFECTED         	WARNING INDICATION        		TO	TAKEOFF        	1			CA						0349					(CAN) ON TO ROLL NR 1 HYDRAULIC ISO VALVE CAUTION LIGHT AND INBOARD ROLL, SPOILER CAUTION LIGHT ILLUMINATED.  INVESTIGAT	ION REVEALED NO LEAKS, HOWEVER, THE NR 1 SYSTEM LEVEL WAS LOW.  HYDRAULIC QUANTITY INDICATOR WAS STUCK WITH AN INDICATIO	N HIGHER THAN WHAT WAS IN THE RESERVOIR.  NORMAL TRANSFER OF FLUID THROUGH THE BRAKE SYSTEM LED TO THE LOW LEVEL SWITCH 	ACTUATING THE ISO VALVE.			2	H	7	2 	4T			RT	A13NM   					 
1999090300280	19990903	00280	NM  	1999	9	3	CA990707059      	1	19990629	G	2750	793T1003	DRIVE UNIT      			BOEING	727   	727260      		NM  	PWA   	JT8   	JT8D17      	52049	NE  					LE FLAP	INOPERATIVE     	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				32   		988553NRC		689961			(CAN) OUTBOARD FLAP ALTERNATE SYSYEM INOPERABLE.  OUTBOARD FLAPS ALT DRIVE UNIT REPLACED.						2	L	7	3 	4F	4	F	RT	A3WE    	E2EA				 
1999081200768	19990812	00768	EA  	1999	8	12	CA990707062      	1	19990608	G	6123	75239	GEAR            			CNDAIR	CL215 	CL2151A10   		EA  						HAMSTD	43E	43E60       	NE  	PROP BLADE	WARPED          	W				E				ENGINE SHUTDOWN         				E			VIBRATION/BUFFET          			CL	CLIMB          	1			CA			2943 	884  					208837		(CAN) ATTEMPT TO FEATHER PROPELLER DUE TO VIBRATION WAS UNSUCCESSFUL, ONE BLADE WOULD NOT FEATHER.  ONE BLADE GEAR SEGME	NT WAS FOUND DAMAGED AND THE FOUR SCREWS ATTACHING THE BLADE BUSHING, PN 75219, WERE SHEARED. ,					2	H	7	2 	4R				A14EA   		6	C	P871	 
1999081200769	19990812	00769	EA  	1999	8	12	CA990707065      	1	19990610	G	3246	1011601	WHEEL           	BFGOODRICH  		CNDAIR	CL215 	CL2156B11415		EA  										NLG	CRACKED         	W				K				NONE                    				K	W		FLUID LOSS                	INADEQUATE Q C            		IN	INSP/MAINT     	1			CA			358  			0793					(CAN) INVESTIGATING A SLOW LEAK WITH THE TIRE, FOUND A CRACK IN WHEEL BEAD AREA.  THIS SHOULD HAVE BEEN PICKED UP WITH N	DT.  TSN:  358  HOURS.					2	H	7	2 	4T			RT	A14EA   					 
1999081200771	19990812	00771	EA  	1999	8	12	CA990707070      	1	19990706	G	2910	AE2460010H0264	HOSE            			CNDAIR	CL600 	CL6002B19   		EA  	GE    	CF34  	CF343A1     	30015	NE  					HYDRAULIC SYSTEM	CRACKED         	W				H				DEACTIVATE SYST/CIRCUITS				K			FLUID LOSS                			CR	CRUISE         	1			CA											(CAN) IN-FLIGHT, NR 2 SYSTEM HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO.  HOSE FOUND CRACKED.						2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999081200772	19990812	00772	NE  	1999	8	12	CA990707073      	3	19990618	G	6111	53546	BEARING         			DHAV  	DHC3  	DHC3        	2800202	EA  	PWA   	R1340 	R134053     	52016	NE  	HAMSTD	3D	3D40        	NE  	COUNTERWEIGHT	BROKEN          	W				E				ENGINE SHUTDOWN         				E			VIBRATION/BUFFET          			CL	CLIMB          	1			CA			983  					P325619A	N404381		(CAN)  COUNTERWEIGHT ON PROPELLER IS BROKEN.						1	H	7	1 	3R	3	R		A815    	5E2			A815	 
1999081200773	19990812	00773	NE  	1999	8	12	CA990707075      	2	19990607	G	7314	5009984C	PUMP            			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					ENGINE	FAILED          	W				C				ABORTED TAKEOFF         				X			ENGINE FLAMEOUT           			TO	TAKEOFF        	1			CA			10711	2789 				120305			(CAN) LOSS OF ENGINE POWER RESULTED IN SHUT-DOWN PROCEDURE.  HMU, FUEL PUMP AND LRU'S SENT FOR TEARDOWN AND REPAIRS.  HM	U P/N 786391-6.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999081200774	19990812	00774	EA  	1999	8	12	CA990707078      	2	19990527	G	8530	O5K21129	CYLINDER HEAD   			PIPER 	PA28  	PA28R200    	7102811	SO  	LYC   	O360  	IO360C1C    	41514	EA  					ENGINE	CRACKED         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			33   					L1621051A			(CAN) CYLINDER HEAD CRACKED.						1	L	7	1 	3O	3	O		2A13    	1E10				 
1999081200775	19990812	00775	EU  	1999	8	12	CA990707079      	1	19990610	G	7800	0292808690	EXHAUST PIPE    			SNIAS 	350   	AS350B      	8680801	EU  	TMECA 	ARRIEL	ARRIEL1B    	6OO30	NE  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								786			(CAN) THREE CRACKS FOUND ON EXHAUST PIPE, WELD JOINT CRACK MID-FORWARD WHERE MO5 FITS INSIDE.  FIRST CRACK ON LEFT SIDE 	WHERE BOLT THAT HOLDS MO5 HEAT SHIELD ATTACHES.					1	G	7	1 	3U	3	U		H9EU    	E19EU				 
1999081200776	19990812	00776	EA  	1999	8	12	CA990707080      	2	19990623	G	7321	324475521	FCU             			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  					NR 1 ENGINE	FAILED          	W				D				RETURN TO BLOCK         				R			PARTIAL RPM/PWR LOSS      			TX	TAXI/GRND HDL  	1			CA				193  				PCE80830			(CAN) WHILE TAXIING, THERE WAS NO POWER CONTROL ON NR 1 ENGINE.  UNABLE TO GO ABOVE IDLE.  FUEL CONTROL UNIT WAS REPLACE	D.					1	L	7	2 	4T	4	T		A24CE   	E4EA				 
1999082000222	19990820	00222	EU  	1999	8	20	CA990715007      	1	19990218	G	6720	ACM29029	SERVO VALVE     	DUNLOP      	AC67244     	SNIAS 	350   	AS350B      	8680801	EU  	TMECA 	ARRIEL	ARRIEL1B    	6OO30	NE  					T/R CONT	DAMAGED         	W				O				OTHER                   				F			FLT CONT AFFECTED         			NR	NOT REPORTED   	1			CA				920  		KS318		836			(CAN) ON DISASSEMBLY, HYDRAULIC SERVO VALVE ASSEMBLY SPRING P/N ACO43242 WAS FOUND BONDED TO INPUT LEVER.  IAW DUNLOP MA	NUAL, GS-40-03, THE SPRING SHOULD NOT BE BONDED.					1	G	7	1 	3U	3	U		H9EU    	E19EU				 
1999082000224	19990820	00224	SO  	1999	8	20	CA990715009      	1	19990526	G	6120	6545104	CONTROL CABLE   			PIPER 	PA32  	PA32300     	7103212	SO  	LYC   	O540  	IO540K1A5   	41532	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	PROP CONTROL	BINDING         	W				C				ABORTED TAKEOFF         				F			FLT CONT AFFECTED         			TO	TAKEOFF        	1			CA								L518548	AW867		(CAN) PILOT REPORTED UNABLE TO MOVE CONTROL BACK TO FINE PITCH AFTER GROUND TESTING.  UPON INVESTIGATION, THE INNER CABL	E WAS FOUND TO HAVE BOUND IN THE OUTER JACKET.  STRANDS OF THE INNER CABLE BENT NEAR THE COCKPIT END OF THE CONTROL.					1	L	7	1 	3O	3	O	 	A3SO    	1E4	5	C	P920	 
1999081200777	19990812	00777	EA  	1999	8	12	CA990715011      	2	19990625	G	7310	3014704	MANIFOLD ASSY   								PWA   	PT6   	PT6A27      	52043	EA  					FUEL SYSTEM	MISMANUFACTURED 	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						SS0007D					(CAN) PREVIOUSLY REPORTED TO P&W BY OPERATOR.   BURRS AND MARKS HAVE BEEN FOUND IN THE PASSAGEWAYS OF THE TRANSFER TUBES	.  DIFFICULTIES ASSOCIATED IN ASSEMBLY IN WHICH THE OPERATOR FEELS COULD RESULT IN A FUEL HAZARD WHERE O-RINGS ARE DAMAG	ED AT INSTALLATION.  ONE TUBE STATED TO HAVE THIS CONDITION.									4	T			E4EA				 
1999081200778	19990812	00778	NE  	1999	8	12	CA990715012      	2	19990615	G	8520		CRANKCASE       			DHAV  	DHC3  	DHC3        	2800202	EA  	WSK   	ASZ62 	ASZ62IRM18  		NE  					ENGINE	CRACKED         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA				371  				KAB406019			(CAN) CRACK FOUND BETWEEN NR 5 AND NR 6 CYLINDERS.						1	H	7	1 	3R	3	R		A815    	E10NE				 
1999081200779	19990812	00779	EA  	1999	8	12	CA990715015      	2	19990428	G	7310	06827M601	LINE            	AEROQUIP    	60100110D008	DHAV  	DHC6  	DHC6200     		EA  	PWA   	PT6   	PT6A20      	52043	EA  	HARTZL	HCB3T	HCB3TN3     	GL  	FUEL SYSTEM	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			1422 					PCE21544	BUA20226		(CAN) AIRCRAFT PARKED FOR 5 MONTHS.  ON INSPECTION, NOTED THAT FUEL WAS RUNNING DOWN STRUT.  FUEL WAS NOTED COMING FROM 	STEEL BRAIDED LINE.  TYPE 601 LINE MFD 2Q90.					1	H	7	2 	3T	3	T		A9EA    	E4EA	6	C	P15EA	 
1999081200780	19990812	00780	EA  	1999	8	12	CA990715017      	2	19990626	G	8520	LW12427	CYLINDER HEAD   			BBAVIA	8     	8GCBC       	1220803	SW  	LYC   	O360  	O360C2E     	41514	EA  					ENGINE	CRACKED         	W				A				UNSCHED LANDING         				R	E		PARTIAL RPM/PWR LOSS      	VIBRATION/BUFFET          		CL	CLIMB          	1			CA				1688 				L2922336A			(CAN) ENGINE VIBRATION AND POWER LOSS WHILE GLIDER IN TOW.  CRACK AROUND NR 2 CYLINDER.  CYLINDER HAD BEEN OVERHAULED SU	BJECT TO FREEDOM FREE PROCESS AND CERMICROME PLATING.					1	H	7	1 	3O	3	O		A21CE   	E286				 
1999081200782	19990812	00782	SO  	1999	8	12	CA990715019      	1	19990705	G	7810		EXHAUST STACK   			PIPER 	PA24  	PA24250     	7102404	SO  	LYC   	O540  	O540A1D5    	41532	EA  					ENGINE	SEPARATED       	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA								L514540			(CAN) EXHAUST STACK TOTALLY SEPARATED INSIDE CARBURETOR HEAT SHROUD.  VISIBLE SIGNS OF PROLONGED FAILURE.						1	L	7	1 	3O	3	O		1A15    	E295				 
1999081200783	19990812	00783	SO  	1999	8	12	CA990715020      	1	19990705	G	2421	MR12N600	ALTERNATOR      			PIPER 	PA24  	PA24250     	7102404	SO  	LYC   	O540  	O540A1D5    	41532	EA  					ENGINE	LOOSE           	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA								L514540			(CAN) ALTERNATOR BRACKET NOT CERTIFIED FOR AVIATION APPLICATION (BOGUS PARTS).  ALTERNATOR INSTALLED 55 AMP.  SPECS CALL	 FOR 70 AMP.  FORWARDED TO M&M FOR CORRECTIVE ACTION.					1	L	7	1 	3O	3	O		1A15    	E295				 
1999082000226	19990820	00226	SW  	1999	8	20	CA990715021      	1	19990622	G	2750	21583	MOUNT           			BBAVIA	8     	8GCBC       	1220803	SW  	LYC   	O360  	O360C2E     	41514	EA  					TE FLAP	CRACKED         	W				O				OTHER                   				F			FLT CONT AFFECTED         			DE	DESCENT        	1			CA			830  					L1868036A			(CAN) IN DESCENT AFTER GLIDER RELEASE AND AFTER EXTENDING FLAPS TO 27 DEGREES, PILOT NOTICED UNCOMMANDED ROLL TO THE RIG	HT.  VISUAL INSPECTION INDICATED THAT THE LEFT FLAP APPEARED TO BE IN APPROPRIATE POSITION, WHILE RIGHT FLAP WAS AT APPR	OXIMATELY 7-12 DEGREES.  CONSTANT STICK LEFT WAS REQUIRED TO MAINTAIN LEVEL ATTITUDE.  ON GROUND, BOTH FLAPS APPEARED TO	 BE OF SIMILAR DEFLECTION AT ALL SETTINGS.  UNCOMMANDED ROLL ONLY OCCURRED AT FULL FLAP GREATER THAN 21 DEGREE SETTINGS.			1	H	7	1 	3O	3	O		A21CE   	E286				 
1999081200784	19990812	00784	EA  	1999	8	12	CA990715023      	3	19990705	G	6111		BLADE           			PIPER 	PA38  	PA38112     	7103812	SO  						SNSNCH	72C	72CK        	EA  	PROPELLER	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				9207 					K3920		(CAN) PROPELLERS RECEIVED WITH BELOW MANUFACTURER'S LIMITS MAINTAINED BY OPERATORS.						1	L	7	1 	3O				A18SO   		5	N	P9045	 
1999082000227	19990820	00227	EU  	1999	8	20	CA990715024      	1	19990705	G	3250	Z4242170001	SPRING          			ZLIN  	242   	Z242L       	9970204	EU  										NLG STEERING	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2741 								(CAN) DURING SCHEDULED INSPECTION, THE RIGHT STEERING SPRING WAS FOUND TO BE BROKEN.  THE SPRING WAS REPLACED USING THE 	MINIMUM COIL DISTANCE SETTING ON THE LT AND RT STEERING SPRINGS.  THE STUDENTS WERE ALSO REMINDED OF THE PROPER TAXIING 	AND TOWING TECHNIQUES...THAT IS, START THE AIRCRAFT ROLLING BEFORE TURNING THE NOSE GEAR.				1	L	7	1 	3O			0	A76EU   					 
1999090300288	19990903	00288	NM  	1999	9	3	CA990715025      	1	19990616	G	5230	622EN526	SWITCH          			BOEING	727   	727221      	1384071	NM  	PWA   	JT8   	JT8D17      	52049	NE  					CARGO DOOR	MALFUNCTIONED   	W				A				UNSCHED LANDING         				O			OTHER                     			CR	CRUISE         	1			CA											(CAN) WHEN MAIN CARGO DOOR SELECTED OPEN, THE DOOR SWITCHES AND SECURING PINS BLEED TO CLOSED AND LOCKED POSITION PREVEN	TING DOOR FROM BEING CLOSED.  MOMENTARY POSITIONING OF DOOR OPERATING SWITCH WILL TEMPORARILY RE-SEQUENCE MECHANISM TO F	ACILITATE DOOR CLOSURE.  REPLACED MAIN CARGO DOOR CLOSED SEQUENCE SWITCH.  CYCLED SEVERAL TIMES AND SERVICEABLE.				2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999081200785	19990812	00785	NE  	1999	8	12	CA990715030      	2	19990627	G	7532		BLEED VALVE     			LEAR  	25    	25B         	5170511	CE  	GE    	CJ610 	CJ6106      	30006	NE  					RT ENGINE	OUT OF ADJUST   	W				A				UNSCHED LANDING         				X			ENGINE FLAMEOUT           			CR	CRUISE         	1			CA								240226A			(CAN) ENGINE FLAME-OUT AT 41,000 FEET UNDER NORMAL CONDITIONS.  FURTHER INSPECTION CARRIED OUT, ADJUSTMENT OF BLEED VALV	ES INLET BLANKET REPOSITIONED.  NO FURTHER FAULTS EXPERIENCED.  CONTACTED OPERATOR, NO ACTION REQUIRED.					2	L	7	2 	4J	4	J		A10CE   	1E16				 
2000081000037	20000810	00037	WP  	2000	8	10	CA990715031      	1	19990617	G	3231	28B4028	TORQUE TUBE     			CVAC  	PBY5  	285ACFBABB  	2421230	WP  	PWA   	R1830 	R183092     	52020	NE  					LT AFT ARM	CORRODED        	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			12767					4239141			(CAN) DURING ANNUAL INSPECTION, A SPECIAL INSPECTION WAS CARRIED OUT DUE TO A REPORT BY THE U.K. GOVERNMENT (AAIB BULLET	IN NR:  1/99, REF:   EW/C98/7/9 CATEGORY: 1.1).  THE BULLETIN DETERMINED THAT THE LT GEAR DOOR COLLAPSED INWARDS DUE TO 	THE INABILITY OF THE CORRODED TORQUE TUBE BEING ABLE TO RESIST THE RANGE OF LOADS WHICH MIGHT BE IMPOSED OVER A WATER LA	NDING.  UPON INSPECTION OF THE NOSE LANDING GEAR DOOR TORQUE TUBES IT WAS DISCOVERED THAT  LT TORQUE TUBE HAD VISIBLE CO	RROSION AT THE AFT OPERATING ARMS - THE SAME LOCATION AS THE CATALINA THAT CRASHED - AND UPON REMOVAL OF THE RT TORQUE T	UBE CORROSION WAS FOUND INTERNALLY.	2	H	7	2 	4R	4	R	 	TC785   	5E4				 
1999081200786	19990812	00786	CE  	1999	8	12	CA990715032      	1	19990705	G	5712	07206078	RIB             			CESSNA	206   	U206B       	2073322	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	3A32C	D3A32C90    	GL  	WS 190	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								245502H	816431		(CAN) THE CENTER RIB AT WS 190.0 OF RT WING FOUND CRACKED AT TRAILING END THAT IS RIVETED TO WING REAR SPAR.  ALSO, FOUN	D SEVERAL LOOSE AND SMOKING RIVETS IN THIS AREA.					1	H	7	1 	3O	3	O		A4CE    	E5CE	5	C	P21EA	 
1999081200787	19990812	00787	EA  	1999	8	12	CA990715033      	1	19990713	G	5540	MS1410210	BEARING         		600210391   	CNDAIR	CL601 	CL6012A12   	1900303	EA  										RUDDER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			7737 								(CAN) SPHERICAL BEARING LOCATED IN THE CENTER LOWER RUDDER HINGE FITTING WAS FOUND CRACKED DURING A ROUTINE CHECK.						2	L	7	2 	4F			RT	A21AE   					 
1999081200788	19990812	00788	NE  	1999	8	12	CA990715034      	2	19990706	G	7322		MFC             			CNDAIR	CL600 	CL6002B19   		EA  	GE    	CF34  	CF343A1     	30015	NE  					E/E BAY	FAILED          	W				E				ENGINE SHUTDOWN         				R			PARTIAL RPM/PWR LOSS      			DE	DESCENT        	1			CA											(CAN) ENGINE WOULD NOT DECELERATE TO IDLE, WITH THE THRUST LEVER AT THE IDLE STOP THE ENGINE PARAMETERS REMAINED AT N1 6	6, ITT 570, N2 82, FF 400. MFC REPLACED.  AIRCRAFT RETURNED TO SERVICE.					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999082000228	19990820	00228	SO  	1999	8	20	CA990715043      	1	19990630	G	2913	318002	POWER PACK      			PIPER 	PA23  	PA23250     	7102308	SO  	LYC   	O540  	IO540C4B5   	41532	EA  					HYDRAULIC SYSTEM	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA				1140 		4987		L372748			(CAN) NOSE LANDING GEAR CREEPED CLOSED WHEN AIRCRAFT HANGARED OVERNIGHT.  SMALL POOL OF HYDRAULIC FLUID ON FLOOR.  PILOT	 REPORTED LANDING GEAR CREEPING DOWN AT TIMES.  HAD TO BE RE-SELECTED AFTER SOME ACTUATORS HAD O-RINGS REPLACED.  WING F	LAPS COMING DOWN TOO SOON WHEN SELECTED.  ON INSPECTION, UNIT FOUND 'WET' WITH HYDRAULIC FLUID INDICATING 'SWEAT LEAKS'.	  NOTE:  SMALL POOL OF FLUID ON FLOOR WAS ASSESSED TO OVERFLOW WHICH OUTLETS ON TOP OF NOSE WHEEL WHEN RETRACTED AS RESE	RVOIR HAD BEEN SERVICED WITH LANDING GEAR DOWN AND FLAPS UP.		1	L	7	2 	3O	3	O		1A10    	1E4				 
1999081200792	19990812	00792	EU  	1999	8	12	CA990715044      	1	19990708	G	7712	3036927	TQ SIG COND     			AEROSP	ATR42 	ATR42300    	8680920	EU  	PWA   	120   	PW120       		NE  	HAMSTD	14SF	14SF5       	NE  	ENGINE	FAILED          	W				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CL	CLIMB          	1			CA			19665	9331 		1814		120619	881231		(CAN) TORQUE SIGNAL CONDITIONER FAILED, THIS CAUSED ATPCS TO FEATHER THE PROPELLER.   IN-FLIGHT SHUTDOWN AND RESTART REM	EDIED THE PROBLEM UNTIL RTU MAINTENANCE FACILITY.					2	H	7	2 	4T	4	T	RT	A53EU   	E20NE	6	C	P7NE	 
1999081200793	19990812	00793	EA  	1999	8	12	CA990715045      	2	19990410	G	8530		EXHAUST VALVE   			PIPER 	PA28  	PA28R200    	7102811	SO  	LYC   	O360  	IO360C1C    	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	CYLINDER	BROKEN          	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA				1576 				RL1143651A	CH5609		(CAN) NR 3 ENGINE EXHAUST VALVE BROKEN AT STEM AND INJESTED.						1	L	7	1 	3O	3	O		2A13    	1E10	5	C	P920	 
1999081200794	19990812	00794	EA  	1999	8	12	CA990715046      	2	19990427	G	8530		CYLINDER        			PIPER 	PA44  	PA44180     	7104402	SO  	LYC   	O360  	O360E1A6    	41514	EA  					ENGINE	SEPARATED       	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA				1405 				L33477T			(CAN) NR 3 CYLINDER SEPARATED FROM CRANKCASE.  CONNECTING ROD SEPARATED FROM PISTON.  CAUSE OF FAILURE BEING CRANKCASE F	RETTING LEADING TO THE LOSS OF TORQUE ON CYLINDER HOLD DOWN NUTS OF NR 3 CYLINDER.  ENGINE REPLACED.					1	L	7	2 	3O	3	O		A19S0   	E286				 
1999082000229	19990820	00229	SO  	1999	8	20	CA990715047      	1	19990618	G	7120	893611002	MOUNT           			PIPER 	PA44  	PA44180     	7104402	SO  	LYC   	O360  	O360E1A6    	41514	EA  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L33477T			(CAN) INSPECTION REVEALED RIGHT ENGINE MOUNT CRACKED AT TOP, OUTBOARD, TUBING CLUSTER BELOW LORD MOUNT ATTACHMENT HOLE.						1	L	7	2 	3O	3	O		A19S0   	E286				 
1999082000230	19990820	00230	SO  	1999	8	20	CA990715048      	1	19990624	G	2434	649031	WIRE            	PRESTOLITE  	ALU8421LS   	PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2B   	41532	EA  					ALTERNATOR	BROKEN          	W				A				UNSCHED LANDING         				H			ELECT. POWER LOSS-50 PC   			CR	CRUISE         	1			CA						5052721		L134861			(CAN) RIGHT ALTERNATOR WENT OFF-LINE AND THE AIRCRAFT STARTED TO LOSE NAVIGATIONAL AIDS.  CREW DISCOVERED NO CHARGE FROM	 ALTERNATOR.  THE AMP TERMINAL END WAS REPLACED AT THE FIELD TERMINAL FOR THE RIGHT ALTERNATOR AND BOTH ALTERNATOR BELTS	 TIGHTENED.				1	L	7	2 	3O	3	O	 	A20SO   	E14EA				 
1999082000231	19990820	00231	CE  	1999	8	20	CA990715049      	1	19990624	G	7920		LINE            			HELIO 	H295  	H295        	4300802	CE  	LYC   	O480  	GO480G1D6   	41527	EA  	HARTZL	HCB3Z	HCB3Z201    	GL  	ENGINE OIL	RUPTURED        	W				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			CL	CLIMB          	1			CA			500  					L57637	AF516		(CAN) PILOT SMELLED SMOKE ON CLIMB-OUT AND SHUT OFF ALTERNATOR AND ELECTRICS.  RETURNED TO DEADMAN'S POND.  INVESTIGATIO	N FOUND MAIN OIL LINE FROM ENGINE TO FILTER RUPTURED AT MID-POINT.  SUSPECT THAT AT SOME TIME, LINE MAY HAVE BEEN IN CLO	SE PROXIMITY TO THE EXHAUST.				1	H	7	1 	3O	3	O		1A8     	E275	5	C	P907	 
1999081200795	19990812	00795	EA  	1999	8	12	CA990715050      	2	19990627	G	8530	890419	CYLINDER        			GRUMAV	TBM   	TBM3AIRTRD  	3950308	EA  	WRIGHT	R2600 	R260020     	67050	EA  	HAMSTD	23E	23E50       	NE  	ENGINE	CONTAMINATED    	W				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			CR	CRUISE         	1			CA				340  				172966	P84440		(CAN) HOLE FOUND IN NR 6 CYLINDER .5 INCH ABOVE MOUNTING FLANGE.  OIL SCREENS HAD METAL CONTAMINATION. THE ENGINE WAS CH	ANGED.  FURTHER INFO:  CONNECTING ROD FAILURE 3.5 INCHES FROM PISTON PIN CUTOUT WAS FOUND DURING STRIP DOWN.					1	L	7	1 	4R	4	R		L82     	TC176	6	C	P603	 
1999081200796	19990812	00796		1999	8	12	CA990715051      	4	19990629	G	8300		GEARBOX         			CNDAIR	CL215 	CL2151A10   		EA  	PWA   	R2800 	CA3         	52026	NE  					OIL SYSTEM	MAKING METAL    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				447  				P33302			(CAN) METAL IN OIL SCREEN OF FRONT SUMP, SUSPECTED REDUCTION GEAR FAILURE.   ENGINE REPLACED.						2	H	7	2 	4R	4	R		A14EA   	E231				 
1999081200797	19990812	00797	EA  	1999	8	12	CA990715052      	1	19990629	G	7810	327628	EXHAUST PIPE    			CNDAIR	CL215 	CL2151A10   		EA  	PWA   	R2800 	CA3         	52026	NE  					CYLINDER	SEPARATED       	W				O				OTHER                   				D			INFLIGHT SEPARATION       			LD	LANDING        	1			CA				160  				P34003			(CAN) EXHAUST SEPARATED FROM NR 13 CYLINDER, ALL THREE STUDS PULLED AWAY FROM CYLINDER HEAD.  CYLINDER REPLACED.						2	H	7	2 	4R	4	R		A14EA   	E231				 
1999081200798	19990812	00798	SO  	1999	8	12	CA990719001      	2	19990630	G	7414	10349276	CAPACITOR       		103493505R  	CESSNA	185   	A185F       	2072821	CE  	CONT  	O520  	IO520D      	17032	SO  	MCAULY	D3A34	D3A34C403   	GL  	RT MAGNETO	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				724  		905452		566561	770031		(CAN) RIGHT MAGNETO CAPACITOR FAILURE.  ENGINE WOULD NOT SHUT DOWN WITH MAGNETO SWITCH.						1	H	7	1 	3O	3	O		3A24    	E5CE	5	C	P47GL	 
1999082000233	19990820	00233	CE  	1999	8	20	CA990719003      	1	19990708	G	3260	MS243311	SWITCH          		11438004115 	BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					MLG	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA				1886 		0807A		PCEPS0128			(CAN) PILOT REPORTED ON APPROACH TO CYBL, GEAR WAS SELECTED DOWN, ALL GEAR WENT DOWN, ALL LIGHTS ILLUMINATED, BUT PILOT 	NOTCED LT MAIN DOWN AND LOCKED LIGHT WAS A DIM GREEN.  ON APPROACH TO YVR, GEAR WAS SELECTED DOWN, LT INDICATION WAS NOT	ED TO BE EVEN DIMMER.  THE PILOT NOTICED, VIEWED THROUGH THE WINDOW, THAT LT GEAR WAS STILL UP.  NO RED IN-TRANSIT LIGHT	 AND NO WARNING HORN.  MANUAL EXTENSION WAS CARRIED OUT AND THE LT GREEN LIGHT WAS NOTED TO BE NOW OF THE SAME INTENSITY	 AS THE OTHERS.  MAINTENANCE SWUNG THE GEAR SEVERAL TIMES. THE LT DOWN AND LOCKED LIGHT DIMMED ERRATICALLY.  AT NO TIME 	DID THE GEAR FAIL TO CYCLE.  THE LT ACTUATOR WAS REPLACED.  GEAR CYCLED WITH NO FAULTS FOUND.	2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999082000234	19990820	00234	SO  	1999	8	20	CA990719004      	1	19990709	G	2720	7891502	TORQUE TUBE     			PIPER 	PA32  	PA32RT300T  	7103216	SO  	LYC   	O540  	TIO540S1AD  	41532	EA  	HARTZL	HCE2Y	HCE2YR1BF   	GL  	RUDDER	CORRODED        	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			2876 					L563861A	DK1311		(CAN) WHEN RUDDER WAS REMOVED FOR PAINTING , IT WAS FOUND THAT THE LOWER ENDS OF THE TORQUE TUBE WERE SEVERELY CORRODED 	BY STANDING WATER IN TUBE OVER A LONG PERIOD.  THERE IS NO DRAIN IN TUBE AND IT FITS ONTO RUDDER BELLCRANK SO TIGHTLY TH	AT THE WATER WILL NOT LEAK.  IT IS IMPOSSIBLE TO SEE UNLESS RUDDER IS REMOVED.				1	L	7	1 	3O	3	O		A3SO    	E14EA	5	C	P9EA	 
1999081200799	19990812	00799		1999	8	12	CA990719007      	1	19990705	G	7810	1379049H401	EXHAUST STUB    								GARRTT	TPE331	TPE33110UG  	01514	WP  					CYLINDER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								P63246C			(CAN) EXHAUST STUB WAS FOUND TO BE CRACKED 75 PERCENT AROUND CIRCUMFERENCE OF THE EXHAUST FLANGE.  RECTIFIED BY IMPLEMEN	TATION OF SB 78-JM7799.										4	T			E4WE				 
1999082000235	19990820	00235	SO  	1999	8	20	CA990719008      	1	19990401	G	7120	89361002	MOUNT           			PIPER 	PA44  	PA44180     	7104402	SO  	LYC   	O360  	O360E1A6    	41514	EA  					LEFT ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L33477T			(CAN) INSPECTION REVEALED CRACKED LEFT ENGINE MOUNT AT TOP TUBE CLUSTER WELD OF TOP OUTBOARD LORD MOUNT HOLE.						1	L	7	2 	3O	3	O		A19S0   	E286				 
1999082000236	19990820	00236	SW  	1999	8	20	CA990719009      	1	19990618	G	5311	206033107049	FRAME           		206033002007	BELL  	206   	206L        	1181522	SW  										FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			11915								(CAN) FRAME AT WATER LINE STATION 67.00 FOUND CRACKED ACROSS THE INNER 75 PERCENT OF THE WEB AND TOTALLY THROUGH THE INN	ER FLANGE.  IT HAS NOW PROPAGATED A 2 INCH CRACK AT THE SAME PLACE ON THE INNER SKIN P/N 206-031-117-253.					1	G	7	1 	3U				H2SW    					 
1999082000237	19990820	00237	SW  	1999	8	20	CA990719010      	1	19990620	G	5410	206033501004	SUPPORT         			BELL  	206   	206L        	1181522	SW  										NACELLE	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			11915								(CAN) RIGHT SUPPORT ASSY WAS REMOVED FOR ACCESS FOR ANOTHER JOB, BUT IT WAS THEN DISCOVERED THAT THE REAR FACE WHICH BUT	TS AGAINST THE FORWARD FIRE WALL WAS FOUND TO BE CORRODED BEYOND LIMITS.  THIS AREA IS NOT VISIBLE DURING NORMAL MAINTEN	ANCE.				1	G	7	1 	3U				H2SW    					 
1999081200800	19990812	00800	GL  	1999	8	12	CA990719011      	2	19990608	G	7210		GEARBOX         			CVAC  	340   	340CVAC     	242270A	WP  	ALLSN 	501D  	501D13      	03004	GL  					LT ENGINE	FAILED          	W				O				OTHER                   				X	J		ENGINE FLAMEOUT           	WARNING INDICATION        		AP	APPROACH       	1			CA				14658				501698			(CAN) LEFT HAND ENGINE FAILURE.  REDUCTION GEARBOX FOUND DE-COUPLED DUE TO INTERNAL FAILURE.  RGB  AND TORQUE SHAFT REPL	ACED.					2	L	7	2 	4R	4	T		6A6     	E282				 
1999090300297	19990903	00297	WP  	1999	9	3	CA990719013      	1	19990617	G	2421	30E029G	GENERATOR       			CVAC  	340   	340CVAC     	242270A	WP  	ALLSN 	501D  	501D13      	03004	GL  					LT ENGINE	FAILED          	W				E				ENGINE SHUTDOWN         				M	N		OVER TEMP                 	FALSE WARNING             		CR	CRUISE         	1			CA				218  		RK5166		501698			(CAN) LEFT GENERATOR OVERHEAT LIGHT CAME ON, WOULD NOT GO OUT, ENGINE SHUT DOWN.  NO PHYSICAL EVIDENCE OF OVERHEAT, GENE	RATOR REPLACED, TEMP PROBE AND WIRING TESTED OK.					2	L	7	2 	4R	4	T		6A6     	E282				 
1999082000238	19990820	00238	EU  	1999	8	20	CA990719014      	1	19990708	G	3250	Z4242170001	SPRING          	MORAVN      	L24242370000	ZLIN  	242   	Z242L       	9970204	EU  										NLG STEERING	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2767 								(CAN) WHILE MOVING AIRCRAFT, THE STUDENT NOTICED THAT THE RUDDER AND NOSE WHEEL DID NOT LINE UP WITH EACH OTHER.  MAINTE	NANCE FOUND THAT THE LT STEERING SPRING WAS BROKEN.  WHEN THE RT STEERING SPRING WAS PREVIOUSLY REPLACED, THE STEERING S	PRINGS WERE NOT TIGHTENED EVENLY PUTTING STRESS ON THE LT SPRING.				1	L	7	1 	3O			0	A76EU   					 
1999082000239	19990820	00239	SO  	1999	8	20	CA990719038      	1	19990710	G	5400	4160401	HEAT SHIELD     			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2B   	41532	EA  					RT NACELLE	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			8090 					L161761			(CAN) REFERENCE:  IPC FIG  82 ITEMS 23, 29, AND 57.  DURING 50 HR INSPECTION FOUND SHIELD P/N 41604-01 WITH 6 CHERRY MAX	 RIVETS PULLED OUT WHICH SECURES HEAT SHIELD TO SKIN P/N 41667-08 AND ANGLE P/N 40667-1 ON RT NACELLE.  HEAT SHIELD SHOW	S TO HAVE BEEN EITHER PREVIOUSLY REPLACED OR RE-INSTALLED.  NO RECORDS FOUND.  COULD HAVE BEEN AS A RESULT OF IMPROPER I	NSTALLATION.  ALSO NOTE PILOT'S INTERPRETATION OF 'EXERCISING PROPELLERS' MAY BEING DONE AT A MAX OF 500 RPM INSTEAD OF 	A MAX OF 200 RPM DROP.		1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999091700409	19990917	00409		1999	9	17	CA990728001      	4	19990716	G	2562	6153681	ANTENNA         			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					ELT	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1360 					CAE820514			(CAN) ELT ANTENNA IS LOCATED ON REAR DOGHOUSE COWLING.  THIS TEL 82 ELT P/N 82101 HAS AN ANTENNA WHICH HAS A PLASTIC THR	EADED BASE AND IF HAND-TIGHTENED TO THE EXTREME, WILL CRACK AND CAN DEPART THE AIRCRAFT IN-FLIGHT.  THIS IS WHAT HAPPENE	D IN THIS INCIDENT.				1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999082000240	19990820	00240	NE  	1999	8	20	CA990728002      	2	19990618	G	7321	324485315	FCU             			DHAV  	DHC8  	DHC8311     	1386006	EA  	PWA   	PW120 	PW123       		NE  					NR 1 ENGINE	FAILED          	W				O				OTHER                   				J			WARNING INDICATION        			LD	LANDING        	1			CA			5217 					123116			(CAN) NR 1 ENGINE LOST POWER ON FINAL.  NO RESPONSE TO P/L MOVEMENT.  ENGINE REMAINED RUNNING.  THE HMFC UNIT WAS REPLAC	ED.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999082000242	19990820	00242	NE  	1999	8	20	CA990728011      	3	19990709	G	6112	7826891	BRUSH BLOCK     			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  	HAMSTD	14SF	14SF7       	NE  	PROP DEICE	WORN            	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			14286			880410		120064	860404		(CAN) NR 1 PROPELLER DEICE PHASE B CIRCUIT BREAKER TRIPS.  PROPELLER DEICE BRUSH BLOCK REPLACED.						2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
1999082000243	19990820	00243	CE  	1999	8	20	CA990728017      	1	19990714	G	7712	31017263	TORQUE SENSOR   			MTSBSI	MU2   	MU2B36      	5780412	CE  	GARRTT	TPE331	TPE3316252M 	01514	NE  					ENGINE	FAILED          	W				A				UNSCHED LANDING         				X	J		ENGINE FLAMEOUT           	WARNING INDICATION        		CR	CRUISE         	1			CA			4212 					P20081C			(CAN) THE FAILURE WAS LIMITED TO THE DIRECT DRIVE GEAR STACK ON THE TORQUE SENSOR.  THIS GEAR DRIVES THE FUEL PUMP AND F	UEL CONTROL THE FAILURE OF WHICH SHUT DOWN THE ENGINE DUE TO LOSS OF FUEL PRESSURE.  THE SHAFT HAD BROKEN IN THE THREAD 	AREA UNDER THE RETAINING NUT FOR THE FORWARD GEAR, CAUSING THE GEAR TO DISENGAGE FROM THE SHAFTS DRIVE SPLINES.  EVIDENC	E INDICATES THAT THE THREADED AREA OF THE SHAFT MAY HAVE BEEN CRACKED 80 PERCENT THROUGH THE SHAFT AT THE THREAD ROOT DU	RING ASSY AT MANUFACTURE.  PN 3101726-3 TORQUE SENSOR.		1	H	7	2 	3T			RT	A10SW   	E2WE				 
1999082000244	19990820	00244		1999	8	20	CA990728019      	1	19990708	G	7920		LINE            								GE    	CF6   	CF680C2*    		GL  					NR 2 ENGINE	WORN            	W				E	B			ENGINE SHUTDOWN         	EMER. DESCENT           			K	J		FLUID LOSS                	WARNING INDICATION        		CR	CRUISE         	1			CA			20885	4925 				702149			(CAN) LOSS OF ALL OIL IN NR 2 ENGINE.  ENGINE SHUT-DOWN.  OIL LEAK ISOLATED TO B-SUPPLY LINE FORWARD OF FUEL NOZZLE AT 9	 O'CLOCK POSITION.  NO REPAIR AVAILABLE.   NR 2 ENGINE REPLACED.										4	F			E23EA				 
1999082000245	19990820	00245	GL  	1999	8	20	CA990728024      	2	19990625	G	7250	6886407	WHEEL           			HUGHES	369   	369E        	4470707	WP  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE SECTION	FAILED          	W				A				UNSCHED LANDING         				K	M	J	FLUID LOSS                	OVER TEMP                 	WARNING INDICATION        	CL	CLIMB          	1			CA								CAE833536			(CAN) ENGINE FAILURE.  INITIAL INVESTIGATION SHOWS FAILURE OF NR 1 GP WHEEL, POSSIBLY DUE TO OVER-TEMPERATURE.   INITIAL	 TESTING OF TEMP SENSING SYSTEM SHOWS ERROR OF 80 DEGREES CELCIUS.					1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999082000246	19990820	00246	EA  	1999	8	20	CA990728025      	2	19990714	G	7414	D6RN3200	MAGNETO         			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	LTIO540J2BD 	41533	EA  					ENGINE	FAILED          	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CL	CLIMB          	1			CA				696  		F17970		RL97668A			(CAN) DUAL MAGNETO WITH COMMON DRIVE FAILED BOTH RIGHT AND LEFT MAGS RESULTING IN POWER LOSS.						1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999082700130	19990827	00130	EA  	1999	8	27	CA990728030      	2	19990715	G	8500		ENGINE          			ROBSIN	R44   	R44         	7640120	WP  	LYC   	O540  	O540F1B5    	41532	EA  					ENGINE BAY	FAILED          	W				O				OTHER                   				Y	J		ENGINE STOPPAGE           	WARNING INDICATION        		TO	TAKEOFF        	1			CA			850  					L2497240A			(CAN) ENGINE FAILURE LOSS OF POWER.  AIRCRAFT CRASH LANDED.  TSB INVESTIGATING INTO CARBURETOR HEAT CLUTCH ASSY AS CAUSE	.  CARBURETOR HEAT MECHANISM (SUBMITTER STATED THIS HAS NOT BEEN SUBSTANTIATED BY TSB).					1	G	7	1 	3O	3	O		H11NM   	E295				 
1999082700131	19990827	00131	EA  	1999	8	27	CA990728031      	2	19990716	G	8500		ENGINE          			ROBSIN	R44   	R44         	7640120	WP  	LYC   	O540  	O540F1B5    	41532	EA  					ENGINE BAY	FAILED          	W				O				OTHER                   				Y	J		ENGINE STOPPAGE           	WARNING INDICATION        		CL	CLIMB          	1			CA			1167 					L2499940A			(CAN) AFTER LIFT OFF, THE HELICOPTER YAWED SLIGHTLY AFTER A LOUD NOISE WAS HEARD. PILOT RETURNED TO PAD AND SHUT DOWN EN	GINE.					1	G	7	1 	3O	3	O		H11NM   	E295				 
1999082700132	19990827	00132	EA  	1999	8	27	CA990728032      	1	19990622	G	3260		DOWNLOCK        			DHAV  	DHC2  	DHC2MK3     	2800107	EA  	PWA   	PT6   	PT6A34      	52043	EA  					MLG	BLOCKED         	W				O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			CA						60137		PCE56839			(CAN) PILOT COMPLAINED ABOUT NO GEAR DOWN INDICATION.  CYCLED GEAR NUMEROUS TIMES WITH NO INDICATION.  A MIRROR CHECK CO	NFIRMED THE GEAR WAS DOWN.  DURING INSPECTION OF THE GEAR, FOUND THE FORWARD FLOAT ROPE STUCK INTO THE GEAR DOWNLOCK.  T	HE END OF THE ROPE DROPPED INTO THE INSPECTION HOLE ON TOP OF THE FLOAT.				1	H	7	1 	3T	4	T		A806    	E4EA				 
1999082000247	19990820	00247	GL  	1999	8	20	CA990728033      	2	19990709	G	7250	6892828	NOZZLE SHIELD   			SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					NR 1 NOZZLE	BROKE           	W				O				OTHER                   				O			OTHER                     			TX	TAXI/GRND HDL  	1			CA								CAE890370S			(CAN) ENGINE WAS SLOW TO START.  REMOVED COMBUSTION LINER FOR TROUBLESHOOTING AND FOUND DEFLECTOR DETACHED FROM NOZZLE S	HIELD PARTIALLY BLOCKING ENTRY TO NOZZLE VANES.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999082000248	19990820	00248	EU  	1999	8	20	CA990728035      	1	19990518	G	2612	875129	FIRE DETECTOR   			FOKKER	F28   	F28MK1000   	4990808	EU  										ENGINE	SHORTED         	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			N			FALSE WARNING             			CL	CLIMB          	1			CA											(CAN) ENGINE SHUT DOWN DUE FIRE WARNING.  FIRE LOOP REPLACED DUE TO SHORTING ELEMENT.						2	L	7	2 	4F			RT	A20EU   					 
1999082700913	19990827	00913	EU  	1999	8	27	CA990728036      	2	19990611	G	7230		COMPRESSOR      			FOKKER	F28   	F28MK1000   	4990808	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					ENGINE	FAILED          	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CL	CLIMB          	1			CA						9284		9284			(CAN) LP 2 COMPRESSOR FAILURE, TEAR-DOWN REPORT TO FOLLOW.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999082700914	19990827	00914	EU  	1999	8	27	CA990728037      	2	19990614	G	7230		BLADE           			FOKKER	F28   	F28MK1000   	4990808	EU  	RROYCE	SPEY  	SPEY55515   	54521	EU  					COMPRESSOR	BROKEN          	W				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			DE	DESCENT        	1			CA						9662		9662			(CAN) FAILURE OF FIRST STAGE COMPRESSOR BLADE, TEAR DOWN REPORT TO FOLLOW.						2	L	7	2 	4F	4	F	RT	A20EU   	E2EU				 
1999082000249	19990820	00249	NM  	1999	8	20	CA990728038      	1	19990615	G	7931	APT761000100DW	TRANSMITTER     			DHAV  	DHC8  	DHC8301     		NM  	PWA   	PW120 	PW123       		NE  					NR 2 ENGINE	MALFUNCTIONED   	W				A				UNSCHED LANDING         				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		CL	CLIMB          	1			CA			17142					123145			(CAN) CREW REPORTED ROUGH RUNNING ENGINE AND THE NR 2 ENGINE OIL PRESSURE WAS DROPPING.  OIL PRESSURE HELD AT 50 PSI, TH	EREFORE, THE ENGINE WAS NOT SHUT DOWN.  INSPECTION VERIFIED PASSENGER TRANSMITTER TO BE FAULTY.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999082000250	19990820	00250	NM  	1999	8	20	CA990728041      	1	19990715	G	5510	35250503	BRACE STRUT     			CHRIS 	HUSKY 	A1          	221020X	NM  	LYC   	O360  	O360C1G     	41514	EA  					LT STABILIZER	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1120 					L3205936A			(CAN) FOUND LOWER END OF FORWARD LEFT TAIL BRACE TUBE BROKEN IN THREADED END FITTING.  SERVICE BULLETIN NOTES A HISTORY 	OF FAILURE TO THE REAR STRUT AND OFFERED TO REPLACE ALL LOWER STRUTS.  ONLY THE REAR STRUTS HAD BEEN CHANGED TO DATE.					1	H	7	1 	3O	3	O	NC	A22NM   	E286				 
1999091700412	19990917	00412	EA  	1999	9	17	CA990728042      	2	19990719	G	8520		CRANKCASE       			PIPER 	PA25  	PA25235     	7102504	SO  	LYC   	O540  	O540B2C5    	41532	EA  					ENGINE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				1429 		L1123440		L1123440			(CAN) WITH THE MAGS REMOVED, MAG DRIVE IDLER WAS FOUND LOOSE.  IT WAS NOTED UPON REMOVAL THAT THE CAST BOSS IN THE AFT E	ND OF THE LEFT CRANKCASE WAS FOUND WORN TO THE POINT THAT THE BEARING FAILED AND WAS MISSING.  SUBMITTER SUGGESTED NOT T	O RUN ENGINE PAST TBO IF ENGINE ON CONDITIONAL MAINTENANCE SCHEDULE.				1	L	7	1 	3O	3	O		2A10    	E295				 
1999082700133	19990827	00133	EA  	1999	8	27	CA990728043      	1	19990621	G	3040		BEARINGS        	MARQUETTE   	149786202   	DHAV  	DHC6  	DHC6300     	2802606	EA  	PWA   	PT6   	PT6A27      	52043	EA  					WINDSHIELD WIPER	UNAPPROVED PART 	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						6993		PCE40782			(CAN) UNIT WAS DISASSEMBLED, IT WAS FOUND THAT THE BEARING INSTALLED WERE NOT OF THE MANUFACTURER'S TYPE.						1	H	7	2 	3T	4	T	RT	A9EA    	E4EA				 
1999082000251	19990820	00251	CE  	1999	8	20	CA990728044      	1	19990429	G	2121	K271B202EL	BEARINGS        	DYNAMICAIR  	C308559A    	BEECH 	99    	99          	1154002	CE  	PWA   	PT6   	PT6A28      		EA  					BLOWER MOTOR	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						273		PCE50392			(CAN) THIS UNIT WAS SENT TO OUR FACILITY FOR OVERHAUL DUE TO A FAILURE OF BEARINGS AND FAN SEPARATION.  IT WAS FOUND THA	T THE BEARINGS INSTALLED IN THE MOTOR  WERE NOT OF THE MANUFACTURER'S TYPE.  THE BEARINGS FOUND IN THE MOTOR WERE FAFNIR	 P/N 202PPCA INSTEAD OF DYNAMIC P/N K271B-202EL.  IT COULD NOT BE DETERMINED IF THE FAN HUB FAILED BEFORE OR AFTER THE B	EARING FAILURE.			1	L	7	2 	3T	4	T		A14CE   	E4EA				 
1999082000252	19990820	00252	SW  	1999	8	20	CA990728045      	1	19990628	G	2435	230321900	SHAFT           	LUCAS       	230790001   	SWRNGN	SA227 	SA227AC     	8780603	SW  						ROTOL	R321	R321482F8   	GL  	START/GEN	MISREPAIRED     	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						3750			DRG234684		(CAN) DURING OVERHAUL AN UNAPPROVED REPAIR WAS DISCOVERED.  DEFECTIVE PARTS REPLACED AND UNIT RETURNED TO SERVICE.						2	L	7	2 	4T			RT	A8SW    		6	C	P61GL	 
1999082000253	19990820	00253	EU  	1999	8	20	CA990728046      	1	19990622	G	2121	K271B200EL	BEARINGS        	DYNAMICAIR  	M4941Z1A    	BAG   	JETSTM	JETSTM3212  	1500217	EU  						ROTOL	R333	R333482F12  	GL  	FAN MOTOR	UNAPPROVED      	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						266			DRG303288		(CAN) UNAPPROVED BEARINGS.						2	L	7	2 	4T			RT	BA15CAA 		6	C	P61GL	 
1999091700413	19990917	00413	SW  	1999	9	17	CA990728047      	1	19990628	G	2435	230321901	DAMPER HUB      	LUCAS       	23081018    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					DRIVE SHAFT	MISREPAIRED     	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						302		CAE860344			(CAN) STARTER/GENERATOR WAS SENT FOR ROUTINE OVERHAUL AND UPON OVERHAUL IT WAS NOTICED THAT IT HAD BEEN PREVIOUSLY ASSEM	BLED WITH A WORN OUT DAMPER HUB AND WAS ALSO MISSING A BRASS SHIM.  HUB WAS SUBSEQUENTLY REPLACED DURING THIS OVERHAUL A	ND RETURNED TO SERVICE.				1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999082000254	19990820	00254	WP  	1999	8	20	CA990728050      	2	19990705	G	7200		ENGINE          			SWRNGN	SA227 	SA227AC     	8780603	SW  	GARRTT	TPE331	TPE33111U   	01514	WP  	ROTOL	R321	R321482F8   	GL  	ENGINE BAY	FAILED          	W				C				ABORTED TAKEOFF         				O			OTHER                     			TO	TAKEOFF        	1			CA								P44248C	DRG234684		(CAN) E.G.T. ERRATIC.  FAULTY CONNECTION ON LEAD FROM TEMP TRANSMITTER.						2	L	7	2 	4T	4	T	RT	A8SW    	E4WE	6	C	P61GL	 
1999090300310	19990903	00310	NM  	1999	9	3	CA990728051      	1	19990708	G	5753	654642821	TRACK           			BOEING	737   	737244      	138448U	NM  	PWA   	JT8   	JT8D9A      	52048	NE  					TE FLAP	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			70563								(CAN) NR 7 FLAP TRACK LUG ON FORWARD ATTACH POINT FOUND BROKEN AT PIVOT BOLT HOLE.  REPLACED.						2	L	7	2 	4F	4	F		A16WE   	E2EA				 
1999082000255	19990820	00255	CE  	1999	8	20	CA990728052      	1	19990709	G	8011	MZB4010R	STARTER         	PRESTOLITE  		CESSNA	182   	TR182       	2072735	CE  	LYC   	O540  	O540L3C5    	41532	EA  	MCAULY	2D34C	B2D34C219   	GL  	ENGINE	FAILED          	W				O				OTHER                   				J			WARNING INDICATION        			TX	TAXI/GRND HDL  	1			CA			3398 	1224 		10K5000001		L2237140A	815040		(CAN) STARTER WOULD ONLY TURN ENGINE OVER AT HALF SPEED.						1	H	7	1 	3O	3	O		3A13    	E295	5	C	P7EA	 
1999090300311	19990903	00311	NM  	1999	9	3	CA990728053      	1	19990715	G	5320		TEAR STRAP      			BOEING	727   	72725       	1384006	NM  	PWA   	JT8   	JT8D7B      	52053	NE  					FUSELAGE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			78620					649100			(CAN) A .315 INCH CRACK FOUND IN THE TEAR STRAP FROM ONE RIVET HOLE.  TEAR STRAP REMOVED AND REPLACED  PER SRM.						2	L	7	3 	4F	4	F		A3WE    	E2EA				 
1999082000256	19990820	00256	NE  	1999	8	20	CA990728054      	2	19990701	G	7300	017407810	DRAIN VALVE     			SNIAS 	350   	AS350B      	8680801	EU  	TMECA 	ARRIEL	ARRIEL1B    	6OO30	NE  					FUEL SYSTEM	LEAKING         	W				A				UNSCHED LANDING         				R	K	J	PARTIAL RPM/PWR LOSS      	FLUID LOSS                	WARNING INDICATION        	AP	APPROACH       	1			CA			2253 					853			(CAN) LOSS OF ENGINE POWER AND ROTOR RPM.  FUEL LEAKING FROM AREA AROUND IGNITION SOLENOID VALVE AND START DRAIN VALVE. 	 IT APPEARS START DRAIN VALVE MAY HAVE BEEN CROSS-THREADED ONTO THE INJECTION PRESSURE SUPPLY T-UNION DURING THE PREVIOU	S INSTALLATION.				1	G	7	1 	3U	3	U		H9EU    	E19EU				 
1999082001008	19990820	01008	GL  	1999	8	20	CA990728055      	2	19990617	G	7200	6875225	ACCUMULATOR     			BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20      	03013	GL  					ENGINE	CRACKED         	W				O				OTHER                   				R			PARTIAL RPM/PWR LOSS      			HO	HOVERING       	1			CA								CAE821394			(CAN) AFTER ENGINE REPLACED, POWER CHECK WAS CARRIED OUT WHERE ENGINE WOULD PRODUCE ONLY 80 PERCENT TORQUE.  INVESTIGATI	ON REVEALED A CRACK IN THE 6 CUBIC INCH ACCUMULATOR IN THE PY LINE.  THE CRACK WAS FOUND IN THE AREA WHERE THE END FITTI	NG FOR THE PY LINE IS WELDED TO THE END OF THE ACCUMULATOR.  THE NEW REPLACEMENT ACCUMULATOR HAD A DOUBLER AT THIS AREA.				1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999082000257	19990820	00257	SO  	1999	8	20	CA990728058      	2	19990704	G	8530	646778	CONNECTING ROD  			CESSNA	310   	310R        	2074245	CE  	CONT  	O520  	IO520M      	17032	SO  	MCAULY	3AF32C	3AF32C87    	GL  	ENGINE	BENT            	W				E				ENGINE SHUTDOWN         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA				3    				270662R	753493		(CAN) NR 5 CYLINDER CONNECTING ROD BENT CAUSING DAMAGE TO NR 5 AND NR 6 CYLINDER, CRANK, AND CAMSHAFTS.						1	L	7	2 	3O	3	O		3A10    	E5CE	5	C	P22EA	 
1999082000258	19990820	00258	CE  	1999	8	20	CA990728059      	1	19990708	G	2910	11458035517	LINE COVER      			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					NLG WW	CRACKED         	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CL	CLIMB          	1			CA			4532 					PCEPS0007			(CAN) AFTER TAKEOFF, A METALLIC BANGING OR RATTLING NOISE WAS HEARD IN COCKPIT AND CABIN.  UPON INSPECTION, IT WAS DISCO	VERED THAT THE HYDRAULIC LINE COVER IN THE NOSE WHEELWELL WAS SEVERELY CRACKED.  THE CRACKS ALLOWED THE PART TO VIBRATE 	AND CAUSE THE NOISE.				2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999082000259	19990820	00259	CE  	1999	8	20	CA990728062      	1	19990706	G	3260	H111541	SWITCH          			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					MLG	DEFECTIVE       	W				O				OTHER                   				N			FALSE WARNING             			CR	CRUISE         	1			CA			1227 					PCEPS0220			(CAN) DURING CRUISE FLIGHT, THE FLIGHT CREW NOTED THE INTRANSIT RED LIGHT ILLUMINATE.  MAINTENANCE FOUND THE LT UPLOCK S	WITCH DEFECTIVE.					2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999082000260	19990820	00260	CE  	1999	8	20	CA990728063      	1	19990720	G	2435	23078019	BEARING         			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					START/GEN	FAILED          	W				D				RETURN TO BLOCK         				B			SMOKE/FUMES/ODORS/SPARKS  			TX	TAXI/GRND HDL  	1			CA				237  				PCEPS0231			(CAN) CREW REPORTED PREVIOUS PROBLEMS WITH GENERATOR STAYING ON-LINE.  DURING TAXI TO HANGAR, AREA SMOKE WAS OBSERVED FR	OM ENGINE COMPARTMENT.  STARTER WAS REMOVED AND REPLACED DUE TO REAR BEARING FAILURE.					2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999082000261	19990820	00261	NE  	1999	8	20	CA990728064      	2	19990623	G	8530		CYLINDER        			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					ENGINE	SEPARATED       	W				C				ABORTED TAKEOFF         				E			VIBRATION/BUFFET          			TO	TAKEOFF        	1			CA				490  				274956			(CAN) NR 6 CYLINDER SEPARATION AT CYLINDER HEAD AND BARREL.  CYLINDER REPLACED.						1	H	7	1 	3R	3	R		A806    	5E1				 
1999082000262	19990820	00262	EU  	1999	8	20	CA990728065      	1	19990705	G	2752	951D1009	ACTUATOR        			PILATS	PC12  	PC12        	7090550	EU  										TE FLAP	MALFUNCTIONED   	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			TO	TAKEOFF        	1			CA			883  			0800A					(CAN) FLAP CAUTION AND PUSHER WARNING LIGHTS CAME ON WHEN FLAPS SELECTED UP.  FLAP ACTUATOR SQUEELING AND GRINDING DURIN	G OPERATION.  FLAP ACTUATOR HAD EXESSIVE PLAY, PARTS REPLACED.					1	L	7	1 	3T			RT	A78EU   					 
1999082700135	19990827	00135	NE  	1999	8	27	CA990728068      	2	19990712	G	7414		SCREW           	BOSCH       	SB9RU3      	DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  	HAMSTD	22D	22D30       	NE  	MAGNETO	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				1343 		B04715		21700	E3095		(CAN) SCREW SECURING ROTOR ASSY TO DISTRIBUTOR DRIVE GEAR FELL OUT BECOMING ENTANGLED IN GEAR TEETH ON DRIVE GEAR (FIBER	), ALL WERE BROKEN OFF.  ROTOR FELL DOWN JAMMING THE COIL AND CASE.  THIS IS THE SECOND TIME THIS HAS OCCURRED.  PREVIOU	SLY, LOOSE SCREWS WERE FOUND DURING INSPECTION.				1	H	7	1 	3R	3	R		A806    	5E1	5	C	P736	 
1999082000263	19990820	00263	EA  	1999	8	20	CA990728069      	2	19990712	G	8540		PUMP            			CESSNA	172   	172M        	2072418	CE  	LYC   	O320  	O320E2D     	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	ENGINE OIL	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2185 					L3482827A	722151		(CAN) AD 96-09-10C FOUND NOT EMBODIED ON AIRCRAFT.  OIL PUMP EMANENT FAILURE WAS TO RESULT.						1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
1999082000264	19990820	00264	EU  	1999	8	20	CA990728070      	1	19990715	G	2497		WIRE            		9598110107  	PILATS	PC12  	PC12        	7090550	EU  										ELECTRICAL SYS	MELTED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			711  								(CAN) AD 99-347 CARRIED OUT ON HEATED WINDSHIELD, POSITIVE WIRING FAULTS FOUND ON TWO AIRCRAFT.						1	L	7	1 	3T			RT	A78EU   					 
1999082700136	19990827	00136	EA  	1999	8	27	CA990728071      	2	19990712	G	7421	AGF26	GLOW PLUG       			DHAV  	DHC6  	DHC6300     	2802606	EA  	PWA   	PT6   	PT6A27      	52043	EA  					LT ENGINE	FAILED          	W				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			CA			100  					PCE40357			(CAN) DURING GLOW PLUG ROUTINE TEST, THE INBOARD PLUG WAS FOUND TO BE DEAD.  SUBMITTER STATED THIS IS THE 4TH PLUG FROM 	BATCH 3B98 THAT HAS FAILED ALL WITH ONLY 100 HOURS.					1	H	7	2 	3T	4	T	RT	A9EA    	E4EA				 
1999082000265	19990820	00265		1999	8	20	CA990728073      	4	19990716	G	3460	LA2E006091K0000	FLT COMPUTER    			AIRBUS	330   	A330322     	3930325	EU  										COCKPIT	MALFUNCTIONED   	W				A				UNSCHED LANDING         				N			FALSE WARNING             			CL	CLIMB          	1			CA			533  			2E0000862					(CAN) DURING CLIMB, FLAPS AND SLATS SELECTED TO ZERO DEGREE POSITION, POSITION FAULT INDICATED ON ECAM.  FLIGHT WARNING 	COMPUTER REPLACED, FAULT FIXED.					2	L	7	2 	4F			RT	A46NM   					 
1999082000266	19990820	00266	NE  	1999	8	20	CA990728074      	3	19990714	G	6111	6101A18	BLADE           													HAMSTD	2D	2D30        	NE  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				100  					N110784		(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION, FOUND CORROSION ON BLADE.																5	C	P206	 
1999082000267	19990820	00267	EA  	1999	8	20	CA990728077      	2	19990721	G	8530	C5263	CYLINDER        			CESSNA	172   	172RG       	2072438	CE  	LYC   	O360  	O360F1A6    	41514	EA  	MCAULY	2D34C	B2D34C220   	GL  	ENGINE	SCORED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L2930536A	860511		(CAN) OIL PASSING CYLINDER, AND ESCAPING THROUGH HUB BREATHER ROLL PINS.						1	H	7	1 	3O	3	O		3A17    	E286	5	C	P7EA	 
1999082000268	19990820	00268	SO  	1999	8	20	CA990728079      	2	19990718	G	8530		CONNECTING ROD  			CESSNA	185   	A185F       	2072821	CE  	CONT  	O520  	IO520D      	17032	SO  					ENGINE	FAILED          	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA				45   				559779			(CAN) NR 1 CONNECTING ROD FAILURE, ENGINE DAMAGE SEVERE.  FURTHER INVESTIGATION AT TEAR-DOWN.						1	H	7	1 	3O	3	O		3A24    	E5CE				 
1999082000270	19990820	00270		1999	8	20	CA990728081      	1	19990721	G	7830	74M200049	BLOCKER DOOR    								PWA   	4168  	PW4168      		NE  					NR 2 ENGINE	DETACHED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			14442					733336			(CAN) DURING DAILY INSPECTION, NR 2 ENGINE BLOCKER DOOR WAS FOUND TO BE HANGING DOWN IN THE FAN BYPASS DUCT.  INVESTIGAT	ION REVEALED A STRUCTURAL FAILURE OF UNKNOWN ORIGIN.  BLOCKER DOOR SENT TO MANUFACTURER FOR ANALYSIS.										4	F			E36NE				 
1999082000274	19990820	00274	EA  	1999	8	20	CA990728087      	2	19990621	G	8530	LW11633	CYLINDER        			CESSNA	150   	152         	2071835	CE  	LYC   	O235  	O235L2C     	41505	EA  					ENGINE	DAMAGED         	W				A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	TO	TAKEOFF        	1			CA				703  				L1918915			(CAN) LOSS OF ENGINE POWER.  VALVE PISTON AND CYLINDER DAMAGE FOUND AT INITIAL INSPECTION, SENT FOR TEARDOWN.						1	H	7	1 	3O	3	O	NT	3A19    	E223				 
1999082000275	19990820	00275	EA  	1999	8	20	CA990728088      	2	19990711	G	8530	75670	CRANKSHAFT      								LYC   	O541  	TIGO541E1A  	41539	EA  					CRANKCASE	SEPARATED       	W				B				EMER. DESCENT           				E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA			25   					L54246			(CAN) CRANKSHAFT AT CONNECTING ROD DAMAGED 25 HOURS POST-OVERHAUL.  X-RAYS WERE TAKEN AT THAT TIME.											3	O			E19EA				 
1999082000276	19990820	00276	GL  	1999	8	20	CA990728089      	2	19990711	G	7260	1347M32G08	CARBON SEAL     								GE    	CF6   	CF680C2*    		GL  					ENGINE	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA								695146			(CAN) OIL QUANTITY AND PRESSURE INDICATION DROPPING WHILE IN-FLIGHT.  CARBON SEAL REPLACED PER M.M.M.E.C.  HAD BEEN REPL	ACED PRIOR TO FLIGHT FOR FUEL LEAK FROM DRAIN MASTER.										4	F			E23EA				 
1999082000277	19990820	00277	SO  	1999	8	20	CA990728091      	1	19990713	G	5610	41543	WINDSHILD       	PPG         	41543       	PIPER 	PA31  	PA31350     	7103110	SO  										COCKPIT	DELAMINATED     	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			11845			6H44162					(CAN) HEATED WINDSHIELD DELAMINATED BEYOND PPG INDUSTRIES PUBLISHED LIMITATIONS.  1.  MORE THAN 2 INCHES FROM CORNER.  2	.  DISTORTING PILOT'S VISIBILITY.  CAUSES:  1.  OVERHEATING BY AIRCRAFT REGULAR DEFROSTER WHEN WINDSHIELD HEAT IS ON. 2.	  WATER INFILTRATION THROUGH FAILED SEALS AND THROUGH RETAINING SCREW HEADS NOT PROPERLY SEALED.   REF:  MOT LETTER OF N	OTIFICATION 24-0019 8 JULY/99.			1	L	7	2 	3O				A20SO   					 
1999082000278	19990820	00278	EA  	1999	8	20	CA990728092      	2	19990722	G	7322	HA61060301	CARBURETOR      								LYC   	O360  	HO360C1A    	41514	EA  					ENGINE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2091 	91   				L3490836A			(CAN) PRECISION HA-6-10-60301. CARBURETOR FAILURE, INTERNAL.											3	O			E286				 
1999082000279	19990820	00279	SO  	1999	8	20	CA990728093      	2	19990721	G	8520	642131	CRANKCASE       			CESSNA	404   	404CESSNA   	2075901	CE  	CONT  	O520  	GTSIO520M   	17032	SO  	MCAULY	3FF32	3FF32C501   	GL  	ENGINE	CRACKED         	W				D				RETURN TO BLOCK         				K			FLUID LOSS                			TX	TAXI/GRND HDL  	1			CA			899  					292315R	951208		(CAN) CRACK FOUND AT NR 5 CYLINDER CRANKCASE THREAD BORE, .750 INCH, RADIATING TO OUTER CASE.						1	L	7	2 	3O	3	O		A25CE   	E7CE	5	C	P45GL	 
1999082000280	19990820	00280	NE  	1999	8	20	CA990728094      	2	19990521	G	8500		ENGINE          			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					ENGINE BAY	FAILED          	W				O				OTHER                   				Y			ENGINE STOPPAGE           			NR	NOT REPORTED   	1			CA				498  				17184			(CAN) COMPLETE ENGINE FAILURE AND ENGINE WAS NOT REPAIRABLE, ENGINE INSTALLED MAY 1995.						1	H	7	1 	3R	3	R		A806    	5E1				 
1999082000281	19990820	00281	SO  	1999	8	20	CA990728098      	1	19990714	G	2434	4111810	ALTERNATOR      	CHRYSLER    	4111810     	PIPER 	PA28  	PA28161     	7102803	SO  	LYC   	O320  	O320D3G     	41508	EA  					ENGINE	FAILED          	W				H				DEACTIVATE SYST/CIRCUITS				H	J		ELECT. POWER LOSS-50 PC   	WARNING INDICATION        		CR	CRUISE         	1			CA						A39558		L803139A			(CAN) REPEATED TRIPPING OF ALTERNATOR FIELD CIRCUIT BREAKER.  ALTERNATOR NOT PROVIDING FULL AMPERAGE.  ALTERNATOR REPLAC	ED.					1	L	7	1 	3O	3	O		2A13    	E274				 
1999082000282	19990820	00282	SO  	1999	8	20	CA990728099      	1	19990714	G	5521	4374300	GUSSET          		5423224     	PIPER 	PA31  	PA31350     	7103110	SO  										ELEVATOR	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			11845								(CAN) DEFECT WAS FOUND DURING CARRYING OUT INSPECTION OF AREA WITH BORESCOPE PER S/B 998A VIA INSPECTION HOLE.  NO OTHER	 DEFECT, CRACK, ETC.  IT APPEARS FAULTY RIVET WAS NOT BUCKED TIGHT ENOUGH AT A PREVIOUS MODIFICATION INSTALLATION AND FR	ETTED LOOSE.  NEW RIVET INSTALLED.  NOTE:  S/B 998A NOW SUPPORTED BY A/D 99-12-05 WHICH BECOMES EFFECTIVE NEXT 23 JULY/9	9 PERSUING REPETITIVE 100 HR INSPECTION, BUT ADDED 1000 HRS LIFE TO ELEVATORS OR IF CRACKS FOUND IN ELEVATOR.			1	L	7	2 	3O				A20SO   					 
1999082000283	19990820	00283		1999	8	20	CA990729001      	4	19990615	G	2565		ESCAPE SLIDE    			AIRBUS	310   	A310304     		EU  										PAX DOOR	FAILED          	W				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			CA											(CAN) ESCAPE SLIDE FAILED TO DEPLOY DURING TEST DUE TO JAMMING OF THE RELEASE LEVER ON THE EMERGENCY OPERATING CLYINDER.	  PERCUSSION MECHANISM INSPECTED AND TESTED PER MM.					2	L	7	2 	4F			RT	A35EU   					 
1999082000284	19990820	00284	EU  	1999	8	20	CA990729002      	1	19990702	G	2844	215N04223	SWITCH          			AIRBUS	310   	A310304     		EU  										FUEL SYSTEM	FAILED          	W				C				ABORTED TAKEOFF         				J			WARNING INDICATION        			TO	TAKEOFF        	1			CA						CEC47768					(CAN) NR 2 FUEL CLOG WARNING, DIFFERENTIAL PRESSURE SWITCH REPLACED.						2	L	7	2 	4F			RT	A35EU   					 
1999082000285	19990820	00285	SO  	1999	8	20	CA990729004      	1	19990712	G	8120	LW12463	BEARING         			PIPER 	PA31  	PA31350     	7103110	SO  	LYC   	O540  	TIO540J2BD  	41532	EA  					TURBOCHARGER	FAILED          	W				A	E			UNSCHED LANDING         	ENGINE SHUTDOWN         			B	R		SMOKE/FUMES/ODORS/SPARKS  	PARTIAL RPM/PWR LOSS      		CL	CLIMB          	1			CA				1    		Y1010262		L254161A			(CAN) TURBINE BEARING FAILURE.  TURBINE SIDE WEARING ON TURBO CASE.						1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999082000287	19990820	00287		1999	8	20	CA990729006      	4	19990624	G	2312	ARC300	TRANSISTOR      			CESSNA	172   	172M        	2072418	CE  										VHF COMM	MELTED          	W				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			CL	CLIMB          	1			CA											(CAN) TRANSISTOR IN NAVCOM UNIT MELTED.						1	H	7	1 	3O			NT	3A12    					 
1999082000288	19990820	00288	SO  	1999	8	20	CA990729007      	2	19990729	G	7414	36066	GEAR            			CESSNA	150   	150J        	2071820	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A101	1A101DCM    	GL  	MAGNETO	SPALLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			3310 					1992879A	65358		(CAN) MAGNETO GEARS WHICH ARE SUSPECTED TO BE UNAPPROVED PARTS.  ONT. SAIB NR CE-98-21R1 WAS RELEASED TO CORRECTLY IDENT	IFY THE GEARS IN THE FIELD.					1	H	7	1 	3O	3	O		3A19    	E252	5	N	P918	 
1999082000289	19990820	00289	NE  	1999	8	20	CA990729008      	2	19990621	G	7261	310137101	BEARING         								PWA   	118   	PW118       		NE  					ENGINE	SPALLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								115498			(CAN) METAL CONTAMINATION OF TURBOMACHINE FROM OIL PUMP DRIVE BEARING SPALLING.											4	T			E20NE				 
1999082000290	19990820	00290	NE  	1999	8	20	CA990729009      	2	19990714	G	7230	210703301	BEARING         								PWA   	120   	PW120       		NE  					ENGINE	SPALLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								121281			(CAN) REF. 99-067.  METAL CONTAMINATION.											4	T			E20NE				 
1999082000291	19990820	00291	GL  	1999	8	20	CA990804002      	2	19990716	G	7250	689633	WHEEL           			SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					TURBINE SECTION	CRACKED         	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			NR	NOT REPORTED   	1			CA			1872 			HX69673		CAE890359S			(CAN) HAIR LINE CRACKS DETECTED DURING NDT OF THE WHEEL AT REPAIR /OVERHAUL FACILITY (ACRO AEROSPACE).						1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999090300316	19990903	00316	EA  	1999	9	3	CA990804008      	2	19990730	G	8500		ENGINE          			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320D2J     	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	FORWARD	MAKING METAL    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L1173939	733708		(CAN) ENGINE MAKING METAL, OIL PRESSURE VARIED WITH THROTTLE MOVEMENT.						1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
1999090300317	19990903	00317	SO  	1999	9	3	CA990804009      	1	19990714	G	7713	4709129001R	CONTROLLER      			PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2C   	41532	EA  					ENGINE	STUCK OPEN      	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			225  					L221961A			(CAN) MANIFOLD PRESSURE LOST, PILOT RETARDED THROTTLE TO IDLE THEN RESET THROTTLE POWER.  THE PROBLEM WENT AWAY.  DIFFER	ENTIAL CONTROLLER CHANGED, SUSPECTED DEBRIS IN VALVE PORT IN CONTROLLER.					1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999090300318	19990903	00318	WP  	1999	9	3	CA990804010      	1	19990721	G	2497		WIRE            			DOUG  	B26   	B26B        	3020514	WP  	PWA   	R2800 	R280079     	52026	NE  					COCKPIT	SHORTED         	W				H	C			DEACTIVATE SYST/CIRCUITS	ABORTED TAKEOFF         			B			SMOKE/FUMES/ODORS/SPARKS  			TO	TAKEOFF        	1			CA								FP043584			(CAN) ON TAKEOFF, PILOT NOTICED SPARKS COMING FROM LOWER INSTRUMENT PANEL.  MASTER SWITCH TURNED OFF, TAKEOFF ABORTED, W	IRES REPAIRED.					2	M	7	2 	4R	4	R	 	L34     	5E8				 
1999082000292	19990820	00292	SO  	1999	8	20	CA990804012      	2	19990722	G	8520	635104	CRANKSHAFT      			CESSNA	404   	404CESSNA   	2075901	CE  	CONT  	O520  	GTSIO520M   	17032	SO  	MCAULY	3FF32	3FF32C501   	GL  	ENGINE	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			444  			B239803N		276450R	803645		(CAN) AN INSPECTION REQUIRED BY CSB99-6 ON GTSIO-520-M ENGINES WAS PERFORMED AND THIS INSPECTION REVEALED A STRESS RISER	 CONDITION CAUSED BY A DISCREPANCY IN THE COUNTERWEIGHT BUSHING INSTALLATION PROCESS.  THE ENGINE WAS REMOVED FOR FURTHE	R  INSPECTION AND REPAIR.  REVISION TO AD 99-09-17 WILL BE MADE TO INCORPORATE THE ADDITIONAL MODEL TYPE GTSIO-520-M ENG	.			1	L	7	2 	3O	3	O		A25CE   	E7CE	5	C	P45GL	 
1999090300320	19990903	00320	CE  	1999	9	3	CA990804013      	1	19990629	G	2434	P17A18	WIRE            	LAMAR       	B002963     	CESSNA	414   	414A        	2075907	CE  	CONT  	O520  	TSIO520NB   	17040	SO  					ALTERNATOR	SHORTED         	W				A				UNSCHED LANDING         				B	J		SMOKE/FUMES/ODORS/SPARKS  	WARNING INDICATION        		CR	CRUISE         	1			CA			3567 			14531		521294			(CAN) ALTERNATOR FIELD WIRE AND VOLTAGE REGULATOR SHORTED, LEFT SYSTEM.						1	L	7	2 	3O	3	O	 	A7CE    	E8CE				 
1999082000293	19990820	00293	CE  	1999	8	20	CA990804033      	1	19990715	G	5741	16911000324	SPAR            			BEECH 	23    	A24R        	1151252	CE  	LYC   	O360  	IO360A1B    	41514	EA  	MCAULY	2D34C	2D34C9      	GL  	WING	HOLE OVERSIZED  	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2371 					L685851F	694582		(CAN) WASHERS ARE REQUIRED BETWEEN BUSHING AND FUSELAGE ATTACH FITTING TO HOLD BUSHING IN PLACE.  THESE WASHERS WERE MIS	SING AND ALLOWED THE BUSHING TO MOVE FORWARD.  THERE WAS NOT ENOUGH BEARING SURFACE AVAILABLE, SO THE BUSHING MOVED ENLA	RGING THE HOLE IN THE SPAR AND FILLER.  CRACKS RESULTED RADIATING FROM THE HOLE AND ALLOWING THE BOLT TO DAMAGE THE ASSO	CIATED FILLER.  REPAIR APPROVAL (0-RA99-103 )RECEIVED JULY 19,1999.			1	L	7	1 	3O	3	O		A1CE    	1E10	5	C	P7EA	 
1999082000294	19990820	00294	CE  	1999	8	20	CA990804034      	1	19990720	G	5741	16911000324	SPAR            			BEECH 	23    	A24R        	1151252	CE  	LYC   	O360  	IO360A1B    	41514	EA  	MCAULY	2D34C	2D34C9      	GL  	WING	HOLE OVERSIZED  	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2269 					L745251A	704567		(CAN) REQUIRED WASHERS NOT INSTALLED BETWEEN BUSHING AND FUSELAGE FITTING.  THIS ALLOWED BUSHING TO MOVE FORWARD.  BECAU	SE THERE WAS NOT ENOUGH BEARING SURFACE, THIS ALLOWED BUSHING TO ENLARGE HOLE IN SPAR AND FILLER CAUSING CRACKS TO RADIA	TE FROM HOLE AND ALLOWING THE BOLT TO DAMAGE THE ASSOCIATED FILLER.  REPAIR APPROVAL 0-RA99-103 RECEIVED JULY 19,1999.				1	L	7	1 	3O	3	O		A1CE    	1E10	5	C	P7EA	 
1999082700152	19990827	00152	EA  	1999	8	27	CA990804036      	1	19990803	G	2752	C2CF341A	ROD             			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					TE FLAP	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								8730			(CAN) DURING INSPECTION, THE RIGHT FLAP ROD ENDS WERE FOUND WORN.  DURING REPLACEMENT, THE TREADS ON THE ROD SNAPPED.  F	URTHER INVESTIGATION REVEALED THEY WERE PARTIALLY CRACKED BEFORE REMOVAL OF THE ROD END.					1	H	7	1 	3R	3	R		A806    	5E1				 
1999082700153	19990827	00153	EA  	1999	8	27	CA990804037      	1	19990803	G	5750	C2W61A	SPAR            		C2W1045A    	DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					TE FLAP	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								8730			(CAN) 2 LENGTHWISE CRACKS ON UPPER RADIUS OF THE REAR SPAR AT THE OUTBOARD FLAP ATTACHMENT BRACKET ON THE LEFT WING.   R	EPAIR SCHEME REQUESTED.					1	H	7	1 	3R	3	R		A806    	5E1				 
1999082700154	19990827	00154	EA  	1999	8	27	CA990804039      	1	19990723	G	3246	2158750224	TIRE            	BFGOODRICH  		CNDAIR	CL215 	CL2156B11415		EA  										MLG	BLOWN           	W				O				OTHER                   				O			OTHER                     			LD	LANDING        	1			CA			599  			1024					(CAN) AIRCRAFT LANDED WITH LEFT BRAKE LOCKED.   AN OVERHEATED BRAKE ORIGINATED THE PROBLEM.						2	H	7	2 	4T			RT	A14EA   					 
1999090300323	19990903	00323	CE  	1999	9	3	CA990804040      	1	19990730	G	7430	C2925010102	SWITCH          			CESSNA	206   	P206        	2073304	CE  	CONT  	O520  	IO520F      	17032	SO  					IGNITION SYSTEM	SHORTED         	W				E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			W	J		INADEQUATE Q C            	WARNING INDICATION        		CR	CRUISE         	1			CA			5006 								(CAN) AD 93-05-06 WAS NOT COMPLIED WITH PRIOR TO IMPORTATION, THE IGNITION SWITCH SHORTED AT ALTITUDE CAUSING ENGINE TO 	FAIL.  RESTART WAS SUCCESSFUL.  SWITCH REPLACED.					1	H	7	1 	3O	3	O		A4CE    	E5CE				 
1999090300326	19990903	00326	EA  	1999	9	3	CA990812003      	2	19990804	G	7414	ES10382807	CAPACITOR       			BEECH 	76    	76          	1153005	CE  	LYC   	O360  	O360A1G     	41514	EA  					MAGNETO	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			700  					L2645836A			(CAN) MAGNETO CAPACITOR FAILED CAUSING EXCESSIVE MAGNETO DROP WHEN TESTED.						1	L	7	2 	3O	3	O		A29CE   	E286				 
1999090300327	19990903	00327	EA  	1999	9	3	CA990812005      	2	19990802	G	7414	10382585	POINTS          			CESSNA	177   	177B        	2073708	CE  	LYC   	O360  	O360A1F6    	41514	EA  					MAGNETO	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			237  					L2245036A			(CAN) ACCELERATED WEAR OF POINTS IN MAGNETO SUSPECTED BY OPERATOR.						1	H	7	1 	3O	3	O		A13CE   	E286				 
1999082700155	19990827	00155	EA  	1999	8	27	CA990812007      	2	19990727	G	7414	67542	BEARING         		LW19096     	ROBSIN	R44   	R44         	7640120	WP  	LYC   	O540  	O540F1B5    	41532	EA  					MAGNETO	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1028 					L2479140A			(CAN) MAGNETO BEARING DESINTEGRATION.  SEE ALSO OPERATOR CONTROL NR 981109044.						1	G	7	1 	3O	3	O		H11NM   	E295				 
1999090300328	19990903	00328		1999	9	3	CA990812008      	1	19990505	G	7810	311178001	DUCT            								PWA   	PT6   	PT6A27      	52043	EA  					EXHAUST	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				4596 				40782100			(CAN) EXHAUST DUCT WAS NOTED TO HAVE A NUMBER OF CRACK INDICATIONS IN AND AROUND THE SEAM WELD AREA THAT ATTACHES THE PO	ST P&W SB1430 INNER CONNECTION TO THE OUTER SKIN OF THE EXHAUST DUCT.  CRACK INDICATIONS ARE LOCATED AROUND ENTIRE CIRCU	MFERENCE.									4	T			E4EA				 
1999090300329	19990903	00329		1999	9	3	CA990812009      	1	19990706	G	7810	311178001	DUCT            								PWA   	PT6   	PT6A21      	52043	EA  					EXHAUST	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			7842 	4041 				PCE24685			(CAN) EXHAUST DUCT WAS NOTED TO HAVE A NUMBER OF CRACK INDICATIONS IN AND AROUND THE SEAM WELD AREA THAT ATTACHES THE PO	ST P&W SB1430 INNER CONNECTION TO THE OUTER SKIN OF THE EXHAUST DUCT.  CRACK INDICATIONS ARE LOCATED AROUND ENTIRE CIRCU	MFERENCE.									4	T			E4EA				 
1999090300330	19990903	00330	EA  	1999	9	3	CA990812012      	2	19990801	G	7230	311176401	BOLT            			EMB   	110   	EMB110P1    	3260122	SO  	PWA   	PT6   	PT6A34      	52043	EA  					COMPRESSOR	STRIPED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				170  				PCE56491			(CAN) REMOVAL OF CT BOLT AT FIRST HSI DIFFICULT TO REMOVE.  THREADS PULLED FROM END OF BOLT, WHICH WAS A POST SB 1439R2 	BOLT.					1	L	7	2 	4T	4	T		A21SO   	E4EA				 
1999082700157	19990827	00157	CE  	1999	8	27	CA990812017      	1	19990707	G	3233	508102443	HOUSING         		50820208    	BEECH 	200   	200BEECH    	1152920	CE  										MLG ACTUATOR	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1309 			C22039					(CAN) WHEN ACTUATOR WAS STRIPPED FOR OVERHAUL INSPECTION, WATER WAS FOUND INSIDE THE HOUSING ALONG WITH THE NORMAL AMOUN	T OF GREASE.  THE HOUSING AND COVER PLATE ARE MANUFACTURED FROM MAGNESIUM AND HAD MAJOR CORROSION.  HOUSING P/N 50810244	3, COVER P/N 50820208.				1	L	7	2 	4T				A24CE   					 
1999082700159	19990827	00159	EU  	1999	8	27	CA990812020      	1	19990811	G	2400	AZS5	CIRCUIT BREAKER 			ZLIN  	242   	Z242L       	9970204	EU  										COCKPIT	FAILED          	W				K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			CA			2969 								(CAN) AS PART OF A SPECIAL INSPECTION OF AIRCRAFT WIRING AND PROTECTIVE DEVICES, FOUND THAT 2 CIRCUIT BREAKERS FAILED TO	 PERFORM INTENDED FUNCTION.  CIRCUIT BREAKERS TESTED FROM 2 TO 5 TIMES.  RATED CURRENT (10-25 AMPS) AND WOULD NOT OPEN U	P AT ALL.  EACH CIRCUIT BREAKER RAN AT 5 TIMES OVERLOAD FOR APPROX 5 HRS.  CB'S APPEAR TO BE NON-MIL SPEC; HOWEVER, REMA	INING 12 CB'S (VARIOUS CURRENT RATINGS) PERFORMED INTENDED FUNCTION.  ALL CB'S TO BE REPLACED BY MS24508-B-(X) MIL SPEC 	CIRCUIT BREAKERS.		1	L	7	1 	3O			0	A76EU   					 
1999090200003	19990902	00003	GL  	1999	9	2	CA990812022      	3	19990709	G	6114	D4716	HUB             													MCAULY	2A34C	D2A34C58    	GL  	PROPELLER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1513 	553  					777568		(CAN)  PROPELLER HUB CRACKED.																5	C	P3EA	 
1999082700160	19990827	00160	GL  	1999	8	27	CA990812023      	3	19990729	G	6110		CYLINDER        		D2A34C67    											MCAULY	2A34C	D2A34C67    	GL  	PROP HUB	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			962  	183  		732984			732984		(CAN) SLOW TO CHANGE PITCH, HUB FOUND FULL OF OIL DUE TO LEAK PASSING CYLINDER.																5	C	P3EA	 
1999082700166	19990827	00166	EA  	1999	8	27	CA990812039      	1	19990809	G	7830	1267587	THRUST REVERSER 	GE          	CF343A      	CNDAIR	CL600 	CL6002B19   		EA  	GE    	CF34  	CF343A      	30015	NE  					NR 1	OUT OF RIG      	W				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			CA											(CAN) LEFT T/R UNLOCK LIGHT ILLUMINATED IN-FLIGHT, SYSTEM DE-ACTIVATED.  PDU RE-RIGGED.  NEXT DAY, THE UNLOCKED ON PEDES	TAL, N1 AND UNSAFE MESSAGE ON EICAS.  T/R DE- ACTIVATED AGAIN.					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999090300335	19990903	00335	GL  	1999	9	3	CA990812040      	3	19990812	G	6111	G90DCA2	BLADE           	MCAULY      	2A34C203B   											MCAULY	2A34C	2A34C203    	GL  	PROPELLER	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			152  			951195			951195		(CAN) BLADE SHANKS FOUND CORRODED BEYOND LIMITS.																5	C	P3EA	 
1999090300336	19990903	00336	GL  	1999	9	3	CA990812041      	3	19990729	G	6111	C3903	RETAINER        	MCAULY      	2A34C203    											MCAULY	2A34C	2A34C203    	GL  	PROP BLADE	SCRAP           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				387  		754122			754122		(CAN) CRACK FOUND IN RADIUS FILLET.																5	C	P3EA	 
1999091700416	19990917	00416	NE  	1999	9	17	CA990812042      	2	19990727	G	7322	39145217CL	CARBURETOR      	BENDIX      		CNDAIR	CL215 	CL2151A10   		EA  	PWA   	R2800 	CA3         	52026	NE  					ENGINE	FAILED          	W				F				ACTIVATE FIRE EXT.      				A			FLAME/FIRE                			NR	NOT REPORTED   	1			CA				52   		799490		P30863			(CAN) AN ENGINE COWL FIRE WAS CAUSED BY THE FAILURE OF A SECTION OF THE ACCELERATION PUMP NR 396653.						2	H	7	2 	4R	4	R		A14EA   	E231				 
1999082700930	19990827	00930	NE  	1999	8	27	CA990817012      	2	19990810	G	7321	7863916	HMU             			DHAV  	DHC8  	DHC8102     	2809003	NM  	PWA   	120   	PW120A      		NE  					ENGINE	MALFUNCTIONED   	W				H				DEACTIVATE SYST/CIRCUITS				N			FALSE WARNING             			CR	CRUISE         	1			CA			2881 					121158			(CAN) 10 PERCENT TORQUE FLUCTUATIONS EXPERIENCED IN CRUISE FLIGHT.  ENGINE ELECTRONIC CONTROL TO MANUAL STABILIZED THE E	NGINE.   INSPECTION AND DIAGNOSTIC TESTING RESULTED IN HMU REPLACEMENT.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999082700167	19990827	00167	NE  	1999	8	27	CA990817021      	3	19990810	G	6111	6915A7	BLADE           			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  	HAMSTD	2D	2D30        	NE  	PROPELLER	WRONG PART      	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						N634512		4222788	D4038		(CAN) NON-APPROVED PARTS (BLADES) IN ASSY.						1	H	7	1 	3R	3	R		A806    	5E1	5	C	P206	 
1999082700935	19990827	00935	NE  	1999	8	27	CA990817024      	2	19990720	G	8530		EXHAUST VALVE   			DHAV  	DHC3  	DHC3        	2800202	EA  	PWA   	R1340 	R134059     	52016	NE  					NR 3 CYLINDER	LOOSE           	W				C				ABORTED TAKEOFF         				E			VIBRATION/BUFFET          			TO	TAKEOFF        	1			CA			213  					ZP100565			(CAN) EXHAUST VALVE LET LOOSE IN  NR 3 CYLINDER, SENT FOR O/H.						1	H	7	1 	3R	3	R		A815    	5E2				 
1999082700936	19990827	00936	SO  	1999	8	27	CA990817026      	2	19990810	G	8530	649163A5	CYLINDER HEAD   			CESSNA	182   	182P        	2075816	CE  	CONT  	O470  	O470S       	17026	SO  	MCAULY	2A34C	2A34C203    	GL  	NR 4	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								463637	750392		(CAN) NR 4 CYLINDER FOUND CRACKED AT THE CYLINDER HEAD SPARK PLUG BOSS.						1	H	7	1 	3O	3	O	NT	TA13    	E273	5	C	P3EA	 
1999082700937	19990827	00937	CE  	1999	8	27	CA990817027      	1	19990810	G	3222	SK18234C	FORK            			CESSNA	182   	182P        	2075816	CE  	CONT  	O470  	O470S       	17026	SO  	MCAULY	2A34C	2A34C203    	GL  	NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								463637	750392		(CAN) CRACK FOUND ON THE NOSE LANDING GEAR UPPER FORK INNER CORNER.  REPLACED.						1	H	7	1 	3O	3	O	NT	TA13    	E273	5	C	P3EA	 
1999101300023	19991013	00023	EU  	1999	10	13	CA990817028      	1	19990514	G	6320	4638302023	BEARING         	ZENITH      	4638001001  	BOLKMS	105   	BO105CBS    	5626008	EU  	ALLSN 	250C  	250C20B     	03013	GL  					M/R GEARBOX	PEELING         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1255 			1122		CAE834907			(CAN) QUANTITY OF 3 BALLS IN SUBJECT BEARING WERE PEELING.						1	G	7	2 	3U	3	U	NC	H3EU    	E4CE				 
1999082700938	19990827	00938	CE  	1999	8	27	CA990817029      	1	19990729	G	2434	PN00315	ALTERNATOR      			CESSNA	180   	180H        	2072618	CE  	CONT  	O470  	O470R       	17026	SO  	MCAULY	2A34C	2A34C66     	GL  	ENGINE	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				450  				49041R	746179		(CAN) ALTERNATOR REAR BEARING FAILURE.  SYSTEM NOT CHARGING.						1	H	7	1 	3O	3	O		5A6     	E273	5	C	P3EA	 
1999082700168	19990827	00168		1999	8	27	CA990817040      	4	19990810	G	3120		WIRE            			MORAVN	Z142  	Z142        		EU  										COCKPIT	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			855  								(CAN) DUE TO A RECENT SHORTING AND MELTING OF THE CLOCK WIRE IN A LIKE PRODUCTION AIRCRAFT.  THE CLOCK WIRE WAS INSPECTE	D FOR THE PRESENCE OF A CIRCUIT PROTECTIVE DEVICE AND NONE WAS FOUND LEAVING THE CLOCK WIRE HOT FROM THE BATTERY SWITCH 	AND ULTIMATELY THE BATTERY.  AN IN-LINE FUSE WAS INSTALLED AT THE BATTERY SWITCH.				1	L	7	1 	3O			NT	A76EU   					 
1999082700169	19990827	00169		1999	8	27	CA990817041      	4	19990809	G	3197		WIRE            			MORAVN	Z142  	Z142        	       	EU  										COCKPIT	FAILED          	W				K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			CA			720  								(CAN) CLOCK HAD BEEN REMOVED FOR REPAIR AND ITS POWER PLUG TAPED UP.  THE TAPE STARTED TO UNWRAP AND DURING A ROUTINE ST	ART UP, PLUG SHORTED OUT ON A GROUND STUD BEHIND PILOT'S PANEL.  WIRE INSULATION BEGAN TO MELT AND SMOKE.  ACFT AND ALL 	EXTERNAL AND ALL ELECTRICAL WAS SHUT DOWN, BUT SMOKE PERSISTED.  THE SMOKE SUBSIDED AFTER BATTERY WAS DISCONNECTED.  INS	ULATION HAD MELTED  AND BURNED OFF.  ENTIRE LENGTH OF CLOCK WIRE PIECE, BUT BECAUSE IT WAS IN MAIN WIRE BUNDLE, IT CAUSE	D SOME MINOR EXTERNAL DAMAGE TO OTHER WIRES (3 SPLICE REPAIRS).  CLOCK WAS CONNECTED TO HOT SIDE OF BATTERY SWITCH (TO K	EEP IT OP), BUT HAD NO CCT PROTECTION.  PERFORMED A NEW WIRE INSTALL TO A VACANT FUSE RECEPTACLE.	1	L	7	1 	3O			NT	A76EU   					 
1999082700948	19990827	00948	EU  	1999	8	27	CA990817042      	1	19990729	G	5712		RIB             			STBROS	SC7   	SC72        	8100510	EU  										LT WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			17610								(CAN) CRACK FOUND IN LEFT STUB WING END RIB EXTENSION FROM LOWER EDGE TO THE AFT LIGHTNING HOLE.  IT EXISTS BENEATH THE 	MLG FAIRING SUPPORT BRACKET WHICH WAS ALSO FOUND TO BE CRACKED.  AVAILABLE EVIDENCE POINTS TO FATIGUE CAUSED BY VIBRATIO	NS AND WORKING OF THE MLG FAIRING. THE END RIB FORMS A BOX THAT SUPPORTS THE GEAR LEG AND OLEO ATTACH FITTINGS.  SUBMITT	ER STATED FAILURE OF THE END RIB MAY CAUSE THE GEAR TO COLLAPSE.			1	H	7	2 	3T				A15EU   					 
1999082700949	19990827	00949	NE  	1999	8	27	CA990817043      	2	19990812	G	7530	LK75573	OUTLET ELBOW    			LKHEED	1011  	1011385114  		WP  	RROYCE	RB211 	RB21122B02  	54555	NE  					NR 1 ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								10066			(CAN) NR 1 ENGINE HP OUTLET ELBOW FOUND CRACKED, POSSIBLY DUE TO HEAT STRESS.  OPERATOR AWAITING COMMENTS FROM ROLLS ROY	CE.					2	L	7	3 	4F	4	F		A23WE   	E12EU				 
1999082700950	19990827	00950		1999	8	27	CA990817044      	4	19990804	G	2312	KX175B	RADIO           	KING        		PIPER 	PA31  	PA31        	7103102	SO  	LYC   	O540  	TIO540A2B   	41532	EA  					COCKPIT VHF	FAILED          	W				D				RETURN TO BLOCK         				H			ELECT. POWER LOSS-50 PC   			NR	NOT REPORTED   	1			CA			8116 					L161761			(CAN) NR 2 COM SET KX175B (A LOANER UNIT) WENT DEAD.  AIRCRAFT IS USUALLY OPERATING WITH A MAC 1700 (KX175B + DIGITAL). 	 AVIONICS SHOP ADVISED THAT TROUBLE ORIGIN APPEARS TO BE A FAILING INTERCOM SYSTEM AND AUDIO PANEL DUE TO UNPROFESSIONAL	 WIRING SHOWING BEHIND RIGHT INSTRUMENT PANEL.				1	L	7	2 	3O	3	O		A20SO   	E14EA				 
1999091700423	19990917	00423	GL  	1999	9	17	CA990818004      	2	19990805	G	7230	23066737	VAIN            		23063379    						ALLSN 	250C  	250C47B     		GL  					COMPRESSOR	SEPARATED       	W				A				UNSCHED LANDING         				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		CR	CRUISE         	1			CA			69   			CAC44046		CAE847027			(CAN) A PIECE OF COMPRESSOR SCROLL TURNING VANE SEPARATED FROM LEFT ENGINE, A CRACK WAS ALSO FOUND ON RIGHT HAND TURNING	 VANE.  FAA MADE AWARE OF THE PROBLEM THROUGH ALLISON ROLLS ROYCE.										3	U			E1GL				 
1999090300339	19990903	00339	EA  	1999	9	3	CA990818005      	2	19990724	G	8530		CONNECTING ROD  			BEECH 	65    	A65         	1152803	CE  	LYC   	O480  	IGSO480A1E6 	41529	EA  					ENGINE	BROKEN          	W				E				ENGINE SHUTDOWN         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CR	CRUISE         	1			CA				699  				L169844			(CAN) ENGINE FAILED, NR 5 CYLINDER CONNECTING ROD BROKEN.						1	L	7	2 	3O	3	O		3A20    	E284				 
1999082700951	19990827	00951	CE  	1999	8	27	CA990818006      	1	19990805	G	2752	995240253	ACTUATOR        		995240253   	BEECH 	100   	100BEECH    	1152916	CE  	PWA   	PT6   	PT6A28      		EA  					TE FLAP	FAILED          	W				O				OTHER                   				F			FLT CONT AFFECTED         			AP	APPROACH       	1			CA				2616 				50054			(CAN) ON APPROACH, WHEN FLAP WAS EXTENDED, THERE WAS NO RESPONSE.  A FLAPLESS LANDING WAS CARRIED OUT.  FLAP MOTOR WAS R	EMOVED, FOUND PLUGGED WITH CARBON DUST FROM BRUSHES.  CLEANED, REINSTALLED.  OPERATIONAL CHECKS SATISFACTORY.  SUGGEST M	OTOR BE REMOVED, CLEANED AND INSPECTED AT 1,000-HOUR INTERVALS.				1	L	7	2 	3T	4	T		A14CE   	E4EA				 
1999082700952	19990827	00952	CE  	1999	8	27	CA990818008      	1	19990807	G	2730	12952409715	BEARING         			BEECH 	1900  	1900D       	1154162	CE  	PWA   	PT6   	PT6A67D     		NE  					ELEVATOR	STIFF           	W				A				UNSCHED LANDING         				F			FLT CONT AFFECTED         			TO	TAKEOFF        	1			CA								PCEPS0007			(CAN) PILOTS REPORTED AFTER TAKEOFF, THE ELEVATOR CONTROLS BECAME JAMMED IN NOSE UP POSITION.  CONTROL COLUMN WAS STIFF 	DUE TO TIGHT BEARINGS IN SUPPORT ASSY. (1295241001 - LOWER ROLLER, 1295241005 - UPPER ROLLER).  MARKS ON THE ROLLERS IND	ICATE POSSIBLE FOD CAUSED TIGHTNESS.				2	L	7	2 	4T	4	T	RT	A24CE   	E26NE				 
1999082700953	19990827	00953	NM  	1999	8	27	CA990818011      	1	19990805	G	2460		HARNESS         			BOEING	757   	757236      		NM  	RROYCE	RB211 	RB211535E4  	54555	NE  					FUSELAGE	CHAFED          	W				K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			CA								30649			(CAN) DURING TAXI BY MAINTENANCE TO POSITION THE AIRCRAFT ON GATE, THE POSITION SENSOR ELECTRONIC UNIT STARTED TO SMOKE.	  AT L1 DOOR AFTER LAVATORY, FOUND A TWELVE WIRE BUNDLE SEVERELY CHAFED BY THE LAVATORY DUMP CABLE WHICH RESULTED IN AN 	ELECTRICAL SHORT BETWEEN A 115 VOLT AC WIRE AND 28 VOLT DC WIRE CAUSING THE PSEU TO SMOKE AND THE MAIN BATTERY CURRENT M	ONITOR, A.P.U. CURRENT MONITOR, AND THE L1 LAVATORY LEVEL DETECTOR TO FAIL.   ALL AFFECTED PARTS REPLACED AND RE-ROUTED 	AWAY FROM THE LAVATORY DUMP CABLE.		2	L	7	2 	4F	4	F	RT	A2NM    	E12EU				 
1999092400200	19990924	00200	NE  	1999	9	24	CA990907001      	2	19990812	G	7260	0292750150	LEAF SPRING     		70BM011040  	SNIAS 	350   	AS350BA     	8680817	EU  	TMECA 	ARRIEL	ARRIEL1B    	6OO30	NE  					POWER TURBINE	LOOSE           	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						255		524			(CAN) LEAF SPRING P/N 0292750150 DISLODGED FROM ITS LOCATION FALLING ONTO AND CUTTING INTO THE POWER TURBINE SHAFT P/N 0	29210875.  THIS FAULT WAS RECOGNIZED ONLY AFTER SOAP SAMPLES REVEALED A HIGH IRON CONTENT 26 PPM AND SUBSEQENT O/H POWER	 SHAFT HAD CUT OF 2.5 MM DEEP AND 17 MM WIDE CIRCUMFERENCIALLY.				1	G	7	1 	3U	3	U	NC	H9EU    	E19EU				 
1999110500561	19991105	00561	CE  	1999	11	5	CA990907005      	1	19990812	G	2435	631847	ADAPTER GEAR    		635050A8    	CESSNA	421   	421B        	2076014	CE  	CONT  	O520  	GTSIO520H   	17032	SO  	MCAULY	3AF34C	3AF34C92    	GL  	STARTER/GEN	STRIPPED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								600417	685549		(CAN) STARTER ADAPTER GEAR STRIPPED CAUSING FURTHER DAMAGE TO CRANKSHAFT GEAR.						1	L	7	2 	3O	3	O		A7CE    	E7CE	5	C	P22EA	 
1999101500520	19991015	00520	GL  	1999	10	15	CA990907012      	3	19990812	G	6111	9333C	BLADE           		V9333C      						LYC   	O435  	GO435C2     	41516	EA  	HARTZL	HC12X	HC12X208    	GL  	PROPELLER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						72756			6035N		(CAN) PER AD 97-18-02, CRACKS FOUND IN BOTH BLADE SHANKS.											3	O			E228	5	C	P845	 
1999092400202	19990924	00202	SO  	1999	9	24	CA990907022      	1	19990826	G	2810	10849	FUEL TANK       			PIPER 	PA18  	PA18150     	7101828	SO  	LYC   	O320  	O320A2B     	41508	EA  					RT WING	DELAMINATED     	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L1675627A			(CAN) DURING A 100 HR INSPECTION, WHITE PARTICULATE WAS FOUND IN FUEL STRAINER AND RIGHT FUEL SIGHT GAUGE.  WHEN SUMP DR	AIN WAS REMOVED, A LARGE AMOUNT OF WHITE FILM FLOWED OUT WITH THE FUEL.  UPON FURTHER INSPECTION OF THE TANK INTERIOR, I	T WAS COATED WITH A WHITE FILM WHICH WAS NOW PEALING OFF.  THE LEFT TANK WAS IN A SIMILAR STATE.  FOUND 'GUN WASH' HELPE	D SOFTEN THE MATERIAL FOR REMOVAL.  STEAM CLEANING WAS  NOT EFFECTIVE.			1	H	7	1 	3O	3	O		1A2     	E274				 
1999110500567	19991105	00567		1999	11	5	CA990907029      	4	19990510	G	3455		ANTENNA         	NARCO       	NA841       															ADF SYSTEM	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						02300					(CAN) SEVERE CORROSION FOUND INTERNALLY.																			 
1999110500568	19991105	00568		1999	11	5	CA990907030      	4	19990510	G	3455		ANTENNA         	NARCO       	NA841       															ADF SYSTEM	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						3168					(CAN) SEVERE INTERNAL CORROSION FOUND.																			 
1999101500522	19991015	00522	GL  	1999	10	15	CA990907046      	2	19990823	G	7230	23064577	VANE            								ALLSN 	250C  	250C47B     		GL  					COMPRESSOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2000 			MA39563		CAE847110			(CAN) THE LEADING EDGE OF THE COMPRESSOR SCROLL TURNING VANE EXHIBITS A CRACK 1 INCH PARALLEL TO AND .5 INCH FROM THE LE	ADING EDGE.										3	U			E1GL				 
1999101500523	19991015	00523	GL  	1999	10	15	CA990907047      	2	19990823	G	7230	23064577	VANE            								ALLSN 	250C  	250C47B     		GL  					COMPRESSOR	BROKEN          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1996 			CAC44154		847043			(CAN) THE LEADING EDGE OF THE COMPRESSOR TURNING VANE BROKE AWAY .1 INCH BY .5 INCH.											3	U			E1GL				 
1999110500572	19991105	00572	NE  	1999	11	5	CA990907052      	2	19990708	G	8530	399353	VALVE           			BEECH 	18    	3TM         	1151046	CE  	PWA   	R985  	R985AN14B   	52008	NE  	HAMSTD	22D	22D30       	NE  	LT ENGINE	FAILED          	W				A				UNSCHED LANDING         				E	R		VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      		CR	CRUISE         	1			CA								9605	168155		(CAN) NR 1 CYLINDER EXHAUST VALVE FAILED.						1	L	7	2 	3R	3	R		A765    	5E1	5	C	P736	 
1999101500005	19991015	00005	NM  	1999	10	15	CA990907064      	1	19990820	G	2752	734386B	TORQUE TUBE     			DHAV  	DHC8  	DHC8201     	2809001	NM  										TE FLAP	DETACHED        	W				C				ABORTED TAKEOFF         				F			FLT CONT AFFECTED         			TO	TAKEOFF        	1			CA			517  								(CAN) OPERATOR REPORTED THAT THE FLAP DRIVE TORQUE TUBE BECAME DETACHED FROM THE OUTBOARD SIDE OF THE NR 3 FLAP SCREW JA	CK PREVENTING RETRACTION OF THE FLAPS.  INSPECTION REVEALED THAT THE TORQUE TUBE TO SCREW JACKPOINT HAD NOT BEEN COMPLET	ELY ENGAGED.				2	H	7	2 	4T			RT	A13NM   					 
1999101500006	19991015	00006	NM  	1999	10	15	CA990907067      	1	19990820	G	3213	10195101	STRUT           		10190105    	DHAV  	DHC8  	DHC8301     		NM  										LT MLG	SHEARED         	W				D				RETURN TO BLOCK         				E			VIBRATION/BUFFET          			TX	TAXI/GRND HDL  	1			CA						365493					(CAN) AFTER TOUCHDOWN, PILOT REPORTED SEVERE VIBRATION.  AT THE GATE, IT WAS FOUND THAT THE LEFT MLG TORQUE LINK HAD BEC	OME DETACHED AT THE UPPER PISTON ATTACHMENT AND WAS DRAGGING ON THE GROUND.  THE INBOARD UPPER TORQUE LINK ATTACH POINT 	ON THE CYLINDER WAS FOUND TO BE SHEARED OFF.  THE OUTBOARD ATTACHMENT POINT HAD DETACHED AND TAKEN OUT PART OF THE CYLIN	DER WALL, DEFLATING THE OLEO.			2	H	7	2 	4T			RT	A13NM   					 
1999102700007	19991027	00007	NE  	1999	10	27	CA990907072      	2	19990817	G	8520	261280	CRANKSHAFT      								PWA   	R985  	R985AN14B   	52008	NE  					ENGINE	CRACKED         	W				A				UNSCHED LANDING         				K			FLUID LOSS                			CR	CRUISE         	1			CA				596  		51714		51714			(CAN) CRACK FOUND UNDER PROP REAR CONE.  CRACK IS HALF WAY AROUND THE CRANK.											3	R			5E1				 
2000012100011	20000121	00011	EA  	2000	1	21	CA990907073      	2	19990711	G	8520	75670	CRANKSHAFT      								LYC   	O541  	TIGO541E1A  	41539	EA  					ENGINE	BROKEN          	W				A				UNSCHED LANDING         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CR	CRUISE         	1			CA			25   			L54662		L54662			(CAN)CRANKSHAFT SEPARATED.  CRANKSHAFT X-RAYED AT PREVIOUS OVERHAUL.											3	O			E19EA				 
1999102900297	19991029	00297	NE  	1999	10	29	CA990907090      	2	19990816	G	7210	310703201	BEARING         								PWA   	120   	PW120A      		NE  					NR 19	SPALLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								120901			(CAN) ELECTROLITIC DAMAGE TO BEARING FOUND CAUSE UNDETERMINED BY OVERHAUL FACILITY.											4	T			E20NE				 
1999102900298	19991029	00298	NE  	1999	10	29	CA990907091      	2	19990819	G	7210	310703201	BEARING         								PWA   	120   	PW120       		NE  					NR 19	SPALLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								120976			(CAN) ELECTROLITIC DAMAGE TO BEARING; CAUSE UNDETERMINED BY OVERHAUL FACILITY.											4	T			E20NE				 
1999100800015	19991008	00015	SW  	1999	10	8	CA990915038      	1	19990827	G	7921	206061432031	IMPELLER        		206061432037	BELL  	206   	206B        	1181511	SW  	ALLSN 	250C  	250C20R1    	03013	GL  					OIL COOLER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				1101 				CAE830551			(CAN) ENGINE OIL COOLER/BLOWER ASSY DISASSEMBLED AT CUSTOMER'S REQUEST.  IMPELLER WAS FOUND CRACKED (1/2) DURING FPI INS	PECTION.  MANUAL SPECIFIES THAT FPI IS CARRIED OUT EVERY 300 HOURS, HOWEVER, THIS CRACK WAS FOUND IN AN AREA NOT SPECIFI	ED IN THE BELL MANUAL, AS REMOVAL OF THE OIL COOLER/BLOWER IS NOT CALLED FOR.				1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999102900307	19991029	00307		1999	10	29	CA990915055      	4	19990902	G	2562		SWITCH          	POINTER     	400010      															ELT	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						408119					(CAN) G-SWITCH FOUND FAULTY.																			 
1999102900308	19991029	00308		1999	10	29	CA990915056      	4	19990902	G	2562		SWITCH          	POINTER     	400010      															ELT	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						408263					(CAN) G-SWITCH FOUND FAULTY.																			 
1999102900309	19991029	00309		1999	10	29	CA990915057      	4	19990907	G	2562		TRANSMITTER     	POINTER     	4000        															ELT	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						106248					(CAN) TRANSMITTER FAULT.																			 
1999101500028	19991015	00028	EA  	1999	10	15	CA990915070      	1	19990830	G	2910	CSP37620	LINE            		72950010453 	DHAV  	DHC7  	DHC7102     	2802708	EA  	PWA   	PT6   	PT6A50      	52043	EA  	HAMSTD	24PF	24PF305     	GL  	HYD SYSTEM	DAMAGED         	W				C				ABORTED TAKEOFF         				F			FLT CONT AFFECTED         			TO	TAKEOFF        	1			CA			18092					8628786594	236948		(CAN) AFTER TAKEOFF, NR 2 SYSTEM FAILURE.  INVESTIGATION REVEALED THAT THE HYDRAULIC LINE FAIRLEADS BETWEEN NR 3 - NR 4 	ENGINES WERE DAMAGED DUE TO HEAT CAUSING ONE OF THE HYDRAULIC LINES TO CHAFE AGAINST THE FAIRLEAD SUPPORT.  SB 7-29-18 R	EPLACED FAIRLEAD WITH ONE OF A HIGHER TEMP RATING.				2	H	7	4 	4T	4	T		A20EA   	E4EA	6	C	P1NE	 
1999102900314	19991029	00314	NE  	1999	10	29	CA990915079      	2	19990909	G	8530		INSERT          			DOUG  	DC3   	DC3         	3021401	WP  	PWA   	R1830 	R183092     	52020	NE  	HAMSTD	23E	23E50       	NE  	ROCKER SHAFT	LOOSE           	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA				912  				363697	NK122770		(CAN) EXHAUST ROCKER SHAFT INSERT FOUND LOOSE ON THE CYLINDER.						2	L	7	2 	4R	4	R		A669    	5E4	6	C	P603	 
1999110500583	19991105	00583	WP  	1999	11	5	CA990916015      	1	19990807	G	6120	65067150	VALVE           	AEROPD      	A6441FN606  	CVAC  	440   	440         	2422902	WP  	ALLSN 	501D  	501D13      	03004	GL  	ALLSN	A6441	A6441FN606  	GL  	PROP GOVERNOR	FAILED          	W				A				UNSCHED LANDING         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CR	CRUISE         	1			CA						WY12314		501084	WY12314		(CAN) SELECTION OF PHASE SYNC CAUSED PROPELLER RPM FLUCTUATIONS, NR 1 PROPELLER VALVE REPLACED.						2	L	7	2 	4R	4	T		6A6     	E282	6	C	P898	 
1999102900319	19991029	00319	WP  	1999	10	29	CA990916017      	1	19990906	G	2612	356080765	FIRE DETECTOR   			CVAC  	440   	440         	2422902	WP  	ALLSN 	501D  	501D13      	03004	GL  	ALLSN	A6441	A6441FN606  	GL  	LT ENGINE	MALFUNCTIONED   	W				A	F	E		UNSCHED LANDING         	ACTIVATE FIRE EXT.      	ENGINE SHUTDOWN         		N			FALSE WARNING             			CR	CRUISE         	1			CA								501084	WY12314		(CAN) IN CRUISE, A ZONE 1 FIRE WARNING ON THE LEFT ENGINE.  ENGINE SHUT DOWN AND PROPELLER FEATHERED.   AIRCRAFT LANDED 	AND AS A PRECAUTION, BOTH BOTTLES FIRED.   SENSING ELEMENT, FIRE BOTTLES, AND CARTRIDGES REPLACED.					2	L	7	2 	4R	4	T		6A6     	E282	6	C	P898	 
1999101500044	19991015	00044	SO  	1999	10	15	CA990927024      	2	19990916	G	7414	1081942	HOUSING         	BENDIX      	107902010   	CESSNA	185   	A185F       	2072821	CE  	CONT  	O520  	IO520D      	17032	SO  					MAGNETO	CORRODED        	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA				759  		G019210DR		286289R			(CAN) THE POLE SHOES IN THE MAGNETO HOUSING WERE FOUND RUSTED AND WERE RUBBED BY THE ARMATURE (ROTATING MAGNET).  PARTIC	LES WERE FOUND SCATTERED IN THE DISTRIBUTOR CAP CAUSING MISFIRING TO GROUND AND OTHER CYLINDERS.  THE SUBMITTER SUGGESTS	 THE CORROSION WAS CAUSED BY OPERATING A NUMBER OF YEARS IN A SALT WATER ENVIRONMENT.				1	H	7	1 	3O	3	O		3A24    	E5CE				 
1999101500051	19991015	00051	SW  	1999	10	15	CA990927036      	1	19990908	G	7120	6306931060	BOLT            	CONT        		MOONEY	M20   	M20K        	5870220	SW  	CONT  	O360  	TSIO360MB   	17025	CE  					ENGINE MOUNT	FAILED          	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA			1024 					279226R			(CAN) THROUGH-BOLT P/N 630693-1060 BROKE THROUGH BEFORE REACHING SPECIFIED TORQUE.  UPON INSPECTION, IT WAS NOTED THAT A	 CRACK HAD DEVELOPED PREVIOUSLY AND ONLY ABOUT 50 PERCENT OF BOLT STILL HOLDING.  PART REMOVED FROM SERVICE.					1	L	7	1 	3O	3	O		2A3     	E9CE				 
1999101500054	19991015	00054	CE  	1999	10	15	CA990927043      	1	19990914	G	2840	05235571	TRANSMITTER     			CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	FUEL QUANTITY	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								RL420276T	728612		(CAN) INVESTIGATION OF FLUCTUATING/NO FUEL QUANTITY, INDICATIONS REVEALED A SHORTED VARIABLE RESISTOR INSIDE THE TRANSMI	TTER, CAUSED BY A SUBSTANDARD REPAIR, IN WHICH A SCREW, USED TO REPLACE A RIVET, INTERFERRED WITH THE WIPER ARM.					1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
1999102900331	19991029	00331	SO  	1999	10	29	CA990927046      	2	19990908	G	8500	055100050	MOUNT           			CESSNA	172   	172         	2072402	CE  	CONT  	O300  	O300A       	17022	SO  	MCAULY	1C172	1C172MDM    	GL  	ENGINE	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								14313D8A	68450		(CAN) ENGINE MOUNT WORN.						1	H	7	1 	3O	3	O	NT	3A12    	E253	5	N	P910	 
1999102900332	19991029	00332	CE  	1999	10	29	CA990927047      	1	19990908	G	7820	05515732	MUFFLER         			CESSNA	172   	172         	2072402	CE  	CONT  	O300  	O300A       	17022	SO  	MCAULY	1C172	1C172MDM    	GL  	ENGINE	MISREPAIRED     	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA								14313D8A	68450		(CAN) UNAPPROVED WELD REPAIR ON RIGHT MUFFLER.						1	H	7	1 	3O	3	O	NT	3A12    	E253	5	N	P910	 
1999102900339	19991029	00339	NM  	1999	10	29	CA990927069      	1	19990908	G	2420	MS3476188S	CONTACTOR BOX   			DHAV  	DHC8  	DHC8*       		NM  	PWA   	120   	PW120       		NE  					GENERATOR	SHORTED         	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			CA			17699								(CAN) DOUBLE AC GENERATOR FAILURE IN CRUISE FLIGHT. MAINTENANCE TRACED THE PROBLEM TO SHORTED PINS E AND F ON THE LEFT A	C CONTACTOR BOX - 2421-P15/J15.  SUBMITTER STATES, THIS EFFECTIVELY SHORTS GCU NR 1/2 PIN D ON EACH (PHASE C) RESULTING 	IN BOTH GENERATORS TAKEN OFF-LINE.				2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999102900352	19991029	00352	GL  	1999	10	29	CA991004023      	3	19990914	G	6114	C84095	SPIDER          	HARTZL      	HCA2VF2B    	CESSNA	310   	310B        	2074208	CE  	CONT  	O470  	O470M       	17026	SO  	HARTZL	HCA2V	HCA2VF2     	GL  	HUB	DAMAGED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4950 	232  		Y2285		531069MR	Y2285		(CAN) PILOT TUBE BORES DAMAGED BEYOND REPAIR.  POSSIBLE BLADE GROUND STRIKE.						1	L	7	2 	3O	3	O		3A10    	E273	5	C	P24EA	 
1999102900354	19991029	00354	EA  	1999	10	29	CA991004031      	2	19990831	G	8530	05K21124CKP	CYLINDER        			HUGHES	269   	269C        	4470504	WP  	LYC   	O360  	HIO360D1A   	41514	EA  					NR 1	WORN            	W				A				UNSCHED LANDING         				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		HO	HOVERING       	1			CA			155  					L2812851A			(CAN) POWER LOSS EXPERIENCED DUE TO STICKY VALVES.						1	G	7	1 	3O	3	O		4H12    	1E10				 
1999102900358	19991029	00358	EA  	1999	10	29	CA991004040      	1	19990917	G	3230	864807	PSEU            			CNDAIR	CL600 	CL6002B19   		EA  	GE    	CF34  	CF343B1     		NE  					AVIONICS BAY	FAILED          	W				O				OTHER                   				J			WARNING INDICATION        			LD	LANDING        	1			CA											(CAN) FLIGHT CREW OBSERVED PROX FAULT STATUS MESSAGE.  PSEU CIRCUIT BREAKER RESET/ MESSAGE WOULD NOT RESET.  WHEN GEAR S	ELECTED DOWN, IT WOULD NOT EXTEND.  EMERGENCY GEAR SELECTED.  MULTIPLE FAILURES RELATED TO FAILED PSEU. AIRCRAFT LANDED 	WITH NO NWS OR ANTI-SKID.				2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999102900359	19991029	00359	EA  	1999	10	29	CA991004041      	1	19990917	G	2752	853D10011	ACTUATOR        			CNDAIR	CL600 	CL6002B19   		EA  	GE    	CF34  	CF343B1     		NE  					TE FLAP	FAILED          	W				H				DEACTIVATE SYST/CIRCUITS				F			FLT CONT AFFECTED         			AP	APPROACH       	1			CA			3345 								(CAN) FLAP FAIL ON APPROACH FROM 8-20 DEGREE FAILURE AT 16 DEGREES.  LEFT OUTBOARD FLAP FOUND TWISTED.   NR 3 AND NR 4 A	CTUATORS FAILED.					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999102900360	19991029	00360	EA  	1999	10	29	CA991004042      	1	19990917	G	2752	601R145011	ACTUATOR        			CNDAIR	CL600 	CL6002B19   		EA  	GE    	CF34  	CF343B1     		NE  					TE FLAP	MALFUNCTIONED   	W				H				DEACTIVATE SYST/CIRCUITS				F			FLT CONT AFFECTED         			AP	APPROACH       	1			CA			4310 								(CAN) FLAP FAILED ON WHEN SELECTED FROM 8-20 DEGREES.  FAILED AT 13 DEGREES.  LEFT OUTBOARD FLAP TWISTED.  INBOARD (JAMM	ED) AND OUTBOARD ACTUATORS REPLACED ALONG WITH FLAP PANEL.					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999102900362	19991029	00362	EA  	1999	10	29	CA991004044      	1	19990926	G	2751	855D1009	BPSU            			CNDAIR	CL600 	CL6002B19   		EA  	GE    	CF34  	CF343B1     		NE  					TE FLAP	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) FLAP FAIL MESSAGE ON SELECTION OF 8 DEGREE FLAP DURING PRE-FLIGHT.  RIGHT BPSU  REPLACED.						2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999101500576	19991015	00576	CE  	1999	10	15	CA991004050      	1	19990812	G	3230	6A0711602	ACTUATOR        	WIPAIR      	4000AMPHIB  	CESSNA	206   	TU206G      	2073357	CE  	CONT  	O520  	TSIO520M    	17040	SO  	MCAULY	D3A34	D3A34C402   	GL  	MLG	CRACKED         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			589  			6A		520296	810310		(CAN) THE FORWARD WHEEL GEAR ACTUATOR ON THE LEFT FLOAT WAS FOUND CRACKED AND LEAKING.  TWO LONGITUDINAL CRACKS WERE LOC	ATED IN THE ACTUATOR CYLINDER.					1	H	7	1 	3O	3	O		A4CE    	E8CE	5	C	P47GL	 
1999110500600	19991105	00600	EU  	1999	11	5	CA991007023      	1	19991001	G	6520	350A331091	GEAR            			SNIAS 	350   	AS350*      		EU  										T/R GEARBOX	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			508  			ZF4912					(CAN) TAIL ROTOR GEARBOX MAKING METAL.  PREMATURE WEAR OF GEAR TEETH/GEAR PAIR S/N ZF4912.  GEAR PAIR WAS REPLACED.						1	G	7	1 	3U				H9EU    					 
1999110500601	19991105	00601	EU  	1999	11	5	CA991007024      	1	19991001	G	6520	350A33109100	GEAR            			SNIAS 	350   	AS350*      		EU  										T/R GEARBOX	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			152  			ZF4956					(CAN) GEAR TOOTH MAKING METAL DUE TO PREMATURE WEAR.  GEAR PAIR S/N ZF4956.  GEAR PAIR REPLACED.						1	G	7	1 	3U				H9EU    					 
1999102900373	19991029	00373	GL  	1999	10	29	CA991007039      	2	19990316	G	7313	6890917	NOZZLE          	ALLSN       	6890917     						ALLSN 	250C  	250C20B     	03013	GL  					FUEL SYSTEM	CRACKED         	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA						AG11495					(CAN) FUEL NOZZEL OUTER AIR SHROUD CRACKED WHEN RECEIVED FROM VENDOR.											3	U			E4CE				 
1999102900381	19991029	00381	EA  	1999	10	29	CA991007066      	2	19990930	G	8530	C0828	ROD             			PIPER 	PA28  	PA28140     	7102802	SO  	LYC   	O320  	O320E2A     	41508	EA  	HARTZL	HC82	HC82VL2     	GL  	PISTON	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				146  				2130827A	167D		(CAN) CORROSION FOUND ON PISTON RODS AND IN CYLINDER FELT GROOVE DURING 6 YEAR CHECK.						1	L	7	1 	3O	3	O		2A13    	E274	5	C	P23EA	 
1999102900382	19991029	00382	CE  	1999	10	29	CA991007068      	1	19990902	G	3211	514110313	TRUNNION        			CESSNA	414   	414A        	2075907	CE  	CONT  	O520  	TSIO520NB   	17040	SO  	MCAULY	3AF32C	3AF32C512   	GL  	LT MLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4207 					L503168	961850		(CAN) DURING SCHEDULED MAINTENANCE, LANDING GEAR WAS INSPECTED IAW CESSNA SB 79-11. THE LEFT MAIN LANDING GEAR TRUNNION 	WAS FOUND CRACKED IN THE UPPER WEB AREA BETWEEN THE ATTACH POINTS.					1	L	7	2 	3O	3	O		A7CE    	E8CE	5	C	P22EA	 
1999110500630	19991105	00630	NM  	1999	11	5	CA991007072      	1	19990918	G	5230	95130345	ROD             		9513013     	DHAV  	DHC8  	DHC8301     		NM  										CARGO DOOR	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2100 								(CAN) THE LATCH ASSY IS COMPOSED OF 3 SHOOTBOLTS THAT ARE INTERCONNECTED BY ACTUATOR RODS.  ON THREE OCCASIONS ACTUATION	 ROD WAS FOUND BROKEN (DUE TO FATIGUE).  FAILURE MAY PREVENT ACCESS FROM THE CABIN TO THE CARGO AREA.   SUBMITTER STATED	 MANUFACTURER IS CONSULTING SUPPLIER ABOUT PROPER HEAT TREATMENT PROCEDURES.				2	H	7	2 	4T			RT	A13NM   					 
1999102900384	19991029	00384	SO  	1999	10	29	CA991007085      	2	19990903	G	8530	639272	ROCKER BOSS     			CESSNA	185   	A185F       	2072821	CE  	CONT  	O520  	IO520D      	17032	SO  					CYLINDER	BROKEN          	W				A				UNSCHED LANDING         				R			PARTIAL RPM/PWR LOSS      			CR	CRUISE         	1			CA			931  					572654			(CAN) BROKEN EXHAUST ROCKER BOSS ON NR 1 CYLINDER.						1	H	7	1 	3O	3	O		3A24    	E5CE				 
1999110500640	19991105	00640	NM  	1999	11	5	CA991007095      	1	19990930	G	7921	28E996	OIL COOLER      			DHAV  	DHC8  	DHC8102     	2809003	NM  										ENGINE OIL	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			6649 	23   		01900472					(CAN) OIL PRESSURE LIGHT ILLUMINATED IN-FLIGHT WITH OIL PRESSURE DROPPING RAPIDLY.  OIL LEAK FOUND AT OIL COOLER.  COOLE	R IN SERVICE FOR ONLY 23.2 HOURS.					2	H	7	2 	4T			RT	A13NM   					 
1999111900190	19991119	00190	NM  	1999	11	19	CA991027034      	1	19990930	G	5540	85545002009	FITTING         		85540002001 	DHAV  	DHC8  	DHC8201     	2809001	NM  										RUDDER	WORN            	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4831 			SSA0161					(CAN) LOWER FLANGE ATTACHMENT HOLE (RUDDER) FOR RADIUS ROD END FITTING, BUSHING WORN AND HOLE ELONGATED EXCESSIVELY.  WE	AR DUE TO RELATIVE WASHER MOVEMENT .018 INCH - .008 INCH.  BOLT HOLE ELONGATION .342 INCH BY .295 INCH.					2	H	7	2 	4T			RT	A13NM   					 
1999121000029	19991210	00029	CE  	1999	12	10	CA991027041      	1	19991008	G	2820	040031164	LINE            			CESSNA	150   	150F        	2071814	CE  	CONT  	O200  	O200A       	17020	SO  					FUEL SYSTEM	CHAFED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			6447 					681797A			(CAN) FUEL LINES FOUND CHAFED AGAINST IMPROPERLY INSTALLED HEADLINER RETAINER BOW.  FUEL LINES CHAFED TO THE POINT WHERE	 MINOR CLEANING OF THE SUSPECT AREA CAUSED LEAKAGE.					1	H	7	1 	3O	3	O		3A19    	E252				 
1999112500189	19991125	00189	EU  	1999	11	25	CA991027079      	1	19990908	G	6410	355A12004004	BLADE           			SNIAS 	350   	AS350*      		EU  										TAIL ROTOR	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2518 	927  							(CAN) OPERATOR NOTICED PAINT CRACK DURING SCHEDULED MAINTENANCE.  TAIL ROTOR BLADE SENT OUT FOR FURTHER INSPECTION WHICH	 LATER REVEALED A 45 MM SPANWISE CRACK AT 45 DEGREE ANGLE ON THRUST SIDE OF NR 1 BLADE.   CRACK FOUND AT BLADE STATION 4	50 MM AND EXTENDED FROM TE RIVET NEAR BLADE ROOT.  REVERSE SIDE OF BLADE ALSO HAD A CHORDWISE CRACK OF 15 MM.				1	G	7	1 	3U				H9EU    					 
1999112500191	19991125	00191	CE  	1999	11	25	CA991028001      	1	19990814	G	7120	075100123	MOUNT           			CESSNA	180   	180         	2072602	CE  	CONT  	O470  	O470K       	17026	SO  					ENGINE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			435  					472826K4			(CAN) ENGINE MOUNT FOUND CRACKED 75 PERCENT THROUGH.						1	H	7	1 	3O	3	O	NC	5A6     	E273				 
1999112500193	19991125	00193	CE  	1999	11	25	CA991028012      	1	19990922	G	8011	64150020	CLUTCH          		O200A       	CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A102	1A102OCM    	GL  	STARTER	WORN            	W				E				ENGINE SHUTDOWN         				D			INFLIGHT SEPARATION       			NR	NOT REPORTED   	1			CA				147  		231203R		231203R	G16984		(CAN) STARTER SEIZED.						1	H	7	1 	3O	3	O		3A19    	E252	5	N	P918	 
1999120400071	19991204	00071	EU  	1999	12	4	CA991028024      	1	19991005	G	6320	4638302023	BEARING         		4038001001  	BOLKMS	105   	BO105S      	5626006	EU  										M/R GEARBOX	SPALLING        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			2864 			1236					(CAN) MAIN TRANSMISSION RIGHT INPUT BEARING SPALLING.  BEARING REPLACED.						1	G	7	2 	3U				H3EU    					 
1999120400072	19991204	00072	EU  	1999	12	4	CA991028025      	1	19991012	G	6320	4638302002	PINION GEAR     	ZENITH      	4638001001  	BOLKMS	105   	BO105S      	5626006	EU  										M/R GEARBOX	MAKING METAL    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				1395 		227					(CAN) MAIN TRANSMISSION PINION GEAR PEELING.  PINION GEAR REPLACED.						1	G	7	2 	3U				H3EU    					 
1999111900218	19991119	00218	EA  	1999	11	19	CA991028028      	1	19991004	G	5210	75210417001	LEVER           			DHAV  	DHC7  	DHC7*       		EA  										PASSENGER DOOR	BROKEN          	W				I				CABIN DEPRESSURIZATION  				D	J		INFLIGHT SEPARATION       	WARNING INDICATION        		AP	APPROACH       	1			CA											(CAN) ON FINAL APPROACH, AIRSTAIR DOOR WARNING CAME ON TOGETHER WITH CABIN DEPRESSURIZATION.  DOOR HANDLE HAD MOVED AND 	DAYLIGHT WAS VISIBLE AROUND THE EDGE OF THE DOOR.  LOCKING LEVER SHEARED.					2	H	7	4 	4T			RT	A20EA   					 
1999111900219	19991119	00219	CE  	1999	11	19	CA991028029      	1	19991008	G	5343	52130285	FITTING         			CESSNA	441   	441         	2076020	CE  	GARRTT	TPE331	TPE33110    	01514	WP  					BS 70	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			4372 					P7724			(CAN) DURING SCHEDULED INSPECTION, A CRACK WAS DETECTED ON THE NOSE GEAR WHEELWELL WEB AND TEE FITTING AT THE LEFT DRAG 	BRACE ATTACH FITTING.					1	L	7	2 	3T	4	T	RT	A28CE   	E4WE				 
1999112500200	19991125	00200	NM  	1999	11	25	CA991028033      	1	19991016	G	2121	219001621	FAN             			DOUG  	MD88  	MD88        	3023688	NM  										AIR DISTRIBUTION	SEIZED          	W				A				UNSCHED LANDING         				B			SMOKE/FUMES/ODORS/SPARKS  			CL	CLIMB          	1			CA											(CAN) MID-AIR TURNBACK DUE TO ODOR IN CABIN.  ON ARRIVAL, TOILETS, GALLEYS AND PASS UNITS CHECKED.  TAIL SECTION AND AIR	 CONDITIONING PACKS, OVERHEAD CEILING CHECKED AND WHEEL WELLS AND CARGO COMPTS.  FOUND RE-CIRCULATING FAN IN AFT CARGO S	EIZED.   DE-ACTIVATED PER MEL.				2	L	7	2 	4F			RT	A6WE    					 
1999111900220	19991119	00220	SO  	1999	11	19	CA991028034      	1	19991019	G	2820	1859400	LINE            			PIPER 	PA23  	PA23        	7102302	SO  	LYC   	O320  	O320A3B     	41508	EA  	HARTZL	HC82X	HC82XL2     	GL  	WS 95	CUT             	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			3457 					L1132127	K895N		(CAN) AIRCRAFT RECEIVED WITH FUEL LEAK AT RT WING.   FOUND FUEL LINE OF AUXILARY TANK AT WS 95 VIBRATED AGAINST RIB AND 	WORE HALF THROUGH TUBING.  THE SUPPORT CLAMP AT THAT STATION WAS NOT INSTALLED.   FOUND ALSO SCOTT FUEL VALVE NOT SHUTTI	NG OFF COMPLETELY.  (PILOT REPORTED FUEL LEAKING  OUT OF ENGINE COWL AND ABOVE EXHAUST AUGMENTOR TUBE REGARDLESS OF FUEL	 VALVE POSITION.) TO INSTALL SUPPORT CLAMP OF FUEL LINE STATION 95 TO THE BRACKET PROVIDED AT THE RIB IS JUST ABOUT IMPO	SSIBLE.  INSTALLED DOUBLER AT BOTTOM AND INSTALLED INSPECTION PLATE.  WHEN INSPECTING LEFT WING ALSO FOUND NO SUPPORT CL	AMP ON WS 95.	1	L	7	2 	3O	3	O		1A10    	E274	5	C	P878	 
1999111900221	19991119	00221	EA  	1999	11	19	CA991028036      	1	19991014	G	2761	2651001013	ACTUATOR        			DHAV  	DHC7  	DHC7102     	2802708	EA  	PWA   	PT6   	PT6A50      	52043	EA  	HAMSTD	24PF	24PF305     	GL  	SPOILER	JAMMED          	W				O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			CA						0280L		8628786594	236948		(CAN) CREW HAD A SPOILER JAM INDICATION ON THE GROUND.  THE CREW CONFIRMED THAT BOTH LEFT ROLL SPOILERS WERE JAMMED UP. 	 ACTUATOR REPLACED.					2	H	7	4 	4T	4	T		A20EA   	E4EA	6	C	P1NE	 
1999120400074	19991204	00074	SW  	1999	12	4	CA991028037      	1	19990806	G	6520	206340103101	SEAL            		206040402105	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					T/R GEARBOX	LEAKING         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			34   			AF52326		CAE895407			(CAN) INPUT SEAL LEAKING HYDRAULIC FLUID.  NEW SEAL INSTALLED.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999112500203	19991125	00203	NE  	1999	11	25	CA991028047      	2	19991011	G	7210		OIL FILTER      			CNDAIR	CL600 	CL6002B19   		EA  	GE    	CF34  	CF343B1     		NE  					LT ENGINE	FAILED          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			CA											(CAN) OIL PRESSURE FLUCTUATIONS.  AIRCRAFT FERRIED BACK TO HOME BASE IN SLOVENIA.						2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999111900228	19991119	00228	EA  	1999	11	19	CA991028049      	1	19991015	G	3230	864202	SENSOR          			CNDAIR	CL600 	CL6002B19   		EA  	GE    	CF34  	CF343B1     		NE  					NLG	MALFUNCTIONED   	W				O				OTHER                   				J			WARNING INDICATION        			AP	APPROACH       	1			CA			10660								(CAN) AFTER LANDING GEAR DOWN SELECTION, THE NLG DID NOT EXTEND.  AFTER 30 SECONDS, THE NLG EXTENDED WITHOUT ACTION FROM	 THE CREW.  PSEU HAD CH27 FAULT AND WIRE PS4MB HAD HIGH RESISTANCE.  NEW WIRE SPLICED IN.					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999112500205	19991125	00205	EA  	1999	11	25	CA991028056      	2	19991002	G	8520	LW13818	CRANKCASE       		IO360C1C6   	PIPER 	PA28  	PA28R201    	7102816	SO  	LYC   	O360  	IO360C1C6   	41514	EA  					NR 2 CYLINDER	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			3717 	1711 		RL2072651A		RL2072651A			(CAN) CRACK EMANATING FROM NR 2 CYLINDER STUD FLANGE TO BLOCK 1.						1	L	7	1 	3O	3	O		2A13    	1E10				 
1999120400078	19991204	00078	SW  	1999	12	4	CA991028072      	1	19990917	G	6510	407340340101	DISC PACK       			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					T/R DRIVE	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			159  					CAE847128			(CAN) NR 7 THOMAS COUPLING DISC WAS FOUND CRACKED (BOTH FRONT AND BACK SEGMENTS WERE BROKEN).						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999112500208	19991125	00208	NE  	1999	11	25	CA991028074      	2	19990930	G	7260	311196801	TOWERSHAFT      								PWA   	PW121 	PW121       	52124	NE  					ENGINE	FRACTURED       	W				A				UNSCHED LANDING         				X	J		ENGINE FLAMEOUT           	WARNING INDICATION        		CR	CRUISE         	1			CA								120604			(CAN) THE TOWER SHAFT WAS FOUND FRACTURED BETWEEN THE UPPER LOCATION DIAMETER AND THE UPPER SPLINED SECTION.  REPORT HAS	 NO FAILURE DETERMINATION.  SEE REPORT EI-078.										4	T			E20NE				 
1999112500209	19991125	00209	NE  	1999	11	25	CA991028075      	2	19990923	G	7210	310062301	BEARING         								PWA   	118   	PW118       		NE  					RGB NR 18 BRG	SPALLED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								115244			(CAN) SPALLING OF NR 18 BEARING FROM ELECTRICAL DISCHARGE, I.E., LIGHTNING STRIKE.											4	T			E20NE				 
1999120400081	19991204	00081	EU  	1999	12	4	CA991103014      	1	19991002	G	6310	341A35017620	BEARING         		341A35002001	SNIAS 	SA341 	SA341G      	8680610	EU  	TMECA 	AST3T 	ASTAZOU3A   	60007	EU  					FREEWHEEL UNIT	COLLAPSED       	W				A				UNSCHED LANDING         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		HO	HOVERING       	1			CA			938  			WAC577					(CAN) WHILE IN HOVER, AIRFRAME/DRIVETRAIN VIBRATION WAS FELT AND ROTORCRAFT THEN LANDED.  SUBSEQUENT INVESTIGATION REVEA	LED THAT FREEWHEELING BEARING FAILED LEAVING SCATTERED FRAGMENTS.  THERE WAS NO PRIOR INDICATION OF IMPENDING FAILURE. D	GAC AD 82-062-030B WAS COMPLIED WITH 1 HOUR PRIOR TO FAILURE, HOWEVER, ALL OPERATING/INDICATIONS WERE NORMAL.  AIRCRAFT 	WAS LOADED LIGHT AND WEATHER WAS CALM AND CLEAR.			1	G	7	1 	3U	3	U		H6EU    	E14EU				 
1999120400082	19991204	00082		1999	12	4	CA991103015      	4	19991020	G	3414		INDICATOR       	AEROMECH    	8502CS20LW  	SKRSKY	S76   	S76         	8143010	NE  										COCKPIT	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						512					(CAN) AIRSPEED INDICATOR WAS FOUND TO BE IN CALIBRATION WITH STANDARD PRESSURE, HOWEVER, SIKORKSY S76 REQUIRES A NON-STA	NDARD PRESSURE TO BE APPLIED TO ACHIEVE THE SPECIAL CALIBRATION FOR THIS AIRCRAFT.  ERROR IN EXCESS OF THE ALLOWABLE TOL	ERANCES WERE EVIDENT ON INITIAL TEST.				1	G	7	2 	3U				H1NE    					 
1999120400083	19991204	00083	EA  	1999	12	4	CA991103016      	1	19991020	G	5741	AN723A	BOLT            	SCWZER      		SCWZER	SG2   	SGS233A     	8051606	EA  										WING ATTACH	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) NEW WING ATTACHMENT BOLTS NDT'D PRIOR TO INSTALLATION REVEALED THAT 9 OUT OF 24 BOLTS (AN 7-23A) WERE REJECTED.  B	OLTS ARE MADE OF ROLLED STEEL AND THERE WAS AN INDICATION OF AN INCOMPLETE ROLLING PROCESS.  SUBMITTER STATED IT IS UNKN	OWN IF THE SEAMS WERE SURFACE OR PENETRATED INTO THE BOLT.				1	K	0	0 					G2EA    					 
1999112500216	19991125	00216	GL  	1999	11	25	CA991103030      	2	19991007	G	7240	23032280	TURBINE WHEEL   								ALLSN 	250C  	250C30P     	03013	GL  					2ND STAGE	FAILED          	W				K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			CA			1463 			CAT95363		CAT95363			(CAN) MANUFACTURER UNABLE TO PROVIDE CONFIRMATION THAT THEY MANUFACTURED THIE S/N WHEEL SPECIFIED.  ITEM SENT TO M&M S.U	.P.										3	U			E1GL				 
1999121800757	19991218	00757		1999	12	18	CA991103046      	4	19990917	G	3414	PH11001DH	INDICATOR       			DHAV  	DHC8  	DHC8301     		NM  	PWA   	PW120 	PW123       		NE  					COCKPIT	FAILED          	W				O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			CA											(CAN) NR 2 AIRSPEED INDICATOR FAILED DURING CRUISE FLIGHT AT FL 210.  A/P AND Y/D ALSO FAILED.  INDICATOR OPERATED ERRAT	ICALLY FOR 1/2 HOUR BEFORE RETURNING TO NORMAL.  UNEVENTFUL LANDING CARRIED OUT AT DESTINATION.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE				 
1999121800758	19991218	00758	EA  	1999	12	18	CA991103049      	1	19991109	G	7603	1603730001	THROTTLE CABLE  		FE247000    	CNDAIR	CL600 	CL6002B16   	1900305	EA  	GE    	CF34  	CF343A1     	30015	NE  					RT ENGINE	SEIZED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			1335 			FR012		807197			(CAN) RIGHT THROTTLE FROZE AT FL 370 AFTER APPROXIMATELY 3.5 HOURS.  THROTTLE CABLE CLEANED WITH DRY NITROGEN.  AIRCRAFT	  RETURNED TO SERVICE.					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999112500219	19991125	00219		1999	11	25	CA991103057      	4	19991028	G	3460	7011702929	FGC             	HONEYWELL   	GC810       	CESSNA	750   	750         	2076810	CE  										E/E BAY	FAILED          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			CA			552  			97050646					(CAN) DURING CRUISE FLIGHT, FLIGHT GUIDANCE CONTROLLER A FAIL LIGHT CAME ON.						2	L	7	2 	4J			RT	T00007WI					 
1999112500222	19991125	00222	NE  	1999	11	25	CA991103064      	3	19991021	G	6114	C6172	THRUST PLATE    													HARTZL	HCE4A	HCE4A3A     	NE  	PROPELLER HUB	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			778  						HJ1081		(CAN) THRUST PLATE TURNED IN HUB NOT ALLOWING PROPPELLER TO REACH FULL FEATHER.																5	C	P10NE	 
1999120400094	19991204	00094	NE  	1999	12	4	CA991103068      	2	19991019	G	7321	6078T55P16	FCU             			CNDAIR	CL600 	CL6002B16   	1900305	EA  	GE    	CF34  	CF343B1     		NE  					ENGINE	FAILED          	W				C				ABORTED TAKEOFF         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		TO	TAKEOFF        	1			CA			774  			872270		872270			(CAN) ENGINE FAILED TO ACCELERATE ABOVE 77 PERCENT N1.  FCU REPLACED AS WELL AS N1 AMPLIFIERS SWAPPED. NO FURTHER DEFECT	S NOTED.					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999120400096	19991204	00096	NE  	1999	12	4	CA991103072      	2	19991025	G	7260	6014T81G23	BEARING         	GE          		CNDAIR	CL600 	CL6002B16   	1900305	EA  	GE    	CF34  	CF343A      	30015	NE  					GEARBOX	MAKING METAL    	W				A				UNSCHED LANDING         				E	J		VIBRATION/BUFFET          	WARNING INDICATION        		CR	CRUISE         	1			CA			4806 			350415		350415			(CAN) BEARING MATERIAL FROM ACCESSORY GEARBOX DETECTED.						2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999121800773	19991218	00773	EA  	1999	12	18	CA991104009      	1	19990901	G	2710		TRANSMITTER     			CNDAIR	CL600 	CL6002B16   	1900305	EA  	GE    	CF34  	CF343A1     	30015	NE  					AILERON POSITION	FAILED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1310 					807197			(CAN) AILERON POSITION TRANSMITTER ARM INCORRECTLY INSTALLED WHICH CAUSED THE ARM TO RUB ON AILERON CABLE.						2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
1999120400103	19991204	00103	NE  	1999	12	4	CA991104015      	2	19991012	G	7230	311206301	COVER           								PWA   	120   	PW120       		NE  					NR 5 BEARING	MAKING METAL    	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA						121133		121133			(CAN) NR 5 BEARING MISSING MATERIAL ON OUTER CAGE.  REF:   REPORT NR  ETR - 0182 ATI.											4	T			E20NE				 
1999121800785	19991218	00785	WP  	1999	12	18	CA991112031      	1	19991104	G	7921	C1861	HUB             		C0075       	ROBSIN	R44   	R44         	7640120	WP  	LYC   	O540  	O540F1B5    	41532	EA  					COOLER BLOWER	SCORED          	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			1212 					L2496640A			(CAN) THE HUB OF THE BLOWER WAS FOUND CRACKED AND SEVERELY DAMAGED DUE TO POSSIBLE MOVEMENT OF THE BLOWER ALONG THE SHAF	TS SURFACE.  THE TWO TOUCHING PIECES HAVE SCORES AND TRANSPOSED METAL.  PIECES SENT TO MFG FOR INVESTIGATION (MATERIAL O	R OTHERWISE).  PARTS REPLACED.				1	G	7	1 	3O	3	O		H11NM   	E295				 
1999121800790	19991218	00790	NM  	1999	12	18	CA991116005      	1	19991017	G	6123	30005000031	TSCU            		PW120       	DHAV  	DHC8  	DHC8101     	2809002	NM  	PWA   	120   	PW120       		NE  	HAMSTD	14SF	14SF7       	NE  	AUTOFEATHER SYS	FAILED          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			TO	TAKEOFF        	1			CA						299		299			(CAN) AFTER TAKEOFF, THE CREW SELECTED THE AUTOFEATHER SYSTEM OFF AND THE ARMED LIGHT STAYED ON.  MAINTENANCE REPLACED T	HE TORQUE SIGNAL CONDITIONING UNIT (TSCU).  GROUND RUNS CARRIED OUT OK, AIRCRAFT RELEASED TO SERVICE.					2	H	7	2 	4T	4	T	RT	A13NM   	E20NE	6	C	P7NE	 
1999121800792	19991218	00792	EA  	1999	12	18	CA991116015      	1	19991112	G	2760	4916405	SECU            			CNDAIR	CL600 	CL6002B19   		EA  										E/E BAY	FAILED          	W				C				ABORTED TAKEOFF         				F			FLT CONT AFFECTED         			TO	TAKEOFF        	1			CA											(CAN) NR 1 SPOILER ELECTRONIC CONTROL UNIT WAS GIVING THE WRONG INDICATIONS REGARDING SPOILER POSITION.  SECU REPLACED.						2	L	7	2 	4F			RT	A21EA   					 
1999121800793	19991218	00793	EA  	1999	12	18	CA991116016      	1	19991112	G	2761	270007	PCU             			CNDAIR	CL600 	CL6002B19   		EA  										SPOILER	LEAKING         	W				O				OTHER                   				K	J		FLUID LOSS                	WARNING INDICATION        		CR	CRUISE         	1			CA											(CAN) NR 1 HYDRAULIC SYSTEM WAS LOSING FLUID ON EICAS, UP TO 10 PERCENT AFTER TOUCH DOWN.  RIGHT INBOARD SPOILER PCU LEA	KING BETWEEN THE TORQUE MOTOR AND VALVE BODY.					2	L	7	2 	4F			RT	A21EA   					 
1999121800796	19991218	00796	EA  	1999	12	18	CA991116019      	1	19991113	G	2750	855D1009	BPSU            			CNDAIR	CL600 	CL6002B19   		EA  										TE  FLAP	FAILED          	W				O				OTHER                   				J			WARNING INDICATION        			DE	DESCENT        	1			CA						235A					(CAN) FLAPS FAIL AT 8 DEGREES ON APPROACH.  BPSU REPLACED.						2	L	7	2 	4F			RT	A21EA   					 
1999121800797	19991218	00797	EA  	1999	12	18	CA991116020      	1	19990408	G	3220		LANDNG GEAR     			CNDAIR	CL600 	CL6002B19   		EA  										NOSE	FAILED          	W				A				UNSCHED LANDING         				J			WARNING INDICATION        			CL	CLIMB          	1			CA											(CAN) AFTER DEPARTURE, GEAR DISAGREE MESSAGE APPEARED WITH SELECTION OF GEAR UP.  HYD 3B SELECTED ON AND GEAR SELECTED D	OWN WITH 3 GREEN AND NO HORN.  ON FINAL APPROACH (RTB), ATC ADVISED FLIGHT CREW THAT NOSE GEAR WAS NOT EXTENDED.  NOSE G	EAR WAS FULLY RETRACTED AND DOORS CLOSED.  MANUAL EXTENSION COMPLETED AND AIRCRAFT LANDED.				2	L	7	2 	4F			RT	A21EA   					 
2000012200362	20000122	00362	CE  	2000	1	22	CA991208063      	1	19991110	G	2460		DC POWER        			BEECH 	1900  	1900D       	1154162	CE  										ELECTRICAL SYS	FAILED          	W				O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			CA			4434 								(CAN) COMPLETE DC POWER FAILURE DUE TO LIGHTNING STRIKE EXPERIENCED.  PART TC:  6,665.						2	L	7	2 	4T			RT	A24CE   					 
2000011500517	20000115	00517	SO  	2000	1	15	CA991208091      	2	19991021	G	8520	530184A2	BEARING         	CONT        	C1452       	CESSNA	172   	172         	2072402	CE  	CONT  	C145  	C1452       	17012	SO  	MCAULY	1A170	1A170DM     	GL  	ENGINE	DISINTEGRATED   	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA				980  		7910D32		7910D32	52245		(CAN) ENGINE EXPERIENCED A NR 6 CONNECTING ROD BEARING FAILURE.  SDR SUBMITTER HAS EMPLOYED AN OIL ANALYSIS PROGRAM BUT 	THE RESULTS OF WHICH, THOUGH SHOWING SOME INDICATIONS OF BREAKDOWN, WERE WRONGLY INTERPRETED.					1	H	7	1 	3O	3	O	NT	3A12    	E253	5	N	P857	 
2000011500518	20000115	00518	EA  	2000	1	15	CA991209003      	2	19991021	G	7532	3020046	WASHER          	PWA         	3027249     	DHAV  	DHC6  	DHC6100     		EA  	PWA   	PT6   	PT6*        	52043	EA  					BLEED VALVE	DISPLACED       	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA				52   		A6614					(CAN) THE NUT HOLDING THE BLEED VALVE PISTON ASSY WAS FOUND TO BE OVERTORQUED THIS..  THIS CAUSED THE SILICONE WASHER TO	 DISPLACE ALLOWING THE FACE PLATE TO SHIFT WHICH CAUSED THE LEAK.					1	H	7	2 	3T	3	T		A9EA    	E2NE				 
2000011500523	20000115	00523	NE  	2000	1	15	CA991209017      	2	19990721	G	7230	310920901	BEARING         								PWA   	PT6   	PT6A67A     	52043	NE  					COMPRESSOR	CRACKED         	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA				1549 		39B651		PCE106061			(CAN) IN-FLIGHT SHUT DOWN BY U.K. OPERATOR.  THE COMPRESSOR ROTOR WAS FOUND SEIZED DUE TO NR 1 BEARING FAILURE, (BEARING	 FRACTURED IN SEVERAL PIECES).										4	T			E26NE				 
2000011500524	20000115	00524	EA  	2000	1	15	CA991209018      	2	19990806	G	7230	311211703	BEARING         								PWA   	PT6   	PT6A45R     	52043	EA  					COMPRESSOR	CRACKED         	W				A				UNSCHED LANDING         				E			VIBRATION/BUFFET          			CR	CRUISE         	1			CA			2132 			FC67351		PCE84200			(CAN) IN-FLIGHT SHUT DOWN BY U.K. OPERATOR.  THE COMPRESSOR ROTOR WAS FOUND SEIZED DUE TO NR 1 BEARING FAILURE.											4	T			E4EA				 
2001032800042	20010328	00042	SO  	2001	3	28	CA991209026      	1	19990203	G	3232	592625	ACTUATOR        	CLEVELAND   	5913        	PIPER 	PA46  	PA46350P    	       	SO  	LYC   	O540  	TIO540AE2A  	41532	EA  					NLG	FAILED          	W				K	 	 	 	NONE                    				K		 	FLUID LOSS                			IN	INSP/MAINT     	1			CA			395  			551					(CAN) NOSE GEAR SEQUENCE ACTUATOR FAILED, CAUSING MAJOR LEAK IN HYDRAULIC SYSTEM,.THIS CAUSED THE GEAR TO NOT FULLY EXTE	ND.					1	L	7	1 	3O	3	O	RT	A25SO   	E14EA				 
2000021200310	20000212	00310	NE  	2000	2	12	CA991209028      	2	19991006	G	8530	399353	EXHAUST VALVE   			BEECH 	18    	3TM         	1151046	CE  	PWA   	R985  	R985AN14B   	52008	NE  					CYLINDER	FAILED          	W				A				UNSCHED LANDING         				E	R	J	VIBRATION/BUFFET          	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	CR	CRUISE         	1			CA				1292 				9605			(CAN)  NR 1 EXHAUST VALVE FAILED.  (X)						1	L	7	2 	3R	3	R		A765    	5E1				 
1999123100025	19991231	00025	SO  	1999	12	31	CA991209045      	1	19991111	G	3222	67054003	TRUNNION        			PIPER 	PA28  	PA28R200    	7102811	SO  	LYC   	O360  	IO360C1C    	41514	EA  	HARTZL	HCC2Y	HCC2YK1     	GL  	NLG	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			3377 					L606951A	CH7499		(CAN) NOSE LANDING GEAR TRUNNION CRACKED.  SUSPECT GROUND HANDLING DAMAGE.  TRUNNION REPLACED WITH NEW  PART.						1	L	7	1 	3O	3	O		2A13    	1E10	5	C	P920	 
1999123100027	19991231	00027	CE  	1999	12	31	CA991209048      	1	19991112	G	3230	762591	RELAY           			CESSNA	441   	441         	2076020	CE  	GARRTT	TPE331	TPE3318     	01514	WP  					MLG	CORRODED        	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								P31442C			(CAN) CREW REPORTED THAT THE LANDING GEAR WARNING SYSTEM WAS INTERMITTANT BOTH OPERATIONALLY AND DURING TEST.  AFTER EXT	ENSIVE TROUBLESHOOTING, MAINTENANCE FOUND A FLASHER RELAY FOR THE LANDING GEAR WARNING CIRCUIT, LOCATED IN THE LEFT SIDE	 ELECTRICAL PANEL BESIDE THE PILOTS SEAT, FAULTY.  THE RELAY WAS INTERNALLY CORRODED AND CONTAMINATED WITH WATER WHICH L	EAKED IN THROUGH THE FOUL WEATHER WINDOW ON THE LEFT SIDE OF THE COCKPIT.			1	L	7	2 	3T	4	T	RT	A28CE   	E4WE				 
1999123100037	19991231	00037	CE  	1999	12	31	CA991209062      	1	19991129	G	5320	57111652	SUPPORT         			CESSNA	441   	441         	2076020	CE  	GARRTT	TPE331	TPE33110    	01514	WP  					DOOR STEP	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			6235 					P77673			(CAN) THE CREW REPORTED A CREAKING NOISE WHILE TREADING ON THE LOWER DOOR STEPS.   MAINTENANCE CREW DISASSEMBLED THE LOW	ER DOOR AND FOUND MULTIPLE CRACKS IN THE LOWER DOOR STEP SUPPORT STRUCTURE.					1	L	7	2 	3T	4	T	RT	A28CE   	E4WE				 
2001032000003	20010320	00003		2001	3	20	CA991210005      	4	19990111	G	3454		COMPUTER        			AMTR  	MK1   	MK1         	05620JY	GL  	LYC   	O235  	O235C       	41505	EA  					NAVIGATIONAL SYS	FAILED          	W				O		 	 	OTHER                   				O	 		OTHER                     			NR	NOT REPORTED   	1			CA											(CAN) ERRONIOUS DATA AND DATA BASE OPERATIONS IN CANADIAN AIRSPACE. ITEM IS TSO APPROVED MFG. AIRSPACE CLASSIFICATION ER	RORS, VOR / AIRPORT & ARTECC ERRORS, EMERGENCY FEATURE SHOWING WRONG INFORMATION.  ITEM ON HOLD AT SUBMITTERS REQUEST UN	TIL THE DATA HAS BEEN ANALYSED BY THE DIRECTOR OF EVENTIDE. SUBSEQUENT CORRECTIVE ACTION HAS BEEN TAKEN 2000,03,13BY THE	 MANUFACTURER. SUBMITTER WILL FOLLOW-UP.			1	H	7	1 	3O	3	O	NC	EXPA1H71	E223				 
2001030800095	20010308	00095	SW  	2001	3	8	CA991210008      	1	19991109	G	2910		HYDRAULIC LINE  			SWRNGN	SA226 	SA226AT     	8780405	SW  	GARRTT	TPE331	TPE33110    	01514	WP  					HYD SYSTEM	CONTAMINATED    	W				K	 	 	 	NONE                    				P	 	 	NO WARNING INDICATION     			CL	CLIMB          	1			CA			14555								(CAN) DURING HEAVY MAINTENANCE, NUMEROUS HYDRAULIC LINES WERE REMOVED AND REPLACED. GROUND TESTING OF HYD AND LANDING GE	AR SYSTEMS WAS CARRIED OUT. DURING THE FIRST FLIGHT AFTER MAINTENANCE, THE NOSE GEAR UP INDICATION WOULD NOT FUNCTION. M	AINTENANCE FOUND AIR IN THE HYDRAULIC SYSTEM AND AFTER SYSTEM BLEEDING THE LANDING GEAR SYSTEM FUNCTIONED NORMALLY.				2	L	7	2 	4T	4	T	RT	A5SW    	E4WE				 
2000011500559	20000115	00559	CE  	2000	1	15	CA991210018      	1	19991124	G	3242	16426A	DISC            			CESSNA	172   	172L        	2072432	CE  	LYC   	O320  	O320E2D     	41508	EA  	MCAULY	1C160	1C160CTM    	GL  	BRAKE	INCORRECT PART  	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA								L4004427A	720159		(CAN) UPON REMOVAL FROM THE WHEEL ASSY, THE BRAKE DISC WAS DETERMINED TO BE AN INCORRECT PART FOR THE WHEEL ASSY TO WHIC	H IT WAS INSTALLED. THE SUBMITTER STATED THAT THE CORRECT BRAKE DISC PART NUMBER IS 164-40 AND THAT THE ONLY PERCEPTIBLE	 DIFFERENCE IS THE DIAMETER OF THE MOUNTING BOLT HOLES.				1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
2000011500560	20000115	00560	SO  	2000	1	15	CA991210020      	1	19991112	G	3260	922AA2YA6P2722A	SENSOR          		2094010000  	EMB   	120   	EMB120ER    	3260203	SO  	PWA   	118   	PW118       		NE  	HAMSTD	14RF	14RF9       	NE  	COCKPIT	DAMAGED         	W				O				OTHER                   				J			WARNING INDICATION        			DE	DESCENT        	1			CA						0036		115283	860529		(CAN) AIRCRAFT RETURNED TO BASE WITH GEAR INDICATION PROBLEMS.  PROXIMITY SENSOR ON RT GEAR EXTENDED WITH OVERRIDE.  ON 	INVESTIGATION, PIN HOLE FOUND IN RED WIRE INSULATION ON SENSOR WITH WATER CONTAMINATION.  HEAT SHRINK WAS INSTALLED OVER	 EACH WIRE TO SOLVE PROBLEM.  WIRE VERY DIFFICULT TO ROUTE.				2	L	7	2 	4T	4	T	RT	A31SO   	E20NE	6	C	P11NE	 
2000011500561	20000115	00561	SO  	2000	1	15	CA991210022      	1	19991129	G	5712	62104001	BRACKET         			PIPER 	PA28  	PA28140     	7102802	SO  	LYC   	O320  	O320E2A     	41508	EA  	SNSNCH	74DM	M74DM       	EA  	WING	CRACKED         	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA			5663 					L1762527A	A53346		(CAN) THE CRACK WAS CREATED BY THE ATTACHMENT OF THE BRACKET ONTO THE RIB WITH AN AN3-4A BOLT.						1	L	7	1 	3O	3	O		2A13    	E274	5	N	P88614	 
2000011500562	20000115	00562	EA  	2000	1	15	CA991210023      	1	19991126	G	2910	215T7519412	LINE            			CNDAIR	CL215 	CL2156B11415		EA  	PWA   	PW120 	PW123       		NE  					HYDRAULIC SYS	CUT             	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			503  					AF0004			(CAN) DURING ANNUAL INSPECTION, AME NOTICED CHAFING BY THE SUBJECT LINE ON THE BULKHEAD.  AFTER REMOVAL OF THE PRC CAULK	ING, FOUND THAT THE REMOVABLE PART OF THE BULKHEAD TOUCHED THE LINE.  THE LATTER WAS GOUGED ALMOST 50 PERCENT IN THICKNE	SS.   LINE REPLACED AND BULKHEAD HOLE ENLARGED.				2	H	7	2 	4T	4	T	RT	A14EA   	E20NE				 
2000011500565	20000115	00565	EA  	2000	1	15	CA991210026      	1	19991018	G	3242	2604141	HOUSING         	BFGOODRICH  	2158750224  	CNDAIR	CL215 	CL2156B11415		EA  	PWA   	PW120 	PW123       		NE  					BRAKE	CRACKED         	W				K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			CA			558  			1008		109075			(CAN) AFTER A FIRE, MISSION WAS CANCELLED AND AIRCRAFT CAME BACK TO PARK, THE LEFT BRAKE STARTED TO LEAK.   A 1.1250 INC	H CRACK WAS FOUND AT THE 12 O'CLOCK POSITION THAT ORIGINATED AT THE BOLT HOLE ALLOWING HYDRAULIC FLUID TO LEAK.   AIRCRA	FT  WEIGHT WAS 4400 POUNDS.				2	H	7	2 	4T	4	T	RT	A14EA   	E20NE				 
2001030800119	20010308	00119	EA  	2001	3	8	CA991210070      	1	19991112	G	2760	4916405	CONTROL UNIT    			CNDAIR	CL600 	CL6002B19   	       	EA  										SPOILER SYS	FAILED          	W				C	 	 	 	ABORTED TAKEOFF         				F	 	 	FLT CONT AFFECTED         			TO	TAKEOFF        	1			CA											(CAN) NR1 SECU WAS GIVING THE WRONG INDICATIONS TO EICAS REGARDING SPOILER SURFACE POSITION.  SECU REPLACED.						2	L	7	2 	4F			RT	A21EA   					 
2001030800120	20010308	00120	EA  	2001	3	8	CA991210071      	1	19991109	G	7732		ENGINE          	GE          	CF343B1     	CNDAIR	CL600 	CL6002B19   	       	EA  	GE    	CF34  	CF343B1     	 	NE  					NR 2 ENGINE	VIBRATION       	W				E	A	 	 	ENGINE SHUTDOWN         	UNSCHED LANDING         			E	J	 	VIBRATION/BUFFET          	WARNING INDICATION        		CL	CLIMB          	1			CA											(CAN) DURING CLIMB OUT NR2 ENGINE VIB IND. IN CONJUNCTION WITH A VIB IN THE POWER LEVERS. ENGINE WAS SECURED AND EMERG. 	LANDING CARRIED OUT. THE VIB INDICATOR RECORDED 4.0 MILS FOR 7.6 SEC. ICING IS SUSPECTED AS COULD NOT BE DUPLICATED ON T	HE GROUND.				2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
2001030800121	20010308	00121	EA  	2001	3	8	CA991210072      	1	19991112	G	2760	270007	PCU             			CNDAIR	CL600 	CL6002B19   	       	EA  										RT SPOILER	LEAKING         	W				O	 	 	 	OTHER                   				J	K	 	WARNING INDICATION        	FLUID LOSS                		CR	CRUISE         	1			CA											(CAN) IN CRUISE, NR1 HYD SYSTEM WAS LOOSING FLUID UP TO 10% FOLLOWING TOUCH DOWN. R/H I/B FLIGHT SPOILER PCU WAS LEAKING	 BETWEEN TORQUE MOTOR AND VALVE BODY					2	L	7	2 	4F			RT	A21EA   					 
2001030900081	20010309	00081	EA  	2001	3	9	CA991210073      	1	19991113	G	2750	855D1009	BPSU            			CNDAIR	CL600 	CL6002B19   	       	EA  										RT WING	FAILED          	W				O	 	 	 	OTHER                   				J	F	 	WARNING INDICATION        	FLT CONT AFFECTED         		DE	DESCENT        	1			CA						235A					(CAN) FLAPS FAILED AT 8 DEG. R/H BPSU REPLACED						2	L	7	2 	4F			RT	A21EA   					 
2001030900082	20010309	00082	EA  	2001	3	9	CA991210074      	1	19991130	G	2750	860D10018	CONTROL UNIT    			CNDAIR	CL600 	CL6002B19   	       	EA  										FLAP	FAILED          	W				O	 	 	 	OTHER                   				F	J	 	FLT CONT AFFECTED         	WARNING INDICATION        		LD	LANDING        	1			CA											(CAN) FLAPS FAIL @ 8 DEG DURING DEPLOYMENT.						2	L	7	2 	4F			RT	A21EA   					 
2001030900088	20010309	00088	EA  	2001	3	9	CA991210080      	1	19991128	G	3234	750006000	SELECTOR VALVE  			CNDAIR	CL600 	CL6002B19   	       	EA  										NLG	MALFUNCTIONED   	W				K	 	 	 	NONE                    				J	 	 	WARNING INDICATION        			CL	CLIMB          	1			CA											(CAN) AFTER T/O, GEAR UP DISAGREE MSG WITH ALL UNSAFE DISPLAY MARKS. 15 SECS LATER NORMAL GEAR SYMBOLS ARE RECOVERED AND	 MSG GOES OUT. BEFORE LANDING GEAR DOWN DISAGREE AND NOSE MESSAGE(LOW SEQUENCE OF NOSEDOOR). NLG DOOR SELECTOR, NLG PRIO	RITY VALVE AND SWITCH D115 REPLACED.				2	L	7	2 	4F			RT	A21EA   					 
2001030900089	20010309	00089	EA  	2001	3	9	CA991210081      	1	19991128	G	2752		ACTUATOR        			CNDAIR	CL600 	CL6002B19   	       	EA  										RT FLAP	FAILED          	W				O	 	 	 	OTHER                   				F	J	 	FLT CONT AFFECTED         	WARNING INDICATION        		AP	APPROACH       	1			CA											(CAN) FLAP FAIL MESSAGE AND FLAP STOPPED @ 24 DEG. RH NR1,2 AND 3 ACTUATORS REPLACED.						2	L	7	2 	4F			RT	A21EA   					 
2001030900090	20010309	00090	EA  	2001	3	9	CA991210082      	1	19991120	G	4900		UNKNOWN         			CNDAIR	CL600 	CL6002B19   	1900309	EA  	GE    	CF34  	CF343A      	30015	NE  					COCKPIT	SMOKE           	W				G	A			O2 MASK DEPLOYED        	UNSCHED LANDING         			B			SMOKE/FUMES/ODORS/SPARKS  			CL	CLIMB          	1			CA											(CAN) AFTER T/O THE CREW OBSERVED AND SMELLED SMOKE IN FLIGHT COMPARTMENT. O2 MASKS DROPPED AND RTB. SUSPECTED DEICING F	LUID IN ENGINES OR APU					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
2001030900091	20010309	00091	EA  	2001	3	9	CA991210083      	1	19991120	G	2750		FLAP            			CNDAIR	CL600 	CL6002B19   	       	EA  										WING	FAILED          	W				O	 	 	 	OTHER                   				F	J	 	FLT CONT AFFECTED         	WARNING INDICATION        		AP	APPROACH       	1			CA											(CAN) ON FINAL APPROACH, FLAPS FAILED AND STOPPED AT 40 DEG						2	L	7	2 	4F			RT	A21EA   					 
2001030900092	20010309	00092	EA  	2001	3	9	CA991210084      	1	19991120	G	2752	852D10011	ACTUATOR        			CNDAIR	CL600 	CL6002B19   	       	EA  										LT FLAP	MALFUNCTIONED   	W				O	 	 	 	OTHER                   				F	J	 	FLT CONT AFFECTED         	WARNING INDICATION        		AP	APPROACH       	1			CA						963A					(CAN) ON APPROACH, FLAPS FAILED UPON SELECTION TO 8 DEG. FLAPS STAYED AT 0 DEG. 33 ACTUATOR L/H REPLACED FOR TORQUE TEST	.					2	L	7	2 	4F			RT	A21EA   					 
2001030900094	20010309	00094	NE  	2001	3	9	CA991210086      	2	19991120	G	7200		ENGINE          	GE          	CF343B1     	CNDAIR	CL600 	CL6002B19   	       	EA  	GE    	CF34  	CF343B1     	 	NE  					NR 2 ENGINE	VIBRATION       	W				E	 	 	 	ENGINE SHUTDOWN         				E	J	 	VIBRATION/BUFFET          	WARNING INDICATION        		CL	CLIMB          	1			CA						807420					(CAN) HIGH VIBS EXPERIENCED ALONG WITH LOW OIL PX AND RAPIDLY REDUCING N2.REPORT REQUIRED.PROJECT NR20000014. FOREIGN AC	 FSR REPORT NOT RECEIVED.					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
2001030900097	20010309	00097	EA  	2001	3	9	CA991210089      	1	19991120	G	2750		FLAP            			CNDAIR	CL600 	CL6002B19   	       	EA  										WING	FAILED          	W				O	 	 	 	OTHER                   				F	J	 	FLT CONT AFFECTED         	WARNING INDICATION        		AP	APPROACH       	1			CA											(CAN) ON APPROACH FLAPS DID NOT MOVE FROM 0 DEG WHEN SELECTED TO 20 DEG WITH FLAP FAIL MESSAGE. SYSTEM RESET.						2	L	7	2 	4F			RT	A21EA   					 
2001030900099	20010309	00099	EA  	2001	3	9	CA991210094      	2	19991122	G	8520		PLUG            	LYC         	O320H2AD    	CESSNA	172   	172N        	2072434	CE  	LYC   	O320  	O320H2AD    	41508	EA  					CRANKSHAFT	LEAKING         	W				A	 	 	 	UNSCHED LANDING         				K	 	 	FLUID LOSS                			CL	CLIMB          	1			CA			1691 			L386576					(CAN) FOUND CRANKSHAFT PLUG INSTALLED INCORRECTLY CAUSING LOSS OF OIL.						1	H	7	1 	3O	3	O	NT	3A12    	E274				 
2001030900101	20010309	00101	NE  	2001	3	9	CA991210097      	2	19991110	G	7260	3040190	CASE            	PWA         	PW118       						PWA   	118   	PW118       	 	NE  					ENGINE	CRACKED         	W				K	 	 	 	NONE                    				K	 	 	FLUID LOSS                			IN	INSP/MAINT     	1			CA						115110					(CAN) ENGINE TEST OIL FOUND TO BE LEAKING FROM THE REAR INLET CASE. ETR NR0186, PROJECT NR 20000013. 4 CONFIRMED EVENTS 	ON PW118 AVERAGING 20000 HRS AND 6 EVENTS ON PW123 ENGINES AVERAGING 11000 HRS. FATIGUE IS RESULTING FROM A LOCAL UNDER 	RADIUS AT THE JUNCTION REFER TO REPORT TC1280/1301. PWC IS PLANNING TO INSTUMENT AN ENGINE TO BETTER UNDERSTAND THE PHEN	OMENON.								4	T			E20NE				 
2001030900117	20010309	00117	CE  	2001	3	9	CA991229016      	1	19991212	G	3220	NAS464P5A42	BOLT            	CESSNA      	12436001    	CESSNA	206   	U206G       	2073356	CE  	CONT  	O520  	IO520F      	17032	SO  	MCAULY	D3A34	D3A34C404   	GL  	NLG DRAG STRUT	BROKEN          	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) DURING 100 HOUR INSPECTION, MAINTENANCE PERSONNEL CHECKED THE BOLT AT THE AFT END OF THE NOSE GEAR DRAG STRUT, WIT	H A WRENCH. LIGHT PRESSURE FRACTURED THE BOLT HEAD FROM THE SHANK. THE SUBMITTER HAS FOUND A NUMBER OF THESE BOLT HEADS 	BROKEN OFF IN VARIOUS C206 AIRCRAFT, AND ROUTINELY CHECKS THEM FOR DAMAGE AND MISSING BOLT HEADS.				1	H	7	1 	3O	3	O	 	A4CE    	E5CE	5	C	P47GL	 
2001030900118	20010309	00118	CE  	2001	3	9	CA991229017      	1	19990921	G	5753	0523920	ROLLER          	CESSNA      		CESSNA	172   	172M        	2072418	CE  	LYC   	O320  	O320E2D     	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	LT FLAP	SEIZED          	W				O	 	 	 	OTHER                   				F	 	 	FLT CONT AFFECTED         			AP	APPROACH       	1			CA			1498 								(CAN) A SEIZED FLAP ROLLER DEVELOPED A FLAT SPOT, CAUSING IT TO BIND IN THE FLAP TRACK, RESULTING IN FLAP SYSTEM MALFUNC	TION.					1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
2001030900122	20010309	00122	EA  	2001	3	9	CA991229021      	1	19991203	G	2841		FUEL LINE       			DHAV  	DHC2  	DHC2MK1     	2800102	EA  	PWA   	R985  	R985AN14B   	52008	NE  					QUANTITY IND	CRACKED         	W				K	 	 	 	NONE                    				K	 	 	FLUID LOSS                			IN	INSP/MAINT     	1			CA											(CAN) FUEL PRESSURE LINE FROM FIREWALL TO GAGE. ONE END FITTING CRACKED RESULTING IN A FUEL LEAK IN THE COCKPIT. FUEL SM	ELL WAS NOTED BY THE PILOT ON LASTTRIP. LINE REPLACE BEFORE FURTHER FLIGHT. THIS PROBLEM & SAFETY ISSUE WAS BROUGHT UP 2	 YRS AGO. ALT FUEL PRESS IND STC ARE AVAILABLE IN THE US.				1	H	7	1 	3R	3	R	 	A806    	5E1				 
2001030700611	20010307	00611	NM  	2001	3	7	CA991229026      	1	19991214	G	2433		COOLING FAN     			DHAV  	DHC8  	DHC8202     	2809007	NM  										TRU	INOPERATIVE     	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) TRU COOLING FAN FOUND INOPERATIVE AT C CHECK						2	H	7	2 	4T			RT	A13NM   					 
2001030700612	20010307	00612	NM  	2001	3	7	CA991229027      	1	19991214	G	2433		COOLING FAN     			DHAV  	DHC8  	DHC8202     	2809007	NM  										TRU	INOPERATIVE     	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) TRU COOLING FAN FOUND INOPERATIVE AT C CHECK						2	H	7	2 	4T			RT	A13NM   					 
2001030700613	20010307	00613	NM  	2001	3	7	CA991229028      	1	19991214	G	2433		COOLING FAN     			DHAV  	DHC8  	DHC8*       	       	NM  										TRU	INOPERATIVE     	W				K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) TRU COOLING FAN FOUND INOPERATIVE AT C CHECK						2	H	7	2 	4T			RT	A13NM   					 
2001030900124	20010309	00124	EU  	2001	3	9	CA991229029      	1	19991210	G	3240	819804484	SLEEVE          		S256UM50001A	BRAERO	DH125 	HS125700A   	4230170	EU  										BRAKE SYSTEM	CORRODED        	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			5741 								(CAN) DURING PREFLIGHT MAINT PERSONNEL OBSERVED BRAKE HOSE EXTERNAL COVERING DISCOLORED AND SWOLLEN. INSPECTION REVEALED	 SLEEVE HOLDING FITTING ON HOSE SEVERLY CORRODED RESULTING IN A HYD LEAK.					2	L	7	2 	4F			 	A3EU    					 
2001030900128	20010309	00128	SW  	2001	3	9	CA991229036      	1	19991203	G	5610	2621126008	WINDSHIELD      	SWRNGN      		SWRNGN	SA227 	SA227AC     	8780603	SW  	GARRTT	TPE331	TPE3311U    	01514	WP  					COCKPIT	CRACKED         	W				O	 	 	 	OTHER                   				O	 	 	OTHER                     			CR	CRUISE         	1			CA			21365								(CAN) DURING CRUISE FLIGHT, A LOUD BANG WAS HEARD AND THE COPILOTS WINDSHIELD INNER PANE SHATTERED						2	L	7	2 	4T	3	T	RT	A8SW    	E3WE				 
2001030900130	20010309	00130	GL  	2001	3	9	CA991229038      	3	19991210	G	6110		PROPELLER       	MCAULY      	D2AF34C305  											MCAULY	2AF34C	D2AF34C305  	GL  	ENGINE	CORRODED        	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA				14   		832454					(CAN) PROPELLOR SEIZED DUE TO CORROSION																5	C	P5EA	 
2001032000011	20010320	00011	GL  	2001	3	20	CA991229045      	1	19991205	G	2710	620075	BOOT            			DIAMON	DA20  	DA20A1      	       	GL  										COCKPIT	LOOSE           	W				D	 	 	 	RETURN TO BLOCK         				F	 	 	FLT CONT AFFECTED         			TX	TAXI/GRND HDL  	1			CA											(CAN) DURING  PRE-FLIGHT WALK AROUND THE PILOT NOTICED THAT THE AILERON TRAVELS WERE NOT EQUAL ON THE LEFT AND RIGHT.IT 	WAS FOUND THAT THE BOOT AT THE BASE OF THE CONTROL STICK HAD MIGRATED DOWN AND SNAP FASTENERS AT THE TOP OF THE BOOT HAD	 LODGED BETWEEN THE CONTROL STICK AND THE SEAT PAN.THE BOOT WAS REPOSITIONED AND SECURED WITH A TIE WRAP.				1	L	7	1 	3O			NT	TA4CH   					 
2001032000020	20010320	00020	CE  	2001	3	20	CA991229055      	1	19991124	G	2810	0523522	STRAP           			CESSNA	172   	172L        	2072432	CE  	LYC   	O320  	O320E2D     	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	FUEL TANK	BROKEN          	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			8410 								(CAN) UPON FUEL TANK REMOVAL, THE REAR FUEL TANK STRAP WAS FOUND BROKEN.						1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
2001032000021	20010320	00021	CE  	2001	3	20	CA991229057      	1	19991213	G	3710		COUPLING        			CESSNA	177   	177B        	2073708	CE  	LYC   	O360  	O360A1F6    	41514	EA  					VACUUM PUMP	FAILED          	W				O	 	 	 	OTHER                   				J	 	 	WARNING INDICATION        			CR	CRUISE         	1			CA			739  								(CAN) DURING CRUISE FLIGHT, THE VACUUM SYSTEM FAILED. MAINTENANCE FOUND THE VACUUM PUMP FAILED AT THE DRIVE COUPLING.						1	H	7	1 	3O	3	O	 	A13CE   	E286				 
2001032000022	20010320	00022	CE  	2001	3	20	CA991229058      	1	19991204	G	2821	710C4X	DRAIN VALVE     			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  					FUEL FILTER	MISSING         	W				E		 	 	ENGINE SHUTDOWN         				K	R	J	FLUID LOSS                	PARTIAL RPM/PWR LOSS      	WARNING INDICATION        	AP	APPROACH       	1			CA											(CAN) ON APPROACH THE RT ENGINE LOST PARTIAL POWER AND THEN FLAMED OUT COMPLETELY.  PILOT NOTICED FLUCTUATING FUEL FLOW 	AND SELECTED STANDBY PUMP ON. AT THIS POINT THE PILOT NOTICED MINIMUM FUEL IN RT MAINTANK.INSPECTION FOUNDTHAT THE VALVE	 ASSEMBLY IS SWAGED INTO THE BODY OF THE FUEL FILTER.THE VALVE ASSEMBLY WAS MISSING AT THE POINT WHERE IT SHOULD HAVE BE	EN SWAGED. THIS CAUSED A RAPID LOSS OF FUEL FROM THE RT FUEL TANK WHICH LED TO FLAME- OUT.			1	L	7	2 	4T	4	T	 	A24CE   	E4EA				 
2001032000023	20010320	00023	CE  	2001	3	20	CA991229059      	1	19991207	G	2120	HE7019	VALVE           			BEECH 	200   	200BEECH    	1152920	CE  	PWA   	PT6   	PT6A41      	52043	EA  	MCAULY	4HFR34	4HFR34C754  	NE  	AIR DISTRIBUTION	WORN            	W				A	 	 	 	UNSCHED LANDING         				J	 	 	WARNING INDICATION        			CR	CRUISE         	1			CA											(CAN) BLEED AIR DETECT LIGHT CAME ON.  DUCT UNDER CABIN FLOOR FOUND WITH HOLES WORN IN SIDE WALL DUE TO INTERNAL CHAFING	 OF CHECK VALVE.					1	L	7	2 	4T	4	T	 	A24CE   	E4EA	6	C	3PNE	 
2001032000030	20010320	00030	CE  	2001	3	20	CA991229069      	1	19991124	G	2810	0526007203	FILLERCAP       			CESSNA	172   	172L        	2072432	CE  	LYC   	O320  	O320E2D     	41508	EA  	MCAULY	1C160	1C160DTM    	GL  	FUEL CELL	CRACKED         	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			8410 								(CAN)  DURING INSPECTION, MAINTENANCE NOTICED THE FUEL TANK FILLER NECK SEEMED TO FLEX MORE THAN NORMAL. AFTER TANK REMO	VAL THE FILLER NECK WAS FOUND TO BE SEALED TO THE TANK WITH AN UNSPECIFIED SEALING COMPOUND. THE SEALER WAS REMOVED, REV	EALING THE NECK TO BE CRACKED AROUND ITS ENTIRE CIRCUMFERENCE.				1	H	7	1 	3O	3	O	NT	3A12    	E274	5	N	P910	 
2001032000040	20010320	00040	CE  	2001	3	20	CA991230015      	1	19991119	G	2710	671109349	SCREW           			CESSNA	750   	750         	2076810	CE  										AILERON CABLES	OUT OF POSITION 	W				O	 	 	 	OTHER                   				F	 	 	FLT CONT AFFECTED         			AP	APPROACH       	1			CA			584  								(CAN) THE FLGHT CREW WAS REQUESTED TO TURN RIGHT BY ATC AND FOUND THE AILERON CONTROLS JAMMED. AFTER TRYING TO MANEUVER 	THE AIRCRAFT, THE CONTROLS RETURNED TO NORMAL WITH A LOUD SNAP. MAINTENANCE FOUND THE LOCK SCREW AND NUT ASSEMBLY, SECUR	ING THE AILERON CABLE ADJUSTMENT BARREL TO BE INTERFERING WITH THE UNDER FLOOR WEB LIGHTENING HOLE EDGE. THE SCREW HAD B	EEN ABLE TO ROTATE OUT OF POSITION DUE TO LOOSE AILERON CABLES			2	L	7	2 	4J			RT	T00007WI					 
2001032000042	20010320	00042	EU  	2001	3	20	CA991230017      	1	19991205	G	2440	LOG15074	RELAY           			BRAERO	DH125 	HS125700A   	4230170	EU  										GROUND POWER	FAILED          	W				O	 	 	 	OTHER                   				H	 	 	ELECT. POWER LOSS-50 PC   			TX	TAXI/GRND HDL  	1			CA						1418					(CAN) AFTER EXTENDED GPU USE THE GROUND POWER RELAY FAILED.						2	L	7	2 	4F			 	A3EU    					 
2001032000049	20010320	00049	EA  	2001	3	20	CA991230026      	2	19991213	G	8550		ENGINE          			MOONEY	M20   	M20J        	5870219	SW  	LYC   	O360  	IO360A3D6D  	41514	EA  	MCAULY	2D34C	B2D34C214   	GL  	FORWARD	FAILED          	W				A	 	 	 	UNSCHED LANDING         				K	 	 	FLUID LOSS                			NR	NOT REPORTED   	1			CA				810  							(CAN) REPAIRED ENGINE INSTALLED AND AC FLOWN WHEN SHORTLY AFTER T/O LOSS OF OIL PRESSURE WAS NOTED. REPORT TO FOLLOW.  R	EAR BEARING DAMAGED, POSSIBLY AT REPAIR.					1	L	7	1 	3O	3	O	 	2A3     	1E10	5	C	P7EA	 
2001032100011	20010321	00011	SO  	2001	3	21	CA991230039      	2	19991218	G	8530	629404	EXHAUST VALVE   	CONT        	O200A       	CESSNA	150   	150M        	2071830	CE  	CONT  	O200  	O200A       	17020	SO  	MCAULY	1A102	1A102OCM    	GL  	NR 3 CYLINDER	STUCK           	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			1100 			253620A					(CAN) NR 3 CYLINDER LOW COMPRESSION THE EXHAUST VALVE WAS FOUND TO BE PARTIALLY STUCK AND BURNED.						1	H	7	1 	3O	3	O	 	3A19    	E252	5	N	P918	 
2001032100013	20010321	00013	CE  	2001	3	21	CA991230041      	1	19991215	G	7712	26060113RX	INDICATOR       			CESSNA	208   	208B        	2073701	CE  	PWA   	PT6   	PT6A114A    	52043	NE  					COCKPIT	DAMAGED         	W				O	 	 	 	OTHER                   				O	 	 	OTHER                     			CR	CRUISE         	1			CA				100  		MD823					(CAN) THE PILOT REPORTED THAT THE ENGINE TORQUE INDICATOR GAUGE SLOWLY FILLED WITH OIL DURING FLIGHT.						1	H	7	1 	3T	3	T	 	A37CE   	E4EA				 
2001032100020	20010321	00020	EA  	2001	3	21	CA991231001      	1	19991102	G	2420	N7118051	RAM AIR TURB    			CNDAIR	CL600 	CL6002B19   	       	EA  	GE    	CF34  	CF343A1     	30015	NE  					AUX POWER	FAILED          	W				K	 	 	 	NONE                    				L	 	 	NO TEST                   			IN	INSP/MAINT     	1			CA			7    								(CAN) DURING PRODUCTION FLT. ADG WOULD NOT DEPLOY IN FLIGHT. BLADES WERE FOUND STUCK BETWEEN THE FUSELAGE AND ADG DOOR. 	NOT PROPERLY STOWED.					2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
2001032100023	20010321	00023	EA  	2001	3	21	CA991231004      	1	19991201	G	5530		ANGLE           			FRCHLD	F27   	F27F        	3373008	EA  	RROYCE	DART  	DART5297E   	54507	EU  					VERTICAL STAB	CRACKED         	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA			35565								(CAN) DURING INSPECTION CARRIED OUT IAW AD 64-21-04, CRACK WAS FOUND ON THE REINFORCEMENT ANGLE AT THE AFT END OF THE RI	B AT W.L. 201.575					2	H	7	2 	4T	4	T	 	7A1     	E297				 
2001032100060	20010321	00060	EA  	2001	3	21	CA991231049      	1	19991217	G	7931		ENGINE          	GE          		CNDAIR	CL600 	CL6002B19   	       	EA  	GE    	CF34  	CF343B1     	 	NE  					NACELLE	MALFUNCTIONED   	W				E	 	 	 	ENGINE SHUTDOWN         				J	 	 	WARNING INDICATION        			AP	APPROACH       	1			CA											(CAN) FOREIGN OPERATED A/C, NO OIL PX READING IFSD COMPLETED, PROBLEM NOT YET IDENTIFIED.						2	L	7	2 	4F	4	F	RT	A21EA   	E15NE				 
2001032800214	20010328	00214	EA  	2001	3	28	CA991231065      	2	19991126	G	8530	SL12596	BOLT            	LYC         	LW10646     						LYC   	O540  	TIO540A2B   	41532	EA  					CONNECTING ROD	FAILED          	W				K	 	 	 	NONE                    				O	 	 	OTHER                     			IN	INSP/MAINT     	1			CA											(CAN) HEAD OF CONNECTING ROD BOLT FOUND IN SUM AFTER TEST RUN. ALL OTHER BOLTS WERE FOUND TO HAVE PROPER TORQUE. ALL BOL	TS REPLACED.										3	O			E14EA				 
2001032800220	20010328	00220	WP  	2001	3	28	CA991231066      	2	19991212	G	7321	89777011	FUEL CONTROL    			GULSTM	690TP 	690D        	3970405	SW  	GARRTT	TPE331	TPE3315     	01514	WP  	ROTOL	R306	R306382F7   	GL  	ENGINE	LEAKING         	W				D	 	 	 	RETURN TO BLOCK         				K	 	 	FLUID LOSS                			TX	TAXI/GRND HDL  	1			CA				1694 							(CAN) FUEL CONTROL LEAKING BEYOND ALLOWABLE LIMITS FROM DRAIN MAST.						1	H	7	2 	3T	4	T	 	2A4     	E4WE	6	C	P8EU	 
1999111100126	19991111	00126	NE  	1999	11	11	CHIR3488         	2	19990816	G	7200	114D32463	DRIVESHAFT      		414D32117   	BOEING	234   	234         	1385049	EA  	LYC   	AL5512	AL5512      	41581	NE  					ENGINE	CRACKED         	B			CHIR	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	238CH	1569 			A2409	MJ005				TWO CRACKS IN OUTBOARD ADAPTER END.  CRACKS GO THROUGH AN OUTBOARD RIVET HOLE AND EXTEND AT A 45 DEGREE ANGLE INBOARD AN	D OUTBOARD TO THE ADAPTER EDGE.  P/N 114D3204-3 ADAPTER END.  (X)					2	G	7	2 	4U	4	U		H9EA    	E4NE				 
1999040200490	19990402	00490	SW  	1999	4	2	CZMA061352       	1	19990325	G	3110	214175122111	PANEL           			BELL  	412   	412         	1182202	SW  										COCKPIT	SHORTED         	E			CZMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SO	03	911BE	44   				36018				EXCHANGE PANEL SHORTED AND FAILED DURING A PREFLIGHT CAUTION LIGHT TEST.  UNIT WAS INSTALLED FOR A TOTAL OF 43.5 HRS AND	 21 DAYS.  INSTALLED ORIGINAL PANEL THAT WAS PRESENT WHEN AIRCRAFT WAS PURCHASED.					1	G	7	2 	4U				H4SW    					 
2003010300013	20030103	00013	SW  	2003	1	3	CZMA082747       	1	19990609	G	5302	NAS62826	BOLT            		212030100147	BELL  	412   	412         	1182202	SW  										TAIL BOOM	BROKEN          	E			CZMA	A				UNSCHED LANDING         				O			OTHER                     			CR	CRUISE         	1			SO	03	412BE	9850 			ADW06035	33036				UPPER LEFT TAILBOOM ATTACH BOLT SNAPPED DURING CRUISE/DESCENT FLIGHT. REMOVED T/B, INSPECTED AIRFRAME AND T/B ATTACH POI	NTS FOR ALIGNMENT, ZYGLOED FITTINGS, REPLACED ALL BOLTS					1	G	7	2 	4U			 	H4SW    					 
2003010300015	20030103	00015	SW  	2003	1	3	CZMA082749       	1	19990628	G	6220	412010190105	SPINDLE         		412010100127	BELL  	412   	412         	1182202	SW  										ROTOR HEAD	DEFECTIVE       	E			CZMA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SO	03	911BE	4857 			A1542	36018				BLADE TRACKING ABOUT 2 FT TO LOW REPLACED SPINDLE ASSY WHICH WAS INCORRECTLY MANUFACTURED						1	G	7	2 	4U			 	H4SW    					 
2000061400226	20000614	00226	WP  	2000	6	14	EIA990295        	1	19991025	G	5330	941530611	SKIN            			DOUG  	DC9   	DC933F      	302207A	WP  										FUSELAGE	DAMAGED         	A			EIAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	09	941F					47193				MZJ - FUSELAGE SKIN REPAIR AT STATION 737 BETWEEN L16-19 RIGHT SIDE ECRA 941-53-061-2 REV A ISSUED.  COMPLIED WITH ECRA 	941-53-061-2 REV A.  FABRICATE DOUBLER/FINGER DOUBLERS, AND INSTALL PER ECRA.  (M)					2	L	7	2 	4F			 	A6WE    					 
2000012200652	20000122	00652	NM  	2000	1	22	EISA99223        	1	19991112	G	5753		SKIN            			BOEING	727   	727225      	1384077	NM  										TE FLAP	GOUGED          	A			EISA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	07	353PA					20622				ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD REVEALED A GOUGE ON LEADING EDGE OF LEFT INBOARD TRAILING EDGE FLAP.  BLENDE	D GOUGE PER SRM 51-10-1.  FABRICATED AND INSTALLED REPAIR DOUBLER  PER SRM 51-40-2.    TT:  65,345:17 HOURS.  TC:  43,81	6.  (X)				2	L	7	3 	4F				A3WE    					 
1999022600374	19990226	00374		1999	2	26	ERAA060582       	4	19990106	G	2211	4033089901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AUTOFLIGHT	MALFUNCTIONED   	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	421EH					33067				UNIT CAUSES PITCH-UP WHEN ALT MODE IS SELECTED.						1	G	7	2 	4U				H4SW    					 
1999022600375	19990226	00375		1999	2	26	ERAA060583       	4	19990106	G	3416	4004437903	ALTIMETER       			BELL  	412   	412         	1182202	SW  										COCKPIT	INOPERATIVE     	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	421EH					33067				RADAR ALTIMETER HAS NO POWER.						1	G	7	2 	4U				H4SW    					 
1999022600376	19990226	00376		1999	2	26	ERAA060584       	4	19990106	G	3454	6221239011	RECEIVER        			SKRSKY	S61   	S61N        	8142104	NE  										COCKPIT	MALFUNCTIONED   	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	563EH					61808				NAV RECEIVER UNIT HAS 54 CYCLES, REMAINS IN G/S WHEN SWITCHED TO GPS.						2	G	7	2 	4U				1H15    					 
1999022600377	19990226	00377	NE  	1999	2	26	ERAA060585       	1	19990111	G	2432	27515002	BATTERY         			SKRSKY	S61   	S61N        	8142104	NE  										E/E BAY	THERMAL RUNAWAY 	H			ERAA	O				OTHER                   				M	J		OVER TEMP                 	WARNING INDICATION        		NR	NOT REPORTED   	1			AL	03	561EH	185  				61471				BATTERY WITH ONLY 184.9 HOURS WENT THERMAL WHILE INSTALLED ON AIRCRAFT.  CELLS 2, 3, 4, 5, 6, 8, AND 13 (THERMAL RUNAWAY	) MELTED.					2	G	7	2 	4U				1H15    					 
1999022600378	19990226	00378		1999	2	26	ERAA060586       	1	19990113	G	6320	4638302024	BEARING         																	M/R GEARBOX	FAILED          	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03										NEW BEARING THAT HAS ROLLER FALLING OUT OF CAGE.																			 
1999022600379	19990226	00379		1999	2	26	ERAA060589       	4	19990119	G	3416	4004437903	ALTIMETER       			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	177EH					33037				RT-220 REPAIRED REF NR 278189.   OFF FLAG COMES ON IN-FLIGHT.						1	G	7	2 	4U				H4SW    					 
1999022600388	19990226	00388	SW  	1999	2	26	ERAA060591       	1	19990127	G	6320	412040123101	QUILL ASSY      			BELL  	412   	412         	1182202	SW  										TRANSMISSION	WORN            	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	169EH	1373 				33064				THE FOUR BOLTS HOLDING THE BEARING RETENTION PLATE IN PLACE LOST TORQUE AND BECAME VERY LOOSE WITH ONLY THE SAFETY WIRE 	HOLDING THEM IN PLACE.  THIS ALLOWED THE BEARING TO SPIN CAUSING DAMAGE TO THE INSIDE OF THE SLEEVE ASSY.					1	G	7	2 	4U				H4SW    					 
1999022600380	19990226	00380		1999	2	26	ERAA060592       	2	19990127	G	7261	23035102	HOUSING         																	OIL FILTER	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03										NEW  OIL FILTER HOUSING REJECTED UPON RECEIVING DUE TO NOT BEING PROPERLY SEATED. (AS MARKED ON PART.)																			 
1999022600381	19990226	00381		1999	2	26	ERAA060593       	4	19990127	G	2210	4025008918	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	MALFUNCTIONED   	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	417EH					33031				HP COMPUTER SENT FOR REPAIR.  REF NR 287249 9-15-99.  AFTER BEING ON AIRCRAFT 344.2  HOURS, PROBLEM WITH  YAW CHANNEL KI	CKING .					1	G	7	2 	4U				H4SW    					 
1999022600382	19990226	00382	GL  	1999	2	26	ERAA060596       	2	19990129	G	7250	23062750	NOZZLE SHIELD   			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					NR 1	CRACKED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	152EH	1674 				S701				NR 1 NOZZLE SHIELD WITH ONLY 1673.6 HOURS SINCE NEW HAS A CRACKED DOME.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999022600383	19990226	00383		1999	2	26	ERAA060597       	2	19990201	G	7313	47073	SPRAY TIP       			BOLKMS	105   	BO105S      	5626006	EU  										FUEL NOZZLE	DAMAGED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	131EH					595				NEW METER SET ISSUED TO 131EH, BUT COULD NOT BE USED DUE TO DENT ON ORIFICE RIM; STREAKS.						1	G	7	2 	3U				H3EU    					 
1999022600384	19990226	00384		1999	2	26	ERAA060599       	2	19990201	G	7250	6886407	WHEEL           			BOLKMS	105   	BO105S      	5626006	EU  										FIRST STAGE	CRACKED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	152EH	713  				S701				NR 1 WHEEL INSTALLED AND REMOVED FROM AIRCRAFT DUE TO BLADE STRETCH.  PLATFORM CRACK INTO BLADE RADIUS.						1	G	7	2 	3U				H3EU    					 
1999022600385	19990226	00385	GL  	1999	2	26	ERAA060600       	2	19990201	G	7250	6898782	WHEEL           			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					SECOND STAGE	PITTED          	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	152EH	713  				S701				NR 2 WHEEL INSTALLED AND REMOVED FROM AIRCRAFT 9-14-99 DUE TO PITTS AND FLAKING ON BLADES.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999022600389	19990226	00389		1999	2	26	ERAA060601       	1	19990204	G	6320	205040233101	SPUR GEAR       																	GEARBOX	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03										NEW GEAR THAT HAS TWO TEETH WITH MANUFACTURING DEFECT.																			 
1999040200439	19990402	00439		1999	4	2	ERAA061002       	1	19990210	G	6410	10531980	BLADE           																	TAIL ROTOR	MISOVERHAULED   	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03		1645 								RECEIVED REPAIRED FROM AEC AND BLADES WILL NOT BALANCE.																			 
1999040200437	19990402	00437		1999	4	2	ERAA061004       	4	19990218	G	3455	066107700	RECEIVER        			SKRSKY	S76   	S76A        	8143006	NE  										ADF	INOPERATIVE     	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	577EH					760222				RECEIVER UNIT REPAIRED 12-4-98.  UNIT INSTALLED ON AIRCRAFT AND WAS REMOVED 02-05-99 INOPERABLE WITH NO DISPLAY.						1	G	7	2 	3U				H1NE    					 
1999040200438	19990402	00438		1999	4	2	ERAA061005       	4	19990218	G	3444	7001840903	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	MISOVERHAULED   	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	419EH					33043				TRANSCEIVER UNIT REPAIRED  10-1-98 AND INSTALLED ON AIRCRAFT.   UNIT FAILS TO PULL FLAGS.						1	G	7	2 	4U				H4SW    					 
1999050700184	19990507	00184		1999	5	7	ERAA061843       	4	19990303	G	2210	7000299901	CONTROLLER      			BELL  	412   	412         	1182202	SW  										AUTOPILOT	MISOVERHAULED   	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	167EH	9523 				33089				CONTROLLER UNIT WAS REPAIRED 1-19-99 REF NR 298713.  WHEN INSTALLED ON AIRCRAFT, WOULD NOT SWITCH TO SAS MODE WHEN IN HP	I ONLY.					1	G	7	2 	4U				H4SW    					 
1999050700185	19990507	00185		1999	5	7	ERAA061844       	4	19990304	G	3416	1901350000	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MISREPAIRED     	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	423EH					S543				RADAR ALTIMETER  REPAIRED 1-11-99.  WAS INSTALLED AND HAD TO BE REMOVED FROM AIRCRAFT BECAUSE IT INDICATES BETWEEN 8-9 F	EET SETTING ON GROUND.					1	G	7	2 	3U				H3EU    					 
1999050700186	19990507	00186		1999	5	7	ERAA061846       	4	19990310	G	3416	1901350000	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MISREPAIRED     	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	296EH					S849				RADAR ALTIMETER RETURNED FROM REPAIR 1-27-99.  HAD TO REMOVE AFTER INSTALLING ON AIRCRAFT BECAUSE READING WAS ERRATIC AB	OVE 1,000 FEET.					1	G	7	2 	3U				H3EU    					 
1999050700187	19990507	00187		1999	5	7	ERAA061847       	4	19990310	G	3416	1901350000	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	298EH					S845				NEW  RADAR ALTIMETER INSTALLED ON AIRCRAFT WITH ONLY 2.3 HOURS AND GIVES FALSE INDICATION.						1	G	7	2 	3U				H3EU    					 
1999050700188	19990507	00188		1999	5	7	ERAA061848       	4	19990310	G	3416	1901304000	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	125EH					S562				NEW RADAR ALTIMETER INDICATOR THAT COULD NOT BE INSTALLED ON AIRCRAFT BECAUSE TEST SWITCH IS BROKEN OFF.						1	G	7	2 	3U				H3EU    					 
1999050700189	19990507	00189	GL  	1999	5	7	ERAA061849       	2	19990311	G	7230	6851574	SCROLL          								ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	CORRODED        	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03										SCROLL ASSEMBLY WAS SENT AS EXCHANGE UNIT ON AERO PROPULSION JOB NR 6514.  ASSEMBLY HAS EXCESSIVE CORROSION.											3	U			E4CE				 
1999050700190	19990507	00190		1999	5	7	ERAA061850       	1	19990316	G	3212	412050017101	COVER           																	FLOAT	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03										FLOAT COVER  MISSING TWO RUBBER BAND ATTACHMENT TABS.																			 
1999050700191	19990507	00191		1999	5	7	ERAA061851       	4	19990316	G	3416	1901350000	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	131EH					S595				ALTIMETER IS  UNRELIABLE.						1	G	7	2 	3U				H3EU    					 
1999050700192	19990507	00192		1999	5	7	ERAA061852       	4	19990316	G	3431	066107800	RECEIVER        			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT NAV	MALFUNCTIONED   	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	576EH					760212				UNIT RECEIVER ORIGINAL WITH AIRCRAFT WHEN PURCHASED.  KNR634 CAUSES DME TO CYCLE.						1	G	7	2 	3U				H1NE    					 
1999050700193	19990507	00193	NE  	1999	5	7	ERAA061854       	1	19990319	G	2820	3007T2	LINE            			SKRSKY	S61   	S61N        	8142104	NE  										FUEL SYSTEM	TWISTED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	561EH					61471				FUEL PURIFIER TO FUEL PUMP FUEL LINE TWISTED AND CRIMPED.						2	G	7	2 	4U				1H15    					 
1999050700194	19990507	00194	GL  	1999	5	7	ERAA061855       	2	19990323	G	7250	6879879	COLLECTOR       			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	151EH					S706				FOURTH TIP PATH AREA OUT OF ROUND ON EXHAUST COLLECTOR.  UNDERSIZED.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999050700195	19990507	00195	NE  	1999	5	7	ERAA061856       	2	19990323	G	7323	25249994	GOVERNOR        			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					POWER SECTION	MISOVERHAULED   	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	421EH	13579				33067				GOVERNOR OVERHAULED 11-12-98.  ENGINE TORQUE SURGING AT LOW POWER.						1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999050700196	19990507	00196		1999	5	7	ERAA061857       	1	19990323	G	3212	D24922117	FLOAT BAG       																	EMERGENCY FLOAT	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03										NEW FLOAT BAG RECEIVED 3-01-99 WITH CHECK VALVES BACKWARDS.  THEY ARE IN THE WRONG PLACE AND NEED TO BE SWITCHED.																			 
1999050700197	19990507	00197		1999	5	7	ERAA061858       	4	19990323	G	2210	4025008918	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	FAILED          	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	417EH					33031				HP COMPUTER TESTED 1-20-99, REF NR  298771 AND RETURNED 3-1-99.  COULD NOT BE USED ON AIRCRAFT DUE TO MULTIPLE HARDOVERS	 IN ROLL CHANNEL (LEFT AND RIGHT.)					1	G	7	2 	4U				H4SW    					 
1999050700198	19990507	00198		1999	5	7	ERAA061859       	4	19990323	G	3416	1901350000	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	ERRATIC         	H			ERAA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	298EH					S845				RADAR ALTIMETER HAS ERRATIC READINGS.						1	G	7	2 	3U				H3EU    					 
1999050700199	19990507	00199		1999	5	7	ERAA061860       	4	19990323	G	3416	1901304000	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	ERRATIC         	H			ERAA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	296EH					S849				TRI-40 INDICATOR HAS ERRATIC READINGS.						1	G	7	2 	3U				H3EU    					 
1999050700200	19990507	00200		1999	5	7	ERAA061861       	4	19990324	G	2213	HUCAB1CM	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	MALFUNCTIONED   	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	167EH					33089				COMPUTER UNIT WILL TEST MANUALLY ONLY.						1	G	7	2 	4U				H4SW    					 
1999050700201	19990507	00201	GL  	1999	5	7	ERAA061862       	2	19990324	G	7230	23004538	NUT             			BOLKMS	105   	BO105A      		EU  	ALLSN 	250C  	250C18      	03011	GL  					COMPRESSOR	LEAKING         	H			ERAA	K				NONE                    				K	W		FLUID LOSS                	INADEQUATE Q C            		IN	INSP/MAINT     	1			AL	03	148EH					S703				NEW NUT; CAP LEAKS.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999050700202	19990507	00202	NE  	1999	5	7	ERAA061863       	1	19990325	G	2931	ST106AD	TRANSMITTER     			SKRSKY	S61   	S61N        	8142104	NE  										HYDRAULIC SYS	MALFUNCTIONED   	H			ERAA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	562EH					61257				NEW PRESSURE TRANSMITTER.  PRESSURE FLUCTUATING.						2	G	7	2 	4U				1H15    					 
1999050700203	19990507	00203		1999	5	7	ERAA061864       	4	19990325	G	2312	064100504	TRANSMITTER     			SKRSKY	S61   	S61N        	8142104	NE  										VHF	MALFUNCTIONED   	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	563EH					61808				TRANSMITTER UNIT HAS HEAVY STATIC IN-FLIGHT.						2	G	7	2 	4U				1H15    					 
1999050700204	19990507	00204	GL  	1999	5	7	ERAA061867       	2	19990412	G	7250	23031939	GP SUPPORT      			BOLKMS	105   	BO105A      		EU  	ALLSN 	250C  	250C18      	03011	GL  					NR 8 BEARING	MISOVERHAULED   	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	148EH					S703				GP SUPPORT SENT FOR OVERHAUL 8-4-98, COULD NOT BE INSTALLED DUE TO ROUGH SURFACE AT NR 8 OIL TUBE SEAL, AND SUMP NUT E-R	ING SEAT.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999050700205	19990507	00205		1999	5	7	ERAA061868       	1	19990412	G	2434	E6840406	NUT             																	TIE BOLT	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03										NEW NUT WILL NOT STRETCH TIE BOLT.																			 
1999050700206	19990507	00206	GL  	1999	5	7	ERAA061869       	2	19990416	G	7250	6888547	SUMP COVER      			BOLKMS	105   	BO105A      		EU  	ALLSN 	250C  	250C18      	03011	GL  					TURBINE	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	148EH					S703				SUMP COVER COULD NOT BE INSTALLED DUE TO LOOSE DEBRIS AND FLAKING OVERSPRAY INSIDE OF COVER.  ONE HOLE CLOGGED.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999050700207	19990507	00207	GL  	1999	5	7	ERAA061871       	2	19990419	G	7230	6851574	SCROLL          			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	131EH					S595				SCROLL  COULD NOT BE INSTALLED DUE TO PLATING FLAKING OFF INSIDE RIGHT TURNING VANE.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999052800242	19990528	00242	EU  	1999	5	28	ERAA062368       	1	19990420	G	6310	4638302093	SHAFT           			BOLKMS	105   	BO105S      	5626006	EU  										FREEWHEEL	LEAKING         	H			ERAA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03	426EH	825  				S552				FREEWHEEL SHAFT IS CAUSING LEAK OF LEFT INPUT SEAL.						1	G	7	2 	3U				H3EU    					 
1999052800243	19990528	00243	EU  	1999	5	28	ERAA062369       	1	19990420	G	6320	4619210902	BEVEL GEAR SET  			BOLKMS	105   	BO105S      	5626006	EU  										TRANSMISSION	MAKING METAL    	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	133EH	110  				S598				TRANSMISSION MAKING METAL.  GEAR SET BREAKING DOWN.						1	G	7	2 	3U				H3EU    					 
1999052800244	19990528	00244		1999	5	28	ERAA062370       	1	19990420	G	6320	10510157	STAND           																	TRANSMISSION	MISMARKED       	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03										TRANSMISSION STAND TAGGED AS LEFT HAND AND IS ACTUALLY RIGHT HAND.  FORWARD ARROW ALSO IS BACKWARDS.																			 
1999052800228	19990528	00228	GL  	1999	5	28	ERAA062371       	2	19990421	G	7313	23062750	SHIELD          			BOLKMS	105   	BO105A      		EU  	ALLSN 	250C  	250C18      	03011	GL  					NR 1 NOZZLE	CRACKED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	141LG	1352 				S704				TURBINE DUE 1,750 HOUR INSPECTION DUE TO NR 1 AND NR  2 WHEEL CYCLE OUT.   DISCOVERED CONDITION OF NR 1 NOZZLE SHIELD DU	RING TEARDOWN.  THE DAMAGE STARTS AT THE MISSING MATERIAL TO HALF THE CIRCUMFERENCE OF THE DOME.  CRACK IS LOCATED WHERE	 THE DOME IS BRAZED TO THE INNER BAND.				1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999052800238	19990528	00238	SW  	1999	5	28	ERAA062379       	1	19990504	G	5711	212030447117S	CAP             		212030100111	BELL  	412   	412         	1182202	SW  										WING	CRACKED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	415EH	10605			ADW06067	33009				LEFT SPAR CAP IS CRACKED.						1	G	7	2 	4U				H4SW    					 
1999052800229	19990528	00229		1999	5	28	ERAA062380       	1	19990504	G	2822	23058146	IMPELLER        																	FUEL PUMP	MISMARKED       	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03										INCORRECT PART NUMBER ISSUED (MISIDENTIFIED)  AFTER CEB-1321 AND CEB-1325 COMPLIED WITH.																			 
1999052800230	19990528	00230	EU  	1999	5	28	ERAA062382       	1	19990505	G	6320	E23031922	ADAPTER         			BOLKMS	105   	BO105S      	5626006	EU  										SPUR GEAR	DAMAGED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	127EH	119  				S571				SHAFT IS MAGNETIC, SCRATCHES ON BEARING RACE.						1	G	7	2 	3U				H3EU    					 
1999052800239	19990528	00239		1999	5	28	ERAA062383       	1	19990505	G	3246	212040229001	TUBE            																	MLG	MISMANUFACTURED 	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03										NEW TUBE RECEIVED THAT IS .50 INCH TOO SHORT IN LENGTH.																			 
1999052800231	19990528	00231		1999	5	28	ERAA062385       	4	19990506	G	3442	MI5853011	RADAR           			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	577EH					760222				RADAR ORIGINAL WITH AIRCRAFT WHEN PURCHASED BY ERA FROM EXXON.  UNIT WAS REPAIRED BY HONEYWELL REF NR 196437 ON 11-12-98	.  SEVERAL BUTTON LIGHTS ARE INOPERABLE.					1	G	7	2 	3U				H1NE    					 
1999052800232	19990528	00232	SW  	1999	5	28	ERAA062387       	1	19990507	G	7312	3019906	FLOW DIVIDER    			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					ENGINE	CRACKED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	177EH					33037				FLOW DIVIDER COULD NOT BE INSTALLED DUE TO CRACK AT OUTLET END OF DUMP FITTING.  FLOW DIVIDER WAS SENT TO KANSAS AVIATIO	N FOR SAME PROBLEM AND WAS INSPECTED AND TESTED  AND RETURNED TO ERA 12-29-98 UNREPAIRED.					1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999052800233	19990528	00233		1999	5	28	ERAA062388       	4	19990507	G	3444	1901350000	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										RADAR ALT	INOPERATIVE     	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	293EH					S844				RADAR ALT RT INOPERABLE.  ERRONEOUS ALTITUDE GIVEN.						1	G	7	2 	3U				H3EU    					 
1999052800234	19990528	00234	GL  	1999	5	28	ERAA062389       	2	19990510	G	7250	E23057111	WHEEL           			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	MISMANUFACTURED 	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	127EH					S571				NEW WHEEL THAT WAS ISSUED TO AIRCRAFT COULD NOT BE INSTALLED BECAUSE WHEEL HAD OVERSIZE DIAMETER AT BLADE TIPS.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999052800240	19990528	00240		1999	5	28	ERAA062390       	1	19990513	G	6320	204040623109	BEARING         																	GEARBOX	ROUGH           	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03										NEW BEARING FEELS ROUGH.																			 
1999052800235	19990528	00235	GL  	1999	5	28	ERAA062391       	2	19990513	G	7240	6870992	CASE            			BOLKMS	105   	BO105A      		EU  	ALLSN 	250C  	250C18      	03011	GL  					COMBUSTION SECT	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	148EH					S703				OUTER COMBUSTION CASE COULD NOT BE INSTALLED BECAUSE AIR TUBE BOSS IS .008 INCH OUT OF ROUND.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999052800236	19990528	00236		1999	5	28	ERAA062392       	4	19990513	G	3444	7000839904	INDICATOR       			BELL  	412   	412         	1182202	SW  										RADAR ALT	MALFUNCTIONED   	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	417EH					33031				REPAIRED AND MODIFIED 10-19-98 BY HONEYWELL REF NR 28446.  LIGHT INOPERABLE.						1	G	7	2 	4U				H4SW    					 
1999052800237	19990528	00237	SW  	1999	5	28	ERAA062393       	1	19990513	G	6240	222375021103	INDICATOR       			BELL  	222   	222B        	1182124	SW  										TRIPLE TACH	FLUCTUATES      	H			ERAA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			AL	03	58RC					47141				RIGHT NEEDLE FLUCTUATES TO HIGH SIDE.  READS 104 PERCENT WHEN ROTOR IS AT 100 PERCENT.						1	G	7	2 	3U				H9SW    					 
1999052800241	19990528	00241		1999	5	28	ERAA062394       	1	19990514	G	5313	212030132109	LONGERON        																	FUSELAGE	BENT            	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03										NEW LONGERON REJECTED UPON RECEIVING BECAUSE IT WAS BENT.																			 
1999070200081	19990702	00081	EU  	1999	7	2	ERAA062561       	1	19990518	G	6310	4638302093	SHAFT           		4638001007  	BOLKMS	105   	BO105S      	5626006	EU  										FREEWHEEL	LEAKING         	H			ERAA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03	290EH	108  			1314	S850				FREEWHEEL SHAFT CAUSING INPUT SEAL LEAK.						1	G	7	2 	3U				H3EU    					 
1999070200082	19990702	00082	EU  	1999	7	2	ERAA062562       	1	19990519	G	6310	4638302093	SHAFT           		4638001007  	BOLKMS	105   	BO105S      	5626006	EU  										FREEWHEEL	LEAKING         	H			ERAA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03	290EH	108  			1314	S850				FREEWHEEL SHAFT CAUSING INPUT SEAL LEAK.						1	G	7	2 	3U				H3EU    					 
1999070200092	19990702	00092	EU  	1999	7	2	ERAA062563       	1	19990526	G	6310	4638302093	SHAFT           			BOLKMS	105   	BO105C      	5626005	EU  										FREEWHEEL	LEAKING         	H			ERAA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03	426EH	11691				S552				FREEWHEEL SHAFT CAUSING INPUT SEAL LEAK.						1	G	7	2 	3U				H3EU    					 
1999070200083	19990702	00083		1999	7	2	ERAA062564       	1	19990526	G	2435	230322111	ARMATURE        																	START/GENERATOR	FAILED          	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03										OVERHAULED BY FUTURE AVIATION ON WORK ORDER NR  99-2-1049 AND RETURNED TO ERA 3-9-99.   ARMATURE FAILED GENERATE TEST WH	EN INSTALLED ON GENERATOR.																		 
1999070200084	19990702	00084	EU  	1999	7	2	ERAA062565       	1	19990526	G	5320	E23001801	NUT             			BOLKMS	105   	BO105S      	5626006	EU  										FUSELAGE	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	148EH					S703				NEW OUTER NUT ISSUED TO AIRCRAFT, BUT COULD NOT BE INSTALLED BECAUSE WRENCH LUG SLOT IS OUT OF LOCATION.						1	G	7	2 	3U				H3EU    					 
1999070200093	19990702	00093		1999	7	2	ERAA062566       	1	19990602	G	5320	LN29522S06022	BOLT            																	FUSELAGE	CORRODED        	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03										NEW BOLT THAT WAS REJECTED UPON RECEIVING DUE TO CORROSION ON BOLT HEAD.   REF: RMA NR R020439.																			 
1999070200090	19990702	00090	SW  	1999	7	2	ERAA062567       	1	19990602	G	6220	214040110003	RETAINER        			BELL  	412   	412         	1182202	SW  										M/R HUB	FLAKING         	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	168EH					33058				NEW RETAINERS ISSUED TO AIRCRAFT, BUT COULD NOT BE INSTALLED.   RETAINERS HAVE SILVER COATING FLAKING ON GROUND RUN.						1	G	7	2 	4U				H4SW    					 
1999070200085	19990702	00085	EU  	1999	7	2	ERAA062568       	1	19990604	G	5320	E23037413	SHAFT           			BOLKMS	105   	BO105S      	5626006	EU  										FUSELAGE	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	148EH					S703				NEW OUTER SHAFT ISSUED TO AIRCRAFT,BUT COULD NOT BE INSTALLED BECAUSE OF UNDERSIZE NR 5 BEARING SHAFT.						1	G	7	2 	3U				H3EU    					 
1999070200086	19990702	00086	GL  	1999	7	2	ERAA062569       	2	19990614	G	7250	23030844	NOZZLE          			BELL  	206   	206L        	1181522	SW  	ALLSN 	250C  	250C20B     	03013	GL  					NR 4	MALFUNCTIONED   	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	405EH					45115				EXCHANGE UNIT SENT TO ERA D/AIRMOTIVE W/O LA0845 6-9-99.  COULD NOT BE USED ON AIRCRAFT DUE TO NR 4 BTP RUNOUT OUT OF LI	MITS.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999070200087	19990702	00087	GL  	1999	7	2	ERAA062570       	2	19990614	G	7250	E68777362	SEAL            			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					LABRINTH	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	151EH					S706				NEW LABYRINTH SEAL THAT COULD NOT BE INSTALLED ON AIRCRAFT DUE TO PILOT DIAMETER OVERSIZED.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999070200088	19990702	00088		1999	7	2	ERAA062571       	1	19990614	G	6320	E23031922	ADAPTER         																	SPUR GEAR	PITTED          	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03										NEW  ADAPTERS REJECTED UPON RECEIVING DUE TO NICKS AND PITS IN INNER RACE AND DEPRESSION IN INNER RACE.  CAN BE FELT WIT	H .020 INCH RADIUS SCRIBE.																		 
1999070200091	19990702	00091		1999	7	2	ERAA062572       	1	19990615	G	5320	412010177105	SPLINED PLATE   																	FUSELAGE	CORRODED        	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03										NEW SPLINED PLATE THAT WAS REJECTED UPON RECEIVING DUE TO CORROSION AND PITTING IN BOLT HOLES.																			 
1999070200089	19990702	00089	GL  	1999	7	2	ERAA062573       	2	19990615	G	7210	6899402	PTO GEAR        			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					GEARBOX	SPALLED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	293EH					S844				PTO GEAR REMOVED FROM AIRCRAFT DUE TO SPALLING ON GEAR TEETH.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999073000126	19990730	00126	NE  	1999	7	30	ERAA062923       	1	19990618	G	6220	S611026400041	DAMPER          			SKRSKY	S61   	S61N        	8142104	NE  										MAIN ROTOR	WEAK            	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	562EH	35   				61257				MAIN ROTOR DAMPER WEAK.						2	G	7	2 	4U				1H15    					 
1999073000127	19990730	00127	NE  	1999	7	30	ERAA062924       	1	19990618	G	6220	S611026400041	DAMPER          			SKRSKY	S61   	S61N        	8142104	NE  										MAIN ROTOR	STIFF           	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	562EH	35   				61257				DAMPER REMOVED FROM AIRCRAFT DUE TO BEING STIFF.						2	G	7	2 	4U				1H15    					 
1999073000128	19990730	00128	GL  	1999	7	30	ERAA062925       	2	19990618	G	7230	6851430	REAR DIFFUSER   			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	MISOVERHAULED   	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	423EH					S543				REAR DIFFUSER SENT FOR OVERHAUL AND RETURNED TO ERA 1-21-99.  GROOVE ON RIBBED SIDE OF MOUNT EAR, AREA A.   ALLISON O/H 	MANUAL FIG. 6-16.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999073000129	19990730	00129	GL  	1999	7	30	ERAA062926       	2	19990708	G	7230	6870813	VANE            			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					DIFFUSER	DAMAGED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	423EH					S543				DIFFUSER VANE ISSUED TO AIRCRAFT BUT COULD NOT BE USED DUE TO BROKEN STUD.   ALL STUDS HAVE OVERSIZE DIAMETER.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999073000130	19990730	00130	GL  	1999	7	30	ERAA062927       	2	19990708	G	7230	6870813	VANE            			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					DIFFUSER	CRACKED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	423EH					S543				DIFFUSER VANE INSPECTED AND ISSUED TO AIRCRAFT, BUT COULD NOT BE INSTALLED DUE TO CRACKED VANE.    INCOMPLETE BRAZE AT E	ND OF VANE.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999073000131	19990730	00131	GL  	1999	7	30	ERAA062928       	2	19990708	G	7261	23053320	SUMP            			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	DAMAGED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	423EH					S543				NEW SUMP CAN HAS IMPERFECTION ON B-NUT FLARE.  ISSUED TO AIRCRAFT BUT COULD NOT BE USED.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999073000132	19990730	00132	GL  	1999	7	30	ERAA062930       	2	19990712	G	7250	6871505	BEARING         			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					NR 5	SPALLED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	298EH	894  				S845				NR 5 BEARING NEW WHEN INSTALLED.  HAS SPALLING AND PITS ON BALLS.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999092400977	19990924	00977		1999	9	24	ERAA064354       	1	19990819	G	2435	230322111	ARMATURE        																	STARTER/GEN	FAILED          	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03										ARMATURE SENT FOR REPAIR AND REC'D AT ERA 6-3-99, BUT COULD NOT BE INSTALLED DUE TO FAILING GENERATE TESTS.																			 
1999092400978	19990924	00978	GL  	1999	9	24	ERAA064355       	2	19990819	G	7250	E23037413	SHAFT           			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE SECTION	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	291EH					S842				NEW OUTER SHAFT HAS UNDERSIZE NR 5 BEARING JOURNAL.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999092400979	19990924	00979	GL  	1999	9	24	ERAA064356       	2	19990825	G	7230	6890530	SUPPORT         			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	MISREPAIRED     	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	423EH					S543				FRONT SUPPORT SENT FOR OVERHAUL, BUT COULD NOT BE INSTALLED DUE TO BEARING BORE OUT OF ALIGNMENT.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999092400982	19990924	00982	EU  	1999	9	24	ERAA064361       	1	19990909	G	6220	10514183035	BUSHING         			BOLKMS	105   	BO105S      	5626006	EU  										M/R GEARBOX	MISMARKED       	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	152EH					S701				ORDERED OVERSIZE  BUSHING AND STANDARD SIZE WAS INSIDE PACKAGE THAT WAS MARKED AS OVERSIZED.						1	G	7	2 	3U				H3EU    					 
1999092400980	19990924	00980	GL  	1999	9	24	ERAA064362       	2	19990909	G	7230	23057142	CASE HALF       			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	DELAMINATING    	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	133EH					S598				CASE HALF OVERHAULED 7/98.  CASE HAS 326.3 HOURS SINCE O/H AND PLASTIC IS DELAMINATING ON SIDE.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999092400981	19990924	00981	GL  	1999	9	24	ERAA064363       	2	19990909	G	7230	23004513	CARBON SEAL     			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	LEAKING         	H			ERAA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03	423EH					S543				NEW PART ISSUED TO AIRCRAFT, BUT COULD NOT BE INSTALLED DUE TO SEAL LEAKING DURING LEAK TEST.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999092400983	19990924	00983	EU  	1999	9	24	ERAA064365       	1	19990910	G	6220	2604067	STRAP           			BOLKMS	105   	BO105S      	5626006	EU  										M/R GEARBOX	DAMAGED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	152EH	9807 				S701				STRAP REMOVED DUE TO ASB-BO105-10-114.  STRAP HAS BROKEN WIRE.  TOTAL FLIGHTS 37,882.						1	G	7	2 	3U				H3EU    					 
1999102900393	19991029	00393	NE  	1999	10	29	ERAA064504       	2	19990920	G	7532		BLEED VALVE     			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					ENGINE	FLUCTUATING     	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	418EH	6846 				33032				POWER SECTION OVERHAULED.  BLEED VALVE FLUCTUATING.						1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999102900398	19991029	00398		1999	10	29	ERAA064506       	1	19990930	G	6320	10510157	STAND           																	TRANSMISSION	MISMARKED       	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03										NEW TRANSMISSION STAND THAT WAS REMOVED FROM STOCK AND HAS INCORRECT PART NUMBER.  STAND HAS P/N 105-10157 ON IT (CORREC	T P/N FOR LEFT FRAME) AND  IS RIGHT A-FRAME AND NOT LEFT.																		 
1999102900394	19991029	00394	EU  	1999	10	29	ERAA064508       	1	19991004	G	7160	23033400	AIR FILTER      			BOLKMS	105   	BO105S      	5626006	EU  										AIR INTAKE	CRACKED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	423EH					S543				THERE ARE SEVERAL CRACKS ON FILTER HOUSING ADJACENT TO O-RING BORE.						1	G	7	2 	3U				H3EU    					 
1999102900395	19991029	00395	NE  	1999	10	29	ERAA064509       	2	19991006	G	7311	8528061	OIL COOLER      			SKRSKY	S61   	S61N        	8142104	NE  	GE    	CT58  	CT581401    	30011	NE  					ENGINE	FAILED          	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	562EH					61257				OIL COOLER REPAIRED AND RETURNED TO ERA 7-14-99.  HIGH TEMP 1 REACHES 121 DEGREES WITHIN 15 MINUTES OF HOVER.  COOLING F	IN PLUGGED UP.					2	G	7	2 	4U	4	U		1H15    	1E3				 
1999102900396	19991029	00396		1999	10	29	ERAA064510       	4	19991006	G	3416	1901350000	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	ERRATIC         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	291EH					S842				INDICATOR UNIT HAS ERRATIC READINGS.						1	G	7	2 	3U				H3EU    					 
1999102900397	19991029	00397	GL  	1999	10	29	ERAA064511       	2	19991013	G	7230	6870813	STUD            			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					VAIN ASSY	BROKEN          	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	134EH					635				VANE RING SENT FOR OVERHAUL 8/30/99.  VANE RING ISSUED TO AIRCRAFT, BUT COULD NOT BE USED  BECAUSE STUD BROKE AT LESS TH	AN 30 INCHES/POUNDS TORQUE.   ALSO NOTED:  EXCESS SLAG AROUND STUDS.  WILL NOT ALLOW PROPER SEATING.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999122300312	19991223	00312	GL  	1999	12	23	ERAA065400       	2	19991021	G	7250	6898731	SEAL            			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					POWER TURBINE	SOFT            	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	297EH					S835				PT SUPPORT OVERHAULED AND RETURNED 2-16-99.  ISSUED TO AIRCRAFT BUT COULD NOT BE INSTALLED DUE TO SOFT 19-24 SEAL.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999122300325	19991223	00325		1999	12	23	ERAA065404       	1	19991102	G	6220	10543082	COVER           																	CONTROL ROD	MISSING         	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	SPARE									CONTROL ROD ASSY REJECTED UPON RECEIVING DUE TO BEARING DUST COVER MISSING.																			 
1999122300326	19991223	00326	EU  	1999	12	23	ERAA065406       	1	19991109	G	6310	4638302093	SHAFT           			BOLKMS	105   	BO105S      	5626006	EU  										FREEWHEEL	LEAKING         	H			ERAA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03	294EH	518  				S846				FREEWHEEL SHAFT HAS 518.4 HOURS TT,  AND INPUT SEAL LEAKS.						1	G	7	2 	3U				H3EU    					 
1999122300313	19991223	00313	GL  	1999	12	23	ERAA065407       	2	19991110	G	7200		ENGINE          			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE BAY	MAKING METAL    	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	133EH	11503				S598				ENGINE MAKING METAL (2 1/2 BEARING FAILURE)						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999122300314	19991223	00314	GL  	1999	12	23	ERAA065408       	2	19991110	G	7210		GEAR            			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					GEARBOX	SPALLED         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	423EH	6294 				S543				ENGINE MAKING METAL.  GEARBOX PINION GEAR AND TORQUE METER GEAR TEETH SPALLING AND PITTING.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999122300315	19991223	00315	GL  	1999	12	23	ERAA065409       	2	19991110	G	7230		BEARING         			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	FAILED          	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	133EH	7435 				S598				ENGINE MAKING METAL; 2 1/2 BEARING FAILED, MINOR FOD 1ST STAGE COMPRESSOR.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999122300316	19991223	00316	GL  	1999	12	23	ERAA065410       	2	19991110	G	7230		BEARING         			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	FAILED          	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	291EH	9430 				S842				ENGINE MAKING METAL;   NR 5 BEARING FAILED, SCROLL CRACKED AT TOP ECU FITTING.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999122300327	19991223	00327	EU  	1999	12	23	ERAA065411       	1	19991110	G	6320	4638001004	BEVEL GEAR      			BOLKMS	105   	BO105S      	5626006	EU  										TRANSMISSION	MAKING METAL    	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	131EH	12070				S595				TRANSMISSION MAKING METAL.  LEFT PINION AND BEVEL GEAR BREAKING DOWN, LEFT INT SHAFT TEETH PITTED, LEFT FREEWHEEL WORN B	EYOND LIMITS.					1	G	7	2 	3U				H3EU    					 
1999122300317	19991223	00317	SW  	1999	12	23	ERAA065418       	1	19991123	G	3212	412050017102	FLOAT COVER     			BELL  	412   	412         	1182202	SW  										MLG	MISREPAIRED     	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	177EH					33037				FLOAT COVER REPAIRED AND REJECTED  BECAUSE DIMENSIONS DID NOT MEET DRAWINGS.						1	G	7	2 	4U				H4SW    					 
1999122300318	19991223	00318	SW  	1999	12	23	ERAA065419       	1	19991123	G	3212	412050017101	FLOAT COVER     			BELL  	412   	412         	1182202	SW  										MLG	MISREPAIRED     	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	174EH					33085				FLOAT COVER REPAIRED.  REJECTED UPON RECEIVING DUE TO DIMENSIONS NOT MEETING DRAWINGS.						1	G	7	2 	4U				H4SW    					 
1999122300319	19991223	00319		1999	12	23	ERAA065420       	1	19991123	G	3212	412050017101	FLOAT COVER     																	MLG	MISREPAIRED     	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	SPARE									FLOAT COVER REPAIRED.  REJECTED UPON RECEIVING DUE TO DIMENSIONS DID NOT MATCH DRAWINGS.																			 
1999122300320	19991223	00320		1999	12	23	ERAA065421       	1	19991123	G	3212	412050017101	FLOAT COVER     																	MLG	MISREPAIRED     	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	SPARE									FLOAT COVER REPAIRED.  DIMENSIONS DID NOT MEET DRAWINGS.																			 
1999122300324	19991223	00324	SW  	1999	12	23	ERAA065422       	1	19991123	G	6200	412010461105	BUSHING         			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	177EH					33037				NEW BUSHINGS COULD NOT BE USED ON AIRCRAFT DUE TO  OUTSIDE DIAMETER. OF BUSHINGS TO BEARING.   UNABLE TO INSTALL BUSHING	S.					1	G	7	2 	4U				H4SW    					 
1999122300328	19991223	00328	EU  	1999	12	23	ERAA065424       	1	19991208	G	6310	4638302093	SEAL            			BOLKMS	105   	BO105C      	5626005	EU  										FREEWHEEL SHAFT	LEAKING         	H			ERAA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03	426EH	543  				S552				INPUT SEAL LEAKING.						1	G	7	2 	3U				H3EU    					 
1999122300321	19991223	00321	NE  	1999	12	23	ERAA065426       	1	19991209	G	2841	S614561247001	INDICATOR       			SKRSKY	S61   	S61N        	8142104	NE  										FUEL QTY	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	563EH					61808				FUEL QUANTITY INDICATOR RECENTLY PURCHASED  IS NOT SERVICEABLE.  WILL NOT CALIBRATE TO EMPTY AND FULL.						2	G	7	2 	4U				1H15    					 
1999122300322	19991223	00322	GL  	1999	12	23	ERAA065428       	2	19991209	G	7210	23034787	BEARING         			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					GEARBOX	FLAKING         	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	294EH	677  				S846				METAL FLAKING OFF OF ROLLER.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999122300323	19991223	00323	GL  	1999	12	23	ERAA065429       	2	19991209	G	7210	23034787	BEARING         			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					GEARBOX	SCRATCHED       	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	125EH					S562				NEW BEARING COULD NOT BE INSTALLED ON AIRCRAFT DUE TO HAVING SCRATCHED ROLLER.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
2000012200455	20000122	00455	EU  	2000	1	22	ERAA065646       	1	19991214	G	6310	4638302093	SHAFT           			BOLKMS	105   	BO105S      	5626006	EU  										FREEWHEEL	LEAKING         	H			ERAA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03	426EH	543  				S552				FREEWHEEL SHAFT HAS 542.5 HOURS AND INPUT SEAL IS LEAKING, SPECIAL COATING IS WORN OFF.						1	G	7	2 	3U				H3EU    					 
2000012200456	20000122	00456	EU  	2000	1	22	ERAA065647       	1	19991214	G	6310	4638302093	SHAFT           			BOLKMS	105   	BO105S      	5626006	EU  										FREEWHEEL	LEAKING         	H			ERAA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03	128EH	283  				S572				FREEWHEEL SHAFT'S SPECIAL COATING WORN CAUSING SEAL TO LEAK.						1	G	7	2 	3U				H3EU    					 
2000012200457	20000122	00457	EU  	2000	1	22	ERAA065648       	1	19991214	G	6310	4638302093	SHAFT           			BOLKMS	105   	BO105S      	5626006	EU  										FREEWHEEL	LEAKING         	H			ERAA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03	292EH					S843				FREEWHEEL SHAFT'S SPECIAL COATING WORN OFF CAUSING SEAL TO LEAK.						1	G	7	2 	3U				H3EU    					 
2000012200465	20000122	00465	EU  	2000	1	22	ERAA065650       	1	19991215	G	6320	10510157	STAND           			BOLKMS	105   	BO105S      	5626006	EU  										TRANSMISSION	MISMARKED       	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03	152EH					S701				TRANSMISSION STAND ISSUED TO AIRCRAFT BUT COULD NOT BE INSTALLED DUE TO PART BEING IMPROPERLY MARKED FROM AEC.  ORDERED 	P/N 105-10157, BUT PART WAS MARKED 105-10156.					1	G	7	2 	3U				H3EU    					 
2000012200458	20000122	00458	EU  	2000	1	22	ERAA065652       	1	19991220	G	6310	4638302093	SHAFT           			BOLKMS	105   	BO105S      	5626006	EU  										FREEWHEEL	WORN            	H			ERAA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	03	128EH	183  				S572				FREEWHEEL SHAFT'S SPECIAL COATING WORN OFF, WHERE SEAL RIDES.						1	G	7	2 	3U				H3EU    					 
2000012200459	20000122	00459	EU  	2000	1	22	ERAA065654       	1	19991227	G	6310	4638302093	SHAFT           			BOLKMS	105   	BO105S      	5626006	EU  										FREEWHEEL	LEAKING         	H			ERAA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			AL	03	292EH					S843				FREEWHEEL SHAFT'S SPECIAL COATING WORN, CAUSING SEAL TO LEAK.						1	G	7	2 	3U				H3EU    					 
2000012200464	20000122	00464		2000	1	22	ERAA065656       	1	19991229	G	2910	212061107013	TUBE            																	HYD SYSTEM	MISMANUFACTURED 	H			ERAA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			AL	03										NEW TUBE THAT COULD NOT BE USED ON AIRCRAFT DUE TO CORROSION OR POSSIBLE DEFECT WHICH OCCURRED DURING MANUFACTURING.  LE	NGTHWISE PITTING.																		 
1999040900724	19990409	00724	SW  	1999	4	9	GJQA061537       	1	19990401	G	3040	204070907101	MOTOR           			BELL  	204   	UH1H        	1181407	SW  										WINDSHIELD WIPER	MALFUNCTIONED   	H			GJQA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	98W	1149 				6413822				PILOT'S WINDSHIELD WIPER MOTOR ERRATIC-WIPER BLADE INTERMITTENTLY OFF SIDE OF WINDSHIELD. REPLACED WIPER MOTOR, RIGGED B	LADE, SWEEP AND GROUND CHECKED OKAY.					1	G	7	1 	4U				EXPA1G71					 
1999040900725	19990409	00725	SW  	1999	4	9	GJQA061540       	1	19990402	G	6320	204040424001	BEARING         		212540002109	BELL  	204   	UH1H        	1181407	SW  										M/R GEARBOX	GALLED          	H			GJQA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NM	01	98W	1212 			A1144	6413822				PILOT REPORTED MAIN ROTOR TRANSMISSION CHIP LIGHT. CLEANED AND INSPECTED. TRANSMISSION OIL MONITOR PLUG.  FOUND SMALL AM	OUNT OF MAGNETIC CHIPS.  RE-INSTALLED CHIP DETECTOR AND WILL MONITOR.  AT 100 HOUR INSPECTION, AT AIRFRAME HOURS 1,058.3	, EVIDENCE OF MINOR AMOUNT OF METAL GENERATION REVEALED.  REMOVED OIL PUMP FOR VISUAL INSPECTION AND NO EVIDENCE OF META	L GENERATION DISCOVERED.  AT 1,214.1 HOURS, FOUND BAD BEARING INNER RACE IN NR 2 HYDRAULIC PUMP QUILL DRIVE.  REPLACED B	EARING AND CORRECTED THE PROBLEM.		1	G	7	1 	4U				EXPA1G71					 
1999091700424	19990917	00424	SW  	1999	9	17	GJQA063836       	1	19990901	G	6320	204040785003	SPIDER          		212040001141	BELL  	212   	212         	1181420	SW  										TRANSMISSION	CRACKED         	H			GJQA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			FS	01	82W	5822 			ABW08077	31177				BELL 212 TRANSMISSION WAS REMOVED FOR FERROUS METAL GENERATION.  INITIAL TEARDOWN INSPECTION REVEALED LOWER SPIDER CRACK	ED. THIS CONDITION WAS PREVIOUSLY EMPHASIZED BY ASB 212-91-66A REQUIRING A SPECIAL NDT MAGNAFLUX INSPECTION.  ASB 212-91	-66 REVISION A WAS PREVIOUSLY COMPLIED WITH ON THIS GEAR 2313.1 HOURS EARLIER WITH NO EVIDENCE OF DEFECTS NOTED.				1	G	7	1 	4U				H4SW    					 
1999051400171	19990514	00171		1999	5	14	HCMA062018       	1	19990216	G	3212	20329200	BAG             																	FLOAT	CUT             	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13										FLOAT BAG IS CUT BY BRACKET.  CANNOT PATCH.																			 
1999051400172	19990514	00172		1999	5	14	HCMA062019       	1	19990216	G	6520	1D1KIT	BEARING         																	TAIL ROTOR	MISMANUFACTURED 	E			HCMA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			WP	13										BEARING KIT SHIPPED INCOMPLETE; THEREFORE, IS UNUSABLE.																			 
1999051400180	19990514	00180	EU  	1999	5	14	HCMA062022       	1	19990224	G	6410	350A33215300	BEARING         			SNIAS 	350   	AS350BA     	8680817	EU  										TAIL ROTOR	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	862BH	668  				2713				RUBBER IS CRACKED AND DETERIORATED BEYOND LIMITS.						1	G	7	1 	3U			NC	H9EU    					 
1999051400181	19990514	00181	EU  	1999	5	14	HCMA062023       	1	19990224	G	6410	350A33215300	BEARING         			SNIAS 	350   	AS350BA     	8680817	EU  										TAIL ROTOR	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	862BH	645  				2713				BEARING IS WORN BEYOND LIMITS.						1	G	7	1 	3U			NC	H9EU    					 
2000030400176	20000304	00176	EU  	2000	3	4	HCMA066307       	1	19990429	G	6500	350A33215300	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	DAMAGED         	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	992BH	606  				2889				BEARING DAMAGED BEYOND LIMITS AND THE T/R WILL NOT BALANCE.						1	G	7	1 	3U				H9EU    					 
2000030400177	20000304	00177	EU  	2000	3	4	HCMA066323       	1	19990525	G	6710	SC5083	SERVO           			SNIAS 	350   	AS350B2     	8680813	EU  	TMECA 	ARRIEL	ARRIEL1D    		NE  					MAIN ROTOR	DEFECTIVE       	E			HCMA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			WP	13	198BH	635  				3126	9587			SERVO CAUSED HARD OVER IN CYCLIC.  REPLACEMENT PART WAS OFF SHELF IN O/H CONDITION.						1	G	7	1 	3U	3	U		H9EU    	E19EU				 
2000030400178	20000304	00178	EU  	2000	3	4	HCMA066335       	1	19990630	G	6520	350A33215300	HINGE           			SNIAS 	350   	AS350BA     	8680817	EU  										TAIL ROTOR	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	862BH	715  				2713				BEARINGS WORN BEYOND LIMITS.						1	G	7	1 	3U			NC	H9EU    					 
2000030400179	20000304	00179	EU  	2000	3	4	HCMA066348       	1	19991020	G	6520	350A33215300	HINGE           			SNIAS 	350   	AS350BA     	8680817	EU  										TAIL ROTOR	TORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	862BH	166  				2713				BEARINGS TORN BEYOND LIMITS.						1	G	7	1 	3U			NC	H9EU    					 
2000030400180	20000304	00180	EU  	2000	3	4	HCMA066350       	1	19991020	G	6520	350A33215300	HINGE           			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	TORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	992BH	556  				2889				HINGE  TORN BEYOND LIMITS.						1	G	7	1 	3U				H9EU    					 
2000030400181	20000304	00181	EU  	2000	3	4	HCMA066354       	1	19991020	G	6520	350A33215300	HINGE           			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	TORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	997BH	653  				2666				BEARINGS TORN BEYOND LIMITS.						1	G	7	1 	3U				H9EU    					 
2000030400182	20000304	00182	EU  	2000	3	4	HCMA066365       	1	19991025	G	6510	350A33214501	BEARING         			SNIAS 	350   	AS350BA     	8680817	EU  										PITCH ROD	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	862BH	783  				2713				PITCH CONTROL WORN BEYOND LIMITS.						1	G	7	1 	3U			NC	H9EU    					 
2000030400183	20000304	00183	EU  	2000	3	4	HCMA066366       	1	19991025	G	6510	350A33214501	BEARING         			SNIAS 	350   	AS350BA     	8680817	EU  										PITCH ROD	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	862BH	617  				2713				PITCH CONTROL WORN BEYOND LIMITS.						1	G	7	1 	3U			NC	H9EU    					 
2000030400184	20000304	00184	EU  	2000	3	4	HCMA066367       	1	19991025	G	6510	350A33214501	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH ROD	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	972BH	846  				2804				PITCH CONTROL WORN BEYOND LIMITS.						1	G	7	1 	3U				H9EU    					 
2000030400185	20000304	00185	EU  	2000	3	4	HCMA066368       	1	19991025	G	6510	350A33214501	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH ROD	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	193BH					2894				PITCH CONTROL WORN BEYOND LIMITS.  TIME ON PART IS UNKNOWN.						1	G	7	1 	3U				H9EU    					 
2000030400186	20000304	00186	EU  	2000	3	4	HCMA066369       	1	19991025	G	6510	350A33214501	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH ROD	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	194BH					2903				PITCH CONTROL WORN BEYOND LIMITS.  TIME ON PART IS UNKNOWN.						1	G	7	1 	3U				H9EU    					 
2000030400187	20000304	00187	EU  	2000	3	4	HCMA066370       	1	19991025	G	6510	350A33214501	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH ROD	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	995BH					2987				PITCH CONTROL  WORN BEYOND LIMITS.  TIME ON PART IS UNKNOWN.						1	G	7	1 	3U				H9EU    					 
2000030400188	20000304	00188	EU  	2000	3	4	HCMA066371       	1	19991025	G	6510	350A33214501	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH ROD	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	197BH					2666				PITCH CONTROL  WORN BEYOND LIMITS.  TIME ON PART IS UNKNOWN.						1	G	7	1 	3U				H9EU    					 
2000030400189	20000304	00189	EU  	2000	3	4	HCMA066372       	1	19991025	G	6510	350A33214501	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH ROD	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	198BH	1199 				3126				PITCH CONTROL WORN BEYOND LIMITS.						1	G	7	1 	3U				H9EU    					 
2000030400190	20000304	00190	EU  	2000	3	4	HCMA066391       	1	19991229	G	6420	350A33215300	HINGE           			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	DEFECTIVE       	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	997BH	660  				2666				BEARINGS DEFECTIVE.  TAIL ROTOR  WILL NOT BALANCE.						1	G	7	1 	3U				H9EU    					 
2001091000227	20010910	00227	EU  	2001	9	10	HCMA075172       	1	19990429	G	6520	350A33215300	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	TORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	992BH	606  				2889				PART IS  TORN BEYOND LIMITS AND THE T/R WILL NOT BALANCE.						1	G	7	1 	3U			 	H9EU    					 
2001091000245	20010910	00245	EU  	2001	9	10	HCMA075233       	1	19991025	G	6420	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	193BH					2894				PART IS WORN BEYOND LIMITS. TIME ON PARTS IS UNKNOWN. PLEASE OVERHAUL PC LINKS.						1	G	7	1 	3U			 	H9EU    					 
2001091000248	20010910	00248	EU  	2001	9	10	HCMA075234       	1	19991025	G	6420	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	194BH					2903				PART IS WORN BEYOND LIMITS. TIME ON PARTS IS UNKNOWN. PLEASE OVERHAUL PC LINKS.						1	G	7	1 	3U			 	H9EU    					 
2001091000250	20010910	00250	EU  	2001	9	10	HCMA075235       	1	19991025	G	6420	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	995BH					2987				PART IS WORN BEYOND LIMITS. TIME ON PARTS IS UNKNOWN. PLEASE OVERHAUL PC LINKS.						1	G	7	1 	3U			 	H9EU    					 
2001091000251	20010910	00251	EU  	2001	9	10	HCMA075236       	1	19991025	G	6420	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HCMA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			WP	13	197BH					2666				PART IS WORN BEYOND LIMITS. TIME ON PART IS UNKNOWN.						1	G	7	1 	3U			 	H9EU    					 
1999012900345	19990129	00345	GL  	1999	1	29	HEEA059983       	2	19990114	G	7240	6899081	LINER           		23035128    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8590X				CAT95099	51494	CAE895487			PART IS CRACKED.  ENGINE REMOVED DUE TO TURBINE OVERHAUL.  UPON INSPECTION OF TURBINE PARTS NOTED:  CRACKED BEYOND SERVI	CEABLE LIMITS ON COMBUSTION LINER AS MARKED.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999012900346	19990129	00346		1999	1	29	HEEA059984       	2	19990114	G	7250	6898730	PT SUPPORT      		6898735     															ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03					CAT37417					PART IS CRACKED.  TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL.  UPON INSPECTION OF TURBINE PARTS NOTED:  CRACKED 	BEYOND SERVICEABLE LIMITS ON POWER TURBINE SUPPORT CLOVER LEAF AS MARKED.																		 
1999012900347	19990129	00347		1999	1	29	HEEA059985       	2	19990114	G	7230	6896888	SCROLL          																	ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										PART IS CRACKED.  SCROLL CRACKED IN BRAZED PATCH AS MARKED.																			 
1999012900387	19990129	00387	SW  	1999	1	29	HEEA059986       	1	19990114	G	3150	214175122105	CAUTION PANEL   			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				NR 1 ENGINE ANTI-ICE SEGMENT NOT GETTING POWER.						2	G	7	2 	4U				H10SW   					 
1999012900388	19990129	00388	SW  	1999	1	29	HEEA059987       	1	19990114	G	2435	206062200113	STARTER         			BELL  	407   	407         		SW  										START/GENERATOR	MALFUNCTONED    	E			HEEA	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SW	03	8595X	208  				53267				STARTER WILL NOT MOTOR AND GENERATOR LIGHT CAME ON IN-FLIGHT.  INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES EX	CESSIVELY WORN AND COMMUTATOR PITTED AND SCARRED.   OVERHAULED AND RETURNED TO SERVICE.					1	G	7	1 	3U			O	H2SW    					 
1999012900389	19990129	00389	SW  	1999	1	29	HEEA059988       	1	19990114	G	7920	407040623101	LINE            			BELL  	407   	407         		SW  										OIL SYSTEM	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	407PH					53003				OIL TUBE HAS PIN HOLE NEXT TO NUT.						1	G	7	1 	3U			O	H2SW    					 
1999012900390	19990129	00390	SW  	1999	1	29	HEEA059990       	1	19990114	G	6240	222375077119	TRANSMITTER     			BELL  	407   	407         		SW  										TORQUE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH					53209				TORQUE TRANSMITTER MAKES GAUGE SHUT OFF.						1	G	7	1 	3U			O	H2SW    					 
1999012900391	19990129	00391	SW  	1999	1	29	HEEA059991       	1	19990114	G	6200	407010206103B	SPRING          			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427PH					53059				AFT BEARING IS UNSTAKED.						1	G	7	1 	3U			O	H2SW    					 
1999012900392	19990129	00392	SW  	1999	1	29	HEEA059995       	1	19990114	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH	2729 				53072				UNIVERSAL HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999012900393	19990129	00393		1999	1	29	HEEA059998       	4	19990114	G	3414	206075725103	INDICATOR       			BELL  	407   	407         		SW  										COCKPIT	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				AIRSPEED INDICATOR READS 5 KNOTS FAST.						1	G	7	1 	3U			O	H2SW    					 
1999012900394	19990129	00394	SW  	1999	1	29	HEEA059999       	1	19990114	G	6410	406312100101	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				TAIL ROTOR BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999012900395	19990129	00395	SW  	1999	1	29	HEEA060000       	1	19990114	G	3212	407350302101	FLOAT BAG       			BELL  	407   	407         		SW  										FLOAT	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH					53209				FLOAT BAG LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999012900396	19990129	00396	SW  	1999	1	29	HEEA060001       	1	19990114	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH	2738 				53072				UNIVERSAL HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999012900397	19990129	00397	SW  	1999	1	29	HEEA060002       	1	19990114	G	6510	406040340101	DISK COUPLING   			BELL  	407   	407         		SW  										T/R DRIVE	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH					53207				BROKEN DISC ON TAIL ROTOR DRIVE.						1	G	7	1 	3U			O	H2SW    					 
1999012900398	19990129	00398	SW  	1999	1	29	HEEA060003       	1	19990114	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH	3448 				53003				UNIVERSAL HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999012900399	19990129	00399		1999	1	29	HEEA060004       	4	19990114	G	3120	M803B205VBATT	INDICATOR       			BELL  	407   	407         		SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				OAT INDICATOR GIVES WRONG TEMPERATURE.						1	G	7	1 	3U			O	H2SW    					 
1999012900400	19990129	00400	SW  	1999	1	29	HEEA060005       	1	19990115	G	7910	206061505115	TANK            			BELL  	407   	407         		SW  										ENGINE OIL	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				TANK ASSEMBLY CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999012900401	19990129	00401	SW  	1999	1	29	HEEA060006       	1	19990115	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	2070 				53016				UNIVERSAL HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999012900402	19990129	00402	SW  	1999	1	29	HEEA060007       	1	19990115	G	7810	407063001101	EXHAUST STACK   			BELL  	407   	407         		SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457PH					53147				EXHAUST STACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999012900403	19990129	00403	SW  	1999	1	29	HEEA060008       	1	19990115	G	7810	407063001101	EXHAUST STACK   			BELL  	407   	407         		SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				EXHAUST STACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999012900404	19990129	00404	SW  	1999	1	29	HEEA060009       	1	19990115	G	6510	406040340101	DISK COUPLING   			BELL  	407   	407         		SW  										T/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				DISK COUPLING HAS EXCESSIVE GAP BETWEEN LAMINATES.						1	G	7	1 	3U			O	H2SW    					 
1999012900405	19990129	00405	SW  	1999	1	29	HEEA060010       	1	19990115	G	6510	406040340101	DISK COUPLING   			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH					53278				DISK COUPLING CRACKED ON TAIL ROTOR DRIVE.						1	G	7	1 	3U			O	H2SW    					 
1999012900406	19990129	00406	SW  	1999	1	29	HEEA060011       	1	19990115	G	7120	407060111101	BIPOD MOUNT     			BELL  	407   	407         		SW  										ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				BIPOD MOUNT HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999012900407	19990129	00407	SW  	1999	1	29	HEEA060012       	1	19990115	G	3210	206052105035	RUBBER          			BELL  	407   	407         		SW  										STRAP ASSY	MISSING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				STRAP ASSEMBLY HAS RUBBER MISSING.						1	G	7	1 	3U			O	H2SW    					 
1999012900408	19990129	00408	SW  	1999	1	29	HEEA060014       	1	19990115	G	2430	206075447101	REGULATOR       			BELL  	407   	407         		SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH					53278				GENERATOR WILL NOT COME ON-LINE.						1	G	7	1 	3U			O	H2SW    					 
1999012900409	19990129	00409	SW  	1999	1	29	HEEA060015       	1	19990115	G	3212	206050247132	COVER           			BELL  	407   	407         		SW  										FLOAT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH					53209				FLOAT COVER HAS AFT CAP MISSING.						1	G	7	1 	3U			O	H2SW    					 
1999012900410	19990129	00410	SW  	1999	1	29	HEEA060016       	1	19990115	G	6510	406040340101	DISK COUPLING   			BELL  	407   	407         		SW  										T/R DRIVE	DENTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH					53278				DISC DENTED AT FORWARD END OF AFT SHORT SHAFT.						1	G	7	1 	3U			O	H2SW    					 
1999012900411	19990129	00411	SW  	1999	1	29	HEEA060017       	1	19990115	G	6510	406040339111	BEARING         		407040303101	BELL  	407   	407         		SW  										T/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH	289  			AFS1120	53277				FAN SHAFT ASSEMBLY HAS WORN BEARINGS.  SERIAL NUMBERS REMOVED ARE A98-0497 AND A98-0500.						1	G	7	1 	3U			O	H2SW    					 
1999012900412	19990129	00412	SW  	1999	1	29	HEEA060018       	1	19990115	G	6510	206061432121	HOUSING         			BELL  	407   	407         		SW  										BLOWER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				BLOWER HOUSING IS CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999012900413	19990129	00413	SW  	1999	1	29	HEEA060019       	1	19990115	G	7910	206061505115	TANK            			BELL  	407   	407         		SW  										ENGINE OIL	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				TANK ASSEMBLY IS CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999012900414	19990129	00414	SW  	1999	1	29	HEEA060020       	1	19990115	G	7810	407062021101	DUCT            			BELL  	407   	407         		SW  										EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				EXHAUST DUCT CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999012900415	19990129	00415	SW  	1999	1	29	HEEA060021       	1	19990115	G	6510	206061432121	HOUSING         			BELL  	407   	407         		SW  										BLOWER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				BLOWER HOUSING IS CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999012900416	19990129	00416	SW  	1999	1	29	HEEA060022       	1	19990115	G	6500	406040339111	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				TAIL ROTOR HAS WORN AND ROUGH BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999012900417	19990129	00417	SW  	1999	1	29	HEEA060023       	1	19990115	G	2436	206075447101	REGULATOR       			BELL  	407   	407         		SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH					53278				GENERATOR WILL NOT COME ON-LINE.						1	G	7	1 	3U			O	H2SW    					 
1999012900418	19990129	00418	SW  	1999	1	29	HEEA060024       	1	19990115	G	6220	222310504101	BEARING         			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	UNBONDED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	230UN					23009				LOWER PLATE CHAFED AND UNBONDED ON MAIN ROTOR.						1	G	7	2 	3U			NC	H9SW    					 
1999012900419	19990129	00419	SW  	1999	1	29	HEEA060025       	1	19990115	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	1869 				53114				UNIVERSAL HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999012900420	19990129	00420	SW  	1999	1	29	HEEA060026       	1	19990115	G	6330	222010500109	FLEXURE ASSY    			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	CHAFED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	230UN					23009				FLEXURE ASSEMBLY CHAFED.						1	G	7	2 	3U			NC	H9SW    					 
1999012900421	19990129	00421	SW  	1999	1	29	HEEA060027       	1	19990115	G	2510	222020763103	SEAT BACK       			BELL  	230   	230         	1182149	SW  										COCKPIT	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	230UN					23009				SEAT BACK IS BROKEN AT LOWER CORNER.						1	G	7	2 	3U			NC	H9SW    					 
1999012900422	19990129	00422	SW  	1999	1	29	HEEA060028       	1	19990115	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	554  				53159				UNIVERSAL HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999012900423	19990129	00423	SW  	1999	1	29	HEEA060029       	1	19990115	G	3246	206053184121	SKID TUBE       			BELL  	407   	407         		SW  										MLG	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				SKID TUBE ASSEMBLY IS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999012900424	19990129	00424	SW  	1999	1	29	HEEA060030       	1	19990115	G	3246	206053184122	SKID TUBE       			BELL  	407   	407         		SW  										MLG	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				SKID TUBE ASSEMBLY IS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999012900425	19990129	00425	SW  	1999	1	29	HEEA060031       	1	19990115	G	6500	406040339111	BEARING         		406040320101	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH				AFS992	53207				SHAFT ASSEMBLY HAS WORN BEARINGS.  SERIAL NUMBERS REMOVED ARE A98-0545 AND A98-0455.						1	G	7	1 	3U			O	H2SW    					 
1999012900573	19990129	00573	EU  	1999	1	29	HEEA060033       	1	19990115	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6100R					2862				ROD, PITCH CONTROL BEARINGS WORN.						1	G	7	1 	3U				H9EU    					 
1999012900574	19990129	00574	EU  	1999	1	29	HEEA060034       	1	19990115	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z					2820				ROD, PITCH CONTROL BEARINGS WORN.						1	G	7	1 	3U				H9EU    					 
1999012900575	19990129	00575	EU  	1999	1	29	HEEA060035       	1	19990115	G	6730	SC50811	SERVO           			SNIAS 	350   	AS350B2     	8680813	EU  										M/R CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350BZ	2997 				2653				SERVO CONTROL HAS WORN BEARINGS.						1	G	7	1 	3U				H9EU    					 
1999012900576	19990129	00576	EU  	1999	1	29	HEEA060036       	1	19990115	G	6510	350A34021006	SHAFT           			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466	1808 				3004				AFT BEARING INNER RACE MOVED ON SHAFT.						1	G	7	1 	3U				H9EU    					 
1999012900577	19990129	00577	EU  	1999	1	29	HEEA060037       	1	19990115	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				ROD, PITCH CONTROL WORN BEARINGS.  SERIAL NUMBERS REMOVED ARE 2239 AND UNKNOWN S/N.						1	G	7	1 	3U				H9EU    					 
1999012900578	19990129	00578	EU  	1999	1	29	HEEA060038       	1	19990115	G	6220	704A3363310951	STOP ASSY       			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	DETERIORATED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951	1396 				2771				SPHERICAL STOP ASSEMBLY HAS DETERIORATED ELASTOMER.  SERIAL NUMBERS REMOVED ARE 12217, 12216, AND 12215.						1	G	7	1 	3U				H9EU    					 
1999012900579	19990129	00579	EU  	1999	1	29	HEEA060039       	1	19990115	G	6410	355A09103601	BEARINGS        			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				TAIL ROTOR BEARINGS CRACKED AND SEPARATED.						1	G	7	1 	3U				H9EU    					 
1999012900580	19990129	00580	EU  	1999	1	29	HEEA060040       	1	19990115	G	7721	56375600010	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				T4 INDICATOR WILL NOT INDICATE.						1	G	7	1 	3U				H9EU    					 
1999012900581	19990129	00581	EU  	1999	1	29	HEEA060042       	1	19990115	G	6220	350A31190703	STARFLEX        			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z	1169 				2820				STARFLEX HAS SPLINTER ON EDGE.						1	G	7	1 	3U				H9EU    					 
1999012900348	19990129	00348		1999	1	29	HEEA060043       	4	19990120	G	2312	064100900	TRANSCEIVER     			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31219					760230				RADIO INTERMITTENTLY WILL NOT TRANSMIT.						1	G	7	2 	3U				H1NE    					 
1999012900349	19990129	00349		1999	1	29	HEEA060044       	4	19990120	G	2312	064100900	TRANSCEIVER     			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5426U					760167				WHEN TRANSMITTING, FOUND CORES OUT, WEAK, AND BROKEN.						1	G	7	2 	3U				H1NE    					 
1999012900350	19990129	00350		1999	1	29	HEEA060045       	4	19990120	G	3451	066103708	TRANSCEIVER     			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT DME	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4253S					760035				NO OUTPUT, INOPERATIVE.  PERFORMED PRELIMINARY INSPECTION, TROUBLESHOT AND REPLACED F101 DUE TO OPENED AT TURN ON.						1	G	7	2 	3U				H1NE    					 
1999012900351	19990129	00351		1999	1	29	HEEA060046       	4	19990120	G	3434	066104400	RECEIVER        			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911MJ					760231				NO AUDIO, NO LIGHTS.  PERFORMED PRELIMINARY INSPECTION, FOUND UNIT TO HAVE INTERMITTENT AUDIO AND NO LIGHTS.						1	G	7	2 	3U				H1NE    					 
1999012900352	19990129	00352		1999	1	29	HEEA060047       	4	19990120	G	3444	066104800	ALTIMETER       			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545K					760047				RADAR ALTIMETER SHOWS 25 FEET WHEN AIRCRAFT IS LANDED.						1	G	7	2 	3U				H1NE    					 
1999012900353	19990129	00353		1999	1	29	HEEA060048       	4	19990120	G	3454	071121615	CONTROL         			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	707AE					760276				MARKER BEACON INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999012900354	19990129	00354	NE  	1999	1	29	HEEA060049       	1	19990120	G	2435	23081002	STARTER         			SKRSKY	S76   	S76A        	8143006	NE  										START/GENERATOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5128	7072 				760181				ARMATURE BINDING ON STARTER/GENERATOR.						1	G	7	2 	3U				H1NE    					 
1999012900355	19990129	00355		1999	1	29	HEEA060050       	2	19990120	G	7314	3944001	FUEL PUMP       			SKRSKY	S76   	S76A        	8143006	NE  										ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911MJ	711  				760231				FUEL PUMP HAS WORN SPLINES ON DRIVE SHAFT.						1	G	7	2 	3U				H1NE    					 
1999012900356	19990129	00356	NE  	1999	1	29	HEEA060051       	1	19990120	G	2612	473205	DETECTOR        	KIDDE       		SKRSKY	S76   	S76A        	8143006	NE  										ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	792CH					760193				FLAME DETECTOR SHORTS OUT INTERMITTENTLY CAUSING FIRE LIGHT TO COME ON.						1	G	7	2 	3U				H1NE    					 
1999012900357	19990129	00357		1999	1	29	HEEA060052       	4	19990120	G	3451	6221233001	DME             			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	WEAK            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	127FH					760063				WEAK SENSITIVITY AFTER UNIT HEATS UP.						1	G	7	2 	3U				H1NE    					 
1999012900358	19990129	00358		1999	1	29	HEEA060053       	4	19990120	G	3444	7000839904	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										RADIO ALTIMETER	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4253S					760035				INDICATOR LIGHT INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999012900359	19990129	00359		1999	1	29	HEEA060054       	4	19990120	G	2210	7611113	AMPLIFIER       			SKRSKY	S76   	S76A        	8143006	NE  										YAW SLICE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1546G					760076				NR 1 YAW INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999012900360	19990129	00360	NE  	1999	1	29	HEEA060055       	1	19990120	G	6220	7610608000049	DAMPER          			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	792CH					760193				MAIN ROTOR DAMPER INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999012900361	19990129	00361	NE  	1999	1	29	HEEA060056       	1	19990120	G	6220	7610608000049	DAMPER          			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	1545X					760050				MAIN ROTOR DAMPER IS WEAK AND LEAKS.						1	G	7	2 	3U				H1NE    					 
1999012900362	19990129	00362	NE  	1999	1	29	HEEA060057       	1	19990120	G	6220	7610608000050	DAMPER          			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	1545X					760050				MAIN ROTOR DAMPER IS WEAK AND LEAKS.						1	G	7	2 	3U				H1NE    					 
1999012900363	19990129	00363	NE  	1999	1	29	HEEA060058       	1	19990121	G	6210	7615009000046A	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	DEBONDING       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1546K	13125				760082				MAIN ROTOR BLADE HAS SKIN DEBONDING CENTER AT STATION 52 ON THE UPPER SURFACE.						1	G	7	2 	3U				H1NE    					 
1999012900364	19990129	00364	NE  	1999	1	29	HEEA060059       	1	19990121	G	6730	7630103902102	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										SERVO SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122G					760232				ACTUATOR HAS LOTS OF BACKLASH ON SHAFT.						1	G	7	2 	3U				H1NE    					 
1999012900365	19990129	00365	NE  	1999	1	29	HEEA060060       	1	19990121	G	2931	7645001078104	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1547D					760077				HYDRAULIC PRESSURE INDICATOR WENT TO 5000 PSI.   DROPPED BACK TO TOP RED LINE THEN WENT BACK TO 5000 PSI AFTER TAKEOFF.						1	G	7	2 	3U				H1NE    					 
1999012900366	19990129	00366	NE  	1999	1	29	HEEA060061       	1	19990121	G	7712	7645001078106	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										DUAL TORQUE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5435V					760158				DUAL TORQUE INDICATOR'S NR 1 NEEDLE INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999012900367	19990129	00367	NE  	1999	1	29	HEEA060062       	1	19990121	G	7712	7645001078106	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										DUAL TORQUE	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122G					760232				DUAL TORQUE INDICATOR'S NR 1 NEEDLE STICKS.						1	G	7	2 	3U				H1NE    					 
1999012900368	19990129	00368	NE  	1999	1	29	HEEA060063       	1	19990121	G	7712	7645001078106	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										DUAL TORQUE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	706AE					760275				DUAL TORQUE INDICATOR'S NR 2 NEEDLE WOULD NOT MOVE WHEN CALIBRATING.						1	G	7	2 	3U				H1NE    					 
1999012900369	19990129	00369	NE  	1999	1	29	HEEA060064       	1	19990121	G	7931	7645001078120	TRANSMITTER     			SKRSKY	S76   	S76A        	8143006	NE  										ENG OIL PRESSURE	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	792CH					760193				ENGINE OIL PRESSURE INDICATES HIGH.						1	G	7	2 	3U				H1NE    					 
1999012900370	19990129	00370	NE  	1999	1	29	HEEA060065       	1	19990121	G	3150	7655001001103	CAUTION PANEL   			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	127FH					760063				PILOT AND COPILOT CAUTION PANEL RESET INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999012900371	19990129	00371		1999	1	29	HEEA060066       	4	19990121	G	2210	7660002113103	GYRO            			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545K					760047				NR 1 AFCS ROLL CHANNEL CHATTERS.  TIME SINCE REPAIR 82:45 HOURS.						1	G	7	2 	3U				H1NE    					 
1999012900372	19990129	00372		1999	1	29	HEEA060067       	4	19990121	G	2200	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5426U					760167				AFCS ACTUATOR INOPERATIVE.  POTS DEFECTIVE IN NULL POSITION.						1	G	7	2 	3U				H1NE    					 
1999012900373	19990129	00373		1999	1	29	HEEA060068       	4	19990121	G	2200	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22342	8864 				760096				AFCS ACTUATOR KICKS.						1	G	7	2 	3U				H1NE    					 
1999012900374	19990129	00374		1999	1	29	HEEA060069       	4	19990121	G	2200	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22342	5774 				760096				AFCS ACTUATOR'S YAW CHANNEL INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999012900375	19990129	00375		1999	1	29	HEEA060070       	4	19990121	G	2210	7690001808102	RATE GYRO       			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545X					760050				GP RATE OF TURN, GYRO FLAG DOES NOT PULL.						1	G	7	2 	3U				H1NE    					 
1999012900376	19990129	00376	NE  	1999	1	29	HEEA060071       	1	19990121	G	6240	7690001881103	AMPLIFIER       			SKRSKY	S76   	S76A        	8143006	NE  										VIB ABSORBER	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1547D					760077				VIBRATION INCREASES WHEN VTA IS TURNED ON.						1	G	7	2 	3U				H1NE    					 
1999012900377	19990129	00377		1999	1	29	HEEA060072       	4	19990121	G	3457	8143902240B	GPS             			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545X					760050				GPS INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999012900378	19990129	00378		1999	1	29	HEEA060073       	4	19990121	G	3457	8143902240B	GPS             			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1546G					760076				GPS RECEIVER SWITCHES TO AUX FROM NAV FUNCTION BY ITSELF.						1	G	7	2 	3U				H1NE    					 
1999012900379	19990129	00379	NE  	1999	1	29	HEEA060074       	1	19990121	G	2460	A1077B	RELAY           			SKRSKY	S76   	S76A        	8143006	NE  										FLT COMPARTMENT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911MJ					760231				RELAY INTERMITTENT.						1	G	7	2 	3U				H1NE    					 
1999012900380	19990129	00380	NE  	1999	1	29	HEEA060075       	1	19990121	G	6210	SB7004103	BEARING         			SKRSKY	S76   	S76A        	8143006	NE  										M/R SPINDLE	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5128					760181				BEARING REMOVED FROM SPINDLE ASSY S/N A134-02545 DUE TO ELASTOMERIC SEPARATION.  REPLACED WITH SERVICEABLE BEARING.						1	G	7	2 	3U				H1NE    					 
1999012900381	19990129	00381		1999	1	29	HEEA060076       	4	19990121	G	3457	0110010400	GPS             			KING A														COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	30PH					BB635				NO ALTITUDE INPUT MESSAGE DISPLAYED UPON POWER UP.																			 
1999012900382	19990129	00382		1999	1	29	HEEA060077       	2	19990121	G	7510	1092T1002W	SERVO MOTOR     																	ENGINE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										SERVO MOTOR DOES NOT OPERATE.																			 
1999012900383	19990129	00383		1999	1	29	HEEA060078       	3	19990121	G	6140	503890571	TACH GENERATOR  			BEECH 	200   	200BEECH    	1152920	CE  										ENGINE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	789DS					BB478				TACHOMETER/GENERATOR MALFUNCTIONS AFTER APPROXIMATELY 10 MINUTES IN WARM-UP FLIGHT.						1	L	7	2 	4T				A24CE   					 
1999012900384	19990129	00384		1999	1	29	HEEA060079       	1	19990121	G	6710	C4264215	SLIDE & SLEEVE  																	M/R CONTROL	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03										SLIDE AND SLEEVE SERVO, S/N RH-3811A, DURING TESTING, EXCESSIVE LEAKAGE COMING FROM PRIMARY SPOOL OF LAP ASSY WITHOUT CY	CLING LEVER.																		 
1999012900385	19990129	00385		1999	1	29	HEEA060080       	1	19990121	G	6710	C4264215	SLIDE & SLEEVE  																	M/R CONTROL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										SLIDE AND SLEEVE SERVO, S/N RH-0730A, CAUSED BINDING WHEN RETURNING TO NEUTRAL POSITION FROM OVERRIDE POSITION.																			 
1999012900386	19990129	00386	NE  	1999	1	29	HEEA060081       	2	19990121	G	7200	3017600	ENGINE          			BELL  	212   	212         	1181420	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					ENGINE BAY	OVERTEMP        	E			HEEA	O				OTHER                   				M	J		OVER TEMP                 	WARNING INDICATION        		NR	NOT REPORTED   	1			SW	03	1082G	13587				31109				ITT ABOVE 900 DEGREES FOR OVER 40 SECONDS.						1	G	7	1 	4U	4	U		H4SW    	E22EA				 
1999012900426	19990129	00426	SW  	1999	1	29	HEEA060083       	1	19990121	G	3340	01077028511	LIGHT           			BELL  	214   	214ST       	1182106	SW  										STROBE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				STROBE LIGHT INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999012900427	19990129	00427		1999	1	29	HEEA060084       	4	19990121	G	2312	066106600	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				TRANSCEIVER INOPERATIVE; HEAVY CORROSION.  BURNT COMPONENTS ON MODULATOR BOARD.						2	G	7	2 	4U				H10SW   					 
1999012900428	19990129	00428		1999	1	29	HEEA060085       	4	19990121	G	3451	066106602	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT DME	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				TRANSCEIVER INOPERATIVE; WILL NOT TURN ON.						2	G	7	2 	4U				H10SW   					 
1999012900429	19990129	00429	SW  	1999	1	29	HEEA060086       	1	19990121	G	6710	214001370101	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										M/R CONTROL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				AARS PITCH WOULD NOT ENGAGE OR MONITOR TEST.						2	G	7	2 	4U				H10SW   					 
1999012900430	19990129	00430	SW  	1999	1	29	HEEA060087       	1	19990121	G	6720	214001540111	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										YAW CHANNEL	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				ACTUATOR ASSY INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999012900431	19990129	00431	SW  	1999	1	29	HEEA060088       	1	19990121	G	6720	214001970111	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										YAW CHANNEL	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				ACTUATOR INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999012900432	19990129	00432		1999	1	29	HEEA060089       	4	19990121	G	2210	214074305105	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										FBW ELEVATOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				AMPLIFIER WILL NOT STAY ON LINE.						2	G	7	2 	4U				H10SW   					 
1999012900433	19990129	00433	SW  	1999	1	29	HEEA060090       	1	19990121	G	6710	214001970111	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										MAIN ROTOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				ACTUATOR WILL NOT MONITOR TEST AND KICKS OFF.						2	G	7	2 	4U				H10SW   					 
1999012900434	19990129	00434	SW  	1999	1	29	HEEA060091       	1	19990121	G	6720	214010200111	PITCH HORN      			BELL  	214   	214ST       	1182106	SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y	2387 				28139				PITCH HORN REMOVED DUE TO EXCESSIVE PLAY IN SHAFT AREA.  WHEN REMOVING HOUSING, NOTICED MOISTURE HAD BUILT UP INSIDE.  I	NSP OF HOUSING REVEALED WORN GEAR, P/N 214-010-210-103, HAD TWO TEETH BROKEN OFF SHAFT.  SUBMITTER STATED FURTHER TEARDO	WN INDICATED SHAFT ASSY INCORRECTLY REBUILT BY PREVIOUS VENDOR, RADIUS RING, P/N 214-010-206-001, INSTALLED BACKWARDS WI	TH SHARP EDGE TOWARDS RADIUS ON PITCH HORN SHAFT, P/N 214-010-203-003.  ALL BEARINGS AND RACES EXHIBITED BRINELLING AND 	CORROSION FAILURE.   PITCH HORN SHAFT, P/N 214-010-203-003, EXHIBITED CORROSION AND BRINELLING.  PITCH HORN, P/N 214-010	-201-111, WAS FOUND UNSERVICEABLE DUE TO HEAVY CORROSION IN BORE AREA BEYOND OEM SPECS.  REPLACED PITCH HORN AND ASSY.	2	G	7	2 	4U				H10SW   					 
1999012900435	19990129	00435	SW  	1999	1	29	HEEA060092       	1	19990121	G	3212	214052200107	FLOAT           			BELL  	214   	214ST       	1182106	SW  										AFT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	8045T	1164 				28101				AFT FLOAT LEAKING AT SEAMS.						2	G	7	2 	4U				H10SW   					 
1999012900436	19990129	00436	SW  	1999	1	29	HEEA060093       	1	19990121	G	2435	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										START/GENERATOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				STARTER SLOW TO SPOOL UP.						2	G	7	2 	4U				H10SW   					 
1999012900437	19990129	00437	SW  	1999	1	29	HEEA060094       	1	19990121	G	2842	214066212105	PROBE           			BELL  	214   	214ST       	1182106	SW  										FUEL SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M					28102				PROBE HAS ERRATIC READINGS.						2	G	7	2 	4U				H10SW   					 
1999012900438	19990129	00438		1999	1	29	HEEA060096       	4	19990121	G	2210	214074104101	SENSOR          			BELL  	214   	214ST       	1182106	SW  										SCAS SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				SCAS PITCH TRIPS IN-FLIGHT.						2	G	7	2 	4U				H10SW   					 
1999012900439	19990129	00439	SW  	1999	1	29	HEEA060097       	1	19990121	G	2913	214076334101	PUMP            			BELL  	214   	214ST       	1182106	SW  										HYDRAULIC SYS	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				HYDRAULIC PUMP MAKING METAL.						2	G	7	2 	4U				H10SW   					 
1999012900440	19990129	00440	SW  	1999	1	29	HEEA060098       	1	19990121	G	3150	214175122107	CAUTION PANEL   			BELL  	214   	214ST       	1182106	SW  										COCKPIT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				BAGGAGE AND BRAKE SEGMENTS DAMAGED ON CAUTION PANEL.						2	G	7	2 	4U				H10SW   					 
1999012900441	19990129	00441	SW  	1999	1	29	HEEA060099       	1	19990121	G	3150	214175122105	CAUTION PANEL   			BELL  	214   	214ST       	1182106	SW  										COCKPIT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				SPARE LIGHT SEGMENT LENS MISSING ON CAUTION PANEL.						2	G	7	2 	4U				H10SW   					 
1999012900442	19990129	00442	SW  	1999	1	29	HEEA060100       	1	19990121	G	2434	214175150105	GENERATOR       			BELL  	214   	214ST       	1182106	SW  										DC SYSTEM	BENT            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				SHAFT IS BENT ON GENERATOR.						2	G	7	2 	4U				H10SW   					 
1999012900443	19990129	00443	SW  	1999	1	29	HEEA060101       	1	19990121	G	7714	214175251111FM	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										TRIPLE TACH	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				TRIPLE TACHOMETER HAS ERRATIC OPERATION.						2	G	7	2 	4U				H10SW   					 
1999012900444	19990129	00444		1999	1	29	HEEA060102       	4	19990121	G	3414	214175299107	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				INSTRUMENT INDICATES APPROXIMATELY 10 KNOTS STATIC.						2	G	7	2 	4U				H10SW   					 
1999012900445	19990129	00445	SW  	1999	1	29	HEEA060103       	1	19990121	G	2432	214175379103	CHARGER         			BELL  	214   	214ST       	1182106	SW  										BATTERY BAY	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				BATTERY CHARGER WILL NOT TOP CHARGE BATTERY.						2	G	7	2 	4U				H10SW   					 
1999012900446	19990129	00446	SW  	1999	1	29	HEEA060104       	1	19990121	G	2432	214175379103	CHARGER         			BELL  	214   	214ST       	1182106	SW  										BATTERY BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				BATTERY CHARGER NOT CHARGING.						2	G	7	2 	4U				H10SW   					 
1999012900447	19990129	00447		1999	1	29	HEEA060105       	4	19990121	G	2212	222305005101	SENSOR          			BELL  	214   	214ST       	1182106	SW  										AFCS	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				ALTITUDE SENSOR ERRATIC ABOVE 1,000 FEET.						2	G	7	2 	4U				H10SW   					 
1999012900448	19990129	00448	SW  	1999	1	29	HEEA060106       	1	19990121	G	7712	222375077111	TRANSMITTER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				TRANSMITTER WILL NOT FUNCTION.						2	G	7	2 	4U				H10SW   					 
1999012900449	19990129	00449		1999	1	29	HEEA060107       	4	19990121	G	3422	2594484	TRANSMITTER     			BELL  	214   	214ST       	1182106	SW  										FLUX VALVE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				TRANSMITTER HAS NO OUTPUT.						2	G	7	2 	4U				H10SW   					 
1999012900450	19990129	00450	SW  	1999	1	29	HEEA060108       	1	19990121	G	2435	36B510954G2	CLUTCH          			BELL  	214   	214ST       	1182106	SW  										START/GENERATOR	SLIPPAGE        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				CLUTCH SLIPPAGE TORQUE IS LOW 275 INCHES/POUNDS.						2	G	7	2 	4U				H10SW   					 
1999012900451	19990129	00451	SW  	1999	1	29	HEEA060109       	1	19990121	G	2435	36B510954G2	CLUTCH          		214060056103	BELL  	214   	214ST       	1182106	SW  										START/GENERATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N	1534 			93H1173	28106				CLUTCH FAILED TORQUE SLIPPAGE TEST, SLIPS AT 300 INCHES/POUNDS AND HAS EXCESSIVE END PLAY AT .017 INCH.						2	G	7	2 	4U				H10SW   					 
1999012900452	19990129	00452		1999	1	29	HEEA060110       	4	19990121	G	2312	40008310103	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				TRANSCEIVER HAS EXCESSIVE GAIN ON 20 MILE AND 40 MILE RANGE.						2	G	7	2 	4U				H10SW   					 
1999012900453	19990129	00453		1999	1	29	HEEA060111       	4	19990121	G	3442	40008310105	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				TRANSCEIVER INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999012900454	19990129	00454		1999	1	29	HEEA060112       	4	19990121	G	3442	40008310105	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				R/T HAS FAULTY DISPLAY.						2	G	7	2 	4U				H10SW   					 
1999012900455	19990129	00455		1999	1	29	HEEA060113       	4	19990121	G	2211	4033089901	COMPUTER        			BELL  	214   	214ST       	1182106	SW  										AUTOFLIGHT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				AUTOPILOT WILL NOT TRACK IN NAV MODE.						2	G	7	2 	4U				H10SW   					 
1999012900456	19990129	00456		1999	1	29	HEEA060114       	4	19990121	G	2211	4033089901	COMPUTER        			BELL  	214   	214ST       	1182106	SW  										AUTOFLIGHT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				COMPUTER FAILED 2.1 ON SST BENCH.						2	G	7	2 	4U				H10SW   					 
1999012900457	19990129	00457		1999	1	29	HEEA060115       	4	19990121	G	3444	7000839904	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										RADIO ALTIMETER	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				RADIO ALTIMETER INDICATOR DOES NOT TEST, PULL FLAG OR INDICATE.						2	G	7	2 	4U				H10SW   					 
1999012900458	19990129	00458	SW  	1999	1	29	HEEA060116       	1	19990121	G	3340	7028521	LIGHT           			BELL  	214   	214ST       	1182106	SW  										STROBE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				STROBE LIGHT CAUSES ANTI-COLLISION CIRCUIT BREAKER TO TRIP.						2	G	7	2 	4U				H10SW   					 
1999012900459	19990129	00459	SW  	1999	1	29	HEEA060117       	1	19990121	G	3340	7028501	STROBE          			BELL  	214   	214ST       	1182106	SW  										STROBE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				STROBE LIGHT TRIPS CIRCUIT BREAKER.						2	G	7	2 	4U				H10SW   					 
1999012900460	19990129	00460		1999	1	29	HEEA060118       	4	19990121	G	2370	93A15130	CONTROL UNIT    			BELL  	214   	214ST       	1182106	SW  										E/E BAY	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				CVR CONTROL HAS TRANSISTOR LOOSE INSIDE UNIT.						2	G	7	2 	4U				H10SW   					 
1999012900461	19990129	00461	SW  	1999	1	29	HEEA060119       	1	19990121	G	2822	9A1746	PUMP            			BELL  	214   	214ST       	1182106	SW  										ENGINE FUEL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				CARTRIDGE INOPERATIVE.   MOTOR NOT FUNCTIONING.						2	G	7	2 	4U				H10SW   					 
1999012900462	19990129	00462	SW  	1999	1	29	HEEA060120       	1	19990121	G	2822	9A1746	PUMP            			BELL  	214   	214ST       	1182106	SW  										ENGINE FUEL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M					28102				CARTRIDGE WILL NOT FUNCTION.						2	G	7	2 	4U				H10SW   					 
1999012900463	19990129	00463		1999	1	29	HEEA060121       	4	19990121	G	3442	MI5853013	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				INDICATOR GOES INTO WAIT MODE AFTER ONE HOUR OF USE.						2	G	7	2 	4U				H10SW   					 
1999012900464	19990129	00464		1999	1	29	HEEA060122       	4	19990121	G	3414	214175299107	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	READS LOW       	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	59805					28141				INDICATOR INDICATES 10 KNOTS LOW OVER 100 KNOTS AIRSPEED.						2	G	7	2 	4U				H10SW   					 
1999012900465	19990129	00465	SW  	1999	1	29	HEEA060123       	1	19990121	G	6240	412075010109	INDICATOR       			BELL  	412   	412         	1182202	SW  										ROTOR TACH	READS HIGH      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2149S					36002				ROTOR TACHOMETER INDICATOR'S N2 INDICATES 2 PERCENT HIGH.						1	G	7	2 	4U				H4SW    					 
1999012900466	19990129	00466	SW  	1999	1	29	HEEA060124       	1	19990121	G	2822	205060606003	PUMP            			BELL  	212   	212         	1181420	SW  										FUEL BOOST	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1079U					31122				LOW FUEL PRESSURE.						1	G	7	1 	4U				H4SW    					 
1999012900467	19990129	00467	SW  	1999	1	29	HEEA060125       	1	19990121	G	2140	205072277009	VALVE           			BELL  	212   	212         	1181420	SW  										HEATER	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										MIXING VALVE NOT FUNCTIONING.						1	G	7	1 	4U				H4SW    					 
1999012900468	19990129	00468	SW  	1999	1	29	HEEA060126       	1	19990121	G	6230	212040136001	BEARING         		204040366021	BELL  	212   	212         	1181420	SW  										MAST	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3131S				A5580	30953				BALLS BREAKING DOWN.  REPLACED WITH SERVICEABLE BEARINGS.						1	G	7	1 	4U				H4SW    					 
1999012900469	19990129	00469	SW  	1999	1	29	HEEA060127       	1	19990121	G	7712	212070160007	INDICATOR       			BELL  	212   	212         	1181420	SW  										TORQUE METER	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5010F					30936				TORQUE METER INDICATOR'S NR 1 NEEDLE STICKS.						1	G	7	1 	4U				H4SW    					 
1999012900470	19990129	00470	SW  	1999	1	29	HEEA060128       	1	19990121	G	2910	212076015001	VALVE           			BELL  	212   	212         	1181420	SW  										HYD CHECK	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3208H					31304				LOWER FITTING CRACKED ON VALVE.						1	G	7	1 	4U				H4SW    					 
1999012900471	19990129	00471		1999	1	29	HEEA060129       	4	19990121	G	3100	212075562003	INDICATOR       			BELL  	212   	212         	1181420	SW  										ITT	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	102PH					30899				ITT INDICATOR READS 125 DEGREES HIGH.						1	G	7	1 	4U				H4SW    					 
1999012900472	19990129	00472	SW  	1999	1	29	HEEA060130       	1	19990121	G	2822	2C273	CARTRIDGE       			BELL  	212   	212         	1181420	SW  										FUEL BOOST	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										FUEL CARTRIDGE UNIT MISSING INLET SCREEN AND UMBRELLA CHECK VALVE.						1	G	7	1 	4U				H4SW    					 
1999012900473	19990129	00473	SW  	1999	1	29	HEEA060131       	1	19990121	G	3212	30905	VALVE           			BELL  	212   	212         	1181420	SW  										FLOAT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5736D					31135				UNCOMMANDED FLOAT INFLATION.  AT TIME OF INFLATION, AIRCRAFT HAD BEEN SHUT DOWN FOR TWO HOURS, THE BATTERIES WERE OFF, T	HE MANUAL INFLATION HANDLE WAS IN THE DOWN AND SAFTIED POSITION.  INSPECTED AIRCRAFT INFLATION RIGGING, FOUND OK.  ELECT	RICAL SQUIB HAD NOT BEEN ACTIVATED.  REPLACED FLOAT INFLATION VALVE ASSY AND RESERVICED FLOAT BOTTLE.				1	G	7	1 	4U				H4SW    					 
1999012900474	19990129	00474	SW  	1999	1	29	HEEA060132       	1	19990121	G	3212	30905	VALVE           			BELL  	212   	212         	1181420	SW  										FLOAT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3131S					30953				VALVE ASSEMBLY HAS BLANK INDICATOR, SYSTEM DEAD.						1	G	7	1 	4U				H4SW    					 
1999012900475	19990129	00475		1999	1	29	HEEA060133       	4	19990122	G	3457	0110005400	GPS             																	COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										GPS 150 WILL NOT ACQUIRE SATELLITE STATIONS.																			 
1999012900476	19990129	00476		1999	1	29	HEEA060134       	4	19990122	G	3457	0110005400	GPS             			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6748D					51106				GPS 150 INOPERATIVE, FACE PLATE BROKEN ON RIGHT HAND SIDE.						1	G	7	1 	3U				H2SW    					 
1999012900477	19990129	00477		1999	1	29	HEEA060135       	4	19990122	G	3457	0110005400	GPS             			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108PH					51334				GPS 150 WILL NOT HOLD MEMORY AND INTERNAL BATTERY IS DEAD.						1	G	7	1 	3U				H2SW    					 
1999012900478	19990129	00478		1999	1	29	HEEA060136       	4	19990122	G	3457	0110005400	GPS             			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A					51611				ENT AND NAV BUTTONS UNREADABLE ON GPS 150.						1	G	7	1 	3U				H2SW    					 
1999012900479	19990129	00479		1999	1	29	HEEA060137       	4	19990122	G	3457	0110005400	GPS             			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21497					51518				GPS 150 TAKES TOO LONG TO COME ON-LINE AND START WORKING.  PERFORMED PRELIMINARY INSPECTION AND FOUND UNIT TAKES LONG TO	 PICK UP SATELLITES AND UNIT HAS SEVERAL UNREADABLE BUTTONS.					1	G	7	1 	3U				H2SW    					 
1999012900480	19990129	00480		1999	1	29	HEEA060138       	4	19990122	G	3457	0110005400	GPS             			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21497					51518				GPS 150 WILL NOT DISPLAY BEARING.  PERFORMED PRELIMINARY INSPECTION AND FOUND UNIT WILL NOT DISPLAY BEARING AND ALSO WPT	 INDICATOR INOPERATIVE.					1	G	7	1 	3U				H2SW    					 
1999012900481	19990129	00481		1999	1	29	HEEA060139       	4	19990122	G	2312	064101900	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	83MT					45492				VERY WEAK POWER OUTPUT.						1	G	7	1 	3U				H2SW    					 
1999012900482	19990129	00482		1999	1	29	HEEA060140       	4	19990122	G	2312	064101900	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1076T					45373				NO TRANSMIT AND NO DISPLAY.						1	G	7	1 	3U				H2SW    					 
1999012900483	19990129	00483		1999	1	29	HEEA060141       	4	19990122	G	2312	064101900	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6160Y					51609				DIGITS FADE IN AND OUT.						1	G	7	1 	3U				H2SW    					 
1999012900484	19990129	00484		1999	1	29	HEEA060142       	4	19990122	G	2312	064101902	TRANSCEIVER     																	COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ON INITIAL INSTALLATION, UNIT WOULD NOT TRANSMIT.  PERFORMED PRELIMINARY INSPECTION AND FOUND NO MODULATION.  REPLACED Q	120, Q121, AND Q122, MODULATION PRESENT BUT UNABLE TO ADJUST TO SPECS.  ALSO OUTPUT POWER TOO HIGH.																		 
1999012900485	19990129	00485		1999	1	29	HEEA060143       	4	19990122	G	2312	064101902	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8588X					51486				WEAK WITH STATIC.						1	G	7	1 	3U				H2SW    					 
1999012900486	19990129	00486		1999	1	29	HEEA060144       	4	19990122	G	2312	064101902	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	513EH					45421				LOSES DISPLAY AFTER WARM UP AND POWER IS BELOW SPECS.						1	G	7	1 	3U				H2SW    					 
1999012900487	19990129	00487		1999	1	29	HEEA060145       	4	19990122	G	2312	064105430	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A					51611				TRANSCEIVER RECEIVER INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999012900488	19990129	00488		1999	1	29	HEEA060146       	4	19990122	G	2312	064105430	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2124Z					45646				TWO YEAR INSPECTION.  PERFORMED PRELIMINARY INSPECTION ON TRANSCEIVER AND FOUND UNIT TRANSMITTING ONLY 5 WATTS OF POWER 	OUT, INTERMITTENTLY GOING TO ZERO WATTS.  ALSO FOUND FREQUENCY 118.00 MHZ NOT TRANSMITTING ON CORRECT FREQUENCY.  FOUND 	DISPLAY TO GO OUT TWICE.  ALL POWER SUPPLY VOLTAGES ARE GOOD.				1	G	7	1 	3U				H2SW    					 
1999012900489	19990129	00489		1999	1	29	HEEA060147       	4	19990122	G	2312	064105430	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3108E					51498				TRANSMITTER DIES AFTER SEVERAL KEYINGS AND SEVERAL MINUTES.						1	G	7	1 	3U				H2SW    					 
1999012900490	19990129	00490		1999	1	29	HEEA060148       	4	19990122	G	2312	064105430	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5007N					45184				USE SIDE OF DISPLAY UNREADABLE ON TRANSCEIVER.  ONLY KHZ NUMBERS ARE DISPLAYED AND R604 SMOKES.						1	G	7	1 	3U				H2SW    					 
1999012900491	19990129	00491	SW  	1999	1	29	HEEA060149       	1	19990122	G	3412	066106103	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2772A					45311				RADAR ALTIMETER OFF 300 FEET AND ERRATIC.						1	G	7	1 	3U				H2SW    					 
1999012900492	19990129	00492		1999	1	29	HEEA060150       	4	19990122	G	3452	066106200	TRANSPONDER     			BELL  	206   	206L4       	1182110	SW  										COCKPIT	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7077B					52037				TRANSPONDER REPORTED INOPERATIVE.  PERFORMED PRELIMINARY INSPECTION AND FOUND SENSITIVITY WEAK AND ERRATIC.  UNABLE TO A	DJUST.					1	G	7	1 	3U			NC	H2SW    					 
1999012900493	19990129	00493		1999	1	29	HEEA060151       	4	19990122	G	3452	066106200	TRANSPONDER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	11027					45411				TRANSPONDER WILL NOT TRANSMIT.						1	G	7	1 	3U				H2SW    					 
1999012900494	19990129	00494		1999	1	29	HEEA060152       	4	19990122	G	3452	066106200	TRANSPONDER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1078G					45398				TRANSPONDER TRANSMITTING WRONG CODE.  PERFORMED PRELIMINARY INSPECTION AND COULD NOT DUPLICATE PROBLEM.  BENCH CHECK GOO	D.					1	G	7	1 	3U				H2SW    					 
1999012900495	19990129	00495		1999	1	29	HEEA060153       	4	19990122	G	3452	066106200	TRANSPONDER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3905B					45598				TRANSPONDER HAS INOPERATIVE MODE A.						1	G	7	1 	3U				H2SW    					 
1999012900496	19990129	00496		1999	1	29	HEEA060154       	4	19990122	G	3452	066106200	TRANSPONDER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	513EH					45421				TRANSPONDER INOPERATIVE, WILL NOT TURN ON.						1	G	7	1 	3U				H2SW    					 
1999012900497	19990129	00497		1999	1	29	HEEA060155       	4	19990122	G	3452	066106200	TRANSPONDER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8594X					51531				TRANSPONDER IS OFF FREQUENCY.						1	G	7	1 	3U				H2SW    					 
1999012900498	19990129	00498		1999	1	29	HEEA060157       	4	19990122	G	3454	066106700	RECEIVER        			BELL  	206   	206L1       	1182107	SW  										COCKPIT	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5744Y					45465				RECEIVER HAS INACCURATE HEADINGS.						1	G	7	1 	3U				H2SW    					 
1999012900499	19990129	00499		1999	1	29	HEEA060158       	4	19990122	G	3425	066304604	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	979BH					51403				REAR CONNECTOR PULLED LOOSE, DIRECTIONAL GYRO INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999012900500	19990129	00500		1999	1	29	HEEA060159       	4	19990122	G	3444	066305401	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										RADAR ALTIMETER	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8594X					51531				CANNOT CALIBRATE RADAR ALTIMETER TO SPECS.						1	G	7	1 	3U				H2SW    					 
1999012900501	19990129	00501		1999	1	29	HEEA060160       	4	19990122	G	3453	066402600	RECEIVER        			BELL  	206   	206L1       	1182107	SW  										LORAN	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	27766					45312				RIGHT OUTER KNOB PULLS OUT BUT DOES NOT SCROLL NUMBERS ON LORAN.						1	G	7	1 	3U				H2SW    					 
1999012900502	19990129	00502		1999	1	29	HEEA060161       	4	19990122	G	3453	066402600	RECEIVER        			BELL  	206   	206L3       	1182108	SW  										LORAN	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	206FS					51506				RIGHT INSIDE KNOB STEM POWER OUT WITH KNOB ON LORAN.						1	G	7	1 	3U				H2SW    					 
1999012900503	19990129	00503		1999	1	29	HEEA060162       	4	19990122	G	2312	069102100	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1077A					45382				WILL NOT RECEIVE OR TRANSMIT.						1	G	7	1 	3U				H2SW    					 
1999012900504	19990129	00504		1999	1	29	HEEA060163       	4	19990122	G	2312	069102100	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2250U					45754				STATIC NOISE ON ANY REQUENCY.						1	G	7	1 	3U				H2SW    					 
1999012900505	19990129	00505		1999	1	29	HEEA060164       	4	19990122	G	2312	069102435	RECEIVER        			BELL  	206   	206L3       	1182108	SW  										NAV/COMM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251X					51552				INOPERATIVE.  DISPLAY BOARD HAS A BURN HOLE ON HIGH VOLTAGE LINE.						1	G	7	1 	3U				H2SW    					 
1999012900506	19990129	00506		1999	1	29	HEEA060165       	4	19990122	G	2312	069102505	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										NAVIGATION	WEAK            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251V					51404				NAV RECEIVER SENSITIVITY WEAK.						1	G	7	1 	3U				H2SW    					 
1999012900507	19990129	00507		1999	1	29	HEEA060166       	4	19990122	G	3457	0845000000	GPS             			BELL  	206   	206L4       	1182110	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	62127					52023				GPS NOT FUNCTIONING CORRECTLY.						1	G	7	1 	3U			NC	H2SW    					 
1999012900508	19990129	00508		1999	1	29	HEEA060167       	4	19990122	G	3457	0845000000	GPS             			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2775A					45297				2 YEAR INSPECTION ON SKYNAV 5000.  FOUND UNIT NOT PICKING UP SATELLITE SIGNAL.						1	G	7	1 	3U				H2SW    					 
1999012900509	19990129	00509		1999	1	29	HEEA060168       	4	19990122	G	3422	103002201	GYRO            			BELL  	206   	206L1       	1182107	SW  										COCKPIT	PRECESSES       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5007Q					45187				DIRECTIONAL GYRO PRECESSES EXCESSIVELY.						1	G	7	1 	3U				H2SW    					 
1999012900510	19990129	00510	SW  	1999	1	29	HEEA060169       	1	19990122	G	2436	104217A	REGULATOR       			BELL  	206   	206B3       	1181506	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2272J					3620				VOLTAGE REGULATOR WILL NOT MAINTAIN 28 VOLTS.						1	G	7	1 	3U				H2SW    					 
1999012900511	19990129	00511		1999	1	29	HEEA060170       	4	19990122	G	3457	13824120234	GPS RECEIVER    			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	129MR					51129				GPS RECEIVER HAD BATTERY WARNING.  RECEIVER FAIL WARNING.  FOUND GLASS BROKEN ON LED SEGMENT.						1	G	7	1 	3U				H2SW    					 
1999012900512	19990129	00512		1999	1	29	HEEA060171       	4	19990122	G	3457	13824120234	GPS RECEIVER    			BELL  	206   	206B3       	1181506	SW  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	107PH					2789				GPS RECEIVER INTERMITTENTLY LOCKING ON TO SATELLITES.   DROPPING OFF-LINE AND DEAD RECKONING AFTER 30 MINUTES.  TIME SIN	CE REPAIR 74:25 HOURS.					1	G	7	1 	3U				H2SW    					 
1999012900513	19990129	00513		1999	1	29	HEEA060172       	4	19990122	G	3457	13824120234	GPS RECEIVER    			BELL  	206   	206B3       	1181506	SW  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22751					3627				GPS RECEIVER INTERMITTENT.  LOSES ITSELF.  COULD NOT DUPLICATE PROBLEM.  PERFORMED PRELIMINARY INSPECTION AND UNIT WOULD	 NOT PASS GPS TEST AND ALSO NEEDS NEW KEYCAPS.					1	G	7	1 	3U				H2SW    					 
1999012900514	19990129	00514		1999	1	29	HEEA060173       	4	19990122	G	3457	13824120234	GPS RECEIVER    			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A					51611				GPS RECEIVER BURNT UP.						1	G	7	1 	3U				H2SW    					 
1999012900515	19990129	00515		1999	1	29	HEEA060174       	4	19990122	G	3457	13824120234	GPS RECEIVER    			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	513EH					45421				GPS RECEIVES NO SIGNAL.  FOUND UNIT DISPLAYING RECEIVER FAIL MESSAGE.						1	G	7	1 	3U				H2SW    					 
1999012900516	19990129	00516		1999	1	29	HEEA060175       	4	19990122	G	3457	13824120234	GPS RECEIVER    			BELL  	206   	206B3       	1181506	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2268V					3605				GPS RECEIVER INOPERATIVE.  DISPLAYS RECEIVER FAIL AND BATTERY BACK-UP FAIL.						1	G	7	1 	3U				H2SW    					 
1999012900517	19990129	00517	SW  	1999	1	29	HEEA060176       	1	19990122	G	2436	15891F	REGULATOR       			BELL  	206   	206B3       	1181506	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2277A					3630				REGULATOR INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999012900518	19990129	00518		1999	1	29	HEEA060177       	4	19990122	G	3457	1624820	ANTENNA         			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	45RP	459  				45521				ANTENNA HAS NO FIX.						1	G	7	1 	3U				H2SW    					 
1999012900519	19990129	00519	SW  	1999	1	29	HEEA060178       	1	19990122	G	2822	164A199	BOOST PUMP      			BELL  	206   	206L1       	1182107	SW  										FUEL SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	10778					45391				BOOST PUMP RIGHT HAND PUMP INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999012900520	19990129	00520	SW  	1999	1	29	HEEA060179       	1	19990122	G	7930	174035201	INDICATOR       		174083904   	BELL  	206   	206L3       	1182108	SW  										ENGINE OIL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6603X					51412				INDICATOR WAS REMOVED FROM BOWL AND CLEANED.  INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK.						1	G	7	1 	3U				H2SW    					 
1999012900521	19990129	00521	SW  	1999	1	29	HEEA060180       	1	19990122	G	7930	174035201	INDICATOR       		174083904   	BELL  	206   	206L3       	1182108	SW  										ENGINE OIL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8592X					51508				INDICATOR WAS REMOVED FROM BOWL AND CLEANED.   INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK.						1	G	7	1 	3U				H2SW    					 
1999012900522	19990129	00522	SW  	1999	1	29	HEEA060181       	1	19990122	G	7930	1740352	INDICATOR       		1740839     	BELL  	206   	206L3       	1182108	SW  										ENGINE OIL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6160Z					51610				INDICATOR WAS REMOVED FROM BOWL AND CLEANED.   INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK.						1	G	7	1 	3U				H2SW    					 
1999012900523	19990129	00523	SW  	1999	1	29	HEEA060182       	1	19990122	G	6220	206001713101	SUPPORT         			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1076Y					45380				SUPPORT ASSEMBLY CORRODED BEYOND LIMITS.  SCRAPPED AND REPLACED WITH SERVICEABLE SUPPORT.						1	G	7	1 	3U				H2SW    					 
1999012900524	19990129	00524	SW  	1999	1	29	HEEA060183       	1	19990122	G	6220	206001713001	SUPPORT         			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2761N					45277				SUPPORT ASSEMBLY CORRODED BEYOND LIMITS.  SCRAPPED AND REPLACED WITH SERVICEABLE SUPPORT.						1	G	7	1 	3U				H2SW    					 
1999012900525	19990129	00525	SW  	1999	1	29	HEEA060184       	1	19990122	G	6230	206010421003	BUSHING         		206010450113	BELL  	206   	206L3       	1182108	SW  										SWASHPLATE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41128				RIJG10015	51134				SWASHPLATE WORN.  REPLACED BUSHINGS AND RETURNED SWASHPLATE ASSY TO SERVICE.						1	G	7	1 	3U				H2SW    					 
1999012900526	19990129	00526	SW  	1999	1	29	HEEA060185       	1	19990122	G	6230	206010421011	BUSHING         		206010450113	BELL  	206   	206L3       	1182108	SW  										SWASHPLATE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41128				RIJG10015	51134				SWASHPLATE WORN.  REPLACED BUSHINGS AND RETURNED SWASHPLATE ASSY TO SERVICE.						1	G	7	1 	3U				H2SW    					 
1999012900527	19990129	00527	SW  	1999	1	29	HEEA060186       	1	19990122	G	6230	206010459001	BUSHING         		206010450113	BELL  	206   	206L3       	1182108	SW  										SWASHPLATE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41128				RIJG10015	51134				SWASHPLATE WORN.  REPLACED BUSHINGS AND RETURNED SWASHPLATE ASSY TO SERVICE.						1	G	7	1 	3U				H2SW    					 
1999012900528	19990129	00528	SW  	1999	1	29	HEEA060187       	1	19990122	G	6230	206010421003	BUSHING         		206010450113	BELL  	206   	206L1       	1182107	SW  										SWASHPLATE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1072T				GDJG10455	45385				SWASHPLATE WORN.  REPLACED BUSHINGS AND RETURNED SWASHPLATE ASSY TO SERVICE.						1	G	7	1 	3U				H2SW    					 
1999012900529	19990129	00529	SW  	1999	1	29	HEEA060188       	1	19990122	G	6230	206010443001	BEARING         		206010450113	BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR MAST	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1072T				GDJG10455	45385				SWASHPLATE PITTED ON RACES.  REPLACED DUPLEX BEARING AND RETURNED SWASHPLATE ASSY TO SERVICE.						1	G	7	1 	3U				H2SW    					 
1999012900530	19990129	00530	SW  	1999	1	29	HEEA060189       	1	19990122	G	6230	206010450113	SWASHPLATE      			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5000K	19070				45167				SWASHPLATE EXPERIENCED GENERAL PREMATURE WEAR, DUE TO OPERATIONS IN HIGH DUST ENVIRONMENT.  ONE SPHERICAL BEARING ON OUT	ER RING EXCEEDED LIMITS IN ADDITION TO COLLECTIVE PIVOT BUSHINGS AT LIMITS.  REPLACED WITH SERVICEABLE SWASHPLATE ASSY.					1	G	7	1 	3U				H2SW    					 
1999012900531	19990129	00531	SW  	1999	1	29	HEEA060190       	1	19990122	G	6230	206010450113	SWASHPLATE      			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	83MT	16435				45492				SLIDERS ARE WORN ON SWASHPLATE.						1	G	7	1 	3U				H2SW    					 
1999012900532	19990129	00532	SW  	1999	1	29	HEEA060191       	1	19990122	G	6230	206010450119	SWASHPLATE      			BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4180F	3711 				51469				WORN SWASHPLATE ASSY, VERTICAL BOUNCE IN HOVER.						1	G	7	1 	3U				H2SW    					 
1999012900533	19990129	00533	SW  	1999	1	29	HEEA060192       	1	19990122	G	6220	206011105001	TRUNNION        		206011100159	BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	ROUGH           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	54641				A285	51184				TRUNNION BEARING ROUGH.  REPLACED WITH SERVICEABLE TRUNNION.						1	G	7	1 	3U				H2SW    					 
1999012900534	19990129	00534	SW  	1999	1	29	HEEA060193       	1	19990122	G	6220	206011105001	TRUNNION        		206011100159	BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	ROUGH           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610C				HB10	51425				TRUNNION BEARING ROUGH.  REPLACED WITH SERVICEABLE TRUNNION.						1	G	7	1 	3U				H2SW    					 
1999012900535	19990129	00535	SW  	1999	1	29	HEEA060194       	1	19990122	G	6230	206011100159	HUB             			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR MAST	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2253E	2298 				45758				OUTBOARD GRIP SEAL LEAKING ON MAIN ROTOR HUB ASSEMBLY.						1	G	7	1 	3U				H2SW    					 
1999012900536	19990129	00536	SW  	1999	1	29	HEEA060195       	1	19990122	G	6220	206011139001	ARM ASSY        			BELL  	206   	206B3       	1181506	SW  										ELASTORMERIC	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2275Y					3626				ARM ASSEMBLY HAS WORN BEARINGS.						1	G	7	1 	3U				H2SW    					 
1999012900537	19990129	00537	SW  	1999	1	29	HEEA060196       	1	19990122	G	6220	206011149105	YOKE            		206011100105	BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR HUB	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	42EA				HB180	51542				YOKE HAS CORROSION, RADIUS RING BORE CORRODED BEYOND LIMITS AND BRINELLING.						1	G	7	1 	3U				H2SW    					 
1999012900538	19990129	00538	SW  	1999	1	29	HEEA060197       	1	19990122	G	6420	206011810013	HUB             			BELL  	206   	206L1       	1182107	SW  										TAIL ROTOR	UNBALANCED      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2770Y	1778 				45291				UNABLE TO BALANCE TAIL ROTOR ASSEMBLY.  PITTING ON TRUNNION SPLINES.   THRUST PLUGS WORN EXCESSIVELY.  HOUSING BOLTS DID	 NOT OBTAIN .025 INCH OF THREAD ENGAGEMENT.					1	G	7	1 	3U				H2SW    					 
1999012900539	19990129	00539	SW  	1999	1	29	HEEA060198       	1	19990122	G	6420	206011810013	HUB             			BELL  	206   	206L1       	1182107	SW  										TAIL ROTOR	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03		4494 								SEPARATION AT TIP OF BLADE, S/N CS7168, PITTING ON TRUNNION SPLINES, THRUST PLUGS WORN EXCESSIVELY, HOUSING BOLTS DID NO	T OBTAIN 0.25 INCH OF THREAD ENGAGEMENT.					1	G	7	1 	3U				H2SW    					 
1999012900540	19990129	00540	SW  	1999	1	29	HEEA060199       	1	19990122	G	6410	206011810141	BLADE           			BELL  	206   	206L1       	1182107	SW  										TAIL ROTOR	DENTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03		3918 								DENTS ON TAIL ROTOR BLADE, S/N CS670, HOUSING BOLTS DID NOT OBTAIN MINIMUM OF 0.25 INCH THREAD ENGAGEMENT.						1	G	7	1 	3U				H2SW    					 
1999012900541	19990129	00541	SW  	1999	1	29	HEEA060200       	1	19990122	G	6420	206011810135	TRUNNION        			BELL  	206   	206L1       	1182107	SW  										TAIL ROTOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	10761	2634 				45381				T/R TRUNNION CAP BOLTS FAILED THREAD ENGAGEMENT CHECK.						1	G	7	1 	3U				H2SW    					 
1999012900542	19990129	00542	SW  	1999	1	29	HEEA060201       	1	19990122	G	6410	206011810149	BLADE           			BELL  	206   	206L3       	1182108	SW  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8589X	6236 				51487				TAIL ROTOR BLADE HAS TIP DAMAGE .						1	G	7	1 	3U				H2SW    					 
1999012900543	19990129	00543	SW  	1999	1	29	HEEA060202       	1	19990122	G	6210	206015001107	BLADE           			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5006F	1485 				45181				BLADE BOLT BUSHING SHIFTED POSITION.						1	G	7	1 	3U				H2SW    					 
1999012900544	19990129	00544	SW  	1999	1	29	HEEA060203       	1	19990122	G	3270	206020110005	TAIL SKID       			BELL  	206   	206L1       	1182107	SW  										TAIL	CUT             	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TAIL SKID WAS CUT.  REPLACED WITH SERVICEABLE SKID.						1	G	7	1 	3U				H2SW    					 
1999012900545	19990129	00545	SW  	1999	1	29	HEEA060204       	1	19990122	G	5302	206020113117	FIN             			BELL  	206   	206L1       	1182107	SW  										TAIL BOOM	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2770Y					45291				TOP AFT BOLT SLEEVE CRACKED ON FIN ASSEMBLY.						1	G	7	1 	3U				H2SW    					 
1999012900546	19990129	00546	SW  	1999	1	29	HEEA060205       	1	19990122	G	5512	206023119151	SKIN            			BELL  	206   	206L3       	1182108	SW  										HORIZ STAB	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3108E					51498				STABILIZER ASSEMBLY HAS CORROSION UNDER UPPER DOUBLER.						1	G	7	1 	3U				H2SW    					 
1999012900547	19990129	00547	SW  	1999	1	29	HEEA060206       	1	19990122	G	5512	206023119151	SKIN            			BELL  	206   	206L3       	1182108	SW  										HORIZ STAB	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8593X					51509				STABILIZER ASSEMBLY CORRODED BEYOND LIMITS ON LEFT EDGE.						1	G	7	1 	3U				H2SW    					 
1999012900548	19990129	00548	SW  	1999	1	29	HEEA060207       	1	19990122	G	5512	206023119151A	SKIN            			BELL  	206   	206L3       	1182108	SW  										HORIZ STAB	DENTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3207Q					51540				STABILIZER ASSEMBLY HAS EXCESSIVE DENTS.						1	G	7	1 	3U				H2SW    					 
1999012900549	19990129	00549	SW  	1999	1	29	HEEA060208       	1	19990122	G	5512	206023119151A	SKIN            			BELL  	206   	206L3       	1182108	SW  										HORIZ STAB	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610C	7146 				51425				STABILIZER ASSEMBLY HAS CORROSION RT LEADING EDGE.						1	G	7	1 	3U				H2SW    					 
1999012900550	19990129	00550	SW  	1999	1	29	HEEA060209       	1	19990122	G	5521	206023119157	BUSHING         			BELL  	206   	206L3       	1182108	SW  										ELEVATOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										LEFT ELEVATOR ASSEMBLY HAS SEPARATED SPAR SPLICED AND BUSHINGS WORN.						1	G	7	1 	3U				H2SW    					 
1999012900551	19990129	00551	SW  	1999	1	29	HEEA060210       	1	19990122	G	5521	206023119159	BUSHING         			BELL  	206   	206L1       	1182107	SW  										ELEVATOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										RIGHT ELEVATOR ASSEMBLY HAS SEPARATED SPAR SPLICED AND BUSHING WORN.						1	G	7	1 	3U				H2SW    					 
1999012900552	19990129	00552	SW  	1999	1	29	HEEA060211       	1	19990122	G	5512	206023126101	SKIN            			BELL  	206   	206L3       	1182108	SW  										HORIZ STAB	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				FIN ASSEMBLY CRACKED AND SEPARATED.						1	G	7	1 	3U				H2SW    					 
1999012900553	19990129	00553	SW  	1999	1	29	HEEA060212       	1	19990122	G	5512	206023126102	SKIN            			BELL  	206   	206L1       	1182107	SW  										HORIZ STAB	DENTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2758N					45267				FIN ASSEMBLY HAS HOLE IN LEADING EDGE, DENTED, AND SEPARATED.						1	G	7	1 	3U				H2SW    					 
1999012900554	19990129	00554	SW  	1999	1	29	HEEA060213       	1	19990122	G	3213	206030104023	FITTING ASSY    			BELL  	206   	206L3       	1182108	SW  										CROSSTUBE	GOUGED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	32041					51539				GOUGES IN THE SIDES FROM THE CROSSTUBE TUBE SADDLE.  CORROSION INSIDE AT THE NUTPLATE.  SCRAPPED AND INSTALLED SERVICEAB	LE FITTINGS.					1	G	7	1 	3U				H2SW    					 
1999012900555	19990129	00555	SW  	1999	1	29	HEEA060214       	1	19990122	G	6330	206031589001	BEARING         			BELL  	206   	206B3       	1181506	SW  										PYLON SUPPORT	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3181J					3771				LINK ASSEMBLY HAS BEARING BORE WORN.						1	G	7	1 	3U				H2SW    					 
1999012900556	19990129	00556	SW  	1999	1	29	HEEA060215       	1	19990122	G	5302	206032409001	FITTING         		206033004175	BELL  	206   	206L4       	1182110	SW  										TAIL BOOM	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	62127	5534 			52023	52023				UPPER LEFT TAILBOOM FITTING CRACKED.  REPLACED WITH SERVICEABLE FITTING.						1	G	7	1 	3U			NC	H2SW    					 
1999012900557	19990129	00557	SW  	1999	1	29	HEEA060216       	1	19990122	G	5330	206033115183	PANEL           			BELL  	206   	206L3       	1182108	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	8593X					51509				PANEL ASSEMBLY MISMANUFACTURED.  WHEN FITTING AIRCRAFT POP-OUT WINDOW TO NEW PANEL, FOUND WINDOW AREA TOO LONG.  WINDOW 	FALLS OUT AND WHEN MATCHED TO OLD PANEL, TOP FLANGE IS .1250 INCH TOO SHORT AND BOTTOM FLANGE IS .50  TOO SHORT.					1	G	7	1 	3U				H2SW    					 
1999012900558	19990129	00558	SW  	1999	1	29	HEEA060217       	1	19990122	G	5330	206033172105	PANEL           			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	2761N					45277				PANEL ASSEMBLY MISMANUFACTURED.  BOLT HOLES IN PANEL THAT THE FUEL ATTACHES TO ARE MISLOCATED.						1	G	7	1 	3U				H2SW    					 
1999012900559	19990129	00559	SW  	1999	1	29	HEEA060218       	1	19990122	G	5330	206033172105	PANEL           			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	2761N					45277				PANEL ASSEMBLY MISMANUFACTURED.  BOLT HOLES IN PANEL THAT THE FUEL ATTACHES TO ARE MISLOCATED. S						1	G	7	1 	3U				H2SW    					 
1999012900560	19990129	00560	SW  	1999	1	29	HEEA060219       	1	19990122	G	5330	206033172117	PANEL           			BELL  	206   	206L3       	1182108	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										PANEL ASSEMBLY MISMANUFACTURED 180 DEGREES.						1	G	7	1 	3U				H2SW    					 
1999012900561	19990129	00561	SW  	1999	1	29	HEEA060220       	1	19990122	G	5210	206033601117	DOOR            			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	1076Y					45380				MISMANUFACTURED DOOR.						1	G	7	1 	3U				H2SW    					 
1999012900562	19990129	00562	SW  	1999	1	29	HEEA060221       	1	19990122	G	5210	206033601117	DOOR            			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	2761N					45277				DOOR MISMANUFACTURED.  OUTER SKIN OF DOOR IS WARPED ALONG THE INNER LINER.						1	G	7	1 	3U				H2SW    					 
1999012900563	19990129	00563	SW  	1999	1	29	HEEA060222       	1	19990122	G	6320	206040140013	BEARING SEAT    		206040004107	BELL  	206   	206L3       	1182108	SW  										M/R GEARBOX	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	206FS				B51711	51506				BEARING SEAT WORN BEYOND LIMITS.  REPLACED WITH SERVICEABLE CARRIER ASSY.						1	G	7	1 	3U				H2SW    					 
1999012900564	19990129	00564	SW  	1999	1	29	HEEA060223       	1	19990122	G	6320	206040184001	PUMP            			BELL  	206   	206B3       	1181506	SW  										OIL SYSTEM	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	104PH					3622				STUDS CORRODED ON PUMP ASSEMBLY.						1	G	7	1 	3U				H2SW    					 
1999012900565	19990129	00565	SW  	1999	1	29	HEEA060224       	1	19990122	G	6320	206040190005	PUMP            			BELL  	206   	206L3       	1182108	SW  										OIL SYSTEM	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610E					51424				PUMP HAS CRACK INDICATION ON HOUSING AND WORN SPLINE ON SHAFT.						1	G	7	1 	3U				H2SW    					 
1999012900566	19990129	00566	SW  	1999	1	29	HEEA060225       	1	19990122	G	6310	206040268001	FREEWHEEL       			BELL  	206   	206L3       	1182108	SW  										CAP	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3207Q					51540				CAP ASSEMBLY HAS CORROSION PITS IN SEAL HOUSING.						1	G	7	1 	3U				H2SW    					 
1999012900567	19990129	00567	SW  	1999	1	29	HEEA060226       	1	19990122	G	6310	206040222009	SHAFT           		206040270009	BELL  	206   	206L3       	1182108	SW  										FREEWHEEL	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	206FS				BMB45992	51506				CORROSION BEYOND LIMITS ON SEAL RIDE.  REPLACED WITH SERVICEABLE SHAFT.						1	G	7	1 	3U				H2SW    					 
1999012900568	19990129	00568	SW  	1999	1	29	HEEA060227       	1	19990122	G	6310	206040222009	SHAFT           		206040270009	BELL  	206   	206L3       	1182108	SW  										FREEWHEEL	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3108E				A430	51498				CORROSION BEYOND LIMITS ON SEAL RIDE.  REPLACED WITH SERVICEABLE SHAFT.						1	G	7	1 	3U				H2SW    					 
1999012900569	19990129	00569	SW  	1999	1	29	HEEA060228       	1	19990122	G	6310	206040222009	SHAFT           		206040270009	BELL  	206   	206L1       	1182107	SW  										FREEWHEEL	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2770Y				BMB45308	45291				CORROSION BEYOND LIMITS ON SEAL RIDE.  REPLACED WITH SERVICEABLE SHAFT.						1	G	7	1 	3U				H2SW    					 
1999012900570	19990129	00570	SW  	1999	1	29	HEEA060229       	1	19990122	G	6510	206040339009	BEARING         		206040370011	BELL  	206   	206L3       	1182108	SW  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31801				VNMK45943	51074				TAIL ROTOR BEARING RUNS HOT.  REPLACED BEARING AND RETURNED T/R DRIVESHAFT TO SERVICE.						1	G	7	1 	3U				H2SW    					 
1999012900571	19990129	00571	SW  	1999	1	29	HEEA060230       	1	19990122	G	6510	206040370013	SHAFT ASSY      			BELL  	206   	206L1       	1182107	SW  										NR 2	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1072T	9959 				45385				NR 2 TAIL ROTOR SHAFT SPLINE WORN.						1	G	7	1 	3U				H2SW    					 
1999012900572	19990129	00572	SW  	1999	1	29	HEEA060231       	1	19990122	G	6520	206040439001	BEARING         		206040402105	BELL  	206   	206L1       	1182107	SW  										TAIL ROTOR	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3892R	251  			AFS2031	45594				WATER DAMAGE CAUSING PITTING ON BEARING INNER RACE.  REPLACED OUTPUT SEAL AND BEARING AND SHAFT.						1	G	7	1 	3U				H2SW    					 
1999012900582	19990129	00582		1999	1	29	HEEA060232       	4	19990122	G	2312	064101902	TRANSCEIVER     			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	624MB					S751				FREQUENCY GOES TO 120.00 MHZ WHEN POWER IS CYCLED.						1	G	7	2 	3U				H3EU    					 
1999020500205	19990205	00205	GL  	1999	2	5	HEEA060350       	2	19990125	G	7250	23055438	NR 2 NOZZLE     		23035128    						ALLSN 	250C  	250C30P     	03013	GL  					ENGINE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03					CAT97895		CAE895336			RECEIVING INSPECTION REVEALED RUNOUT BEYOND SERVICEABLE LIMITS ON NR 2 NOZZLE, 1ST STAGE TIP PATH OBTAINED .005 INCH.											3	U			E1GL				 
1999020500206	19990205	00206	GL  	1999	2	5	HEEA060351       	2	19990125	G	7250	23038213	SUPPORT         			BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					ENGINE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	8590X					51494				OVERSPRAY ON 25/28 SEAL BORE.  RECEIVING INSPECTION REVEALED EXCESSIVE SPRAY ON POWER TURBINE.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999020500207	19990205	00207	GL  	1999	2	5	HEEA060352       	2	19990128	G	7230	23056634	GEARSHAFT       		23051643    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					SPUR ADAPTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5435V	953  			CAC90623	760158	CAE890627S			ENGINE REMOVED DUE TO TURBINE 1 AND 2 WHEEL CYCLES.  UPON VISUAL INSPECTION ON COMPRESSOR NOTED:  STEP WEAR BEYOND SERVI	CEABLE LIMITS ON SPUR GEAR SHAFT SPLINES.  FAILED NO-GO GAUGE.  INSTALLED A NEW SPUR GEAR SHAFT.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999020500208	19990205	00208	GL  	1999	2	5	HEEA060353       	2	19990128	G	7230	23056634	GEARSHAFT       		23051643    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					SPUR ADAPTER	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5435V	953  			CAC90511	760158	CAE890507S			ENGINE REMOVED DUE TO TURBINE OVERHAUL.  UPON INSPECTION ON COMPRESSOR NOTED:  STEP WEAR BEYOND SERVICEABLE LIMITS ON SH	AFT FORWARD AND AFT SPLINES.  FAILED NO-GO GAUGE.  INSTALLED A NEW SPUR GEAR SHAFT.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999020500209	19990205	00209	GL  	1999	2	5	HEEA060354       	2	19990128	G	7230	23030974	ADAPTER         		23033185    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					ENGINE	FLAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406EH	611  			CAT70217	45183	CAE860038			ENGINE REMOVED DUE TO CRACKED SCROLL.  TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL.   UPON INSPECTION OF TURBINE 	PARTS NOTED:  COATING MISSING AND FLAKING OF SPLINE ADAPTER.  INSTALLED A NEW SPLINE ADAPTER.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999020500210	19990205	00210	GL  	1999	2	5	HEEA060355       	2	19990128	G	7230	6887619	SEAL            		23051643    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30P     	03013	GL  					ENGINE	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545X	732  			CAC90402	760050	CAE890397S			ENGINE REMOVED DUE TO METAL.  UPON INSPECTION OF COMPRESSOR PARTS NOTED:  PITS BEYOND SERVICEABLE LIMITS ON SEAL CARBON 	FACE.  INSTALLED A NEW SEAL.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999020500211	19990205	00211	SW  	1999	2	5	HEEA060356       	1	19990127	G	2435	206062200113	STARTER         			BELL  	407   	407         		SW  										START/GENERATOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				FAILED 300 HOUR INSPECTION.  INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES WORN BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999020500212	19990205	00212	SW  	1999	2	5	HEEA060357       	1	19990127	G	2435	206062200113	STARTER         			BELL  	407   	407         		SW  										START/GENERATOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH	1253 				53142				FAILED 300 HOUR INSPECTION.  INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES WORN BEYOND LIMITS						1	G	7	1 	3U			O	H2SW    					 
1999020500213	19990205	00213	SW  	1999	2	5	HEEA060358       	1	19990127	G	6320	206040530001	CASE ASSY       			BELL  	206   	206L1       	1182107	SW  										M/R GEARBOX	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50034					45169				WORN I/P LINER AND CORROSION IN STUD HOLE OF MATING SURFACE (UPPER).  ALSO CORROSION AT I/P MATING SURFACE.						1	G	7	1 	3U				H2SW    					 
1999020500214	19990205	00214	SW  	1999	2	5	HEEA060359       	1	19990127	G	6320	206040530101	CASE ASSY       			BELL  	206   	206L4       	1182110	SW  										M/R GEARBOX	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7077F	4483 				52038				CRACK INDICATION.  REPLACED WITH SERVICEABLE CASE.						1	G	7	1 	3U			NC	H2SW    					 
1999020500215	19990205	00215	SW  	1999	2	5	HEEA060360       	1	19990127	G	3212	206050168009	FLOAT BAG       			BELL  	206   	206B3       	1181506	SW  										FLOAT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2275Y					3626				FLOAT BAG LEAKING.						1	G	7	1 	3U				H2SW    					 
1999020500216	19990205	00216	SW  	1999	2	5	HEEA060361       	1	19990127	G	6210	206015001107	BLADE           			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										MAIN ROTOR BLADE RECEIVED WITH FACTORY DEFECT.						1	G	7	1 	3U				H2SW    					 
1999020500217	19990205	00217	SW  	1999	2	5	HEEA060362       	1	19990127	G	6210	206015001107	BLADE           			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	MISMANUFACTURED 	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										MAIN ROTOR BLADES RECEIVED WITH FACTORY DEFECT.						1	G	7	1 	3U				H2SW    					 
1999020500218	19990205	00218	SW  	1999	2	5	HEEA060363       	1	19990128	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T	37   				28101				STARTER SWITCH DID NOT DISENGAGE AND START ENGINE ENGAGE LIGHT STAYED ILLUMINATED.						2	G	7	2 	4U				H10SW   					 
1999020500219	19990205	00219	SW  	1999	2	5	HEEA060364       	1	19990128	G	7722	206375006101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	MALFUCNTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	513EH					45421				INDICATOR MOVES WHEN VHF RADIO IS USED.						1	G	7	1 	3U				H2SW    					 
1999020500220	19990205	00220	SW  	1999	2	5	HEEA060365       	1	19990128	G	7722	206375006101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50046					45173				OVERTEMP LIGHT WILL NOT ILLUMINATE.						1	G	7	1 	3U				H2SW    					 
1999020500221	19990205	00221	SW  	1999	2	5	HEEA060366       	1	19990128	G	7722	206375006101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2125M					45649				TOT INDICATOR NEEDLE STICKS BETWEEN 100 AND 200 DEGREES.						1	G	7	1 	3U				H2SW    					 
1999020500222	19990205	00222	SW  	1999	2	5	HEEA060367       	1	19990128	G	7722	206375006101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	10761					45381				TOT INDICATOR INCREASES IN TEMP WHEN VHF IS KEYED.						1	G	7	1 	3U				H2SW    					 
1999020500223	19990205	00223	SW  	1999	2	5	HEEA060368       	1	19990128	G	7722	206375006101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50046					45173				TOT INDICATOR HAD NO INDICATION, STUCK AT ZERO.  TIME SINCE REPAIR 88:25 HOURS.						1	G	7	1 	3U				H2SW    					 
1999020500224	19990205	00224	SW  	1999	2	5	HEEA060369       	1	19990128	G	7722	206375006101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2772A					45311				TOT INDICATOR HAD NO INDICATION.						1	G	7	1 	3U				H2SW    					 
1999020500225	19990205	00225	SW  	1999	2	5	HEEA060370       	1	19990128	G	7722	206375006101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50046					45173				TOT INDICATOR NEEDLE STUCK AT ZERO.						1	G	7	1 	3U				H2SW    					 
1999020500226	19990205	00226	SW  	1999	2	5	HEEA060371       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3116L					51529				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999020500227	19990205	00227	SW  	1999	2	5	HEEA060372       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	16938					45157				ACTUATOR WILL NOT ACTUATE IN EITHER DIRECTION.						1	G	7	1 	3U				H2SW    					 
1999020500228	19990205	00228	SW  	1999	2	5	HEEA060373       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31077					51520				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999020500229	19990205	00229	SW  	1999	2	5	HEEA060374       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31073					51519				ACTUATOR INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999020500230	19990205	00230	SW  	1999	2	5	HEEA060375       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										DROOP BAY	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	32041					51539				ACTUATOR WILL NOT ADJUST TO DECREASE STROKE.						1	G	7	1 	3U				H2SW    					 
1999020500231	19990205	00231	SW  	1999	2	5	HEEA060376       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										DROOP BAY	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3116L					51529				ACTUATOR CANNOT ADJUST STROKE.						1	G	7	1 	3U				H2SW    					 
1999020500232	19990205	00232	SW  	1999	2	5	HEEA060377       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206B3       	1181506	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	39122					3312				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999020500233	19990205	00233	SW  	1999	2	5	HEEA060378       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2125M					45649				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999020500234	19990205	00234	SW  	1999	2	5	HEEA060379       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5742N					45477				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999020500235	19990205	00235	SW  	1999	2	5	HEEA060380       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2125M					45649				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999020500236	19990205	00236	SW  	1999	2	5	HEEA060381       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31073					51519				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999020500237	19990205	00237	SW  	1999	2	5	HEEA060382       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	129MR					51129				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999020500238	19990205	00238	SW  	1999	2	5	HEEA060383       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	32041					51539				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999020500239	19990205	00239	SW  	1999	2	5	HEEA060384       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3892R					45594				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999020500240	19990205	00240	SW  	1999	2	5	HEEA060385       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										DROOP BAY	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8593X					51509				ACTUATOR HANGS UP AND STICKS, ERRATIC.						1	G	7	1 	3U				H2SW    					 
1999020500241	19990205	00241	SW  	1999	2	5	HEEA060386       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP BAY	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5737T					45454				CANNOT ADJUST ACTUATOR FOR PROPER RANGE.						1	G	7	1 	3U				H2SW    					 
1999020500242	19990205	00242	SW  	1999	2	5	HEEA060387       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP BAY	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2251A					45755				UNABLE TO ADJUST STROKE ON ACTUATOR.						1	G	7	1 	3U				H2SW    					 
1999020500243	19990205	00243	SW  	1999	2	5	HEEA060388       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L4       	1182110	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	62127					52023				ACTUATOR INOPERATIVE.  WILL NOT BEEP UP AND DOWN.						1	G	7	1 	3U			NC	H2SW    					 
1999020500244	19990205	00244	SW  	1999	2	5	HEEA060389       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2251A					45755				ACTUATOR INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999020500245	19990205	00245	SW  	1999	2	5	HEEA060390       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	10814					45415				ACTUATOR WILL NOT FUNCTION.						1	G	7	1 	3U				H2SW    					 
1999020500246	19990205	00246	SW  	1999	2	5	HEEA060391       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81SP					51029				ACTUATOR WILL NOT EXTEND.						1	G	7	1 	3U				H2SW    					 
1999020500247	19990205	00247	SW  	1999	2	5	HEEA060392       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										DROOP BAY	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31801					51074				UNABLE TO ADJUST STROKE ON ACTUATOR.						1	G	7	1 	3U				H2SW    					 
1999020500248	19990205	00248	SW  	1999	2	5	HEEA060393       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP BAY	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2770Y					45291				SCREW BROKEN, ACTUATOR HAS INTERMITTENT OPERATION.						1	G	7	1 	3U				H2SW    					 
1999020500249	19990205	00249	SW  	1999	2	5	HEEA060394       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP BAY	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5742N					45477				ACTUATOR INTERMITTENT.						1	G	7	1 	3U				H2SW    					 
1999020500250	19990205	00250	SW  	1999	2	5	HEEA060395       	1	19990128	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP BAY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ACTUATOR NON-FUNCTIONABLE.						1	G	7	1 	3U				H2SW    					 
1999020500251	19990205	00251	SW  	1999	2	5	HEEA060396       	1	19990128	G	7714	206070266009	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5014V					45217				NEEDLE STICKS THROUGHOUT SCALE.						1	G	7	1 	3U				H2SW    					 
1999020500252	19990205	00252	SW  	1999	2	5	HEEA060397       	1	19990128	G	7714	206070266009	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5745S					45491				LENS FOGS UP AND ERRATIC AT LOW END.						1	G	7	1 	3U				H2SW    					 
1999020500253	19990205	00253	SW  	1999	2	5	HEEA060398       	1	19990128	G	7714	206070266009	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	10761					45381				INDICATOR STICKS AT ZERO AND 55 PERCENT WITH SEVERE FLUCTUATION.						1	G	7	1 	3U				H2SW    					 
1999020500254	19990205	00254	SW  	1999	2	5	HEEA060399       	1	19990128	G	7714	206070266009	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FOGGED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	513EH					45421				FOGGED GLASS ON INDICATOR, NEEDLE ERRATIC AND INTERMITTENT.						1	G	7	1 	3U				H2SW    					 
1999020500255	19990205	00255	SW  	1999	2	5	HEEA060400       	1	19990128	G	7714	206070266009	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1078C					45392				INDICATOR INOPERATIVE,  WILL NOT INDICATE.						1	G	7	1 	3U				H2SW    					 
1999020500256	19990205	00256	SW  	1999	2	5	HEEA060401       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	363BH					51345				INDICATOR READS HIGH OUT OF TOLERANCE.						1	G	7	1 	3U				H2SW    					 
1999020500257	19990205	00257	SW  	1999	2	5	HEEA060402       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4180F					51469				TOT INDICATOR VIBRATES AND FLUCTUATES ON START-UP.						1	G	7	1 	3U				H2SW    					 
1999020500258	19990205	00258	SW  	1999	2	5	HEEA060403       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TOT INDICATOR NEEDLE SPINS WHEN POWERED DOWN.   ALSO LOOSE PART INSIDE.						1	G	7	1 	3U				H2SW    					 
1999020500259	19990205	00259	SW  	1999	2	5	HEEA060404       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8589X					51487				TOT INDICATOR NEEDLE STICKS AT ZERO.						1	G	7	1 	3U				H2SW    					 
1999020500260	19990205	00260	SW  	1999	2	5	HEEA060405       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A					51611				TOT INDICATOR WILL NOT INDICATE.						1	G	7	1 	3U				H2SW    					 
1999020500261	19990205	00261	SW  	1999	2	5	HEEA060406       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1072T					45385				TOT INDICATOR WILL NOT INDICATE.						1	G	7	1 	3U				H2SW    					 
1999020500262	19990205	00262	SW  	1999	2	5	HEEA060407       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8589X					51487				TOT INDICATOR NEEDLE STICKS INTERMITTENTLY IN THE RESET POSITION (POWER OFF) DURING START.  USUALLY DURING THE FIRST STA	RT OF THE DAY.					1	G	7	1 	3U				H2SW    					 
1999020500263	19990205	00263	SW  	1999	2	5	HEEA060408       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6603X					51412				TOT INDICATOR NEEDLE STUCK AT ZERO.						1	G	7	1 	3U				H2SW    					 
1999020500264	19990205	00264	SW  	1999	2	5	HEEA060409       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L4       	1182110	SW  										TOT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7077F					52038				TOT INDICATOR NEEDLE STUCK AT ZERO ON START.						1	G	7	1 	3U			NC	H2SW    					 
1999020500265	19990205	00265	SW  	1999	2	5	HEEA060410       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8587X					51464				TOT INDICATOR NEEDLE STICKS ON ZERO AT START.						1	G	7	1 	3U				H2SW    					 
1999020500266	19990205	00266	SW  	1999	2	5	HEEA060411       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41128					51134				TOT INDICATOR HAS NO INDICATION DURING LIGHT-OFF, STICKS AND OSCILLATES THROUGHOUT.						1	G	7	1 	3U				H2SW    					 
1999020500267	19990205	00267	SW  	1999	2	5	HEEA060412       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	92MT					51175				TOT INDICATOR HAS NO INDICATION, STICKS AT ZERO.						1	G	7	1 	3U				H2SW    					 
1999020500268	19990205	00268	SW  	1999	2	5	HEEA060413       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3207Q					51540				TOT INDICATOR HAS NO INDICATION ON UNIT.						1	G	7	1 	3U				H2SW    					 
1999020500269	19990205	00269	SW  	1999	2	5	HEEA060414       	1	19990128	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	49EA					51507				TOT INDICATOR HAS NO INDICATION ON UNIT.						1	G	7	1 	3U				H2SW    					 
1999020500270	19990205	00270	SW  	1999	2	5	HEEA060415       	1	19990128	G	3212	206050247101	COVER           			BELL  	206   	206L1       	1182107	SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1072T					45385				FLOAT COVER WORN.						1	G	7	1 	3U				H2SW    					 
1999020500271	19990205	00271	SW  	1999	2	5	HEEA060416       	1	19990128	G	3212	206050247101	COVER           			BELL  	206   	206L4       	1182110	SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	62127					52023				FLOAT COVER WORN.						1	G	7	1 	3U			NC	H2SW    					 
1999020500272	19990205	00272	SW  	1999	2	5	HEEA060417       	1	19990128	G	3212	206050247101	COVER           			BELL  	206   	206L3       	1182108	SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3116P					51530				FLOAT COVER WORN.						1	G	7	1 	3U				H2SW    					 
1999020500273	19990205	00273	SW  	1999	2	5	HEEA060418       	1	19990128	G	3212	206050247101	COVER           			BELL  	206   	206L3       	1182108	SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31073					51519				FLOAT COVER WORN AND TORN.						1	G	7	1 	3U				H2SW    					 
1999020500274	19990205	00274	SW  	1999	2	5	HEEA060419       	1	19990128	G	3212	206050247101	COVER           			BELL  	206   	206L1       	1182107	SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1073W					45386				FLOAT COVER WORN AND TORN.						1	G	7	1 	3U				H2SW    					 
1999020500275	19990205	00275	SW  	1999	2	5	HEEA060420       	1	19990128	G	3212	206050247101	COVER           			BELL  	206   	206L3       	1182108	SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3207Q					51540				FLOAT COVER WORN AND TORN.						1	G	7	1 	3U				H2SW    					 
1999020500276	19990205	00276	SW  	1999	2	5	HEEA060421       	1	19990128	G	3212	206050247101	COVER           			BELL  	206   	206L3       	1182108	SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41128					51134				FLOAT COVER WORN AND TORN.						1	G	7	1 	3U				H2SW    					 
1999020500277	19990205	00277	SW  	1999	2	5	HEEA060422       	1	19990128	G	3212	206050248117	FLOAT BAG ASSY  			BELL  	206   	206L3       	1182108	SW  										MLG	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8593X					51509				LARGE BLISTER IN CENTER AREA OF FLOAT BAG.						1	G	7	1 	3U				H2SW    					 
1999020500278	19990205	00278	SW  	1999	2	5	HEEA060423       	1	19990128	G	3201	206053109007	CROSSTUBE       			BELL  	206   	206L1       	1182107	SW  										AIRFRAME FWD	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2761N					45277				FORWARD CROSSTUBE HAS CORROSION BEYOND LIMITS.  REPLACED WITH SERVICEABLE CROSSTUBE.						1	G	7	1 	3U				H2SW    					 
1999020500279	19990205	00279	SW  	1999	2	5	HEEA060424       	1	19990128	G	3246	206053184101	TUBE            			BELL  	206   	206L1       	1182107	SW  										LT SKID	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2761N					45277				LEFT SKID TUBE HAS CORROSION BEYOND LIMITS.  REPLACED WITH SERVICEABLE CROSSTUBE.						1	G	7	1 	3U				H2SW    					 
1999020500280	19990205	00280	SW  	1999	2	5	HEEA060425       	1	19990128	G	3246	206053184102	TUBE            			BELL  	206   	206L1       	1182107	SW  										SKID	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2761N					45277				SKID TUBE ASSEMBLY HAS CORROSION BEYOND LIMITS.  REPLACED WITH SERVICEABLE CROSSTUBE.						1	G	7	1 	3U				H2SW    					 
1999020500281	19990205	00281	SW  	1999	2	5	HEEA060426       	1	19990128	G	3201	206053203103	CROSSTUBE       			BELL  	206   	206L1       	1182107	SW  										AIRFRAME	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2761N					45277				CROSSTUBE HAS CORROSION BEYOND LIMITS.  REPLACED WITH SERVICEABLE CROSSTUBE.						1	G	7	1 	3U				H2SW    					 
1999020500282	19990205	00282	SW  	1999	2	5	HEEA060427       	1	19990128	G	3201	206053203115	CROSSTUBE       			BELL  	206   	206L1       	1182107	SW  										AIRFRAME FWD	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1076Y					45380				CORROSION BEYOND LIMITS ON LOWER PORTION OF TUBE IN AREA A.  SCRAPPED FORWARD CROSSTUBE AND REPLACED WITH SERVICEABLE CR	OSSTUBE.					1	G	7	1 	3U				H2SW    					 
1999020500283	19990205	00283	SW  	1999	2	5	HEEA060428       	1	19990128	G	3201	206053203117	CROSSTUBE       			BELL  	206   	206L1       	1182107	SW  										AIRFRAME AFT	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1076Y					45380				CORROSION UNDER PAD OF AFT CROSSTUBE.  SCRAPPED AFT CROSSTUBE AND REPLACED WITH SERVICEABLE CROSSTUBE.						1	G	7	1 	3U				H2SW    					 
1999020500284	19990205	00284	SW  	1999	2	5	HEEA060429       	1	19990128	G	6710	206062721113	ACTUATOR        			BELL  	206   	206B3       	1181506	SW  										MAIN ROTOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2285B					3642				ACTUATOR MOTOR RUNS, BUT SHAFT DOES NOT MOVE.						1	G	7	1 	3U				H2SW    					 
1999020500285	19990205	00285	SW  	1999	2	5	HEEA060430       	1	19990128	G	6230	206064904013	RING ASSY       			BELL  	206   	206L1       	1182107	SW  										M/R MAST	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1076Y					45380				RING ASSY CORRODED UNDER NUTPLATE.  SCRAPPED AND REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U				H2SW    					 
1999020500286	19990205	00286	SW  	1999	2	5	HEEA060431       	1	19990128	G	2435	23081018	STARTER         			BELL  	206   	206L3       	1182108	SW  										START/GENERATOR	VIBRATES        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41791					51465				STARTER/GENERATOR PRODUCING HIGH FREQUENCY VIBRATION.						1	G	7	1 	3U				H2SW    					 
1999020500287	19990205	00287	SW  	1999	2	5	HEEA060432       	1	19990128	G	2435	200SGL132Q	STARTER         			BELL  	206   	206L3       	1182108	SW  										START/GENERATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6160Y	12088				51609				STARTER/GENERATOR WILL NOT COME ON LINE DURING SHUT DOWN.  INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND STARTER/GENERA	TOR WAS INOPERATIVE.					1	G	7	1 	3U				H2SW    					 
1999020500288	19990205	00288		1999	2	5	HEEA060433       	4	19990125	G	3457	0110005400	GPS 150         			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81992					S827				GPS 150 DISPLAYS BATTERY DEAD MESSAGE.						1	G	7	2 	3U				H3EU    					 
1999020500289	19990205	00289		1999	2	5	HEEA060434       	4	19990125	G	3457	0110005400	GPS 150         			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4294R					S860				GPS 150 INOPERATIVE.						1	G	7	2 	3U				H3EU    					 
1999020500290	19990205	00290		1999	2	5	HEEA060435       	4	19990125	G	3457	0110010600	GPS             			BOLKMS	117   	BK117B1     	5626012	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	217UC					7152				GPS WILL NOT SHOW TRACK.  PERFORMED PRELIMINARY INSPECTION, AND FOUND UNIT TAKES LONG TIME TO LOCK ON TO SATELLITES.						1	G	7	2 	3U				H13EU   					 
1999020500291	19990205	00291		1999	2	5	HEEA060436       	4	19990125	G	2312	064101900	TRANSCEIVER     			BOLKMS	105   	BO105S      	5626006	EU  										E/E BAY	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50293					S677				TRANSCEIVER HAS LOW POWER AND SENSITIVITY ON HIGH END OF FREQUENCY BAND.						1	G	7	2 	3U				H3EU    					 
1999020500292	19990205	00292		1999	2	5	HEEA060437       	4	19990125	G	2312	064101902	TRANSCEIVER     			BOLKMS	105   	BO105S      	5626006	EU  										E/E BAY	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	135AE					S838				TRANSCEIVER HAS LOW POWER OUT ON HIGH END OF FREQUENCY BAND.						1	G	7	2 	3U				H3EU    					 
1999020500293	19990205	00293	EU  	1999	2	5	HEEA060438       	1	19990125	G	3412	066106103	TRANSCEIVER     			BOLKMS	117   	BK117A4     	5626017	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RZ					7092				RADAR ALTIMETER INOPERATIVE ABOVE 500 FEET.						1	G	7	2 	3U				H13EU   					 
1999020500294	19990205	00294	EU  	1999	2	5	HEEA060439       	1	19990125	G	6220	1051410112	HUB             		117141081   	BOLKMS	117   	BK117B1     	5626012	EU  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	134AE	2866 			050126	7237				ROTOR STAR HAS WEAR IN ZONES 3-4.  WEAR IN ZONE 2,  DUE TO BEARING P/N F32827 AND BEARING P/N F32828 SPINNING IN BORE.						1	G	7	2 	3U				H13EU   					 
1999020500295	19990205	00295	EU  	1999	2	5	HEEA060440       	1	19990125	G	7933	10590872	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	133AE					S800				NR 2 ENGINE OIL TEMP INTERMITTENTLY FLUCTUATES - WORKS CORRECTLY MOST OF THE TIME.						1	G	7	2 	3U				H3EU    					 
1999020500296	19990205	00296	EU  	1999	2	5	HEEA060441       	1	19990125	G	7120	1176261403	BUSHING         			BOLKMS	117   	BK117A4     	5626017	EU  										ENGINE MOUNT	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8765J					7054				PITTING AND WEAR TO OUTER DIAMETER OF BUSHINGS.  REPLACED WITH SERVICEABLE BUSHINGS.						1	G	7	2 	3U				H13EU   					 
1999020500297	19990205	00297	EU  	1999	2	5	HEEA060442       	1	19990125	G	7120	1176261503	BUSHING         			BOLKMS	117   	BK117A4     	5626017	EU  										ENGINE MOUNT	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8765J					7054				PITTING AND WEAR TO OUTER DIAMETER OF BUSHINGS.  REPLACED WITH SERVICEABLE BUSHINGS.						1	G	7	2 	3U				H13EU   					 
1999020500298	19990205	00298	EU  	1999	2	5	HEEA060443       	1	19990125	G	7120	1176262001	BUSHING         			BOLKMS	117   	BK117A4     	5626017	EU  										ENGINE MOUNT	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8765J					7054				PITTING AND WEAR TO OUTER DIAMETER OF BUSHINGS.  REPLACED WITH SERVICEABLE BUSHINGS.						1	G	7	2 	3U				H13EU   					 
1999020500299	19990205	00299		1999	2	5	HEEA060444       	4	19990125	G	2210	11788904	TRANSDUCER      			BOLKMS	117   	BK117B1     	5626012	EU  										YAW SYSTEM	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911TL					7198				YAW TRANSDUCER HAS ERRATIC READING WHEN ADJUSTING.						1	G	7	2 	3U				H13EU   					 
1999020500300	19990205	00300	EU  	1999	2	5	HEEA060445       	1	19990125	G	7714	1179405303	INDICATOR       			BOLKMS	117   	BK117B2     	5626013	EU  										TRIPLE TACH	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911LK					7068				WHEN AIRCRAFT REACHED FLIGHT IDLE, ABOUT 70 PERCENT, NR 1 ENGINE NEEDLE PEGGED OUT FULL SCALE.						1	G	7	2 	3U			NC	H13EU   					 
1999020500301	19990205	00301	EU  	1999	2	5	HEEA060446       	1	19990125	G	7714	1179405303	INDICATOR       			BOLKMS	117   	BK117B2     	5626013	EU  										TRIPLE TACH	RATCHETS        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911LK					7068				ROTOR TACHOMETER NEEDLE RATCHETING AROUND 70 PERCENT.						1	G	7	2 	3U			NC	H13EU   					 
1999020500302	19990205	00302	EU  	1999	2	5	HEEA060447       	1	19990125	G	7714	1179405603	INDICATOR       			BOLKMS	117   	BK117B2     	5626013	EU  										NR 1 ENGINE N1	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911LK					7068				NR 1 ENGINE NEEDLE PEGS OUT BEFORE REACHING 70 PERCENT N2.						1	G	7	2 	3U			NC	H13EU   					 
1999020500303	19990205	00303	EU  	1999	2	5	HEEA060448       	1	19990125	G	7930	174035201	INDICATOR       		174083901   	BOLKMS	105   	BO105S      	5626006	EU  										ENGINE OIL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911FL				NA	S717				INDICATOR WAS REMOVED FROM BOWL AND CLEANED.   INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK.						1	G	7	2 	3U				H3EU    					 
1999020500304	19990205	00304	EU  	1999	2	5	HEEA060449       	1	19990125	G	7930	174035201	INDICATOR       		174083904   	BOLKMS	105   	BO105S      	5626006	EU  										ENGINE OIL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6607K				NA	S841				INDICATOR WAS REMOVED FROM BOWL AND CLEANED.   NSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK.						1	G	7	2 	3U				H3EU    					 
1999020500305	19990205	00305	EU  	1999	2	5	HEEA060450       	1	19990125	G	7930	174035201	INDICATOR       		174083904   	BOLKMS	105   	BO105S      	5626006	EU  										ENGINE OIL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911FL				NA	S717				INDICATOR WAS REMOVED FROM BOWL AND CLEANED.   INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK.						1	G	7	2 	3U				H3EU    					 
1999020500306	19990205	00306	EU  	1999	2	5	HEEA060452       	1	19990125	G	2435	23032048	STARTER         			BOLKMS	105   	BO105S      	5626006	EU  										START/GENERATOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724MB	8915 				S756				STARTER/GENERATOR NOISY AND ARCING.						1	G	7	2 	3U				H3EU    					 
1999020500307	19990205	00307	EU  	1999	2	5	HEEA060453       	1	19990125	G	2435	23032048	STARTER         			BOLKMS	105   	BO105S      	5626006	EU  										START/GENERATOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911FL					S717				STARTER/GENERATOR HAS WORN BRUSHES.						1	G	7	2 	3U				H3EU    					 
1999020500308	19990205	00308		1999	2	5	HEEA060454       	4	19990125	G	2312	4000103000	TRANSCEIVER     			BOLKMS	117   	BK117B1     	5626012	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911TL					7198				TRANSCEIVER WILL NOT TRANSMIT CORRECTLY.						1	G	7	2 	3U				H13EU   					 
1999020500309	19990205	00309		1999	2	5	HEEA060455       	4	19990125	G	2312	4000106000	CONTROL UNIT    			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911HM					S683				CONTROL UNIT INOPERATIVE.  WILL NOT LOAD FREQUENCIES.						1	G	7	2 	3U				H3EU    					 
1999020500310	19990205	00310		1999	2	5	HEEA060456       	4	19990125	G	2312	4000106000	CONTROL UNIT    			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	133AE					S800				CONTROL UNIT DIALS DO NOT CHANGE FREQUENCY AND GUARD IS INOPERATIVE.						1	G	7	2 	3U				H3EU    					 
1999020500311	19990205	00311		1999	2	5	HEEA060457       	4	19990125	G	2312	4000106000	CONTROL UNIT    			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911EB					S812				CONTROL UNIT TRANSMITS CONSTANTLY.  PERFORMED PRELIMINARY INSPECTION AND FOUND THUMBWHEEL INTERMITTENT.						1	G	7	2 	3U				H3EU    					 
1999020500312	19990205	00312		1999	2	5	HEEA060458       	4	19990125	G	3421	4021541671	HORIZON         			BOLKMS	117   	BK117B1     	5626012	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911TL					7198				ARTIFICAL HORIZON SLOW TO PULL FLAG.						1	G	7	2 	3U				H13EU   					 
1999020500313	19990205	00313	EU  	1999	2	5	HEEA060459       	1	19990125	G	6320	4638001001	TRANSMISSION    			BOLKMS	105   	BO105S      	5626006	EU  										M/R GEARBOX	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81982	13125				S818				TRANSMISSION HAS METAL IN OIL.						1	G	7	2 	3U				H3EU    					 
1999020500314	19990205	00314	EU  	1999	2	5	HEEA060460       	1	19990125	G	6320	4638001004	TRANSMISSION    			BOLKMS	105   	BO105S      	5626006	EU  										M/R GEARBOX	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	818SH	8414 				S753				TRANSMISSION HAS METAL IN OIL.						1	G	7	2 	3U				H3EU    					 
1999020500315	19990205	00315		1999	2	5	HEEA060461       	4	19990125	G	2312	6222093001	POWER SUPPLY    			BOLKMS	105   	BO105S      	5626006	EU  										COMM EQUIPMENT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3520T					S539				NO TRANSMIT LIGHT ON ROLL VHF WHEN KEYED.						1	G	7	2 	3U				H3EU    					 
1999020500316	19990205	00316	EU  	1999	2	5	HEEA060462       	1	19990125	G	7930	6607190A	SWITCH          			BOLKMS	105   	BO105S      	5626006	EU  										OIL PRESSURE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	91070					S145				WARNING LIGHT WILL NOT ILLUMINATE ZERO PRESSURE.						1	G	7	2 	3U				H3EU    					 
1999020500317	19990205	00317		1999	2	5	HEEA060464       	4	19990125	G	2340	AA20030	AMPLIFIER       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5031U					S678				POWER COMES ON, BUT THERE IS NO OUTPUT.						1	G	7	2 	3U				H3EU    					 
1999020500318	19990205	00318		1999	2	5	HEEA060465       	4	19990125	G	2340	AA20030	AMPLIFIER       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5031U					S678				NOISE IN PA SPEAKER AT ALL TIMES.						1	G	7	2 	3U				H3EU    					 
1999020500319	19990205	00319		1999	2	5	HEEA060466       	4	19990125	G	2340	AA20030	AMPLIFIER       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5031U					S678				PA AMPLIFIER WILL NOT COME ON.						1	G	7	2 	3U				H3EU    					 
1999020500320	19990205	00320	EU  	1999	2	5	HEEA060467       	1	19990125	G	3340	A413AHDACF1428	POWER SUPPLY    			BOLKMS	105   	BO105S      	5626006	EU  										STROBE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7136H					S833				NO OUTPUT VOLTAGE.						1	G	7	2 	3U				H3EU    					 
1999020500321	19990205	00321	EU  	1999	2	5	HEEA060468       	1	19990125	G	2844	BSE206150G3	TRANSDUCER      			BOLKMS	105   	BO105S      	5626006	EU  										FUEL SYSTEM	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4573B					S673				TRANSDUCER READS EXCESSIVLEY LOW.						1	G	7	2 	3U				H3EU    					 
1999020500322	19990205	00322	EU  	1999	2	5	HEEA060469       	1	19990125	G	2840	DK042	TRANSMITTER     			BOLKMS	105   	BO105S      	5626006	EU  										FUEL SYSTEM	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	86CH					S557				PRESSURE TRANSMISSION CAUSING FLUCTUATIONS; READS HIGH OUT OF TOLERANCE ABOVE 16 PSI.						1	G	7	2 	3U				H3EU    					 
1999020500323	19990205	00323	EU  	1999	2	5	HEEA060470       	1	19990125	G	7714	DL41239	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4302G					S853				NEEDLE INTERMITTENTLY STAYS ON ZERO, CANNON PLUG BROKEN.						1	G	7	2 	3U				H3EU    					 
1999020500324	19990205	00324	EU  	1999	2	5	HEEA060471       	1	19990125	G	7714	DL41239	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	86CH					S557				SMALL NEEDLE OSCILLATES.						1	G	7	2 	3U				H3EU    					 
1999020500325	19990205	00325	EU  	1999	2	5	HEEA060472       	1	19990125	G	7714	DL43638	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										TRIPLE TACH	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911FL					S717				NR 1 NEEDLE STICKS ON STAMP ON START-UP, OTHERS ERRATIC.						1	G	7	2 	3U				H3EU    					 
1999020500326	19990205	00326	EU  	1999	2	5	HEEA060473       	1	19990125	G	6220	F32827	BEARING         		117141081   	BOLKMS	117   	BK117B1     	5626012	EU  										M/R HUB	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911TL				050016	7198				BEARINGS SPINNING IN HUB.  REPLACED WITH SERVICEABLE BEARINGS.						1	G	7	2 	3U				H13EU   					 
1999020500327	19990205	00327	EU  	1999	2	5	HEEA060474       	1	19990125	G	7712	G555674	TRANSDUCER      			BOLKMS	117   	BK117A3     	5626015	EU  										ENGINE TORQUE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	401PH					7050				PRESSURE TRANSDUCER'S TORQUE INDICATION FELL TO ZERO.						1	G	7	2 	3U				H13EU   					 
1999021900464	19990219	00464	GL  	1999	2	19	HEEA060475       	2	19990204	G	7250	23007210	VANE            		23033193    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					TURBINE	MISMANUFACTURED 	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6160Y				CAC90816	51609	CAE895092			RECEIVING INSPECTION REVEALED:  MEASURED .009 INCH OUT OF ROUND ON VANE ASSEMBLY INSIDE DIAMETER.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999021900465	19990219	00465	GL  	1999	2	19	HEEA060476       	2	19990209	G	7250	23008064	NOZZLE          		23035128    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					1ST STAGE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5435V	953  			CAT90011	760158	CAE890627S			ENGINE REMOVED DUE TO CYCLES.  UPON INSPECTION OF TURBINE PARTS NOTED:  CRACKED BEYOND SERVICEABLE LIMITS ON NR 1 NOZZLE	 VANES.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999021900466	19990219	00466	GL  	1999	2	19	HEEA060477       	2	19990209	G	7250	23055438	NOZZLE          		23035128    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					GP SECTION	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5435V	953  			CAT90011	760158	CAE890627S			ENGINE REMOVED DUE TO CYCLES.  UPON INSPECTION OF TURBINE PARTS NOTED:  CRACKED BEYOND SERVICEABLE LIMITS ON NR 2 NOZZLE	 VANES THROUGH OUTER BAND.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999021900467	19990219	00467	GL  	1999	2	19	HEEA060478       	2	19990209	G	7230	23007210	VANE            		23033193    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					DIFFUSER	MISMANUFACTURED 	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6160Y				CAC90816	51609	CAE895092			RECEIVING INSPECTION REVEALED:  MEASURED .009 INCH OUT OF ROUND ON VANE ASSEMBLY.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999021900468	19990219	00468	SW  	1999	2	19	HEEA060479       	1	19990204	G	2435	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										STARTER/GEN	FAILED          	E			HEEA	K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			SW	03	6957Y					28139				ARMATURE LOOKS AND SMELLS BURNT.						2	G	7	2 	4U				H10SW   					 
1999021900469	19990219	00469	SW  	1999	2	19	HEEA060480       	1	19990204	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z					33077				SHORT IN ACTUATOR HARNESS, WILL OPERATE WHEN HARNESS BENT.						1	G	7	2 	4U				H4SW    					 
1999021900470	19990219	00470	SW  	1999	2	19	HEEA060481       	1	19990204	G	5260	212075418103	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										WILL NOT WORK FROM STOCK.  CASE DENTED.						1	G	7	2 	4U				H4SW    					 
1999021900471	19990219	00471	SW  	1999	2	19	HEEA060482       	1	19990204	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										STEP ACTUATOR INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999021900472	19990219	00472		1999	2	19	HEEA060483       	4	19990204	G	2210	214074303115	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										AUTOFLIGHT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				ALTITUDE HOLD INOPERATIVE IN AUTOFLIGHT.						2	G	7	2 	4U				H10SW   					 
1999021900473	19990219	00473	SW  	1999	2	19	HEEA060484       	1	19990209	G	6420	407012101107	HUB             			BELL  	407   	407         		SW  										TAIL ROTOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH	1117 				53198				HUB FROZEN TO T/R GEARBOX SHAFT; USED 5 TONS OF HYDRAULIC PRESSURE TO FREE.						1	G	7	1 	3U			O	H2SW    					 
1999021900474	19990219	00474	SW  	1999	2	19	HEEA060485       	1	19990209	G	5310	222035256109	SLAT ASSY       			BELL  	230   	230         	1182149	SW  										FUSELAGE	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	230UN					23009				RIGHT SLAT ASSEMBLY SEPARATED.  UNABLE TO PROVIDE ASSY, PURCHASED PIECE PARTS:  4 EACH, 222-035-002-101, SUPPORT;  1 EAC	H, 222-035-002-103, SUPPORT;  1 EACH, 222-035-002-105, SUPPORT;  1 EACH, 222-035-003-111, RIGHT SLAT.					1	G	7	2 	3U			NC	H9SW    					 
1999021900475	19990219	00475	SW  	1999	2	19	HEEA060486       	1	19990209	G	6510	406040339111	BEARING         		407040303101	BELL  	407   	407         		SW  										T/R DRIVE	ROUGH           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH				AFS1138	53278				FAN SHAFT ASSEMBLY HAS ROUGH BEARINGS; COMPLY WITH ASB 407-98-23.  SERIAL NUMBERS REMOVED ARE H98-0666 AND H98-0672.						1	G	7	1 	3U			O	H2SW    					 
1999021900476	19990219	00476	SW  	1999	2	19	HEEA060487       	1	19990209	G	6520	406040400115	GEARBOX         			BELL  	407   	407         		SW  										TAIL ROTOR	FROZEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH	775  				53198				T/R TRUNNION FROZEN ON OUTPUT SHAFT AND INPUT SEAL LEAKS.						1	G	7	1 	3U			O	H2SW    					 
1999021900477	19990219	00477	SW  	1999	2	19	HEEA060488       	1	19990209	G	6510	406040339111	BEARING         		407040303101	BELL  	407   	407         		SW  										T/R DRIVE	ROUGH           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	722PH				AFS1124	53288				FAN SHAFT ASSEMBLY HAS ROUGH BEARINGS.  COMPLY WITH ASB 407-98-23.  SERIAL NUMBERS REMOVED ARE A98-0555 AND A98-0567.						1	G	7	1 	3U			O	H2SW    					 
1999021900478	19990219	00478	SW  	1999	2	19	HEEA060489       	1	19990209	G	6510	406040339111	BEARING         		406040320101	BELL  	407   	407         		SW  										T/R DRIVE	ROUGH           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH				AFS922	53114				SHAFT ASSEMBLY HAS ROUGH BEARINGS.  COMPLY WITH ASB 407-98-23.  SERIAL NUMBERS REMOVED ARE H98-0638 AND H98-0649.						1	G	7	1 	3U			O	H2SW    					 
1999021900479	19990219	00479	SW  	1999	2	19	HEEA060491       	1	19990209	G	6220	407010103101	HORN            			BELL  	407   	407         		SW  										M/R HUB	MISINSTALLED    	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	402PH	1701 				53159				BUSHING FOR PITCH LINK UNIVERSAL INSTALLED INCORRECTLY.  FOUND DEFORMATION OF HORN EAR.						1	G	7	1 	3U			O	H2SW    					 
1999021900480	19990219	00480	SW  	1999	2	19	HEEA060492       	1	19990209	G	6230	406010401115	SWASHPLATE      			BELL  	407   	407         		SW  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	405PH	1284 				53207				UPPER GREASE SEAL LEAKING ON SWASHPLATE.						1	G	7	1 	3U			O	H2SW    					 
1999021900482	19990219	00482	SW  	1999	2	19	HEEA060494       	1	19990209	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH	2807 				53072				UNIVERSAL HAS BEARINGS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999021900483	19990219	00483	SW  	1999	2	19	HEEA060495       	1	19990209	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427PH	1874 				53059				UNIVERSAL HAS BEARINGS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999021900484	19990219	00484	SW  	1999	2	19	HEEA060496       	1	19990209	G	5311	206032308103S	FRAME           			BELL  	407   	407         		SW  										FUSELAGE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				FRAME HAS CRACK AT RIGHT UPPER BOLT HOLE.						1	G	7	1 	3U			O	H2SW    					 
1999021900485	19990219	00485	SW  	1999	2	19	HEEA060497       	1	19990209	G	7714	407375008101	INDICATOR       			BELL  	407   	407         		SW  										DUAL TACHOMETER	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				DUAL TACHOMETER'S N2 NEEDLE INOPERATIVE.						1	G	7	1 	3U			O	H2SW    					 
1999021900486	19990219	00486	SW  	1999	2	19	HEEA060498       	1	19990209	G	3212	212073905001	GAUGE           			BELL  	407   	407         		SW  										FLOAT	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				NEEDLE INACCURATE ON PRESSURE GAUGE.						1	G	7	1 	3U			O	H2SW    					 
1999021900487	19990219	00487	SW  	1999	2	19	HEEA060499       	1	19990209	G	6220	407010150103	FRAHM ASSY      			BELL  	407   	407         		SW  										MAIN ROTOR	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				MR VIBRATION.						1	G	7	1 	3U			O	H2SW    					 
1999021900488	19990219	00488	SW  	1999	2	19	HEEA060500       	1	19990209	G	3212	212073905001	GAUGE           			BELL  	407   	407         		SW  										FLOAT	CONTAMINATED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				PRESSURE GAUGE HAS WATER INSIDE OF GLASS.						1	G	7	1 	3U			O	H2SW    					 
1999021900489	19990219	00489	SW  	1999	2	19	HEEA060501       	1	19990209	G	6330	222320823121	RESTRAINT ASSY  			BELL  	230   	230         	1182149	SW  										M/R TRANSMISSION	FRAYED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	230UN					23009				RESTRAINT ASSEMBLY FRAYED AND I.D. TAG UNREADABLE.						1	G	7	2 	3U			NC	H9SW    					 
1999021900490	19990219	00490	SW  	1999	2	19	HEEA060502       	1	19990209	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				DISK COUPLING PITTED.						1	G	7	1 	3U			O	H2SW    					 
1999021900491	19990219	00491	SW  	1999	2	19	HEEA060503       	1	19990209	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				DISK COUPLING PITTED.						1	G	7	1 	3U			O	H2SW    					 
1999021900492	19990219	00492	SW  	1999	2	19	HEEA060504       	1	19990209	G	6420	406312100101	BEARING         		407012101107	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH	512  			A249	53038				TAIL ROTOR HUB ASSEMBLY HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999021900493	19990219	00493	SW  	1999	2	19	HEEA060505       	1	19990209	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				LINK HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999021900494	19990219	00494	SW  	1999	2	19	HEEA060506       	1	19990209	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				LINK HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999021900495	19990219	00495	SW  	1999	2	19	HEEA060507       	1	19990209	G	5210	222031200139S	DOOR            			BELL  	230   	230         	1182149	SW  										COCKPIT	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	230UN					23009				DOOR HAS CORROSION BEYOND LIMITS.						1	G	7	2 	3U			NC	H9SW    					 
1999021900496	19990219	00496	SW  	1999	2	19	HEEA060508       	1	19990209	G	5210	222031200121S	BEARINGS        			BELL  	230   	230         	1182149	SW  										CREW DOOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	230UN					23009				DOOR HAS WORN BEARINGS.						1	G	7	2 	3U			NC	H9SW    					 
1999021900497	19990219	00497	SW  	1999	2	19	HEEA060509       	1	19990209	G	5210	222031244106	SUPPORT         			BELL  	230   	230         	1182149	SW  										CREW DOOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	230UN					23009				SUPPORT ASSEMBLY FOR DOOR FOUND CRACKED.						1	G	7	2 	3U			NC	H9SW    					 
1999021900498	19990219	00498	SW  	1999	2	19	HEEA060510       	1	19990209	G	6510	206061432116	BLOWER HOUSING  			BELL  	407   	407         		SW  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				BLOWER HOUSING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999021900499	19990219	00499	SW  	1999	2	19	HEEA060511       	1	19990209	G	6410	406312100101	BEARING         		407012101105	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH				53187	53188				BEARINGS WORN AND CORRODED.						1	G	7	1 	3U			O	H2SW    					 
1999021900500	19990219	00500	SW  	1999	2	19	HEEA060512       	1	19990210	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	MISINSTALLED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				DISK COUPLING FOUND UNDER TORQUED.						1	G	7	1 	3U			O	H2SW    					 
1999021900501	19990219	00501	SW  	1999	2	19	HEEA060513       	1	19990210	G	6300	222010510101	FITTING         			BELL  	230   	230         	1182149	SW  										M/R DRIVE	CHAFED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	230UN					23009				FITTING ASSEMBLY CHAFED BEYOND LIMITS.						1	G	7	2 	3U			NC	H9SW    					 
1999021900502	19990219	00502	SW  	1999	2	19	HEEA060514       	1	19990210	G	2822	407362013101	SWITCH          			BELL  	407   	407         		SW  										ENGINE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				PRESSURE SWITCH HAS NO LIGHT.						1	G	7	1 	3U			O	H2SW    					 
1999021900503	19990219	00503	SW  	1999	2	19	HEEA060515       	1	19990210	G	6220	222310503103	BEARING         			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	DEBONDED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	230UN					23009				METAL PLATE DEBONDED.						1	G	7	2 	3U			NC	H9SW    					 
1999021900504	19990219	00504	SW  	1999	2	19	HEEA060517       	1	19990210	G	6322	206061432121	HOUSING         			BELL  	407   	407         		SW  										BLOWER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457PH					53147				BLOWER HOUSING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999021900505	19990219	00505	SW  	1999	2	19	HEEA060518       	1	19990210	G	6330	222010548105	BEARING LINER   			BELL  	230   	230         	1182149	SW  										XMSN MOUNT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	230UN					23009				BEARING LINER COATING IS DAMAGED AND METAL IS CHAFED.						1	G	7	2 	3U			NC	H9SW    					 
1999021900506	19990219	00506	SW  	1999	2	19	HEEA060519       	1	19990210	G	6220	407010150103	FRAHM ASSY      			BELL  	407   	407         		SW  										MAIN ROTOR	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				MR VIBRATION IN-FLIGHT.  FOUND RUBBER MISSING ON MR PACK.						1	G	7	1 	3U			O	H2SW    					 
1999021900507	19990219	00507	SW  	1999	2	19	HEEA060523       	1	19990210	G	3212	206050247135	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				FLOAT COVER IS TORN.						1	G	7	1 	3U			O	H2SW    					 
1999021900508	19990219	00508	SW  	1999	2	19	HEEA060524       	1	19990210	G	2841	407375006101	INDICATOR       			BELL  	407   	407         		SW  										COCKPIT	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				FUEL QUANTITY INDICATOR INDICATES 500 POUNDS OF FUEL WITH 800 POUNDS OF FUEL IN AIRCRAFT.						1	G	7	1 	3U			O	H2SW    					 
1999021900509	19990219	00509	SW  	1999	2	19	HEEA060527       	1	19990210	G	6322	206061432121	HOUSING         			BELL  	407   	407         		SW  										BLOWER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				BLOWER HOUSING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999021900510	19990219	00510	SW  	1999	2	19	HEEA060528       	1	19990210	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				DISK COUPLING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999021900511	19990219	00511	SW  	1999	2	19	HEEA060529       	1	19990210	G	5330	407070620158	PANEL           			BELL  	407   	407         		SW  										FUSELAGE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				LOWER RIGHT DOOR PANEL CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999021900512	19990219	00512	SW  	1999	2	19	HEEA060530       	1	19990210	G	6300	206362002103	SEAL            			BELL  	407   	407         		SW  										M/R DRIVE	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	510PH					53209				CAP SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999021900513	19990219	00513	SW  	1999	2	19	HEEA060531       	1	19990210	G	3212	206050247137	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				FLOAT COVER TORN.						1	G	7	1 	3U			O	H2SW    					 
1999021900514	19990219	00514	SW  	1999	2	19	HEEA060532       	1	19990210	G	5320	407070620156	HEADLINER       			BELL  	407   	407         		SW  										FUSELAGE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				HEAD LINER ASSEMBLY CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999021900515	19990219	00515	SW  	1999	2	19	HEEA060533       	1	19990210	G	5330	407070620158	PANEL           			BELL  	407   	407         		SW  										FUSELAGE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				LOWER RIGHT DOOR PANEL CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999021900516	19990219	00516	SW  	1999	2	19	HEEA060534       	1	19990210	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH	1233 				53072				UNIVERSAL BEARINGS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999021900517	19990219	00517	SW  	1999	2	19	HEEA060535       	1	19990210	G	3212	206050247135	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				FLOAT COVER TORN.						1	G	7	1 	3U			O	H2SW    					 
1999021900518	19990219	00518	SW  	1999	2	19	HEEA060536       	1	19990210	G	7332	7G1056	LIGHT           			BELL  	230   	230         	1182149	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	230UN					23009				FUEL PRESSURE LIGHT WILL NOT ILLUMINATE.						1	G	7	2 	3U			NC	H9SW    					 
1999021900519	19990219	00519	SW  	1999	2	19	HEEA060538       	1	19990210	G	6310	406040500123	FREEWHEEL UNIT  			BELL  	407   	407         		SW  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	720PH	409  				53277				FREEWHEEL UNIT LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999021900521	19990219	00521	SW  	1999	2	19	HEEA060542       	1	19990210	G	3310	AN33201	RELAY           			BELL  	407   	407         		SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	457PH					53147				RELAY NOT MAKING CONTACT.						1	G	7	1 	3U			O	H2SW    					 
1999021900522	19990219	00522	SW  	1999	2	19	HEEA060543       	1	19990210	G	6720	406012129101	LINK            			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427PH					53059				LINK ASSEMBLY BEARINGS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999021900523	19990219	00523	SW  	1999	2	19	HEEA060544       	1	19990210	G	3310	MS2774324	RELAY           			BELL  	407   	407         		SW  										COCKPIT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427PH					53059				RELAY INTERMITTENTLY STICKS.						1	G	7	1 	3U			O	H2SW    					 
1999021900524	19990219	00524		1999	2	19	HEEA060545       	4	19990210	G	2340	PM212302	SWITCH          			BELL  	407   	407         		SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				NO PILOTS ICS OR RADIO TRANSMIT.						1	G	7	1 	3U			O	H2SW    					 
1999021900525	19990219	00525	SW  	1999	2	19	HEEA060546       	1	19990210	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				DISC SEPARATION.						1	G	7	1 	3U			O	H2SW    					 
1999021900526	19990219	00526	SW  	1999	2	19	HEEA060547       	1	19990210	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	WARPED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				DISK COUPLING WARPED.						1	G	7	1 	3U			O	H2SW    					 
1999021900527	19990219	00527	SW  	1999	2	19	HEEA060548       	1	19990210	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	WARPED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				DISK COUPLING WARPED.						1	G	7	1 	3U			O	H2SW    					 
1999021900528	19990219	00528	SW  	1999	2	19	HEEA060549       	1	19990210	G	6300	406040500119	SUPPORT SEAL    			BELL  	407   	407         		SW  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	722PH	438  				53288				LEAKS AT SEAL.						1	G	7	1 	3U			O	H2SW    					 
1999021900529	19990219	00529	SW  	1999	2	19	HEEA060550       	1	19990210	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				DISK COUPLING PITTED.						1	G	7	1 	3U			O	H2SW    					 
1999021900530	19990219	00530	SW  	1999	2	19	HEEA060551       	1	19990210	G	2500	407370720101	RESTRAINT ASSY  			BELL  	407   	407         		SW  										CABIN	FRAYED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				RESTRAINT ASSEMBLY FRAYED.						1	G	7	1 	3U			O	H2SW    					 
1999021900531	19990219	00531	SW  	1999	2	19	HEEA060552       	1	19990210	G	2500	407370720101	RESTRAINT ASSY  			BELL  	407   	407         		SW  										CABIN	FRAYED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				RESTRAINT ASSEMBLY FRAYED.						1	G	7	1 	3U			O	H2SW    					 
1999021900532	19990219	00532	SW  	1999	2	19	HEEA060553       	1	19990210	G	6420	406312100101	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH					53266				WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999021900533	19990219	00533	SW  	1999	2	19	HEEA060554       	1	19990210	G	7921	406360500101	COOLER          			BELL  	407   	407         		SW  										OIL SYSTEM	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	57416					53070				COOLER LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999021900534	19990219	00534	SW  	1999	2	19	HEEA060555       	1	19990210	G	2435	206062200113	STARTER         			BELL  	407   	407         		SW  										STARTER/GEN	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH	493  				53278				STARTER/GENERATOR WILL NOT MOTOR.  INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND TWO BRUSHES AND BRUSH BOXES BURNT.  AL	SO FOUND MOTOR SHORTED.					1	G	7	1 	3U			O	H2SW    					 
1999021900535	19990219	00535	SW  	1999	2	19	HEEA060556       	1	19990210	G	2435	206062200113	STARTER         			BELL  	407   	407         		SW  										STARTER/GEN	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH	2078 				53266				STARTER/GENERATOR FAILED 300-HOUR INSPECTION.   INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES EXCESSIVELY WORN 	AND SCARRING ON COMMUTATOR.					1	G	7	1 	3U			O	H2SW    					 
1999021900536	19990219	00536	EU  	1999	2	19	HEEA060562       	1	19990204	G	6410	355A09103601	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6100R					2862				BEARINGS WORN.  PART SCRAPPED ON SITE.						1	G	7	1 	3U				H9EU    					 
1999021900537	19990219	00537	EU  	1999	2	19	HEEA060565       	1	19990204	G	6730	SC5084	SERVO           			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	6097Z	1594 				2820				SERVO LEAKING.						1	G	7	1 	3U				H9EU    					 
1999021900538	19990219	00538	EU  	1999	2	19	HEEA060566       	1	19990208	G	6220	704A33633109	THRUST BEARING  			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L	2190 				2873				BEARINGS BULGING AND BLISTERING.  SERIAL NUMBERS REMOVED ARE 9735, 9736, AND 9746.  REPLACEMENT PART SERIAL NUMBERS ARE 	12161, 12173, AND 12113.					1	G	7	1 	3U				H9EU    					 
1999031900283	19990319	00283	SW  	1999	3	19	HEEA060627       	1	19990216	G	5302	205032811077A	PANEL           		212030100121	BELL  	412   	412         	1182202	SW  										TAIL BOOM	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	107X				33113	33113				PANEL ASSEMBLY MISMANUFACTURED.  CONTOUR OF PANEL DOES NOT FIT TAILBOOM ASSY.  WHEN PANEL IS PLACED AGAINST THE SIDE OF 	THE TAILBOOM, THERE IS A GAP OF APPROXIMATELY .25 INCH.  WHEN THE PANEL IS CLAMPED TO THE TAILBOOM TO ELIMINATE THIS GAP	, THE UPPER AND LOWER ATTACH FLANGES ARE PUSHED AWAY FROM THE LONGERONS CREATING A .25 INCH GAP.				1	G	7	2 	4U				H4SW    					 
1999031900284	19990319	00284	SW  	1999	3	19	HEEA060628       	1	19990216	G	5330	205032816079	PANEL           		212030100121	BELL  	412   	412         	1182202	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	107X				33113	33113				PANEL ASSEMBLY MISMANUFACTURED.  WHILE PREPARING TO LOCATE PANEL, NOTICED THAT AREAS OF THE TOP, CORRUGATED SKIN HAD FLA	T HIGH POINTS, INSTEAD OF ROUNDED HIGH POINTS.  UPON FURTHER OBSERVATION, AND THE REMOVAL OF THE PRIMER COAT IN A FEW AR	EAS, FOUND THE HIGH POINTS OF THE CORRUGATED SKIN HAD BEEN SANDED THROUGH, APPARENTLY DURING PANEL CLEAN UP.				1	G	7	2 	4U				H4SW    					 
1999031900285	19990319	00285	SW  	1999	3	19	HEEA060629       	1	19990216	G	6320	212070116009	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRANSMISSION OIL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7128R					36007				NEEDLE ON PRESSURE SIDE PEGGED OUT AND DID NOT RETURN TO NORMAL.  REPAIRED AND RETURNED TO SERVICE.						1	G	7	2 	4U				H4SW    					 
1999031900286	19990319	00286		1999	3	19	HEEA060630       	4	19990216	G	3416	212070238007	ALTIMETER       			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				WHEN BARO KNOB IS TURNED, BAROMETRIC PRESSURE CARD DOES NOT MOVE ACCORDINGLY.						1	G	7	2 	4U				H4SW    					 
1999031900287	19990319	00287	SW  	1999	3	19	HEEA060631       	1	19990216	G	7722	212075067105	INDICATOR       			BELL  	412   	412         	1182202	SW  										ITT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893N					33010				ITT INDICATOR WILL NOT INDICATE.						1	G	7	2 	4U				H4SW    					 
1999031900288	19990319	00288	SW  	1999	3	19	HEEA060632       	1	19990216	G	6230	214040125101	BEARING         		412040366105	BELL  	412   	412         	1182202	SW  										MAST	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	293CA	9281 			A900230	330055				WORN AND CORRODED.  REPLACED LINER AND RETURNED TO SERVICE.						1	G	7	2 	4U				H4SW    					 
1999031900289	19990319	00289	SW  	1999	3	19	HEEA060633       	1	19990216	G	2432	39563001	BATTERY         			BELL  	412   	412         	1182202	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	800Y					33134				INSPECTED BY ACCESSORY SHOP AND FOUND BATTERY ONLY IN SERVICE FOR TWO HOURS FROM THE VENDOR.						1	G	7	2 	4U				H4SW    					 
1999031900290	19990319	00290		1999	3	19	HEEA060634       	4	19990216	G	2210	4025008918	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				WHEN AFCS COMPUTER INSTALLED, CAUSED YAW CHANNEL TO OSCILLATE, YAW CHANNEL TOO SENSITIVE.						1	G	7	2 	4U				H4SW    					 
1999031900291	19990319	00291	SW  	1999	3	19	HEEA060635       	1	19990216	G	6220	412010427101	BEARING         			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22608					33075				WORN BEARING.  REPLACED WITH SERVICEABLE BEARING.						1	G	7	2 	4U				H4SW    					 
1999031900292	19990319	00292	SW  	1999	3	19	HEEA060636       	1	19990216	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	MISMANUFACTURED 	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2149S	10903				36002				WILL NOT FLY WITH OTHER BLADE SINCE THE NEW 18 INCH DOUBLER WAS BONDED NEAR THE TIP.						1	G	7	2 	4U				H4SW    					 
1999031900293	19990319	00293	SW  	1999	3	19	HEEA060637       	1	19990216	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										EROSION SHIELD	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023	9656 				33080				EROSION SHIELD TORN ON THE OUTER END.						1	G	7	2 	4U				H4SW    					 
1999031900294	19990319	00294	SW  	1999	3	19	HEEA060638       	1	19990216	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2149S	12453				36002				OUTBOARD LEADING EDGE STRIP HAS EROSION HOLES.						1	G	7	2 	4U				H4SW    					 
1999031900295	19990319	00295	SW  	1999	3	19	HEEA060639       	1	19990216	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2258F	4206 				33073				BLADE DAMAGED ON THE UPPER SURFACE CENTER AT STA 120.						1	G	7	2 	4U				H4SW    					 
1999031900296	19990319	00296	SW  	1999	3	19	HEEA060641       	1	19990216	G	6230	412040102101	LINER           		412040366105	BELL  	412   	412         	1182202	SW  										MAST	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	293CA	9281 			A900230	330055				LINER/MAST WORN AND CORRODED.  REPLACED WITH SERVICEABLE PART.						1	G	7	2 	4U				H4SW    					 
1999031900297	19990319	00297	SW  	1999	3	19	HEEA060642       	1	19990216	G	6230	412040104103	NUT             		412040366105	BELL  	412   	412         	1182202	SW  										MAST	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	293CA	9281 			A900230	330055				CORROSION ON THREADS.  REPLACED WITH SERVICEABLE PART.						1	G	7	2 	4U				H4SW    					 
1999031900298	19990319	00298	SW  	1999	3	19	HEEA060643       	1	19990216	G	6320	412040123101	QUILL ASSY      			BELL  	412   	412         	1182202	SW  										TRANSMISSION	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2149S	4600 				36002				ONE EACH DISK, P/N 9440791-1, WORN BEYOND LIMITS AND ONE EACH FLANGE, P/N 209-040-177-101, WORN BEYOND LIMITS.  SCRAPPED	 DISK AND FLANGE AND REPLACED WITH SERVICEABLE PARTS.					1	G	7	2 	4U				H4SW    					 
1999031900299	19990319	00299	SW  	1999	3	19	HEEA060644       	1	19990216	G	6240	412075010109	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				ALL NEEDLES FLUCTUATE AND INTERMITTENTLY DROP OFF-LINE.						1	G	7	2 	4U				H4SW    					 
1999031900300	19990319	00300	SW  	1999	3	19	HEEA060645       	1	19990216	G	6220	412310400107	BEARING         		412010406115	BELL  	412   	412         	1182202	SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22608				A999	33075				LINK ASSEMBLY HAS WORN BEARING.  REPLACED WITH SERVICEABLE BEARING.						1	G	7	2 	4U				H4SW    					 
1999031900301	19990319	00301	SW  	1999	3	19	HEEA060646       	1	19990216	G	6220	412310400107	BEARING         		412010406115	BELL  	412   	412         	1182202	SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008				A1044	36004				LINK ASSEMBLY HAS WORN BEARING.  REPLACED WITH SERVICEABLE BEARING.						1	G	7	2 	4U				H4SW    					 
1999031900302	19990319	00302	SW  	1999	3	19	HEEA060647       	1	19990216	G	6220	412310400107	BEARING         		412010406115	BELL  	412   	412         	1182202	SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008				A2313	36004				LINK ASSEMBLY HAS WORN BEARING.  REPLACED WITH SERVICEABLE BEARING.						1	G	7	2 	4U				H4SW    					 
1999031900303	19990319	00303	SW  	1999	3	19	HEEA060648       	1	19990216	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z					33077				NR 1 ENGINE GENERATOR WOULD NOT COME ON-LINE WITH NR 2 GENERATOR ON.						1	G	7	2 	4U				H4SW    					 
1999031900304	19990319	00304	SW  	1999	3	19	HEEA060649       	1	19990216	G	3340	7028521	LIGHT           			BELL  	412   	412         	1182202	SW  										STROBE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2148K					36001				STROBE LIGHT TOTALLY INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999031900305	19990319	00305	SW  	1999	3	19	HEEA060650       	1	19990216	G	3340	7028511	LIGHT           			BELL  	412   	412         	1182202	SW  										STROBE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141PH					33197				STROBE LIGHT DRAWS EXCESSIVE CURRENT.						1	G	7	2 	4U				H4SW    					 
1999031900306	19990319	00306	SW  	1999	3	19	HEEA060651       	1	19990216	G	3340	7028521	LIGHT           			BELL  	412   	412         	1182202	SW  										STROBE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2148K					36001				WHEN POWER TURNED ON, ANTI-COLLISION CIRCUIT BREAKER TRIPS.						1	G	7	2 	4U				H4SW    					 
1999031900307	19990319	00307		1999	3	19	HEEA060652       	4	19990216	G	3457	8143902240B	GPS             			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	142PH					33150				EACH SECOND TIME THE FPL BUTTON IS PRESSED, THE UNIT TURNS OFF THEN COMES ON AT THE START OF THE INITIAL CYCLE.						1	G	7	2 	4U				H4SW    					 
1999031900308	19990319	00308		1999	3	19	HEEA060653       	4	19990216	G	3442	MI5851352	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22347					36005				NO NOISE BAND WHEN RADAR WAS IN TEST MODE.  PERFORMED PRELIMINARY INSPECTION AND FOUND PROGRAMMER BOARD BAD, REPLACED U2	202, U2203, U2205, C2210, Q2212.  REPAIRED.  ADJUSTED STC AND GAIN VOLTAGE.  BENCH CHECK GOOD.					1	G	7	2 	4U				H4SW    					 
1999031900309	19990319	00309	SW  	1999	3	19	HEEA060654       	1	19990216	G	2435	200SGL132Q	STARTER         			BELL  	206   	206L3       	1182108	SW  										START/GENERATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8592X	477  				51508				STARTER/GENERATOR WILL NOT MOTOR FOR START OR GENERATE.						1	G	7	1 	3U				H2SW    					 
1999031900310	19990319	00310	GL  	1999	3	19	HEEA060655       	2	19990216	G	7323	25246929	GOVERNOR        			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					ENGINE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2761N					45277				IN CRUISE FLIGHT, PILOT EXPERIENCED TORQUE OSCILLATIONS AND YAW WITH CORRESPONDING TORQUE, TOT, N1 AND N2 INDICATIONS. R	EMOVED GOVERNOR AND FOUND SHAFT HARD TO TURN.  A LARGE AMOUNT OF METAL PARTICLES WERE FOUND IN THE MOUNTING FLANGE AREA.	  FOUND DRIVE BEARINGS TO HAVE FAILED, SUSPECT A BEARING WASH-OUT.  UNIT OVERHAULED TO MFG SPECS.				1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999031900311	19990319	00311	SW  	1999	3	19	HEEA060656       	1	19990216	G	2432	32007001	BATTERY         			BELL  	206   	206L3       	1182108	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41128					51134				BATTERY HAD NUMEROUS BURNT CELLS.						1	G	7	1 	3U				H2SW    					 
1999031900312	19990319	00312	SW  	1999	3	19	HEEA060657       	1	19990216	G	6510	327211	DISC SET        			BELL  	206   	206L3       	1182108	SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				DISC CORRODED AND CRACKED.  REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U				H2SW    					 
1999031900313	19990319	00313	SW  	1999	3	19	HEEA060658       	1	19990216	G	6510	327211	DISC SET        			BELL  	206   	206L1       	1182107	SW  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2761N					45277				DISC CORRODED BEYOND LIMITS.  REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U				H2SW    					 
1999031900314	19990319	00314	SW  	1999	3	19	HEEA060659       	1	19990216	G	6510	327211	DISC SET        			BELL  	206   	206L1       	1182107	SW  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1076Y					45380				DISC CORRODED BEYOND LIMITS.  REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U				H2SW    					 
1999031900315	19990319	00315	GL  	1999	3	19	HEEA060660       	2	19990216	G	7314	3881005	PUMP            			BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					FUEL SYSTEM	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81SP					51029				WORN DRIVE SHAFT SPLINES AND GEARS.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999031900316	19990319	00316	SW  	1999	3	19	HEEA060661       	1	19990216	G	6310	406340102101	CARBON SEAL     		406040500113	BELL  	206   	206L4       	1182110	SW  										M/R DRIVE	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	7077B	420  			A1716	52037				SEAL LEAKING.  REPLACED WITH SERVICEABLE SEAL.						1	G	7	1 	3U			NC	H2SW    					 
1999031900317	19990319	00317		1999	3	19	HEEA060662       	4	19990216	G	3453	4530103	RECEIVER        			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	10814					45415				ARNAV 21 LOCKS UP.						1	G	7	1 	3U				H2SW    					 
1999031900318	19990319	00318		1999	3	19	HEEA060663       	4	19990216	G	3422	5050031904	GYRO            			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										FLAG INTERMITTENTLY PULLS THEN DROPS BACK DOWN.  BENCH CHECK UNIT.  FLAG INTERMITTENTLY PULLS THEN DROPS INTO VIEW UNTIL	 ROTOR ATTAINS A SPEED OF 22,000 RPM AND FLAG WILL PULL OUT OF VIEW.  THIS FLAG CIRCUIT FUNCTIONS PROPERLY.  UNIT BENCH 	CHECK GOOD.				1	G	7	1 	3U				H2SW    					 
1999031900319	19990319	00319	SW  	1999	3	19	HEEA060664       	1	19990216	G	6220	568331S59	PACKING         		206011100159	BELL  	206   	206L3       	1182108	SW  										M/R HUB	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	6610C				HB10	51425				LEAKING.  REPLACED WITH NEW SERVICEABLE EXCLUDER.						1	G	7	1 	3U				H2SW    					 
1999031900320	19990319	00320	SW  	1999	3	19	HEEA060665       	1	19990216	G	7910	70056L000Y374	FITTING         			BELL  	206   	206L1       	1182107	SW  										ENGINE OIL	WRONG PART      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2758N					45267				WRONG TYPE FITTING INSTALLED ON HOSE ASSEMBLY.						1	G	7	1 	3U				H2SW    					 
1999031900321	19990319	00321	SW  	1999	3	19	HEEA060666       	1	19990216	G	3212	8226003	FUSIBLE PLUG    			BELL  	206   	206L1       	1182107	SW  										FLOAT	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50182					45242				FLOAT BOTTLE PRESSURE LEAKING THROUGH FUSIBLE PLUG.  REPLACED WITH SERVICEABLE PLUG.						1	G	7	1 	3U				H2SW    					 
1999031900322	19990319	00322	SW  	1999	3	19	HEEA060667       	1	19990216	G	7722	9429100133	INDICATOR       			BELL  	206   	206B3       	1181506	SW  										TOT	MISMARKED       	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	2275Q	86   				3625				TOT INDICATOR HAS IMPROPER MARKINGS.						1	G	7	1 	3U				H2SW    					 
1999031900323	19990319	00323		1999	3	19	HEEA060668       	4	19990216	G	2340	AA20030	AMPLIFIER       			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	49EA					51507				PA AMP HAS NO POWER (LIGHT OUT).						1	G	7	1 	3U				H2SW    					 
1999031900324	19990319	00324		1999	3	19	HEEA060669       	4	19990216	G	3140	MI5851345	DISPLAY         																	CENTRAL COMPUTER	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										INDICATOR DOES NOT PAINT CLEAR AZIMUTH MARKERS ON 60 DEGREE OR 120 DEGREE PAINTS.  SCRATCHY, UNDEFINED MARKERS.  PERFORM	ED PRELIMINARY INSPECTION.  FOUND DISPLAY SPIKING AT TIMES, FOUND PROBLEM ON LOGIC NR 1 BOARD.  REPLACED IC U1226, U1236	, U1231.  REPAIRED.  ALSO REPLACED 5 EACH SOCKET TERMINALS ON CONNECTOR J1201.  REPAIRED INTERMITTENT PROBLEM.  BENCH CH	ECK GOOD.																 
1999031900325	19990319	00325	SW  	1999	3	19	HEEA060670       	1	19990216	G	6220	S30769	EXCLUDER        		206011100159	BELL  	206   	206L3       	1182108	SW  										M/R HUB	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	6610C				HB10	51425				EXCLUDER LEAKING.  REPLACED WITH SERVICEABLE PARTS.						1	G	7	1 	3U				H2SW    					 
1999031900326	19990319	00326	SW  	1999	3	19	HEEA060671       	1	19990216	G	6220	S30769	EXCLUDER        		206011100159	BELL  	206   	206L3       	1182108	SW  										M/R HUB	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	54641				A285	51184				EXCLUDER LEAKING.  REPLACED WITH SERVICEABLE PARTS.						1	G	7	1 	3U				H2SW    					 
1999031900327	19990319	00327	SW  	1999	3	19	HEEA060672       	1	19990216	G	6220	S30769	EXCLUDER        		206011100105	BELL  	206   	206L3       	1182108	SW  										M/R HUB	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8594X	617  			MR030598	51531				EXCLUDER WORN - SLINGING GREASE.  REPLACED WITH SERVICEABLE PARTS.						1	G	7	1 	3U				H2SW    					 
1999031900328	19990319	00328	SW  	1999	3	19	HEEA060673       	1	19990216	G	2430	206075447007	REGULATOR       			BELL  	206   	206L3       	1182108	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6160Y					51609				GENERATOR WILL NOT COME ON-LINE.  ADJUSTED VOLTAGE TO 28 VOLTS GENERATOR OUTPUT - REGULATOR WILL NOT CLOSE LINE CONTROL 	RELAY.					1	G	7	1 	3U				H2SW    					 
1999031900329	19990319	00329	SW  	1999	3	19	HEEA060674       	1	19990216	G	7330	206075676117	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1076T					45373				LOADMETER NEEDLE IS STUCK ON 80 PERCENT (WILL NOT COME DOWN AT ALL).						1	G	7	1 	3U				H2SW    					 
1999031900330	19990319	00330	SW  	1999	3	19	HEEA060675       	1	19990216	G	2842	EA4703587	SENSOR          			BELL  	206   	206B3       	1181506	SW  										FUEL CELL	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2269A					3608				FLOAT LEAKING.  UNIT WAS PURCHASED ON 6-7-89.						1	G	7	1 	3U				H2SW    					 
1999031900331	19990319	00331		1999	3	19	HEEA060676       	4	19990216	G	3416	D120P2T	ENCODER         			BELL  	206   	206L3       	1182108	SW  										ALTIMETER	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251V					51404				ENCODER IS OFF APPROXIMATELY 1500 TO 2000 FEET ON AIRCRAFT.  TIME SINCE REPAIR 0:00 HOURS.						1	G	7	1 	3U				H2SW    					 
1999031900332	19990319	00332	SW  	1999	3	19	HEEA060677       	1	19990216	G	2844	BSE20630G	TRANSDUCER      			BELL  	206   	206L3       	1182108	SW  										FUEL PRESSURE	CORROED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				WHILE REMOVING FUEL PRESSURE TRANSDUCER, IT WAS NOTED THAT THE CANNON PLUG ATTACHED HAD BEEN EXPOSED TO VARIOUS CORROSIV	E ELEMENTS AND HAD CORRODED TO THE EXTENT THAT THE PLUG COULD NOT BE REMOVED WITHOUT DAMAGING THE PLUG AND TRANSDUCER. R	EPLACED WITH SERVICEABLE CANNON PLUG AND TRANSDUCER.				1	G	7	1 	3U				H2SW    					 
1999031900333	19990319	00333	SW  	1999	3	19	HEEA060678       	1	19990219	G	5311	212061812113	FRAME           			BELL  	412   	412         	1182202	SW  										BS 113	MISMANUFACTURED 	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	107X					33113				FRAME MISMANUFACTURED.  OPENING FOR DOOR - 113 FRAME TOO SMALL BY .25 INCH IN HEIGHT AND TOO SMALL BY .8750 INCH IN LENG	TH AS MARKED ON NEW FRAME LOCATIONS.  THIS -113 KELVAR FRAME WAS SUBSTITUTED FOR -106 METAL FRAME ORDERED.					1	G	7	2 	4U				H4SW    					 
1999031900334	19990319	00334		1999	3	19	HEEA060679       	4	19990222	G	2312	064100900	TRANSCEIVER     			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545X					760050				TRANSCEIVER HAS WEAK AND SCRATCHY OPERATION.						1	G	7	2 	3U				H1NE    					 
1999031900335	19990319	00335	NE  	1999	3	19	HEEA060680       	2	19990222	G	7200	3017600	ENGINE          			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					POWER SECTION	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893P	16633				33012				HIGH OIL CONSUMPTION.						1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999031900336	19990319	00336	NE  	1999	3	19	HEEA060681       	2	19990222	G	7200	3017600	BLADE           			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023	11466				33080				ROTOR BLADE FAILURE.						1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999031900337	19990319	00337	NE  	1999	3	19	HEEA060682       	2	19990222	G	7210	3024780	GEARBOX         			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					COMBINING	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S	13800				33022				COMBINING GEARBOX MAKING METAL.						1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999031900338	19990319	00338		1999	3	19	HEEA060683       	2	19990223	G	7322	2543391	SHAFT           																	THROTTLE	FAULTY          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										THROTTLE SHAFT LEVERS WILL NOT INSTALL FAR ENOUGH ONTO THROTTLE SHAFTS TO FACILITATE INSTALLATION OF RETAINING PINS.																			 
1999031900339	19990319	00339		1999	3	19	HEEA060684       	4	19990223	G	3442	7007700705	INDICATOR       																	COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										INTERMITTENTLY SHUTS OFF.																			 
1999031900340	19990319	00340		1999	3	19	HEEA060685       	4	19990222	G	2312	064100900	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	WEAK            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22608					33075				VERY WEAK AND FOUND WATER IN RADIO.						1	G	7	2 	4U				H4SW    					 
1999031900341	19990319	00341		1999	3	19	HEEA060686       	4	19990222	G	2312	064100900	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22608					33075				TRANSCEIVER WILL NOT TRANSMIT O.D. RECEIVE.						1	G	7	2 	4U				H4SW    					 
1999031900342	19990319	00342		1999	3	19	HEEA060687       	4	19990222	G	2312	064100900	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22608					33075				TRANSCEIVER HAS INTERMITTENT OPERATION.						1	G	7	2 	4U				H4SW    					 
1999031900343	19990319	00343		1999	3	19	HEEA060688       	4	19990222	G	2312	064100900	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5759N					33002				TRANSCEIVER HAS INTERMITTENT WEAK TRANSMISSION AND LOW SIDE TONE.						1	G	7	2 	4U				H4SW    					 
1999031900344	19990319	00344		1999	3	19	HEEA060689       	4	19990222	G	3454	071121627	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2148K					36001				NAVIGATION CONTROL CANNOT CHANGE FREQUENCY.						1	G	7	2 	4U				H4SW    					 
1999031900345	19990319	00345		1999	3	19	HEEA060690       	4	19990222	G	3455	066104701	RECEIVER        			BELL  	412   	412         	1182202	SW  										ADF	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22608					33075				TRANSCEIVER WILL NOT RECEIVE AND POINT TO STATION.						1	G	7	2 	4U				H4SW    					 
1999031900346	19990319	00346		1999	3	19	HEEA060691       	4	19990222	G	3455	066104701	RECEIVER        			BELL  	412   	412         	1182202	SW  										ADF	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893P					33012				TRANSCEIVER WILL NOT RECEIVE.						1	G	7	2 	4U				H4SW    					 
1999031900347	19990319	00347		1999	3	19	HEEA060692       	4	19990222	G	3455	066104701	RECEIVER        			BELL  	412   	412         	1182202	SW  										ADF	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893P					33012				ADF TRANSCEIVER RECEIVED AUDIO INTERMITTENT, BFO AUDIO CONSTANT EVEN WITH SWITCH OFF.						1	G	7	2 	4U				H4SW    					 
1999031900348	19990319	00348		1999	3	19	HEEA060693       	4	19990222	G	3431	066107800	RECEIVER        			BELL  	412   	412         	1182202	SW  										COCKPIT NAV	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22347					36005				VHF NAVIGATOR RECEIVER INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999031900349	19990319	00349		1999	3	19	HEEA060694       	4	19990222	G	3431	066400700	RECEIVER        			BELL  	412   	412         	1182202	SW  										COCKPIT VOR	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	293CA					330055				GLIDE SLOPE DEFECTIVE, OUT OF SPECS.						1	G	7	2 	4U				H4SW    					 
1999031900350	19990319	00350		1999	3	19	HEEA060695       	4	19990222	G	3425	071107600	AMPLIFIER       			BELL  	412   	412         	1182202	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893L					33006				TRANSCEIVER INOPERATIVE.  NEEDLE SPINNING.						1	G	7	2 	4U				H4SW    					 
1999031900351	19990319	00351		1999	3	19	HEEA060696       	4	19990222	G	3425	071107600	AMPLIFIER       			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893P					33012				TRANSCEIVER CAUSES VOR NEEDLE TO SWING ALL THE TIME.						1	G	7	2 	4U				H4SW    					 
1999031900352	19990319	00352		1999	3	19	HEEA060697       	4	19990222	G	3452	071119208	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2149S					36002				KFS CONTROL DOES NOT TURN ON.						1	G	7	2 	4U				H4SW    					 
1999031900353	19990319	00353		1999	3	19	HEEA060698       	4	19990222	G	3450	071121004	CONTROL BOX     			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141PH					33197				NUMBERS WILL NOT CHANGE WITH DIAL ON CONTROL BOX.						1	G	7	2 	4U				H4SW    					 
1999031900354	19990319	00354		1999	3	19	HEEA060699       	4	19990222	G	3420	1113025	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT HSI	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893P					33012				HSI INDICATOR LIGHTS DIM AND FLICKERING.						1	G	7	2 	4U				H4SW    					 
1999031900355	19990319	00355		1999	3	19	HEEA060700       	4	19990222	G	3420	1113025	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT HSI	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	800Y					33134				GLIDESLOPE FLAG WILL NOT PULL OUT OF VIEW.  STICKS INTERMITTENTLY.						1	G	7	2 	4U				H4SW    					 
1999031900356	19990319	00356		1999	3	19	HEEA060701       	4	19990222	G	3420	1113025	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT HSI	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T					33112				FLAG WILL NOT PULL EXCEPT WHEN TAPPED.						1	G	7	2 	4U				H4SW    					 
1999031900357	19990319	00357		1999	3	19	HEEA060702       	4	19990222	G	3420	1113025	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT HSI	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T					33112				HSI INDICATOR VERTICAL ADJUSTMENT KNOB INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999031900358	19990319	00358		1999	3	19	HEEA060703       	4	19990222	G	3420	1113034	INDICATOR       			BELL  	212   	212         	1181420	SW  										ATTITUDE	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1082G					31109				INDICATOR SPHERE IS ERRATIC IN PITCH.						1	G	7	1 	4U				H4SW    					 
1999031900359	19990319	00359		1999	3	19	HEEA060704       	4	19990222	G	3420	1113034	INDICATOR       			BELL  	412   	412         	1182202	SW  										ATTITUDE	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5759N					33002				GS POINTER STICKS, PITCH ADJUSTED.  KNOB SLOW TO REACT.						1	G	7	2 	4U				H4SW    					 
1999031900360	19990319	00360	SW  	1999	3	19	HEEA060705       	1	19990222	G	6520	212040004009	GEARBOX         			BELL  	412   	412         	1182202	SW  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	142PH	14239				33150				CORROSION PITS ON OUTPUT SHAFT.						1	G	7	2 	4U				H4SW    					 
1999031900361	19990319	00361	SW  	1999	3	19	HEEA060706       	1	19990222	G	7712	212075037101	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2261D					33076				N1 INDICATION STICKS ON ZERO.						1	G	7	2 	4U				H4SW    					 
1999031900362	19990319	00362	SW  	1999	3	19	HEEA060707       	1	19990222	G	7722	212075067105	INDICATOR       			BELL  	412   	412         	1182202	SW  										ITT	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				GAUGE FLUCTUATES RAPIDLY DURING FLIGHT.						1	G	7	2 	4U				H4SW    					 
1999031900363	19990319	00363	SW  	1999	3	19	HEEA060708       	1	19990222	G	7722	212075067109	INDICATOR       			BELL  	412   	412         	1182202	SW  										ITT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2258F					33073				STICKS INTERMITTENTLY AT ZERO.						1	G	7	2 	4U				H4SW    					 
1999031900364	19990319	00364	SW  	1999	3	19	HEEA060709       	1	19990222	G	5260	212075418103	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				STEP ACTUATOR WILL NOT ACTUATE.						1	G	7	2 	4U				H4SW    					 
1999031900365	19990319	00365	SW  	1999	3	19	HEEA060710       	1	19990222	G	5260	212075418103	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008					36004				STEP ACTUATOR WILL NOT ACTUATE.						1	G	7	2 	4U				H4SW    					 
1999031900366	19990319	00366	SW  	1999	3	19	HEEA060711       	1	19990222	G	5260	212075418103	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2148K					36001				STEP ACTUATOR WILL NOT ACTUATE.						1	G	7	2 	4U				H4SW    					 
1999031900367	19990319	00367	SW  	1999	3	19	HEEA060712       	1	19990222	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				STEP ACTUATOR ROD END BROKEN.						1	G	7	2 	4U				H4SW    					 
1999031900368	19990319	00368	SW  	1999	3	19	HEEA060713       	1	19990222	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S					33022				STEP ACTUATOR STUCK IN MID-TRAVEL.						1	G	7	2 	4U				H4SW    					 
1999031900369	19990319	00369	SW  	1999	3	19	HEEA060714       	1	19990222	G	6730	212076005105	CYLINDER        			BELL  	412   	412         	1182202	SW  										M/R CONTROL	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	22347	10636				36005				CYLINDER ASSEMBLY LEAKING.						1	G	7	2 	4U				H4SW    					 
1999031900370	19990319	00370	SW  	1999	3	19	HEEA060715       	1	19990222	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										M/R CONTROL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z					33077				ROTARY ACTUATOR BRAKE STICK WILL NOT RELEASE.						1	G	7	2 	4U				H4SW    					 
1999031900371	19990319	00371	SW  	1999	3	19	HEEA060716       	1	19990222	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										M/R CONTROL	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	293CA					330055				ROTARY ACTUATOR STICKS INTERMITTENTLY.   DATE OF MFG 10-29-98.						1	G	7	2 	4U				H4SW    					 
1999031900372	19990319	00372	SW  	1999	3	19	HEEA060717       	1	19990222	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										M/R CONTROL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	293CA					330055				AFCS IN ATT. MODE HAS CONSTANT ROLL MOTORING.						1	G	7	2 	4U				H4SW    					 
1999031900373	19990319	00373	SW  	1999	3	19	HEEA060718       	1	19990222	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										M/R CONTROL	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893P					33012				ROTARY ACTUATOR STICKS.						1	G	7	2 	4U				H4SW    					 
1999031900374	19990319	00374	SW  	1999	3	19	HEEA060719       	1	19990222	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										M/R CONTROL	BINDING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7128R					36007				ROTARY ACTUATOR BINDING.						1	G	7	2 	4U				H4SW    					 
1999031900375	19990319	00375	SW  	1999	3	19	HEEA060720       	1	19990222	G	6340	214074280107	DETECTOR        			BELL  	412   	412         	1182202	SW  										RPM LIMIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				WARNING LIGHT AND AUDIO COME ON INTERMITTENTLY.						1	G	7	2 	4U				H4SW    					 
1999031900376	19990319	00376	SW  	1999	3	19	HEEA060721       	1	19990222	G	6340	214074280107	DETECTOR        			BELL  	412   	412         	1182202	SW  										RPM LIMIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893L					33006				RPM LIMIT INDICATOR CAUSES CHIRPING IN AUDIO.						1	G	7	2 	4U				H4SW    					 
1999031900377	19990319	00377	SW  	1999	3	19	HEEA060722       	1	19990222	G	6340	214074280107	DETECTOR        			BELL  	412   	412         	1182202	SW  										RPM LIMIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				RPM LIMIT DICTATOR INTERMITTENT.						1	G	7	2 	4U				H4SW    					 
1999031900378	19990319	00378		1999	3	19	HEEA060723       	4	19990222	G	3424	214075244001	GYRO            			BELL  	212   	212         	1181420	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1079U					31122				RATE GYRO TURN NEEDLE INOPERATIVE.						1	G	7	1 	4U				H4SW    					 
1999031900379	19990319	00379		1999	3	19	HEEA060724       	4	19990222	G	3425	71252	GYRO            			BELL  	412   	412         	1182202	SW  										HSI	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2261D					33076				GYRO NEEDLE INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999031900380	19990319	00380		1999	3	19	HEEA060725       	4	19990222	G	3424	214075244101	GYRO            			BELL  	412   	412         	1182202	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	800Y					33134				RATE GYRO NEEDLE WILL NOT MOVE.						1	G	7	2 	4U				H4SW    					 
1999031900381	19990319	00381	SW  	1999	3	19	HEEA060726       	1	19990222	G	6340	214074280107	DETECTOR        			BELL  	412   	412         	1182202	SW  										RPM LIMIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893P					33012				CANNOT ADJUST AUDIO ON RPM LIMIT DETECTOR.						1	G	7	2 	4U				H4SW    					 
1999031900382	19990319	00382		1999	3	19	HEEA060727       	4	19990222	G	2211	222305004105	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				LIGHTS ON MOTE SELECT UNIT INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999031900383	19990319	00383	SW  	1999	3	19	HEEA060728       	1	19990222	G	2435	23046020	STARTER         			BELL  	412   	412         	1182202	SW  										START/GENERATOR	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023	15558				33080				STARTER/GENERATOR WILL NOT COME ON LINE.						1	G	7	2 	4U				H4SW    					 
1999031900384	19990319	00384	SW  	1999	3	19	HEEA060729       	1	19990222	G	2435	23046020	STARTER         			BELL  	412   	412         	1182202	SW  										START/GENERATOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5759N	25647				33002				ENGINE STARTS SLOW.						1	G	7	2 	4U				H4SW    					 
1999031900385	19990319	00385		1999	3	19	HEEA060730       	4	19990222	G	2200	2593996333	TARSYN 333      			BELL  	412   	412         	1182202	SW  										AUTOFLIGHT	PRECESSING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893P					33012				TARSYN KICKS FORE AND AFT.  DG NOISY AND PRECESSES.						1	G	7	2 	4U				H4SW    					 
1999031900386	19990319	00386	SW  	1999	3	19	HEEA060731       	1	19990222	G	2842	391046200	PROBE           			BELL  	412   	412         	1182202	SW  										FUEL QUANTITY	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S					33022				PROBE READS HIGH OUT OF TOLERANCE.						1	G	7	2 	4U				H4SW    					 
1999031900387	19990319	00387	SW  	1999	3	19	HEEA060732       	1	19990222	G	2842	381065009	TRANSMITTER     			BELL  	412   	412         	1182202	SW  										FUEL QUANTITY	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S					33022				TRANSMITTER READS HIGH.						1	G	7	2 	4U				H4SW    					 
1999031900388	19990319	00388	SW  	1999	3	19	HEEA060733       	1	19990222	G	2432	39563001	BATTERY         			BELL  	412   	412         	1182202	SW  										DC SYSTEM	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	293CA					330055				BATTERY PACK TRIPS CIRCUIT BREAKER.  TIME SINCE REPAIR 522:10 HOURS.						1	G	7	2 	4U				H4SW    					 
1999031900389	19990319	00389		1999	3	19	HEEA060734       	4	19990222	G	2210	4020936903	GYRO            			BELL  	412   	412         	1182202	SW  										TARSYN	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	800Y					33134				GYRO INDICATOR CAUSES KICK IN AFCS PITCH.						1	G	7	2 	4U				H4SW    					 
1999031900390	19990319	00390		1999	3	19	HEEA060735       	4	19990222	G	2210	4025008918	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2149S					36002				SERVO PRE AMP FAILS TESTS 32.1 AND 32.2.						1	G	7	2 	4U				H4SW    					 
1999031900391	19990319	00391		1999	3	19	HEEA060736       	4	19990222	G	2210	4025008918	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	293CA					330055				JIA PIN 54 BROKEN.						1	G	7	2 	4U				H4SW    					 
1999031900392	19990319	00392		1999	3	19	HEEA060737       	4	19990222	G	2210	4025008918	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3911L					33023				KICKS OFF-LINE INTERMITTENTLY.  TIME SINCE REPAIR 312:35 HOURS.						1	G	7	2 	4U				H4SW    					 
1999031900393	19990319	00393		1999	3	19	HEEA060738       	4	19990222	G	2210	4033089901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				COMPUTER WILL NOT TRACK IN NAV MODE.						1	G	7	2 	4U				H4SW    					 
1999031900394	19990319	00394		1999	3	19	HEEA060739       	4	19990222	G	2210	4033089901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				FAILED TEST 2.2, 2.3, 4.2 AND 4.3 ON SST.  TIME SINCE REPAIR 0:00 HOURS.						1	G	7	2 	4U				H4SW    					 
1999031900395	19990319	00395	SW  	1999	3	19	HEEA060740       	1	19990222	G	6220	412010190103	SPINDLE         			BELL  	412   	412         	1182202	SW  										MAIN ROTOR HEAD	UNBONDED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2261D	5004 				33076				SPINDLE BEARING UNBONDED.						1	G	7	2 	4U				H4SW    					 
1999031900396	19990319	00396	SW  	1999	3	19	HEEA060741       	1	19990222	G	6220	412010190103	SPINDLE         			BELL  	412   	412         	1182202	SW  										MAIN ROTOR HEAD	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2261D	3317 				33076				SPINDLE DAMPER SEPARATED.						1	G	7	2 	4U				H4SW    					 
1999031900397	19990319	00397	SW  	1999	3	19	HEEA060742       	1	19990222	G	6220	412010190103	SPINDLE         			BELL  	412   	412         	1182202	SW  										MAIN ROTOR HEAD	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2261D	2647 				33076				SPINDLE DAMPER SEPARATED.						1	G	7	2 	4U				H4SW    					 
1999031900398	19990319	00398	SW  	1999	3	19	HEEA060743       	1	19990222	G	6220	412010190103	SPINDLE         			BELL  	412   	412         	1182202	SW  										MAIN ROTOR HEAD	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2261D	2647 				33076				SPINDLE DAMPER SEPARATED.						1	G	7	2 	4U				H4SW    					 
1999031900399	19990319	00399	SW  	1999	3	19	HEEA060744       	1	19990222	G	6220	412010190103	SPINDLE         			BELL  	412   	412         	1182202	SW  										MAIN ROTOR HEAD	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023					33080				SPINDLE DAMPER SEPARATED.						1	G	7	2 	4U				H4SW    					 
1999031900400	19990319	00400	SW  	1999	3	19	HEEA060745       	1	19990222	G	6320	412040002103	TRANSMISSION    			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	OVERTORQUED     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03		11273								OVERTORQUE TO 110 PERCENT MOMENTARY LESS THAN 2 SECONDS.  5 SECONDS OPERATION, BRASS FOUND IN INTERNAL FILTER AND EXTERN	AL FILTER.					1	G	7	2 	4U				H4SW    					 
1999031900401	19990319	00401	SW  	1999	3	19	HEEA060746       	1	19990222	G	6320	412050013109	VALVE           			BELL  	412   	412         	1182202	SW  										FLOAT	STRIPPED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z					33077				AFT RELIEF VALVE THREADS STRIPPED.						1	G	7	2 	4U				H4SW    					 
1999031900402	19990319	00402	SW  	1999	3	19	HEEA060747       	1	19990222	G	3212	412050013113	FLOAT           			BELL  	412   	412         	1182202	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2149S	6038 				36002				FLOAT BAG LEAKING.						1	G	7	2 	4U				H4SW    					 
1999031900403	19990319	00403	SW  	1999	3	19	HEEA060748       	1	19990222	G	3212	412050013113	FLOAT           			BELL  	412   	412         	1182202	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2149S	3612 				36002				FLOAT BAG LEAKING.						1	G	7	2 	4U				H4SW    					 
1999031900404	19990319	00404	SW  	1999	3	19	HEEA060749       	1	19990222	G	3212	412050013115	FLOAT           			BELL  	412   	412         	1182202	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3893L					33006				FLOAT BAG ASSY LEAKING.  MANUFACTURED 12/93.						1	G	7	2 	4U				H4SW    					 
1999031900405	19990319	00405	SW  	1999	3	19	HEEA060750       	1	19990222	G	3212	D24922113	FLOAT           			BELL  	412   	412         	1182202	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3893L					33006				FLOAT BAG LEAKING.  MANUFACTURED 9/92.						1	G	7	2 	4U				H4SW    					 
1999031900406	19990319	00406	SW  	1999	3	19	HEEA060751       	1	19990222	G	3212	412050013119	FLOAT           			BELL  	412   	412         	1182202	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3893N	2349 				33010				FLOAT BAG LEAKING.						1	G	7	2 	4U				H4SW    					 
1999031900407	19990319	00407	SW  	1999	3	19	HEEA060752       	1	19990222	G	3212	412050017135	COVER           			BELL  	412   	412         	1182202	SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893N					33010				COVER ASSY WORN.						1	G	7	2 	4U				H4SW    					 
1999031900408	19990319	00408	SW  	1999	3	19	HEEA060753       	1	19990222	G	7712	412075008111	INDICATOR       			BELL  	412   	412         	1182202	SW  										DUAL TORQUE	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2261D					33076				NR 1 NEEDLE STICKS ON TORQUE INDICATOR.						1	G	7	2 	4U				H4SW    					 
1999031900409	19990319	00409	SW  	1999	3	19	HEEA060754       	1	19990222	G	6240	206075681105	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										DUAL TACHOMETER	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5005B					45175				DUAL TACHOMETER INDICATOR NEEDLE STICKS ON START.						1	G	7	1 	3U				H2SW    					 
1999031900410	19990319	00410	SW  	1999	3	19	HEEA060755       	1	19990222	G	7712	412075008111	INDICATOR       			BELL  	412   	412         	1182202	SW  										DUAL TORQUE	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893L					33006				NR 2 NEEDLE STUCK ON HIGH SIDE ON TORQUE INDICATOR.						1	G	7	2 	4U				H4SW    					 
1999031900411	19990319	00411	SW  	1999	3	19	HEEA060756       	1	19990222	G	7712	412075008111	INDICATOR       			BELL  	412   	412         	1182202	SW  										DUAL TORQUE	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3911L					33023				NEEDLE STUCK ON TORQUE INDICATOR.						1	G	7	2 	4U				H4SW    					 
1999031900412	19990319	00412		1999	3	19	HEEA060757       	4	19990222	G	3414	412075009105	INDICATOR       			BELL  	412   	412         	1182202	SW  										AIRSPEED	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008					36004				INDICATION HIGH ON AIRSPEED INDICATOR.						1	G	7	2 	4U				H4SW    					 
1999031900413	19990319	00413		1999	3	19	HEEA060758       	4	19990222	G	3414	412075009105	INDICATOR       			BELL  	412   	412         	1182202	SW  										AIRSPEED	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	142PH					33150				AIRSPEED INDICATOR INDICATES HIGH OUT OF TOLERANCE THROUGHOUT SCALE.						1	G	7	2 	4U				H4SW    					 
1999031900414	19990319	00414	SW  	1999	3	19	HEEA060759       	1	19990222	G	6240	412075010109	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				TRIPLE TACHOMETER INDICATOR'S NR 1 NEEDLE FOR N2 FAILED.						1	G	7	2 	4U				H4SW    					 
1999031900415	19990319	00415	SW  	1999	3	19	HEEA060760       	1	19990222	G	6240	412075010111	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				TRIPLE TACHOMETER INDICATOR'S NR 1 ENGINE NEEDLE STICKS AT 20 PERCENT.						1	G	7	2 	4U				H4SW    					 
1999031900416	19990319	00416	SW  	1999	3	19	HEEA060761       	1	19990222	G	2436	15891F	REGULATOR       			BELL  	206   	206B3       	1181506	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2272J					3620				UNABLE TO ADJUST ABOVE 26.5 VDC.						1	G	7	1 	3U				H2SW    					 
1999031900417	19990319	00417	SW  	1999	3	19	HEEA060762       	1	19990222	G	7722	9429100135	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8594X					51531				TOT INDICATOR HAS NO DIGITAL READ-OUT.						1	G	7	1 	3U				H2SW    					 
1999031900418	19990319	00418	SW  	1999	3	19	HEEA060763       	1	19990222	G	2422	412075101101	INVERTER        			BELL  	412   	412         	1182202	SW  										AC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3911L					33023				INVERTER FLUCTUATES BELOW 100 VOLTS.						1	G	7	2 	4U				H4SW    					 
1999031900419	19990319	00419	SW  	1999	3	19	HEEA060764       	1	19990222	G	2841	412375001105	INDICATOR       			BELL  	412   	412         	1182202	SW  										FUEL QUANTITY	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6559Z					36019				FUEL INDICATOR READS ERRATIC.						1	G	7	2 	4U				H4SW    					 
1999031900420	19990319	00420	SW  	1999	3	19	HEEA060765       	1	19990222	G	6240	412075010105	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S					33022				TRIPLE TACHOMETER INDICATOR HAS 4 PERCENT SPLIT BETWEEN  NR 1 AND  NR 2 NEEDLES.						1	G	7	2 	4U				H4SW    					 
1999031900421	19990319	00421	SW  	1999	3	19	HEEA060766       	1	19990222	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONTROL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023					33080				GENERATOR WOULD NOT COME ON LINE.						1	G	7	2 	4U				H4SW    					 
1999031900422	19990319	00422	SW  	1999	3	19	HEEA060767       	1	19990222	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONTROL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S					33022				CONTROL UNIT CAUSES GENERATOR TO KICK OFF-LINE.						1	G	7	2 	4U				H4SW    					 
1999031900423	19990319	00423	SW  	1999	3	19	HEEA060768       	1	19990222	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONTROL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T					33112				CONTROL UNIT HAS NO OUTPUT, UNABLE TO ADJUST.						1	G	7	2 	4U				H4SW    					 
1999031900424	19990319	00424	SW  	1999	3	19	HEEA060769       	1	19990222	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONTROL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T					33112				NR 2 GENERATOR KICKING OFF-LINE.  TIME SINCE REPAIR 1214:30 HOURS.						1	G	7	2 	4U				H4SW    					 
1999031900425	19990319	00425	SW  	1999	3	19	HEEA060770       	1	19990222	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONTROL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023					33080				NR 1 GENERATOR WILL NOT COME ON-LINE.						1	G	7	2 	4U				H4SW    					 
1999031900426	19990319	00426	SW  	1999	3	19	HEEA060771       	1	19990222	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONTROL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z					33077				NR 1 GENERATOR WOULD NOT COME ON-LINE WITH  NR 2 GENERATOR ON.						1	G	7	2 	4U				H4SW    					 
1999031900427	19990319	00427	SW  	1999	3	19	HEEA060772       	1	19990222	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONTROL	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				GENERATOR INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999031900428	19990319	00428		1999	3	19	HEEA060773       	4	19990222	G	2211	7000298901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	293CA					330055				AFCS COMPUTER FAILS DATT & PCPL LOGIC 14.1 TEST.						1	G	7	2 	4U				H4SW    					 
1999031900429	19990319	00429		1999	3	19	HEEA060774       	4	19990222	G	2211	7000298901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				NR 2 HELIPILOT WOULD NOT ENGAGE.  CAUSES SAS AND ATT LIGHTS TO STAY ILLUMINATED.						1	G	7	2 	4U				H4SW    					 
1999031900430	19990319	00430		1999	3	19	HEEA060775       	4	19990222	G	2210	7000299901	CONTROLLER      			BELL  	412   	412         	1182202	SW  										AUTOPILOT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2148K					36001				ATT/SAS BUTTON STICKS.						1	G	7	2 	4U				H4SW    					 
1999031900431	19990319	00431	SW  	1999	3	19	HEEA060776       	1	19990222	G	6730	7001482	CONTROL ROD     			BELL  	412   	412         	1182202	SW  										PITCH AXIS	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z					33077				PITCH STUCK IN UP POSITION AND WILL NOT TEST FORE AND AFT; CAUSE AFCS LIGHT TO CYCLE CONTINUOUSLY IN-FLIGHT.						1	G	7	2 	4U				H4SW    					 
1999031900432	19990319	00432	SW  	1999	3	19	HEEA060777       	1	19990222	G	6720	7001484	ACTUATOR        			BELL  	412   	412         	1182202	SW  										YAW CONTROL	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z					33077				YAW INOPERATIVE WILL NOT ACTUATE.						1	G	7	2 	4U				H4SW    					 
1999031900433	19990319	00433		1999	3	19	HEEA060778       	4	19990222	G	2312	7001840913	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3911L					33023				RECEIVER/TRANSMITTER INTERMITTENT IN-FLIGHT.						1	G	7	2 	4U				H4SW    					 
1999031900434	19990319	00434		1999	3	19	HEEA060779       	4	19990222	G	2312	7001840913	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	800Y					33134				RECEIVER/TRANSMITTER INDICATES 300 FOOT ERROR.						1	G	7	2 	4U				H4SW    					 
1999031900435	19990319	00435	SW  	1999	3	19	HEEA060780       	1	19990222	G	3340	7028506	LIGHT           			BELL  	412   	412         	1182202	SW  										FUSELAGE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6559Z					36019				ANTI-COLLISION LIGHT INOPERATIVE.  TIME SINCE REPAIR 124:55 HOURS.						1	G	7	2 	4U				H4SW    					 
1999031900436	19990319	00436	SW  	1999	3	19	HEEA060781       	1	19990222	G	2841	71122002	INDICATOR       			BELL  	412   	412         	1182202	SW  										FUEL QUANTITY	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893P					33012				FUEL QUANTITY INDICATOR STICKS AT 200 POUNDS AND DROPS TO ZERO WHEN AIRCRAFT LANDS.						1	G	7	2 	4U				H4SW    					 
1999031900437	19990319	00437	SW  	1999	3	19	HEEA060782       	1	19990222	G	3212	D24921115	FLOAT           			BELL  	412   	412         	1182202	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	6559Z					36019				FLOAT BAG ASSY'S FORWARD CHAMBER LEAKING.						1	G	7	2 	4U				H4SW    					 
1999031900438	19990319	00438	SW  	1999	3	19	HEEA060784       	1	19990222	G	3212	206050247103	COVER           			BELL  	206   	206L3       	1182108	SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	54641					51184				FLOAT COVER WORN.						1	G	7	1 	3U				H2SW    					 
1999031900439	19990319	00439	SW  	1999	3	19	HEEA060785       	1	19990222	G	3212	206050247101	COVER           			BELL  	206   	206L3       	1182108	SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81SP					51029				FLOAT COVER WORN AND TORN.						1	G	7	1 	3U				H2SW    					 
1999031900440	19990319	00440	SW  	1999	3	19	HEEA060786       	1	19990222	G	3212	206050247103	COVER           			BELL  	206   	206L3       	1182108	SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3207Q					51540				FLOAT COVER WORN AND TORN.						1	G	7	1 	3U				H2SW    					 
1999031900441	19990319	00441	SW  	1999	3	19	HEEA060787       	1	19990222	G	3212	206050247103	COVER           			BELL  	206   	206L1       	1182107	SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										FLOAT COVER WORN.						1	G	7	1 	3U				H2SW    					 
1999031900442	19990319	00442	SW  	1999	3	19	HEEA060788       	1	19990222	G	3212	206050248107	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				FLOAT BAG ASSEMBLY HAS PLY SEPARATION.						1	G	7	1 	3U				H2SW    					 
1999031900443	19990319	00443	SW  	1999	3	19	HEEA060789       	1	19990222	G	3212	206050248107	FLOAT           			BELL  	206   	206L1       	1182107	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2761N					45277				FLOAT BAG ASSEMBLY FAILED 6 MONTH INSPECTION DUE TO NUMEROUS PIN HOLE LEAKS.						1	G	7	1 	3U				H2SW    					 
1999031900444	19990319	00444	SW  	1999	3	19	HEEA060790       	1	19990222	G	3212	206050248107	FLOAT           			BELL  	206   	206L1       	1182107	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	1076Y					45380				FLOAT BAG ASSEMBLY HAS SLOW LEAK FROM LOWER OUTER SEAM NEAR MOUNT AREA.  TOTAL TIME 11/1991.						1	G	7	1 	3U				H2SW    					 
1999031900445	19990319	00445	SW  	1999	3	19	HEEA060791       	1	19990222	G	3212	206050248111	FLOAT           			BELL  	206   	206L1       	1182107	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	1076Y					45380				FLOAT BAG ASSEMBLY LEAKS FROM LOWER INBOARD SEAM.						1	G	7	1 	3U				H2SW    					 
1999031900446	19990319	00446	SW  	1999	3	19	HEEA060792       	1	19990222	G	3212	206050248111	FLOAT           			BELL  	206   	206L1       	1182107	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2764F					45279				FLOAT BAG ASSEMBLY WILL NOT STAY INFLATED.						1	G	7	1 	3U				H2SW    					 
1999031900447	19990319	00447	SW  	1999	3	19	HEEA060793       	1	19990222	G	3212	206050248113	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	42EA					51542				FLOAT BAG ASSEMBLY LEAKING.						1	G	7	1 	3U				H2SW    					 
1999031900448	19990319	00448	SW  	1999	3	19	HEEA060794       	1	19990222	G	3212	206050248115	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8593X					51509				ATTACHMENT GRID COMING LOOSE ON FLOAT BAG ASSEMBLY, FORWARD END.						1	G	7	1 	3U				H2SW    					 
1999031900449	19990319	00449	SW  	1999	3	19	HEEA060795       	1	19990222	G	3212	206050248115	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8593X					51509				ATTACHMENT GRID COMING LOOSE, ON FLOAT BAG ASSEMBLY, FORWARD END.						1	G	7	1 	3U				H2SW    					 
1999031900450	19990319	00450	SW  	1999	3	19	HEEA060796       	1	19990222	G	3212	206050248115	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	206FS					51506				FLOAT BAG ASSEMBLY FAILED 6 HOUR LEAK TEST AFTER 2 HOURS.						1	G	7	1 	3U				H2SW    					 
1999031900451	19990319	00451	SW  	1999	3	19	HEEA060797       	1	19990222	G	3212	206050248115	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	206FS					51506				FLOAT BAG ASSEMBLY FAILED 6 HOUR LEAK TEST AFTER 2 HOURS.						1	G	7	1 	3U				H2SW    					 
1999031900452	19990319	00452	SW  	1999	3	19	HEEA060798       	1	19990222	G	3212	206050248115	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	42EA					51542				FLOAT BAG ASSEMBLY LEAKING.						1	G	7	1 	3U				H2SW    					 
1999031900453	19990319	00453	SW  	1999	3	19	HEEA060799       	1	19990222	G	3212	206050248113	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	108PH					51334				FLOAT BAG ASSEMBLY'S CHECK VALVE LEAKING.						1	G	7	1 	3U				H2SW    					 
1999031900454	19990319	00454	SW  	1999	3	19	HEEA060800       	1	19990222	G	3212	206050248115	FLOAT           			BELL  	206   	206L1       	1182107	SW  										MLG	DAMAGED         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2251Z					45756				FLOAT BAG ASSEMBLY HAS  HOLE IN RIGHT HAND CHAMBER.						1	G	7	1 	3U				H2SW    					 
1999031900455	19990319	00455	SW  	1999	3	19	HEEA060801       	1	19990222	G	3212	206050248115	FLOAT           			BELL  	206   	206L1       	1182107	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	1076Y					45380				FLOAT BAG ASSEMBLY LEAKS FROM INBOARD VALVE.						1	G	7	1 	3U				H2SW    					 
1999031900456	19990319	00456	SW  	1999	3	19	HEEA060802       	1	19990222	G	3212	206050248115	FLOAT           			BELL  	206   	206L1       	1182107	SW  										MLG	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	2775A					45297				FLOAT BAG ASSEMBLY FAILED 180-DAY INSPECTION.  TOTAL TIME 11/1994.						1	G	7	1 	3U				H2SW    					 
1999031900457	19990319	00457	SW  	1999	3	19	HEEA060803       	1	19990222	G	3212	206050248117	FLOAT           			BELL  	206   	206L1       	1182107	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	1073W					45386				FLOAT BAG ASSEMBLY LEAKING.  TOTAL TIME 10/1994.						1	G	7	1 	3U				H2SW    					 
1999031900458	19990319	00458	SW  	1999	3	19	HEEA060804       	1	19990222	G	3212	206050248117	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	6610Y					51419				FLOAT BAG ASSEMBLY FAILED 6 MONTH PRESSURE TEST.						1	G	7	1 	3U				H2SW    					 
1999031900459	19990319	00459		1999	3	19	HEEA060805       	2	19990222	G	7510	206062625003	ACTUATOR        			BELL  	206   	206B3       	1181506	SW  										ENGINE DEICE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2753F					2729				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999031900460	19990319	00460	SW  	1999	3	19	HEEA060806       	1	19990222	G	6710	206062721103	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31073					51519				ACTUATOR UNABLE TO ADJUST SPREAD.						1	G	7	1 	3U				H2SW    					 
1999031900461	19990319	00461	SW  	1999	3	19	HEEA060807       	1	19990222	G	6710	206062721113	ACTUATOR        			BELL  	206   	206B3       	1181506	SW  										MAIN ROTOR	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2753F					2729				ACTUATOR WILL NOT EXTEND OR RETRACT.						1	G	7	1 	3U				H2SW    					 
1999031900462	19990319	00462	SW  	1999	3	19	HEEA060808       	1	19990222	G	6710	206062721113	ACTUATOR        			BELL  	206   	206B3       	1181506	SW  										MAIN ROTOR	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2272J					3620				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999031900463	19990319	00463	SW  	1999	3	19	HEEA060809       	1	19990222	G	6710	206062721113	ACTUATOR        			BELL  	206   	206B3       	1181506	SW  										MAIN ROTOR	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2285B					3642				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999031900464	19990319	00464	SW  	1999	3	19	HEEA060810       	1	19990222	G	6710	206062721113	ACTUATOR        			BELL  	206   	206B3       	1181506	SW  										MAIN ROTOR	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2272V					3621				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999031900465	19990319	00465	SW  	1999	3	19	HEEA060811       	1	19990222	G	6710	206062721113	ACTUATOR        			BELL  	206   	206B3       	1181506	SW  										MAIN ROTOR	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2268V					3605				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999031900466	19990319	00466	SW  	1999	3	19	HEEA060812       	1	19990222	G	6710	206062721113	ACTUATOR        			BELL  	206   	206B3       	1181506	SW  										MAIN ROTOR	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2277A					3630				ACTUATOR WILL NOT ACTUATE.						1	G	7	1 	3U				H2SW    					 
1999031900467	19990319	00467	SW  	1999	3	19	HEEA060813       	1	19990222	G	6710	206062721113	ACTUATOR        			BELL  	206   	206B3       	1181506	SW  										MAIN ROTOR	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	104PH					3622				ACTUATOR HAS NO MOVEMENT OR ACTIVATION.						1	G	7	1 	3U				H2SW    					 
1999031900468	19990319	00468	SW  	1999	3	19	HEEA060814       	1	19990222	G	2810	206063632001	FUEL CELL       			BELL  	206   	206L1       	1182107	SW  										DRAIN	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2770Y					45291				FUEL CELL LEAKING IN DRAIN.						1	G	7	1 	3U				H2SW    					 
1999031900469	19990319	00469	SW  	1999	3	19	HEEA060815       	1	19990222	G	2810	206063632001	FUEL CELL       			BELL  	206   	206L1       	1182107	SW  										SUMP	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2761N					45277				SUMP FLANGE CORRODED.						1	G	7	1 	3U				H2SW    					 
1999031900470	19990319	00470	SW  	1999	3	19	HEEA060816       	1	19990222	G	2810	206063632003	FUEL CELL       			BELL  	206   	206L1       	1182107	SW  										SUMP	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2761N					45277				SUMP FLANGE CORRODED.						1	G	7	1 	3U				H2SW    					 
1999031900471	19990319	00471	SW  	1999	3	19	HEEA060817       	1	19990222	G	2841	206063633001	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										FUEL QUANTITY	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2758N					45267				FUEL QUANTITY INDICATOR HAS A CRACKED GLASS AND READS LOW AT 400 POUNDS AND ABOVE.						1	G	7	1 	3U				H2SW    					 
1999031900472	19990319	00472	SW  	1999	3	19	HEEA060818       	1	19990222	G	2841	206063633101	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										FUEL QUANTITY	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	205FC					51130				FUEL QUANTITY INDICATOR'S NEEDLE STICKS THROUGHOUT RANGE.						1	G	7	1 	3U				H2SW    					 
1999031900473	19990319	00473	SW  	1999	3	19	HEEA060819       	1	19990222	G	2841	206063633103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										FUEL QUANTITY	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81671					51301				FUEL QUANTITY INDICATOR HAS FLUCTUATION.						1	G	7	1 	3U				H2SW    					 
1999031900474	19990319	00474	SW  	1999	3	19	HEEA060820       	1	19990222	G	2841	206063633103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										FUEL QUANTITY	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8593X					51509				BEZEL GASKET SHRUNK ON FUEL QUANTITY INDICATOR.  GLASS APPEARS TO BE CRACKED.						1	G	7	1 	3U				H2SW    					 
1999031900475	19990319	00475	SW  	1999	3	19	HEEA060821       	1	19990222	G	2810	206064611001	FUEL CELL       			BELL  	206   	206L1       	1182107	SW  										FLANGE	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2761N					45277				FUEL CAP FLANGE CORRODED.						1	G	7	1 	3U				H2SW    					 
1999031900476	19990319	00476	SW  	1999	3	19	HEEA060822       	1	19990222	G	2810	206064633105	FUEL CELL       			BELL  	206   	206L3       	1182108	SW  										FUSELAGE	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3207Q					51540				LEAKAGE THROUGH FABRIC AND BLISTERS INSIDE OF CELL.						1	G	7	1 	3U				H2SW    					 
1999031900477	19990319	00477	SW  	1999	3	19	HEEA060823       	1	19990222	G	2810	206064633105	FUEL CELL       			BELL  	206   	206L3       	1182108	SW  										FUSELAGE	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6160Z					51610				FUEL CELL HAS BLISTERS INSIDE AND OUTSIDE OF CELL.						1	G	7	1 	3U				H2SW    					 
1999031900478	19990319	00478	SW  	1999	3	19	HEEA060824       	1	19990222	G	7810	206064300005	EXHAUST STACK   			BELL  	206   	206L1       	1182107	SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2250U					45754				EXHAUST ASSEMBLY HAS CRACKED FLANGE.						1	G	7	1 	3U				H2SW    					 
1999031900479	19990319	00479	SW  	1999	3	19	HEEA060825       	1	19990222	G	7810	206064300005	EXHAUST STACK   			BELL  	206   	206L1       	1182107	SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406EH					45183				EXHAUST ASSEMBLY CRACKED.						1	G	7	1 	3U				H2SW    					 
1999031900480	19990319	00480	SW  	1999	3	19	HEEA060826       	1	19990222	G	7810	206064300005	EXHAUST STACK   			BELL  	206   	206L1       	1182107	SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406EH					45183				EXHAUST ASSEMBLY CRACKED.						1	G	7	1 	3U				H2SW    					 
1999031900481	19990319	00481	SW  	1999	3	19	HEEA060827       	1	19990222	G	7810	206064300005	EXHAUST STACK   			BELL  	206   	206L1       	1182107	SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	27766					45312				EXHAUST ASSEMBLY CRACKED.						1	G	7	1 	3U				H2SW    					 
1999031900482	19990319	00482	SW  	1999	3	19	HEEA060828       	1	19990222	G	7810	206064300005	EXHAUST STACK   			BELL  	206   	206L3       	1182108	SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31077					51520				EXHAUST ASSEMBLY CRACKED.						1	G	7	1 	3U				H2SW    					 
1999031900483	19990319	00483	SW  	1999	3	19	HEEA060829       	1	19990222	G	7810	206064300005	EXHAUST STACK   			BELL  	206   	206L3       	1182108	SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41791					51465				EXHAUST ASSEMBLY CRACKED.						1	G	7	1 	3U				H2SW    					 
1999031900484	19990319	00484	SW  	1999	3	19	HEEA060830       	1	19990222	G	7810	206064300005	EXHAUST STACK   			BELL  	206   	206L4       	1182110	SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7077B					52037				EXHAUST ASSEMBLY CRACKED.						1	G	7	1 	3U			NC	H2SW    					 
1999031900485	19990319	00485	SW  	1999	3	19	HEEA060831       	1	19990222	G	7712	206075185001	TORQUE GAUGE    			BELL  	206   	206B3       	1181506	SW  										ENGINE	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2269A					3608				TORQUE GAUGE READS LOW.						1	G	7	1 	3U				H2SW    					 
1999031900486	19990319	00486	SW  	1999	3	19	HEEA060832       	1	19990222	G	7712	206075185101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TORQUE METER	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5007Q					45187				TORQUE METER INDICATOR'S NEEDLE STICKS INTERMITTENTLY.						1	G	7	1 	3U				H2SW    					 
1999031900487	19990319	00487	SW  	1999	3	19	HEEA060833       	1	19990222	G	7712	206075185103	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TORQUE METER	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1076Y					45380				TORQUE INDICATOR READS HIGH OUT OF TOLERANCE.						1	G	7	1 	3U				H2SW    					 
1999031900488	19990319	00488	SW  	1999	3	19	HEEA060834       	1	19990222	G	2840	206075186005	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3905B					45598				DUAL INDICATOR'S LIGHTING IS INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999031900489	19990319	00489	SW  	1999	3	19	HEEA060835       	1	19990222	G	2840	206075186005	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										FUEL SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1078D					45397				FUEL PRESSURE ON INDICATION.						1	G	7	1 	3U				H2SW    					 
1999031900490	19990319	00490		1999	3	19	HEEA060836       	4	19990223	G	3421	214075244001	GYRO            			BELL  	412   	412         	1182202	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141PH					33197				RATE GYRO INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999031900491	19990319	00491	SW  	1999	3	19	HEEA060837       	1	19990223	G	7933	35712519129	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	513EH					45421				TOT INDICATOR HAS NO MOVEMENT ON LIGHT-OFF.						1	G	7	1 	3U				H2SW    					 
1999031900492	19990319	00492	SW  	1999	3	19	HEEA060838       	1	19990223	G	2840	206075186005	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5012V					45200				DUAL INDICATOR HAS A LIGHT BROKEN, GLASS OILED AND STAINED.						1	G	7	1 	3U				H2SW    					 
1999031900493	19990319	00493	SW  	1999	3	19	HEEA060839       	1	19990223	G	7931	206075187003	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										ENGINE OIL	LEAKS           	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2245Y					45751				LEAKS INTERMITTENTLY.						1	G	7	1 	3U				H2SW    					 
1999031900494	19990319	00494	SW  	1999	3	19	HEEA060840       	1	19990223	G	7931	206075187003	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										ENGINE OIL	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406EH					45183				ENGINE OIL AND TEMPERATURE PRESSURE INDICATIONS READ HIGH, OUT OF TOLERANCE.						1	G	7	1 	3U				H2SW    					 
1999031900495	19990319	00495	SW  	1999	3	19	HEEA060841       	1	19990223	G	7931	206075187003	INDICATOR       			BELL  	206   	206B3       	1181506	SW  										ENGINE OIL	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2753F					2729				ENGINE OIL TEMPERATURE READS 15 DEGREES LOW AT STATIC, WILL NOT GO ABOVE 30 DEGREES WITH ENGINE RUNNING.						1	G	7	1 	3U				H2SW    					 
1999031900496	19990319	00496	SW  	1999	3	19	HEEA060842       	1	19990223	G	7931	206075187003	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										ENGINE OIL	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	10761					45381				ENGINE OIL AND TEMPERATURE INDICATORS INDICATES HIGH, FLUCTUATES AT LOW END.						1	G	7	1 	3U				H2SW    					 
1999031900497	19990319	00497	SW  	1999	3	19	HEEA060843       	1	19990223	G	7933	206075188003	INDICATOR       			BELL  	206   	206B3       	1181506	SW  										TOT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2268V					3605				TEMPERATURE NEEDLE STICKS - GLASS CLOUDY.						1	G	7	1 	3U				H2SW    					 
1999031900498	19990319	00498	SW  	1999	3	19	HEEA060844       	1	19990223	G	6320	206075188005	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TRANSMISSION OIL	LEAKS           	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	1076Y					45380				INDICATOR HAS INTERNAL LEAK.						1	G	7	1 	3U				H2SW    					 
1999031900499	19990319	00499	SW  	1999	3	19	HEEA060845       	1	19990223	G	6320	206075188005	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5014V					45217				BEZEL SEPARATING FROM INDICATOR.						1	G	7	1 	3U				H2SW    					 
1999031900500	19990319	00500	SW  	1999	3	19	HEEA060846       	1	19990223	G	7933	206075188005	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TRANSMISSION OIL	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5745S					45491				TEMPERATURE INDICATOR INDICATES HIGH.						1	G	7	1 	3U				H2SW    					 
1999031900501	19990319	00501	SW  	1999	3	19	HEEA060847       	1	19990223	G	2841	206075189001	INDICATOR       			BELL  	206   	206B3       	1181506	SW  										FUEL QUANTITY	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	39122					3312				FUEL QUANTITY INDICATOR HAS EXCESSIVE FRICTION ERROR.						1	G	7	1 	3U				H2SW    					 
1999031900502	19990319	00502	SW  	1999	3	19	HEEA060848       	1	19990223	G	2841	206075189101	INDICATOR       			BELL  	206   	206B3       	1181506	SW  										FUEL QUANTITY	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	104PH					3622				FUEL QUANTITY INDICATOR'S NEEDLE STICKS LOW AND HIGH ENDS OF SCALE INACCURATE.						1	G	7	1 	3U				H2SW    					 
1999031900503	19990319	00503	SW  	1999	3	19	HEEA060849       	1	19990223	G	2430	206075447007	REGULATOR       			BELL  	206   	206L1       	1182107	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50034					45169				VOLTAGE FLUCTUATES.						1	G	7	1 	3U				H2SW    					 
1999031900504	19990319	00504	SW  	1999	3	19	HEEA060850       	1	19990223	G	2430	206075447007	REGULATOR       			BELL  	206   	206L3       	1182108	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A					51611				GENERATOR WILL NOT COME ON LINE.						1	G	7	1 	3U				H2SW    					 
1999031900505	19990319	00505	SW  	1999	3	19	HEEA060851       	1	19990223	G	2430	206075447007	REGULATOR       			BELL  	206   	206L3       	1182108	SW  										DC SYSTEM	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A					51611				VOLTAGE REGULATOR'S ADJUSTING SCREW WILL NOT ADJUST, SPINS FREELY.						1	G	7	1 	3U				H2SW    					 
1999031900506	19990319	00506	SW  	1999	3	19	HEEA060852       	1	19990223	G	2430	206075447007	REGULATOR       			BELL  	206   	206L3       	1182108	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	205FC					51130				VOLTAGE REGULATOR WILL NOT COME ON-LINE.						1	G	7	1 	3U				H2SW    					 
1999031900507	19990319	00507	SW  	1999	3	19	HEEA060853       	1	19990223	G	2430	206075447007	REGULATOR       			BELL  	206   	206L3       	1182108	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21497					51518				GENERATOR WILL NOT COME ON LINE.						1	G	7	1 	3U				H2SW    					 
1999031900508	19990319	00508	SW  	1999	3	19	HEEA060854       	1	19990223	G	2430	206075447007	REGULATOR       			BELL  	206   	206L1       	1182107	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3905B					45598				VOLTAGE REGULATOR CAUSES STARTER/GENERATOR TO LOCK-UP IN START MODE.						1	G	7	1 	3U				H2SW    					 
1999031900509	19990319	00509	SW  	1999	3	19	HEEA060855       	1	19990223	G	2430	206075447007	REGULATOR       			BELL  	206   	206L1       	1182107	SW  										DC SYSTEM	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5014Y					45219				LOAD METER FUEL PRESSURE FLUCTUATION.						1	G	7	1 	3U				H2SW    					 
1999031900510	19990319	00510		1999	3	19	HEEA060856       	4	19990223	G	3421	206075607103	GYRO            			BELL  	206   	206L3       	1182108	SW  										ATTITUDE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6603X					51412				ATTITUDE GYRO WILL NOT CAGE WHEN UNIT RUNNING.						1	G	7	1 	3U				H2SW    					 
1999031900511	19990319	00511	SW  	1999	3	19	HEEA060857       	1	19990223	G	7931	206075677103	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										ENGINE OIL	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1073W	924  				45386				OIL TEMPERATURE INDICATOR FLUCTUATES.						1	G	7	1 	3U				H2SW    					 
1999031900512	19990319	00512	SW  	1999	3	19	HEEA060858       	1	19990223	G	7931	206075678103	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	10814					45415				TEMPERATURE INDICATOR STICKS AT 90 AND INDICATES LOW.						1	G	7	1 	3U				H2SW    					 
1999031900513	19990319	00513	SW  	1999	3	19	HEEA060859       	1	19990223	G	6320	206075678107	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TRANSMISSION OIL	LEAKS           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3116L					51529				INDICATOR LEAKS AT CASE.						1	G	7	1 	3U				H2SW    					 
1999031900514	19990319	00514	SW  	1999	3	19	HEEA060860       	1	19990223	G	6320	206075678107	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TRANSMISSION OIL	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8593X					51509				PRESSURE READS HIGH, MARKINGS FADED.						1	G	7	1 	3U				H2SW    					 
1999031900515	19990319	00515	SW  	1999	3	19	HEEA060861       	1	19990223	G	6320	206075678107	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TRANSMISSION OIL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5012V					45200				NO TEMPERATURE INDICATION.						1	G	7	1 	3U				H2SW    					 
1999031900516	19990319	00516	SW  	1999	3	19	HEEA060862       	1	19990223	G	7722	206075680105	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2245Y					45751				TOT INDICATOR READS 10 DEGREES HIGH.						1	G	7	1 	3U				H2SW    					 
1999031900517	19990319	00517	SW  	1999	3	19	HEEA060863       	1	19990223	G	7722	206075680105	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2764F					45279				TOT INDICATOR'S NEEDLE STICKS UP AND DOWN SCALE.						1	G	7	1 	3U				H2SW    					 
1999031900518	19990319	00518	SW  	1999	3	19	HEEA060864       	1	19990223	G	7722	206075680105	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406EH					45183				TOT INDICATOR FLUCTUATES AND STICKS ON START-UP.						1	G	7	1 	3U				H2SW    					 
1999031900519	19990319	00519	SW  	1999	3	19	HEEA060865       	1	19990223	G	7714	206075681101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2124Z					45646				DUAL TACHOMETER'S INDICATOR  NEEDLE STICKS.						1	G	7	1 	3U				H2SW    					 
1999031900520	19990319	00520	SW  	1999	3	19	HEEA060866       	1	19990223	G	6240	206075681105	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										DUAL TACHOMETER	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				ROTOR AND TURBINE NEEDLES OSCILLATE ON DUAL TACHOMETER.						1	G	7	1 	3U				H2SW    					 
1999031900521	19990319	00521	SW  	1999	3	19	HEEA060867       	1	19990223	G	6240	206075681105	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										DUAL TACHOMETER	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	42EA					51542				TURBINE INDICATOR STICKS, ROTOR WILL NOT INDICATE.						1	G	7	1 	3U				H2SW    					 
1999031900522	19990319	00522	SW  	1999	3	19	HEEA060868       	1	19990223	G	6240	206075681109	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										DUAL TACHOMETER	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31801					51074				ROTOR AND TURBINE NEEDLES REMAIN SPLIT ABOUT 2 PERCENT ON DUAL TACHOMETER.						1	G	7	1 	3U				H2SW    					 
1999031900523	19990319	00523		1999	3	19	HEEA060869       	4	19990223	G	3421	214175241101	GYROSCOPE       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M					28102				GYROSCOPE WILL NOT ERECT.						2	G	7	2 	4U				H10SW   					 
1999031900524	19990319	00524	SW  	1999	3	19	HEEA060870       	1	19990223	G	6240	206075681117	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										DUAL TACHOMETER	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	32041					51539				ALL NEEDLES ON DUAL TACHOMETER MALFUNCTIONED.						1	G	7	1 	3U				H2SW    					 
1999031900525	19990319	00525	SW  	1999	3	19	HEEA060871       	1	19990223	G	6240	206075681117	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										DUAL TACHOMETER	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	27766					45312				DUAL TACHOMETER INDICATORS HAVE 3 PERCENT SPLIT.						1	G	7	1 	3U				H2SW    					 
1999031900526	19990319	00526	SW  	1999	3	19	HEEA060872       	1	19990223	G	6240	206075681117	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										DUAL TACHOMETER	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A					51611				BOTH NEEDLES STUCK ON DUAL TACHOMETER.						1	G	7	1 	3U				H2SW    					 
1999031900527	19990319	00527	SW  	1999	3	19	HEEA060873       	1	19990223	G	6240	206075681117	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										DUAL TACHOMETER	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108PH					51334				NEEDLE STICKS THROUGHOUT SCALE ON DUAL TACHOMETER.						1	G	7	1 	3U				H2SW    					 
1999031900528	19990319	00528	SW  	1999	3	19	HEEA060874       	1	19990223	G	3110	206075681117	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										DUAL TACHOMETER	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8593X					51509				INDICATOR NEEDLES ERRATIC AND STICK ON DUAL TACHOMETER.						1	G	7	1 	3U				H2SW    					 
1999031900529	19990319	00529	SW  	1999	3	19	HEEA060875       	1	19990223	G	6240	206075681117	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										DUAL TACHOMETER	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1078D					45397				BOTH TURBINE AND ROTOR NEEDLES WILL NOT FUNCTION ON DUAL TACHOMETER.						1	G	7	1 	3U				H2SW    					 
1999031900530	19990319	00530	SW  	1999	3	19	HEEA060876       	1	19990223	G	7714	206075682001	INDICATOR       			BELL  	206   	206B3       	1181506	SW  										COCKPIT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2285B					3642				INDICATOR INTERMITTENT AND STICKS ON GAS PROD GAUGE.						1	G	7	1 	3U				H2SW    					 
1999031900531	19990319	00531	SW  	1999	3	19	HEEA060877       	1	19990223	G	7714	206075682001	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50034					45169				WILL NOT ENGAGE UNTIL 15 PERCENT - 20 PERCENT ON GAS PROD GAUGE.						1	G	7	1 	3U				H2SW    					 
1999031900532	19990319	00532	SW  	1999	3	19	HEEA060878       	1	19990223	G	7714	206075682107	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										GAS PRODUCER	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										NEEDLE STICKING ON START-UP ON GAS PROD GAUGE.						1	G	7	1 	3U				H2SW    					 
1999031900533	19990319	00533	SW  	1999	3	19	HEEA060879       	1	19990223	G	7712	206075739103	TORQUEMETER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	32041					51539				NEEDLE STICKING ON TORQUEMETER.						1	G	7	1 	3U				H2SW    					 
1999031900534	19990319	00534	SW  	1999	3	19	HEEA060880       	1	19990223	G	7712	206075739103	TORQUEMETER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4180F					51469				INDICATOR FLUCTUATING, NEEDLE STICKS ON TORQUEMETER.						1	G	7	1 	3U				H2SW    					 
1999031900535	19990319	00535	SW  	1999	3	19	HEEA060881       	1	19990223	G	7712	206075739103	TORQUEMETER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6603X					51412				TORQUEMETER HAS FLUCTUATION OF NEEDLE WITHOUT TORQUE.						1	G	7	1 	3U				H2SW    					 
1999031900536	19990319	00536	SW  	1999	3	19	HEEA060882       	1	19990223	G	7712	206075739103	TORQUEMETER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8592X					51508				TORQUE OSCILLATION NEEDLE STICKS ON TORQUEMETER.						1	G	7	1 	3U				H2SW    					 
1999031900537	19990319	00537	SW  	1999	3	19	HEEA060883       	1	19990223	G	7712	206075739103	TORQUEMETER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108PH					51334				TORQUEMETER FLUCTUATES AND NEEDLE STICKS AT 50 PERCENT.						1	G	7	1 	3U				H2SW    					 
1999031900538	19990319	00538	SW  	1999	3	19	HEEA060884       	1	19990223	G	7712	206075739103	TORQUEMETER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3107N					51512				TORQUEMETER HAS EXCESSIVE FLUCTUATION IN CRUISE FLIGHT.  NEEDLE STICKS.						1	G	7	1 	3U				H2SW    					 
1999031900539	19990319	00539	SW  	1999	3	19	HEEA060885       	1	19990223	G	7712	206075739103	TORQUEMETER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251V					51404				TORQUE INDICATOR FLUCTUATES AND STICKS.						1	G	7	1 	3U				H2SW    					 
1999031900540	19990319	00540	SW  	1999	3	19	HEEA060886       	1	19990223	G	7712	206075739103	TORQUEMETER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				NEEDLE STICKING AND BOUNCING ON TORQUEMETER.						1	G	7	1 	3U				H2SW    					 
1999031900541	19990319	00541	SW  	1999	3	19	HEEA060887       	1	19990223	G	2913	206076030101	PUMP            			BELL  	206   	206L1       	1182107	SW  										HYDRAULIC SYS	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5744Y					45465				SPLINES WORN ON PUMP.						1	G	7	1 	3U				H2SW    					 
1999031900542	19990319	00542	SW  	1999	3	19	HEEA060888       	1	19990223	G	2913	206076030101	PUMP            			BELL  	206   	206L1       	1182107	SW  										HYDRAULIC SYS	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5745S					45491				PUMP LEAKING FROM SHAFT.						1	G	7	1 	3U				H2SW    					 
1999031900543	19990319	00543	SW  	1999	3	19	HEEA060889       	1	19990223	G	2913	206076030101	PUMP            			BELL  	206   	206L3       	1182108	SW  										HYDRAULIC SYS	NOISY           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31801					51074				PUMP HAS LOUD HOWLING NOISE.						1	G	7	1 	3U				H2SW    					 
1999031900544	19990319	00544	SW  	1999	3	19	HEEA060890       	1	19990223	G	6730	206076062003	CYLINDER        			BELL  	206   	206L3       	1182108	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	6610Y	20077				51419				CYLINDER LEAKING.						1	G	7	1 	3U				H2SW    					 
1999031900545	19990319	00545	SW  	1999	3	19	HEEA060891       	1	19990223	G	6730	206076062003	CYLINDER        			BELL  	206   	206L1       	1182107	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	5017G	20095				45228				CYLINDER LEAKING.						1	G	7	1 	3U				H2SW    					 
1999031900546	19990319	00546	SW  	1999	3	19	HEEA060892       	1	19990223	G	6730	206076062003	CYLINDER        			BELL  	206   	206L3       	1182108	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3207Q	6766 				51540				ACTUATOR VALVE BOOT TORN (LEAKING).						1	G	7	1 	3U				H2SW    					 
1999031900547	19990319	00547	SW  	1999	3	19	HEEA060893       	1	19990223	G	6730	206076062003	CYLINDER        			BELL  	206   	206L3       	1182108	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	6610Y	13214				51419				CYLINDER LEAKING.						1	G	7	1 	3U				H2SW    					 
1999031900548	19990319	00548	SW  	1999	3	19	HEEA060894       	1	19990223	G	7722	206375007101	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31077					51520				NEEDLE STICKS AT ZERO ON TOT INDICATOR.						1	G	7	1 	3U				H2SW    					 
1999031900549	19990319	00549	SW  	1999	3	19	HEEA060895       	1	19990223	G	7722	206375007101	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3116P					51530				TOT INDICATOR READS HIGH BETWEEN 600 AND 800 AFTER WARM-UP.						1	G	7	1 	3U				H2SW    					 
1999031900550	19990319	00550	SW  	1999	3	19	HEEA060896       	1	19990223	G	7722	206375007101	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	MISMARKED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8587X					51464				TOT INDICATOR HAS WRONG MARKINGS, NEEDLE RACHETS INCREASING AND DECREASING.						1	G	7	1 	3U				H2SW    					 
1999031900551	19990319	00551	SW  	1999	3	19	HEEA060897       	1	19990223	G	2435	23032048	STARTER         			BELL  	206   	206B3       	1181506	SW  										START/GENERATOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22743	3471 				3624				STARTER/GENERATOR ARCHING AND MAKING NOISE.						1	G	7	1 	3U				H2SW    					 
1999031900552	19990319	00552	SW  	1999	3	19	HEEA060898       	1	19990223	G	2435	23081018	STARTER         			BELL  	206   	206L3       	1182108	SW  										START/GENERATOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A	12851				51611				STARATER/GENERATOR DROPS OFF-LINE WHEN RPM IS LOWER.						1	G	7	1 	3U				H2SW    					 
1999031900553	19990319	00553	SW  	1999	3	19	HEEA060899       	1	19990223	G	2435	23032048	STARTER         			BELL  	206   	206L3       	1182108	SW  										START/GENERATOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										STARTER/GENERATOR HAS PITTED END BELL.						1	G	7	1 	3U				H2SW    					 
1999031900554	19990319	00554	SW  	1999	3	19	HEEA060900       	1	19990223	G	2435	23032048	STARTER         			BELL  	206   	206B3       	1181506	SW  										START/GENERATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3181J	12506				3771				STARTER WILL NOT TURN OVER.						1	G	7	1 	3U				H2SW    					 
1999031900555	19990319	00555	SW  	1999	3	19	HEEA060901       	1	19990223	G	2435	23032048	STARTER         			BELL  	206   	206B3       	1181506	SW  										START/GENERATOR	NOISY           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2753F	5400 				2729				GRINDING NOISE AND THROWING SPARKS.						1	G	7	1 	3U				H2SW    					 
1999031900556	19990319	00556	SW  	1999	3	19	HEEA060902       	1	19990223	G	2435	23032048	STARTER         			BELL  	206   	206B3       	1181506	SW  										START/GENERATOR	FAULTY          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2268V	2405 				3605				STARTER/GENERATOR UNABLE TO ATTAIN 15 PERCENT N1 FOR START.						1	G	7	1 	3U				H2SW    					 
1999031900557	19990319	00557	SW  	1999	3	19	HEEA060903       	1	19990223	G	2435	23032048	STARTER         			BELL  	206   	206B3       	1181506	SW  										START/GENERATOR	ARCED           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22743	3471 				3624				STARTER/GENERATOR ARCHING AND MAKING NOISE.						1	G	7	1 	3U				H2SW    					 
1999031900558	19990319	00558		1999	3	19	HEEA060904       	4	19990223	G	3421	2360041902	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										COCKPIT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6603X					51412				ATTITUDE INDICATOR'S PRE-LOAD NUTS LOOSE.  HARD TO BALANCE.						1	G	7	1 	3U				H2SW    					 
1999031900559	19990319	00559	SW  	1999	3	19	HEEA060905       	1	19990223	G	7603	2543392	THROTTLE SHAFT  			BELL  	206   	206B3       	1181506	SW  										POWER LEVER	MISMANUFACTURED 	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										THROTTLE SHAFT LEVERS WILL NOT INSTALL FAR ENOUGH ONTO THROTTLE SHAFTS TO FACILITATE INSTALLATION OF RETAINING RING.						1	G	7	1 	3U				H2SW    					 
1999031900560	19990319	00560		1999	3	19	HEEA060906       	4	19990223	G	3422	2891ESR	GYRO            			BELL  	206   	206L1       	1182107	SW  										COCKPIT DG	PRECESSING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5742N					45477				DIRECTIONAL GYRO PRECESSES IN-FLIGHT.						1	G	7	1 	3U				H2SW    					 
1999031900561	19990319	00561	SW  	1999	3	19	HEEA060907       	1	19990223	G	7722	35712519129	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	513EH					45421				RISE IN TOT INDICATION WHEN VHF MIC.  KEYED-LIGHT PIN BROKEN.						1	G	7	1 	3U				H2SW    					 
1999031900562	19990319	00562		1999	3	19	HEEA060908       	4	19990223	G	3416	5035P2P42	ALTIMETER       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	513EH					45421				ALTIMETER HAS EXCESSIVE CASE LEAKAGE.						1	G	7	1 	3U				H2SW    					 
1999031900563	19990319	00563		1999	3	19	HEEA060909       	4	19990223	G	3422	5050017904	GYRO            			BELL  	206   	206B3       	1181506	SW  										COCKPIT	PRECESSING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2272V					3621				DIRECTIONAL GYRO PRECESSES 30 DEGREES IN 5-10 MINUTES.						1	G	7	1 	3U				H2SW    					 
1999031900564	19990319	00564		1999	3	19	HEEA060910       	4	19990223	G	3422	5208100001	GYRO            			BELL  	206   	206L1       	1182107	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2761X					45283				GYRO WILL NOT SPIN UP, NO OUTPUT.						1	G	7	1 	3U				H2SW    					 
1999031900565	19990319	00565		1999	3	19	HEEA060911       	4	19990223	G	3425	5222638006	INDICATOR       			BEECH 	200   	200BEECH    	1152920	CE  										HSI	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	30PH					BB635				INSTRUMENT STICKS.						1	L	7	2 	4T				A24CE   					 
1999031900566	19990319	00566		1999	3	19	HEEA060912       	4	19990223	G	3414		ALTIMETER       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	16938					45157				ALTIMETER HAS EXCESSIVE CASE LEAKAGE AND NEEDLE IS STUCK.						1	G	7	1 	3U				H2SW    					 
1999031900567	19990319	00567		1999	3	19	HEEA060913       	4	19990223	G	3414		ALTIMETER       			BELL  	206   	206L3       	1182108	SW  										COCKPIT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	8591X					51495				ALTIMETER HAS EXCESSIVE CASE LEAKAGE.  LOSES 200 FEET PER MINUTE.						1	G	7	1 	3U				H2SW    					 
1999031900568	19990319	00568		1999	3	19	HEEA060914       	4	19990223	G	2312	6222078001	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	WEAK            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	515KA					51048				VHF251 HAS WEAK TRANSMIT/RECEIVE SIGNAL.						1	G	7	1 	3U				H2SW    					 
1999031900569	19990319	00569	SW  	1999	3	19	HEEA060915       	1	19990223	G	3110	7502869	LIGHT           			BELL  	206   	206B3       	1181506	SW  										INSTRUMENT PANEL	SHORTED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2270G					3610				ENGINE OUT SEGMENT CAUSES CAUTION LIGHT CIRCUIT BREAKER TO TRIP.  SEVERAL BULBS OUT.						1	G	7	1 	3U				H2SW    					 
1999031900570	19990319	00570	SW  	1999	3	19	HEEA060916       	1	19990223	G	7921	8543909	OIL COOLER      			BELL  	206   	206L3       	1182108	SW  										ENGINE OIL	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31077					51520				HIGH OIL TEMPERATURE INDICATION AND CORROSION FOUND ON OIL COOLER.						1	G	7	1 	3U				H2SW    					 
1999031900571	19990319	00571	SW  	1999	3	19	HEEA060917       	1	19990223	G	7921	8543909	OIL COOLER      			BELL  	206   	206L1       	1182107	SW  										ENGINE OIL	CLOGGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50182					45242				CORE CLOGGED, HIGH OIL TEMPERATURE INDICATION ON OIL COOLER.						1	G	7	1 	3U				H2SW    					 
1999031900572	19990319	00572	SW  	1999	3	19	HEEA060918       	1	19990223	G	7921	8543909	OIL COOLER      			BELL  	206   	206L4       	1182110	SW  										ENGINE OIL	CLOGGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7077B					52037				OIL COOLER HAS HIGH OIL TEMPERATURE AND CORE IS CLOGGED.						1	G	7	1 	3U			NC	H2SW    					 
1999031900573	19990319	00573	SW  	1999	3	19	HEEA060919       	1	19990223	G	7714	8DJ81WBS4	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										GAS PRODUCER	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2124Z					45646				GAS PROD INDICATION SLOW TO REACT.						1	G	7	1 	3U				H2SW    					 
1999031900574	19990319	00574		1999	3	19	HEEA060920       	4	19990223	G	3416	8503S20LW5V	ALTIMETER       			BELL  	206   	206L3       	1182108	SW  										COCKPIT	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				ALTIMETER HAS NEEDLE SPLIT 4-5 DEGREES.						1	G	7	1 	3U				H2SW    					 
1999031900575	19990319	00575	SW  	1999	3	19	HEEA060921       	1	19990223	G	2436	15891F	REGULATOR       			BELL  	206   	206B3       	1181506	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2272J					3620				VOLTAGE WENT PAST 30 PLUS VOLTS - WILL NOT ADJUST.						1	G	7	1 	3U				H2SW    					 
1999031900576	19990319	00576		1999	3	19	HEEA060922       	4	19990223	G	3416	A30	ENCODER         			BELL  	206   	206L3       	1182108	SW  										ALTIMETER	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8592X					51508				ENCODER READS 500 HIGH.						1	G	7	1 	3U				H2SW    					 
1999031900577	19990319	00577		1999	3	19	HEEA060923       	4	19990223	G	3416	A30	ENCODER         			BELL  	206   	206B3       	1181506	SW  										ALTIMETER	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3181J					3771				TRANSPONDER MODE C INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999031900578	19990319	00578	SW  	1999	3	19	HEEA060924       	1	19990223	G	2450	A1077	RELAY           			BELL  	206   	206L1       	1182107	SW  										DC SYSTEM	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3905B					45598				RELAY HAS BROKEN SCREW, MISSING ROD.						1	G	7	1 	3U				H2SW    					 
1999031900579	19990319	00579	SW  	1999	3	19	HEEA060925       	1	19990223	G	3340	A490A	POWER SUPPLY    			BELL  	206   	206L1       	1182107	SW  										STROBE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5005B					45175				POWER SUPPLY HAS LOOSE PIECES INSIDE,  INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999031900580	19990319	00580	SW  	1999	3	19	HEEA060926       	1	19990223	G	3340	A490A	POWER SUPPLY    			BELL  	206   	206L3       	1182108	SW  										STROBE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A					51611				POWER SUPPLY IS INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999031900581	19990319	00581	SW  	1999	3	19	HEEA060927       	1	19990223	G	3340	A490ATSDF1428	POWER SUPPLY    			BELL  	206   	206L1       	1182107	SW  										STROBE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2770Y					45291				POWER SUPPLY HAS NO POWER OUT.						1	G	7	1 	3U				H2SW    					 
1999031900582	19990319	00582	SW  	1999	3	19	HEEA060928       	1	19990223	G	3340	A490A	POWER SUPPLY    			BELL  	206   	206L3       	1182108	SW  										STROBE	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41128					51134				FLASH SEQUENCE IS NOT NORMAL ON POWER SUPPLY.						1	G	7	1 	3U				H2SW    					 
1999031900583	19990319	00583	SW  	1999	3	19	HEEA060929       	1	19990223	G	3340	A490A	POWER SUPPLY    			BELL  	206   	206L3       	1182108	SW  										STROBE	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41128					51134				FLASH SEQUENCE ON POWER SUPPLY IS NOT NORMAL.						1	G	7	1 	3U				H2SW    					 
1999031900584	19990319	00584	SW  	1999	3	19	HEEA060930       	1	19990223	G	3340	A490ATSDF1428	POWER SUPPLY    			BELL  	206   	206L1       	1182107	SW  										STROBE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5007Y					45192				POWER SUPPLY HAS NO POWER OUT AND TRIPS CIRCUIT BREAKER.						1	G	7	1 	3U				H2SW    					 
1999031900585	19990319	00585	SW  	1999	3	19	HEEA060931       	1	19990223	G	3340	A490ATSDF1428	POWER SUPPLY    			BELL  	206   	206L3       	1182108	SW  										STROBE	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				POWER SUPPLY DOES NOT FLASH AT CORRECT RATE.						1	G	7	1 	3U				H2SW    					 
1999031900586	19990319	00586	SW  	1999	3	19	HEEA060932       	1	19990223	G	3340	A490A	POWER SUPPLY    			BELL  	206   	206L1       	1182107	SW  										STROBE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	16938					45157				POWER SUPPLY HAS NO POWER OUT.						1	G	7	1 	3U				H2SW    					 
1999031900587	19990319	00587	SW  	1999	3	19	HEEA060933       	1	19990223	G	3340	A490A	POWER SUPPLY    			BELL  	206   	206B3       	1181506	SW  										STROBE	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2270G					3610				POWER SUPPLY WILL NOT POWER LIGHT AT END OF TRAIL.						1	G	7	1 	3U				H2SW    					 
1999031900588	19990319	00588	SW  	1999	3	19	HEEA060934       	1	19990223	G	3340	A490ATSDF1428	POWER SUPPLY    			BELL  	206   	206L1       	1182107	SW  										STROBE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1076Y					45380				POWER SUPPLY HAS NO POWER OUT, DOES NOT WORK.						1	G	7	1 	3U				H2SW    					 
1999031900589	19990319	00589	SW  	1999	3	19	HEEA060935       	1	19990223	G	3340	A490A	POWER SUPPLY    			BELL  	206   	206L1       	1182107	SW  										STROBE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	10761					45381				POWER SUPPLY HAS NO POWER OUT.						1	G	7	1 	3U				H2SW    					 
1999031900590	19990319	00590	SW  	1999	3	19	HEEA060936       	1	19990223	G	2844	BSE20630G	TRANSDUCER      			BELL  	206   	206L3       	1182108	SW  										FUEL PRESSURE	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8593X					51509				TRANSDUCER TRANSMITS LOW, OUT OF TOLERANCE.						1	G	7	1 	3U				H2SW    					 
1999031900591	19990319	00591	SW  	1999	3	19	HEEA060937       	1	19990223	G	2844	BSE20630G	TRANSDUCER      			BELL  	206   	206L1       	1182107	SW  										FUEL PRESSURE	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3905B					45598				TRANSDUCER HIGH OUT OF TOLERANCE.						1	G	7	1 	3U				H2SW    					 
1999031900592	19990319	00592		1999	3	19	HEEA060938       	4	19990223	G	3416	D120P2T	ENCODER         			BELL  	206   	206L3       	1182108	SW  										ALTIMETER	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A					51611				BENT PIN ON CONNECTOR, ENCODER DOES NOT FUNCTION CORRECTLY.						1	G	7	1 	3U				H2SW    					 
1999031900593	19990319	00593		1999	3	19	HEEA060939       	4	19990223	G	3416	D120P2T	ENCODER         			BELL  	206   	206B3       	1181506	SW  										ALTITUDE	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2270G					3610				ALTITUDE REPORTING OFF 600 FEET.  TIME SINCE REPAIR 243:45 HOURS.						1	G	7	1 	3U				H2SW    					 
1999031900594	19990319	00594	SW  	1999	3	19	HEEA060940       	1	19990223	G	3212	D24976117	FLOAT           			BELL  	206   	206L1       	1182107	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	11027	600  				45411				FORWARD RELIEF VALVE LEAKING ON FLOAT BAG.						1	G	7	1 	3U				H2SW    					 
1999031900595	19990319	00595	SW  	1999	3	19	HEEA060941       	1	19990223	G	3212	D24972113	FLOAT           			BELL  	206   	206L1       	1182107	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03										FLOAT ASSEMBLY LEAKING AT BOTTOM VALVE.  AFTER PERFORMING ACTUAL INFLATION TEST, IT WAS NOTICED THAT THE FORWARD FLOAT H	AD LOST PRESSURE.					1	G	7	1 	3U				H2SW    					 
1999031900596	19990319	00596		1999	3	19	HEEA060942       	4	19990223	G	2562	DK100	PINGER          			BELL  	206   	206L3       	1182108	SW  										LOCATOR BEACON	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4282Z					51499				BEACON FAILED BATTERY TESTING DUE TO LOW VOLTAGE.						1	G	7	1 	3U				H2SW    					 
1999031900597	19990319	00597		1999	3	19	HEEA060943       	4	19990223	G	2562	ELT910	BATTERY         			BELL  	206   	206L3       	1182108	SW  										ELT	DISCHARGED      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	979BH					51403				ELT BATTERY WEAK.						1	G	7	1 	3U				H2SW    					 
1999031900598	19990319	00598		1999	3	19	HEEA060944       	4	19990223	G	2562	ELT910	TRANSMITTER     			BELL  	206   	206L3       	1182108	SW  										ELT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	206LS					51070				ELT ACTIVATED FOR UNKNOWN AMOUNT OF TIME. S						1	G	7	1 	3U				H2SW    					 
1999031900599	19990319	00599		1999	3	19	HEEA060945       	4	19990224	G	2562	ELT910	TRANSMITTER     			BELL  	206   	206L3       	1182108	SW  										ELT	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8589X					51487				CORROSION ON ONE PIN OF REMOTE INDICATOR PLUG IN ELT SIDE.  RECURRENT FALSE ACTUATION LIGHTS ON THE REMOTE INDICATOR.						1	G	7	1 	3U				H2SW    					 
1999031900600	19990319	00600		1999	3	19	HEEA060946       	4	19990224	G	2562	ELT910	TRANSMITTER     			BELL  	206   	206L1       	1182107	SW  										ELT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50046					45173				ELT SELF-ACTIVATES INTERMITTENTLY.						1	G	7	1 	3U				H2SW    					 
1999031900601	19990319	00601		1999	3	19	HEEA060947       	4	19990224	G	2562	ELT910	TRANSMITTER     			BELL  	206   	206L3       	1182108	SW  										ELT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8588X					51486				ELT WILL NOT TURN OFF/RESET.						1	G	7	1 	3U				H2SW    					 
1999031900602	19990319	00602		1999	3	19	HEEA060948       	4	19990224	G	2562	ELT910	TRANSMITTER     			BELL  	206   	206L3       	1182108	SW  										ELT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										G-TEST FAILED IN ARM POSITION ON ELT.						1	G	7	1 	3U				H2SW    					 
1999031900603	19990319	00603		1999	3	19	HEEA060949       	4	19990224	G	2562	ELT910	TRANSMITTER     			BELL  	206   	206L3       	1182108	SW  										ELT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ELT UNIT STAYS ON ALL OF THE TIME.						1	G	7	1 	3U				H2SW    					 
1999031900604	19990319	00604		1999	3	19	HEEA060950       	4	19990224	G	2562	ELT910	TRANSMITTER     			BELL  	206   	206L3       	1182108	SW  										ELT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										SWITCH ON ELT NOT FUNCTIONING.						1	G	7	1 	3U				H2SW    					 
1999031900605	19990319	00605		1999	3	19	HEEA060951       	4	19990224	G	2562	ELT910	TRANSMITTER     			BELL  	206   	206L3       	1182108	SW  										ELT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8593X					51509				ELT SELF-ACTIVATES SPORATICALLY.						1	G	7	1 	3U				H2SW    					 
1999031900606	19990319	00606		1999	3	19	HEEA060952       	4	19990224	G	2562	ELT910	TRANSMITTER     			BELL  	206   	206L3       	1182108	SW  										ELT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251X					51552				COMES ON AND OFF IN-FLIGHT.						1	G	7	1 	3U				H2SW    					 
1999031900607	19990319	00607		1999	3	19	HEEA060953       	4	19990224	G	2562	ELT910	TRANSMITTER     			BELL  	206   	206L1       	1182107	SW  										ELT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50046					45173				FAILED G-FORCE TEST ON ELT 12 MONTH.						1	G	7	1 	3U				H2SW    					 
1999031900608	19990319	00608		1999	3	19	HEEA060954       	4	19990224	G	3421	RCA26BK12	GYRO            			BELL  	206   	206L1       	1182107	SW  										COCKPIT	PRECESSING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21240					45647				HORIZONTAL GYRO INDICATES DOWN TO THE LEFT AND PRECESSES.						1	G	7	1 	3U				H2SW    					 
1999031900609	19990319	00609	SW  	1999	3	19	HEEA060955       	1	19990224	G	2430	UC2814	DC CONVERTER    			BELL  	206   	206L3       	1182108	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108PH					51334				NO POWER OUT WHEN USING A/C GENERATOR.						1	G	7	1 	3U				H2SW    					 
1999031900610	19990319	00610	SW  	1999	3	19	HEEA060956       	1	19990224	G	6320	214040013115FM	GEARBOX         			BELL  	214   	214ST       	1182106	SW  										COMBINING	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T	6262 				28101				EXCESSIVE CORROSION AND WEAR BENEATH P/N 214-040-160-105 TRIPOD ENGINE MOUNT AND P/N 214-040-151-103 BIPOD ENGINE MOUNT 	(BEYOND ALLOWABLE LIMITS) CASE ASSY P/N 214-040-991-109, S/N A518, T.T. UNK T.S.O. 283:00 HOURS.					2	G	7	2 	4U				H10SW   					 
1999031900611	19990319	00611	SW  	1999	3	19	HEEA060958       	1	19990226	G	6710	214001970111	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										MAIN ROTOR	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	59806					28140				ACTUATOR ASSEMBLY WILL NOT MONITOR TEST AND 5-MINUTES AFTER ENGAGING - KICKS OFF.						2	G	7	2 	4U				H10SW   					 
1999031900612	19990319	00612	SW  	1999	3	19	HEEA060959       	1	19990301	G	5302	407030801101	SKIN            			BELL  	407   	407         		SW  										TAILBOOM	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH	1342 				53207				CRACKED ON LEFT SIDE FORWARD OF HORIZONTAL STABILIZER.						1	G	7	1 	3U			O	H2SW    					 
1999031900613	19990319	00613	SW  	1999	3	19	HEEA060962       	1	19990304	G	6320	407040006107	TRANSMISSION    			BELL  	407   	407         		SW  										MAIN ROTOR	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM	72   				53060				TRANSMISSION ASSEMBLY MAKING METAL.						1	G	7	1 	3U			O	H2SW    					 
1999031900614	19990319	00614	SW  	1999	3	19	HEEA060963       	1	19990305	G	6210	407015001117	BLADE           			BELL  	407   	407         		SW  										MAIN ROTOR	DEBONDED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724PH	9    				53327				MAIN ROTOR TRIM TAB IS DEBONDED ALONG THE TOP INBOARD EDGE.						1	G	7	1 	3U			O	H2SW    					 
1999031900615	19990319	00615	SW  	1999	3	19	HEEA060966       	1	19990305	G	2840	222366621103	FUEL FILTER     			BELL  	407   	407         		SW  										FUEL SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH	746  				53199				BLEED/BYPASS BUTTON STUCK ON FUEL FILTER.						1	G	7	1 	3U			O	H2SW    					 
1999031900616	19990319	00616	SW  	1999	3	19	HEEA060967       	1	19990305	G	6520	406040400115	GEARBOX         			BELL  	407   	407         		SW  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH	1222 				53209				CORRODED SPLINES WHERE TAIL ROTOR IS MOUNTED.						1	G	7	1 	3U			O	H2SW    					 
1999031900617	19990319	00617	SW  	1999	3	19	HEEA060969       	1	19990305	G	6420	406312100101	BEARING         		407012101105	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416	1012 			53025	53070				TAIL ROTOR HUB AND BLADE HAVE WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999031900618	19990319	00618	SW  	1999	3	19	HEEA060970       	1	19990305	G	6420	406312100101	BEARING         		407012101105	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH	1222 			53209	53209				TAIL ROTOR HUB AND BLADE HAVE WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999031900619	19990319	00619	SW  	1999	3	19	HEEA060971       	1	19990305	G	6420	406312100101	BEARING         		407012101105	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM	969  			53069	53060				TAIL ROTOR BLADE AND HUB HAVE WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999031900620	19990319	00620	EU  	1999	3	19	HEEA060972       	1	19990303	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4034Q					2918				ROD, PITCH CONTROL HAS PLAY IN BEARINGS.						1	G	7	1 	3U				H9EU    					 
1999031900621	19990319	00621	EU  	1999	3	19	HEEA060973       	1	19990303	G	6730	SC50811	SERVO           			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				RIGHT AND LEFT SERVO CONTROLS LEAKING HYDRAULIC FLUID.						1	G	7	1 	3U				H9EU    					 
1999031900622	19990319	00622	EU  	1999	3	19	HEEA060974       	1	19990303	G	6720	704A34240015	ACCUMULATOR     			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				ACCUMULATOR WILL NOT HOLD PRESSURE.						1	G	7	1 	3U				H9EU    					 
1999031900623	19990319	00623	EU  	1999	3	19	HEEA060975       	1	19990303	G	3310	704A46814049	LIGHT           			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				LIGHT GRADUATOR HAS RUBBER SEPARATED.						1	G	7	1 	3U				H9EU    					 
1999031900624	19990319	00624	EU  	1999	3	19	HEEA060976       	1	19990303	G	6220	ELT302301	FREQ ADAPTER    			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6100R					2862				FREQUENTY ADAPTER HAS RUBBER SEPARATED.  SERIAL NUMBERS REMOVED ARE 9401, 9421, AND 9395.						1	G	7	1 	3U				H9EU    					 
1999031900625	19990319	00625	EU  	1999	3	19	HEEA060977       	1	19990303	G	6710	SC5083	SERVO           			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350BZ	1891 				2653				SERVO LEAKING HYDRAULIC FLUID.						1	G	7	1 	3U				H9EU    					 
1999031900626	19990319	00626	EU  	1999	3	19	HEEA060978       	1	19990303	G	6321	350A32050002	BRAKE ASSY      			SNIAS 	350   	AS350B2     	8680813	EU  										ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4034Q					2918				BRAKE ASSEMBLY WORN BEYOND LIMITS.						1	G	7	1 	3U				H9EU    					 
1999031900627	19990319	00627	EU  	1999	3	19	HEEA060979       	1	19990303	G	3201	350A38104020	CROSSBEAM       			SNIAS 	350   	AS350B2     	8680813	EU  										MLG	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				CROSSBEAM OUT OF LIMITS.						1	G	7	1 	3U				H9EU    					 
1999031900628	19990319	00628	EU  	1999	3	19	HEEA060980       	1	19990303	G	6420	350A33200405	SPIDER          			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466	447  				3004				TAIL ROTOR HAS WORN BEARINGS.						1	G	7	1 	3U				H9EU    					 
1999031900629	19990319	00629	EU  	1999	3	19	HEEA060981       	1	19990303	G	6730	SC5084	SERVO           			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	40466	1983 				3004				SERVO LEAKING.						1	G	7	1 	3U				H9EU    					 
1999031900630	19990319	00630	EU  	1999	3	19	HEEA060982       	1	19990303	G	6321	350A32050002	BRAKE ASSY      			SNIAS 	350   	AS350B2     	8680813	EU  										ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6100R					2862				BRAKE ASSEMBLY HAS RUBBER SEPARATED.						1	G	7	1 	3U				H9EU    					 
1999031900631	19990319	00631	EU  	1999	3	19	HEEA060983       	1	19990303	G	6220	704A3363310951	STOP ASSY       			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z	1279 				2820				SPHERICAL STOP ASSEMBLY HAS RUBBER SEPARATION BEYOND LIMITS.						1	G	7	1 	3U				H9EU    					 
1999031900632	19990319	00632	EU  	1999	3	19	HEEA060984       	1	19990303	G	6220	ELT302301	FREQ ADAPTER    			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z					2820				RUBBER SEPARATED ON FREQUENCY ADAPTER.  SERIAL NUMBERS REMOVED ARE 11114, 11101, AND 11102.						1	G	7	1 	3U				H9EU    					 
1999031900633	19990319	00633	EU  	1999	3	19	HEEA060985       	1	19990303	G	6710	SC5083	SERVO           			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466	1983 				3004				SERVO LEAKING.						1	G	7	1 	3U				H9EU    					 
1999031900634	19990319	00634	EU  	1999	3	19	HEEA060986       	1	19990303	G	6210	355A11002011	BLADE           			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	ERODED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z	5987 				2820				MAIN ROTOR BLADE HAS FIBERGLASS ERODED AT CENTER JOINT, TRIM TABS CORRODED.						1	G	7	1 	3U				H9EU    					 
1999040200440	19990402	00440	SW  	1999	4	2	HEEA061137       	1	19990315	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH	746  				53199				UNIVERSAL HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999040200441	19990402	00441	SW  	1999	4	2	HEEA061138       	1	19990315	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM	2509 				53060				UNIVERSAL HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999040200442	19990402	00442	SW  	1999	4	2	HEEA061139       	1	19990315	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM	2494 				53060				UNIVERSAL HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999040200443	19990402	00443	SW  	1999	4	2	HEEA061140       	1	19990315	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH	1263 				53188				UNIVERSAL HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999040200444	19990402	00444	SW  	1999	4	2	HEEA061142       	1	19990315	G	6230	406010427109	GIMBAL RING     			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH	611  				53199				GIMBAL RING WEARING IN PIN AREA AND BUSHING.						1	G	7	1 	3U			O	H2SW    					 
1999040200445	19990402	00445	SW  	1999	4	2	HEEA061143       	1	19990315	G	2841	407375006101	INDICATOR       			BELL  	407   	407         		SW  										FUEL QUANTITY	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				FUEL QUANTITY INDICATION INTERMITTENTLY GOES TO FULL SCALE AND ALL SEGMENTS LIT.						1	G	7	1 	3U			O	H2SW    					 
1999040200446	19990402	00446	SW  	1999	4	2	HEEA061144       	1	19990315	G	2841	407375006101	INDICATOR       			BELL  	407   	407         		SW  										FUEL QUANTITY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				FUEL QUANTITY INDICATION GOES BLANK.						1	G	7	1 	3U			O	H2SW    					 
1999040200447	19990402	00447	SW  	1999	4	2	HEEA061145       	1	19990315	G	7931	407375004101	INDICATOR       			BELL  	407   	407         		SW  										ENGINE OIL PRESS	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				NO ENGINE OIL TEMPERATURE INDICATIONS.						1	G	7	1 	3U			O	H2SW    					 
1999040200448	19990402	00448	SW  	1999	4	2	HEEA061146       	1	19990315	G	7931	407375004101	INDICATOR       			BELL  	407   	407         		SW  										ENGINE OIL PRESS	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				NO ENGINE OIL TEMPERATURE INDICATIONS.						1	G	7	1 	3U			O	H2SW    					 
1999040200449	19990402	00449	SW  	1999	4	2	HEEA061149       	1	19990315	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				DISK COUPLING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999040200450	19990402	00450	SW  	1999	4	2	HEEA061150       	1	19990315	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				DISK COUPLING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999040200451	19990402	00451	SW  	1999	4	2	HEEA061151       	1	19990315	G	3212	206050247137	COVER ASSY      			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457PH					53147				FLOAT COVER ASSY TORN.						1	G	7	1 	3U			O	H2SW    					 
1999040200452	19990402	00452	SW  	1999	4	2	HEEA061152       	1	19990315	G	5302	407030801101	SKIN            			BELL  	407   	407         		SW  										TAIL BOOM	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH	1264 				53198				SKIN ON TAILBOOM CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999040200453	19990402	00453	SW  	1999	4	2	HEEA061153       	1	19990316	G	7910	206061505115	TANK            			BELL  	407   	407         		SW  										ENGINE OIL	CRACKED         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	437PH					53072				TANK ASSY CRACKED AROUND UPPER FITTING.						1	G	7	1 	3U			O	H2SW    					 
1999040200454	19990402	00454	SW  	1999	4	2	HEEA061154       	1	19990316	G	6320	406340100101	PUMP            			BELL  	407   	407         		SW  										TRANSMISSION OIL	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	427PH					53059				TRANSMISSION OIL PUMP LEAKING FROM SEAL DRAIN.						1	G	7	1 	3U			O	H2SW    					 
1999040200455	19990402	00455	SW  	1999	4	2	HEEA061155       	1	19990316	G	2912	206076035103	FILTER          			BELL  	407   	407         		SW  										HYDRAULIC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH					53207				BUTTON WILL NOT POP ON FILTER ASSEMBLY.						1	G	7	1 	3U			O	H2SW    					 
1999040200456	19990402	00456	SW  	1999	4	2	HEEA061156       	1	19990316	G	7714	407375201101	PICKUP          			BELL  	407   	407         		SW  										N1 INDICATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				N1 INDICATOR WENT TO ZERO.						1	G	7	1 	3U			O	H2SW    					 
1999040200457	19990402	00457		1999	4	2	HEEA061157       	4	19990316	G	3120	M803B205VBATT	CLOCK           			BELL  	407   	407         		SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				CLOCK/OAT/VOLTS SWITCH OVER BUTTON.						1	G	7	1 	3U			O	H2SW    					 
1999040200458	19990402	00458	SW  	1999	4	2	HEEA061158       	1	19990316	G	6320	214040806003	SWITCH          			BELL  	407   	407         		SW  										M/R GEARBOX	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH					53198				PRESSURE SWITCH INTERMITTENT AND INOPERATIVE.						1	G	7	1 	3U			O	H2SW    					 
1999040200459	19990402	00459	SW  	1999	4	2	HEEA061159       	1	19990316	G	6300	407010206103	BEARING         			BELL  	407   	407         		SW  										MAIN ROTOR DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				SPRING BEARINGS WORN IN MAIN ROTOR DRIVE.						1	G	7	1 	3U			O	H2SW    					 
1999040200460	19990402	00460	SW  	1999	4	2	HEEA061160       	1	19990316	G	6300	407010206103B	BEARINGS        			BELL  	407   	407         		SW  										MAIN ROTOR DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				WORN BEARINGS, DELAMINATION IN MAIN ROTOR DRIVE.						1	G	7	1 	3U			O	H2SW    					 
1999040200461	19990402	00461	SW  	1999	4	2	HEEA061161       	1	19990316	G	3212	407350301101	FLOAT           			BELL  	407   	407         		SW  										LT MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	404PH					53188				LEFT FLOAT BAG LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999040200462	19990402	00462	SW  	1999	4	2	HEEA061162       	1	19990316	G	6322	206061432121	HOUSING         			BELL  	407   	407         		SW  										BLOWER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				BLOWER HOUSING CRACKED AT UPPER OUTLET.						1	G	7	1 	3U			O	H2SW    					 
1999040200463	19990402	00463	SW  	1999	4	2	HEEA061163       	1	19990316	G	2810	P49389	VALVE           			BELL  	407   	407         		SW  										FUEL SYSTEM	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	447PH					53114				VALVE RELEASE FAILED PRESSURE TEST.						1	G	7	1 	3U			O	H2SW    					 
1999040200464	19990402	00464	SW  	1999	4	2	HEEA061164       	1	19990316	G	2432	28SP100	CELL            			BELL  	407   	407         		SW  										BATTERY	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH					53198				BURNT CELL IN BATTERY.						1	G	7	1 	3U			O	H2SW    					 
1999040200465	19990402	00465	SW  	1999	4	2	HEEA061165       	1	19990319	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH					53207				DISK COUPLING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999040200466	19990402	00466	SW  	1999	4	2	HEEA061166       	1	19990319	G	6310	406040500123	FREEWHEEL UNIT  			BELL  	407   	407         		SW  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	447PH	2160 				53114				FREEWHEEL UNIT LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999040200467	19990402	00467	SW  	1999	4	2	HEEA061167       	1	19990319	G	6320	407040006107	TRANSMISSION    			BELL  	407   	407         		SW  										MAIN ROTOR	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	2160 				53114				TRANSMISSION ASSY MAKING METAL.						1	G	7	1 	3U			O	H2SW    					 
1999040200468	19990402	00468	SW  	1999	4	2	HEEA061168       	1	19990319	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				DISK COUPLING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999040200469	19990402	00469	SW  	1999	4	2	HEEA061169       	1	19990319	G	6240	222375077119	TRANSMITTER     			BELL  	407   	407         		SW  										TORQUE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				DEGRADE LIGHT.  TRANSMITTER MALFUNCTIONED.						1	G	7	1 	3U			O	H2SW    					 
1999040200470	19990402	00470	EU  	1999	4	2	HEEA061171       	1	19990316	G	7712	305731365	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										ENGINE TORQUE	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				TORQUE INDICATOR HAS NEEDLE FLUCTUATION.						1	G	7	1 	3U				H9EU    					 
1999040200471	19990402	00471	EU  	1999	4	2	HEEA061173       	1	19990319	G	6520	350A33020005	GEARBOX         			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	LEAKS           	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	6097Z	2337 				2820				LEAK FROM INPUT AND MAYBE FROM OUTPUT IN TAIL ROTOR GEARBOX.						1	G	7	1 	3U				H9EU    					 
1999040200472	19990402	00472	EU  	1999	4	2	HEEA061174       	1	19990319	G	7921	420800001	BLOWER          			SNIAS 	350   	AS350B2     	8680813	EU  										AIR DISTRIBUTION	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6095S					2777				BLOWER INOPERATIVE AND BROKEN.						1	G	7	1 	3U				H9EU    					 
1999040200473	19990402	00473	SW  	1999	4	2	HEEA061317       	1	19990323	G	5302	407030800101B	SKIN            			BELL  	407   	407         		SW  										TAIL BOOM	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM	2525 				53060				SKIN ON TAILBOOM CRACKED ON LT SIDE IN AREA OF HORIZONTAL STABILIZER.						1	G	7	1 	3U			O	H2SW    					 
1999040200474	19990402	00474	SW  	1999	4	2	HEEA061323       	1	19990323	G	6300	406040500119	SUPPORT SEAL    			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				INSPECTED AND REPAIRED SUPPORT AS NECESSARY DUE TO WORN SEAL.						1	G	7	1 	3U			O	H2SW    					 
1999040200475	19990402	00475	SW  	1999	4	2	HEEA061324       	1	19990323	G	6520		BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				WORN TRUNNION BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999040200476	19990402	00476	SW  	1999	4	2	HEEA061325       	1	19990323	G	6520	PHI407112	BOOT            			BELL  	407   	407         		SW  										TAIL ROTOR	SPLIT           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				OUTPUT SEAL BOOT ON HOUSING SPLITTING.						1	G	7	1 	3U			O	H2SW    					 
1999040200477	19990402	00477	SW  	1999	4	2	HEEA061327       	1	19990324	G	5320	214031202101	BEAM            			BELL  	214   	214ST       	1182106	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										MISMANUFACTURED.  BAD TOOLING MAKES BEND IN RADIUS.  WHEN CLAMPED INTO PLACE FOUND RADIUS TOO TIGHT, CAUSED APPROXIMATEL	Y .1250 INCH GAP BETWEEN BEAM AND AIRCRAFT.					2	G	7	2 	4U				H10SW   					 
1999040200478	19990402	00478	SW  	1999	4	2	HEEA061329       	1	19990324	G	6410	206016201131	BLADE           			BELL  	206   	206L1       	1182107	SW  										TAIL ROTOR	MISOVERHAULED   	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										TAIL ROTOR BLADE RECEIVED WITH CONCEALED DAMAGE.						1	G	7	1 	3U				H2SW    					 
1999040200479	19990402	00479	SW  	1999	4	2	HEEA061330       	1	19990324	G	6230	214010492105	LEVER ASSY      			BELL  	214   	214ST       	1182106	SW  										M/R MAST	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										MISMANUFACTURED.  PINS WOULD NOT ENGAGE SLEEVE ASSY, MIC'ED PINS AND FOUND TO BE .010 INCH OVERSIZED.						2	G	7	2 	4U				H10SW   					 
1999040200480	19990402	00480	SW  	1999	4	2	HEEA061332       	1	19990324	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										M/R CONTROL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893L	38   				33006				ACTUATOR ROTARY UNIT INSTALLED ON 2-15-99, FAILED ON 2-25-99 AND REMOVED ON 3-14-99.  SUSPECTED RELEASE BAD.						1	G	7	2 	4U				H4SW    					 
1999040200481	19990402	00481	SW  	1999	4	2	HEEA061333       	1	19990324	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										M/R CONTROL	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023					33080				FORCE TRIM STICKING ON ACTUATOR ROTARY.						1	G	7	2 	4U				H4SW    					 
1999040200482	19990402	00482	SW  	1999	4	2	HEEA061334       	1	19990324	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										M/R CONTROL	BINDING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03		24   								ACTUATOR ROTARY CAUSES BINDING IN FLIGHT CONTROLS.						1	G	7	2 	4U				H4SW    					 
1999040200483	19990402	00483	SW  	1999	4	2	HEEA061335       	1	19990324	G	5260	212075418103	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										STEP ACTUATOR BAD FROM SUPPLY, WON'T RETRACT.  FUNCTIONAL TESTED BY BELL ON 1-22-99.						1	G	7	2 	4U				H4SW    					 
1999040200484	19990402	00484	SW  	1999	4	2	HEEA061336       	1	19990325	G	6320	212040059001	CASE ASSY       			BELL  	212   	212         	1181420	SW  										M/R GEARBOX	MISOVERHAULED   	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										CASE ASSEMBLY RECEIVED WITH CONCEALED DAMAGE.   GOUGES ON RIGHT HAND SIDE OF TOP CASE, APPROX. 10 EACH, DEPTH RANGE FROM	 0.008 INCH TO 0.012 INCH.					1	G	7	1 	4U				H4SW    					 
1999040900680	19990409	00680	NE  	1999	4	9	HEEA061541       	1	19990402	G	2435	200SGL115Q	STARTER         			SKRSKY	S76   	S76A        	8143006	NE  										START/GENERATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31219	9130 				760230				STARTER/GENERATOR WILL NOT MOTOR ENGINE.						1	G	7	2 	3U				H1NE    					 
1999040900681	19990409	00681	SW  	1999	4	9	HEEA061542       	1	19990329	G	6300	406010425107	LEVER ASSEMBLY  			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416	2475 				53070				LEVER ASSEMBLY WORN.						1	G	7	1 	3U			O	H2SW    					 
1999040900682	19990409	00682	SW  	1999	4	9	HEEA061543       	1	19990329	G	6300	406010425107	LEVER ASSEMBLY  			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416	2475 				53070				LEVER ASSEMBLY WORN.						1	G	7	1 	3U			O	H2SW    					 
1999040900683	19990409	00683	SW  	1999	4	9	HEEA061544       	1	19990329	G	6300	406010426101	LINK ASSEMBLY   			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416	2475 				53070				LINK ASSEMBLY WORN. SERIAL NUMBERS REMOVED ARE AFS-1315 AND AFS-1344. REPLACEMENT PART SERIAL NUMBERS ARE AFS-1926 AND A	FS-1940.					1	G	7	1 	3U			O	H2SW    					 
1999040900684	19990409	00684	SW  	1999	4	9	HEEA061545       	1	19990329	G	6230	406010428109	HUB BUSHING     			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416	2475 				53070				HUB BUSHING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999040900685	19990409	00685	SW  	1999	4	9	HEEA061546       	1	19990329	G	6230	406010427109	GIMBAL RING     			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416	2475 				53070				GIMBAL RING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999040900686	19990409	00686	GL  	1999	4	9	HEEA061547       	2	19990329	G	7261	204040760109	FILTER          			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE OIL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				BYPASS BUTTON POPPED.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999040900687	19990409	00687	SW  	1999	4	9	HEEA061548       	1	19990329	G	7700	407375016103	SIGNAL COND     			BELL  	407   	407         		SW  										ENGINE	CONTAMINATED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH					53266				SUSPECT OIL CONTAMINATION AT SIGNAL COND. LOW LEVEL FUEL INTERMITTENT.						1	G	7	1 	3U			O	H2SW    					 
1999040900688	19990409	00688	SW  	1999	4	9	HEEA061549       	1	19990329	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH					53207				CRACKED DISC COUPLING.						1	G	7	1 	3U			O	H2SW    					 
1999040900689	19990409	00689	SW  	1999	4	9	HEEA061550       	1	19990329	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				CRACKED DISC COUPLING.						1	G	7	1 	3U			O	H2SW    					 
1999040900690	19990409	00690	SW  	1999	4	9	HEEA061551       	1	19990329	G	6220	407010150103	FRAHM ASSY      			BELL  	407   	407         		SW  										MAIN ROTOR	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				FRAHM ASSEMBLY MAKING METAL.						1	G	7	1 	3U			O	H2SW    					 
1999040900691	19990409	00691	SW  	1999	4	9	HEEA061552       	1	19990329	G	6720	406012129101	LINK ASSEMBLY   			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				BEARINGS WORN ON LINK ASSEMBLY.						1	G	7	1 	3U			O	H2SW    					 
1999040900692	19990409	00692	SW  	1999	4	9	HEEA061553       	1	19990329	G	7120	407060111101	BIPOD MOUNT     			BELL  	407   	407         		SW  										ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427PH					53059				BEARING HAS AXIAL PLAY BEYOND .005 INCH ON BIPOD MOUNT.						1	G	7	1 	3U			O	H2SW    					 
1999040900693	19990409	00693	SW  	1999	4	9	HEEA061554       	1	19990329	G	6230	407001523101	IDLER ASSY      			BELL  	407   	407         		SW  										M/R CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				IDLER ASSEMBLY HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999040900694	19990409	00694	SW  	1999	4	9	HEEA061555       	1	19990329	G	2840	407362005103	SWITCH          			BELL  	407   	407         		SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH					53266				FUEL LOW LIGHT STAYS ON.						1	G	7	1 	3U			O	H2SW    					 
1999040900695	19990409	00695	SW  	1999	4	9	HEEA061557       	1	19990330	G	2435	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805	88   				28141				STARTER WOULD NOT START AIRCRAFT.						2	G	7	2 	4U				H10SW   					 
1999040900696	19990409	00696	SW  	1999	4	9	HEEA061562       	1	19990401	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH	237  				53228				UNIVERSAL HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999040900697	19990409	00697	SW  	1999	4	9	HEEA061563       	1	19990402	G	2436	163404731	VOLT REGULATOR  			BELL  	206   	206L1       	1182107	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3178K					45765				VOLTAGE REGULATOR WILL NOT COME ON LINE.						1	G	7	1 	3U				H2SW    					 
1999040900698	19990409	00698	GL  	1999	4	9	HEEA061564       	2	19990402	G	7261	174000101	FILTER          			BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					ENGINE OIL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6748D					51106				FILTER WILL NOT BYPASS.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999040900699	19990409	00699	GL  	1999	4	9	HEEA061565       	2	19990402	G	7261	174000103	FILTER          			BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					ENGINE OIL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6160Z					51610				FILTER NOT BYPASS.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999040900700	19990409	00700	GL  	1999	4	9	HEEA061566       	2	19990402	G	7261	174000103	FILTER          			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					ENGINE OIL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1073W					45386				FILTER WILL NOT BYPASS.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999040900701	19990409	00701	GL  	1999	4	9	HEEA061567       	2	19990402	G	7261	174000103	FILTER          			BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE OIL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22743					3624				FILTER FAILS BYPASS CHECK.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999040900702	19990409	00702	GL  	1999	4	9	HEEA061568       	2	19990402	G	7261	174000103	FILTER          			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					ENGINE OIL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50046					45173				FILTER WILL NOT BYPASS.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999040900703	19990409	00703	GL  	1999	4	9	HEEA061569       	2	19990402	G	7261	174000103	FILTER          			BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					ENGINE OIL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	206FS					51506				FILTER WILL NOT BYPASS.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999040900704	19990409	00704	SW  	1999	4	9	HEEA061570       	1	19990402	G	6710	206001342001	TUBE            			BELL  	206   	206L1       	1182107	SW  										CYCLIC	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1076Y					45380				TUBE ASSEMBLY HAS CORROSION BEYOND LIMITS. REPLACED WITH SERVICEABLE CYCLIC TUBE.						1	G	7	1 	3U				H2SW    					 
1999040900705	19990409	00705	SW  	1999	4	9	HEEA061571       	1	19990402	G	6230	206010450119	SWASHPLATE      			BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3108E	6751 				51498				UNABLE TO ADJUST FRICTION ON M/R SWASHPLATE.						1	G	7	1 	3U				H2SW    					 
1999040900706	19990409	00706	SW  	1999	4	9	HEEA061572       	1	19990402	G	6420	206011810013	BLADE           			BELL  	206   	206L1       	1182107	SW  										TAIL ROTOR	PEELING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	27702	5687 				45300				TAIL ROTOR ASSEMBLY HAS WORN FEATHERING BEARINGS AND PAINT PEELING FROM BLADES.						1	G	7	1 	3U				H2SW    					 
1999040900707	19990409	00707	SW  	1999	4	9	HEEA061573       	1	19990402	G	5532	206020113163A	SKIN            			BELL  	206   	206L3       	1182108	SW  										VERTICAL STAB	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				VERTICAL FIN CORRODED AND SEPARATED.						1	G	7	1 	3U				H2SW    					 
1999040900708	19990409	00708	SW  	1999	4	9	HEEA061574       	1	19990402	G	5532	206020113207	SKIN            			BELL  	206   	206B3       	1181506	SW  										VERTICAL STAB	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										VERTICAL FIN HAD DEEP SCRATCHES ALONG LEADING EDGES AND TRAILING EDGES.						1	G	7	1 	3U				H2SW    					 
1999040900709	19990409	00709	SW  	1999	4	9	HEEA061576       	1	19990402	G	5510	206023119151	STRUCTURE       			BELL  	206   	206L1       	1182107	SW  										HORIZONTAL STAB	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2246Q					45752				HORIZONTAL STABILIZER ASSEMBLY HAD CORROSION.						1	G	7	1 	3U				H2SW    					 
1999040900710	19990409	00710	SW  	1999	4	9	HEEA061577       	1	19990402	G	5330	206031124111A	PANEL           			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										FOUND PANEL NOT FITTING PROPERLY AT LEFT SKIN ASSEMBLY.						1	G	7	1 	3U				H2SW    					 
1999040900711	19990409	00711	SW  	1999	4	9	HEEA061578       	1	19990402	G	5330	206032117069A	PANEL           			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										PANEL ASSEMBLY MISMANUFACTURED.						1	G	7	1 	3U				H2SW    					 
1999040900712	19990409	00712	SW  	1999	4	9	HEEA061579       	1	19990402	G	6320	206040190005	PUMP            			BELL  	206   	206L3       	1182108	SW  										M/R TRANSMISSION	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	49EA					51507				ALIGNMENT HOLE IN WRONG LOCATION FOR DRAIN ORIENTATION. IN DIFFERENT LOCATION THAN OTHER PUMPS.						1	G	7	1 	3U				H2SW    					 
1999040900713	19990409	00713	SW  	1999	4	9	HEEA061580       	1	19990402	G	6510	206040370103	WHEEL           			BELL  	206   	206L1       	1182107	SW  										BLOWER	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2761N					45277				TAIL ROTOR ASSEMBLY HAD CORROSION ON BLOWER WHEEL.						1	G	7	1 	3U				H2SW    					 
1999040900714	19990409	00714	SW  	1999	4	9	HEEA061581       	1	19990402	G	3212	206050248117	FLOAT BAG ASSY  			BELL  	206   	206L3       	1182108	SW  										MLG	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	129MR					51129				FLOAT BAG ASSEMBLY DID NOT PASS FLOAT INSPECTION, FRONT SECTION LEAKING.						1	G	7	1 	3U				H2SW    					 
1999040900715	19990409	00715	SW  	1999	4	9	HEEA061582       	1	19990402	G	3212	206050248117	FLOAT BAG ASSY  			BELL  	206   	206L1       	1182107	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	5006F					45181				FLOAT BAG ASSEMBLY'S AFT COMPARTMENT LEAKING.						1	G	7	1 	3U				H2SW    					 
1999040900716	19990409	00716	SW  	1999	4	9	HEEA061583       	1	19990402	G	7810	206061230001	BELLMOUTH       			BELL  	206   	206B3       	1181506	SW  										ENGINE	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	103PH					3000				CORROSION PITS BEYOND LIMITS ON MOUNTING SURFACE AT BELLMOUTH. REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U				H2SW    					 
1999040900717	19990409	00717	SW  	1999	4	9	HEEA061584       	1	19990402	G	2430	206075447007	VOLT REGULATOR  			BELL  	206   	206L1       	1182107	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2758N					45267				AMMETER SPIKES WHEN RADIO MIKE KEYED ON VOLTAGE REGULATOR.						1	G	7	1 	3U				H2SW    					 
1999040900718	19990409	00718		1999	4	9	HEEA061585       	4	19990402	G	3421	206075607103	GYRO            			BELL  	206   	206L3       	1182108	SW  										COCKPIT	PRECESSING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6160Z					51610				ATTITUDE GYRO PRECESSES 4 DEGREES DURING CLIMB AND DIVE ERECTION RATES.						1	G	7	1 	3U				H2SW    					 
1999040900719	19990409	00719	SW  	1999	4	9	HEEA061586       	1	19990402	G	6320	206075678107	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2758N					45267				INDICATOR'S PRESSURE NEEDLE INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999040900720	19990409	00720	SW  	1999	4	9	HEEA061587       	1	19990402	G	6240	206076373001	TACH GENERATOR  			BELL  	206   	206L3       	1182108	SW  										ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31077					51520				LIP OF HOUSING BROKEN AT BEARING SEAT ON TACHOMETER GENERATOR.						1	G	7	1 	3U				H2SW    					 
1999040900721	19990409	00721	GL  	1999	4	9	HEEA061590       	2	19990402	G	7261	174000103	FILTER ASSEMBLY 			BOLKMS	105   	BO105CBS    	5626008	EU  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE OIL	LEAKS           	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	911RS					S670				FILTER ASSEMBLY LEAKS WITH NEW SEALS INSTALLED.						1	G	7	2 	3U	3	U	NC	H3EU    	E4CE				 
1999040900722	19990409	00722	GL  	1999	4	9	HEEA061591       	2	19990402	G	7261	174000103	FILTER ASSEMBLY 			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE OIL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	54191					S804				FILTER ASSEMBLY WILL NOT BYPASS.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999040900723	19990409	00723	GL  	1999	4	9	HEEA061592       	2	19990402	G	7261	174000103	FILTER ASSEMBLY 			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE OIL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	135AE					S838				FILTER ASSEMBLY WILL NOT BYPASS.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999042300006	19990423	00006		1999	4	23	HEEA061593       	4	19990405	G	3421	258719343	GYRO            			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	PRECESSING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	127FH					760063				GYRO PRECESSES.						1	G	7	2 	3U				H1NE    					 
1999042300007	19990423	00007		1999	4	23	HEEA061594       	4	19990405	G	3422	258719342	GYRO COMPASS    			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5426U					760167				COMPASS WARNING LIGHT ILLUMINATES ON AND OFF.						1	G	7	2 	3U				H1NE    					 
1999042300008	19990423	00008	NE  	1999	4	23	HEEA061595       	2	19990405	G	7532	3033063	BLEED VALVE     			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					ENGINE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	108X	2899 				33115				ENGINE OSCILLATES.						1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999042300009	19990423	00009	NE  	1999	4	23	HEEA061596       	2	19990405	G	7532	3033063	BLEED VALVE     			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					ENGINE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	142PH					33150				ENGINE OSCILLATES.						1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999042300010	19990423	00010		1999	4	23	HEEA061597       	4	19990405	G	2312	4000103000	TRANSCEIVER     																	COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TRANSCEIVER'S POWER SUPPLY BOARD BAD.																			 
1999042300011	19990423	00011		1999	4	23	HEEA061598       	4	19990405	G	2312	4000106010	CONTROL         			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5128					760181				NUMBER DOESN'T PICK UP AT WINDOW WHEN CHANGED ON CONTROL UNIT.						1	G	7	2 	3U				H1NE    					 
1999042300012	19990423	00012		1999	4	23	HEEA061599       	4	19990405	G	2312	4000106010	CONTROL         			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5128					760181				WHEN TURNING WHEELS NR 2 AND NR 4, MAKES DIFFERENT CHANGE AT WINDOW ON CONTROL UNIT.  PERFORMED PRELIMINARY INSPECTION A	ND FOUND THUMBWHEEL INTERMITTENT.  ALSO FOUND TRANSMIT INCORRECT CTSS TONES.					1	G	7	2 	3U				H1NE    					 
1999042300013	19990423	00013		1999	4	23	HEEA061600       	4	19990405	G	3453	453105004	BUTTON          			SKRSKY	S76   	S76A        	8143006	NE  										LORAN	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31219					760230				ENTER BUTTON INOPERATIVE.  REPLACED RUBBER KEYPAD.  REPAIRED.  TESTED.  FUNCTION CHECK GOOD.						1	G	7	2 	3U				H1NE    					 
1999042300014	19990423	00014		1999	4	23	HEEA061601       	1	19990405	G	2510	504339401	SEAT BELT       																	COCKPIT	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										SEAT BELT MISMANUFACTURED.  MOUNTING HOLES TOO SMALL.																			 
1999042300015	19990423	00015		1999	4	23	HEEA061602       	4	19990405	G	3421	7000466915	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	127FH					760063				ADI NEEDS FUNCTION TEST.  FAILED FIRST STEP IN SST CHECK-OUT.						1	G	7	2 	3U				H1NE    					 
1999042300016	19990423	00016		1999	4	23	HEEA061603       	4	19990405	G	3421	7000466915	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	127FH					760063				ADI NEEDS FUNCTION TEST.  FAILED FIRST STEP IN SST CHECK-OUT.						1	G	7	2 	3U				H1NE    					 
1999042300017	19990423	00017		1999	4	23	HEEA061604       	4	19990405	G	2210	7611123	AMPLIFIER       			SKRSKY	S76   	S76A        	8143006	NE  										PITCH SLICE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1546G					760076				NR 2 PITCH AFCS DOES NOT WORK.						1	G	7	2 	3U				H1NE    					 
1999042300018	19990423	00018		1999	4	23	HEEA061605       	4	19990405	G	2210	7611133	AMPLIFIER       			SKRSKY	S76   	S76A        	8143006	NE  										ROLL SLICE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545K					760047				NR 1 ROLL CHANNEL CHATTERS, ALSO HAS BURN SPOT ON LOWER CORNER AT P NR 2.						1	G	7	2 	3U				H1NE    					 
1999042300019	19990423	00019	NE  	1999	4	23	HEEA061606       	1	19990405	G	6210	7615009043050	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										TIP CAP DOUBLER	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	15460					760223				INTERNAL DOUBLER SEPARATED ON TIP CAP.						1	G	7	2 	3U				H1NE    					 
1999042300020	19990423	00020	NE  	1999	4	23	HEEA061607       	1	19990405	G	6210	7615009043050	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										TIP CAP DOUBLER	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	706AE					760275				FIBERGLASS BETWEEN THE INNER AND OUTER DOUBLER ON THE UPPER SURFACE IS BROKEN.						1	G	7	2 	3U				H1NE    					 
1999042300021	19990423	00021	NE  	1999	4	23	HEEA061608       	1	19990405	G	6210	7615009043050	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										TIP CAP	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1547D					760077				EXTREME TRAILING EDGE AND TIP BROKEN OFF.						1	G	7	2 	3U				H1NE    					 
1999042300022	19990423	00022	NE  	1999	4	23	HEEA061609       	1	19990405	G	6210	7615009000049A	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31219	12344				760230				LEADING EDGE SEPARATED AND CRACKED AT STATIONS 65 AND 76 ON MAIN ROTOR BLADE.						1	G	7	2 	3U				H1NE    					 
1999042300023	19990423	00023	NE  	1999	4	23	HEEA061610       	1	19990405	G	6210	7615009000049A	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31219	14932				760230				LEADING EDGE CRACKED AND SEPARATION AT STATIONS 145 AND 168.						1	G	7	2 	3U				H1NE    					 
1999042300024	19990423	00024	NE  	1999	4	23	HEEA061611       	1	19990405	G	6210	7615009100051A	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31219	11669				760230				LEADING EDGE SPLICE SEPARATED AND BLADE IS DUE FOR TIME EXTENSION.						1	G	7	2 	3U				H1NE    					 
1999042300025	19990423	00025	NE  	1999	4	23	HEEA061612       	1	19990405	G	6210	7615009100048A	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	BULGING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545X	8570 				760050				LEADING EDGE BULGING OUTWARD.						1	G	7	2 	3U				H1NE    					 
1999042300026	19990423	00026		1999	4	23	HEEA061613       	4	19990406	G	3416	1003511424	ALTIMETER       																	COCKPIT	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										READS 1,500 FEET HIGHER THAN FIELD ELEVATION.    TIME SINCE REPAIR 0:00 HOURS.																			 
1999042300027	19990423	00027	NE  	1999	4	23	HEEA061614       	1	19990406	G	6210	7615009043050	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										TIP CAP	SPLIT           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1546K					760082				TRAILING EDGE SPLIT OPEN NEAR THE TIP.						1	G	7	2 	3U				H1NE    					 
1999042300028	19990423	00028	NE  	1999	4	23	HEEA061615       	1	19990406	G	6210	7615009043050	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										TIP CAP	SPLIT           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22342					760096				TRAILING EDGE SPLIT OPEN NEAR THE OUTER TIP.						1	G	7	2 	3U				H1NE    					 
1999042300029	19990423	00029	NE  	1999	4	23	HEEA061617       	1	19990406	G	6320	7635109500043	TRANSMISSION    			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1546K	10395				760082				MAST SEAL LEAKING ON TRANSMISSION.						1	G	7	2 	3U				H1NE    					 
1999042300030	19990423	00030	NE  	1999	4	23	HEEA061618       	1	19990406	G	6320	7635109500043	TRANSMISSION    			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	CONTAMINATED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1546G	7219 				760076				METAL IN OIL.						1	G	7	2 	3U				H1NE    					 
1999042300031	19990423	00031	NE  	1999	4	23	HEEA061619       	1	19990406	G	6510	7636104007041	SUPPORT         			SKRSKY	S76   	S76A        	8143006	NE  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5128	5014 				760181				BEARING SUPPORT CORRODED AND DAMPER UNBONDED.						1	G	7	2 	3U				H1NE    					 
1999042300032	19990423	00032	NE  	1999	4	23	HEEA061620       	1	19990406	G	6510	7636105201041	DRIVESHAFT      			SKRSKY	S76   	S76A        	8143006	NE  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31217					760229				DRIVESHAFT HAS CORROSION PITS.						1	G	7	2 	3U				H1NE    					 
1999042300033	19990423	00033	NE  	1999	4	23	HEEA061621       	1	19990406	G	6510	7636105201041	DRIVESHAFT      			SKRSKY	S76   	S76A        	8143006	NE  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31217					760229				DRIVESHAFT HAS CORROSION PITS.						1	G	7	2 	3U				H1NE    					 
1999042300034	19990423	00034	NE  	1999	4	23	HEEA061622       	1	19990406	G	7714	7645001076101	GAS GEN TACH    			SKRSKY	S76   	S76A        	8143006	NE  										N1 NEEDLE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4253S					760035				GENERATOR/TACHOMETER NOT INDICATING ZERO PERCENT TO 10 PERCENT.						1	G	7	2 	3U				H1NE    					 
1999042300035	19990423	00035	NE  	1999	4	23	HEEA061623       	1	19990406	G	2421	7655009005106	GENERATOR       			SKRSKY	S76   	S76A        	8143006	NE  										AC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911MJ	310  				760231				A/C GENERATOR HAD BEARING LIGHT ON INDICATOR PANEL.						1	G	7	2 	3U				H1NE    					 
1999042300036	19990423	00036		1999	4	23	HEEA061624       	4	19990406	G	3420	7660002113103	GYRO            			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	792CH					760193				VERTICAL GYRO CAUSES NR 2 PITCH CHANNEL TO KICK AND OPERATE ERRATIC.						1	G	7	2 	3U				H1NE    					 
1999042300037	19990423	00037		1999	4	23	HEEA061625       	4	19990406	G	3420	7660002113103	GYRO            			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911MJ					760231				VERTICAL GYRO FALLS OFF TO A 30 DEGREE BANK SOMETIMES.						1	G	7	2 	3U				H1NE    					 
1999042300038	19990423	00038		1999	4	23	HEEA061626       	4	19990406	G	3420	7660002113103	GYRO            			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545X					760050				VERTICAL GYRO INOPERATIVE.  WILL NOT COME UP TO SPEED.						1	G	7	2 	3U				H1NE    					 
1999042300039	19990423	00039		1999	4	23	HEEA061627       	4	19990406	G	3420	7660002113103	GYRO            			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	706AE					760275				VERTICAL GYRO WILL NOT ERECT.						1	G	7	2 	3U				H1NE    					 
1999042300040	19990423	00040		1999	4	23	HEEA061628       	4	19990406	G	3420	7660002113103	GYRO            			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2743E					760155				NR 2 PITCH KICKS IN-FLIGHT.						1	G	7	2 	3U				H1NE    					 
1999042300041	19990423	00041		1999	4	23	HEEA061629       	4	19990406	G	3420	7660002113103	GYRO            			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	PRECESSING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1546K					760082				PILOT ATTITUDE INDICATOR PRECESSES.						1	G	7	2 	3U				H1NE    					 
1999042300042	19990423	00042	NE  	1999	4	23	HEEA061630       	1	19990406	G	6200	7665001802102	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	5128					760181				ACTUATOR LEAKING.						1	G	7	2 	3U				H1NE    					 
1999042300043	19990423	00043	NE  	1999	4	23	HEEA061631       	1	19990406	G	6200	7665001802102	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	1545X					760050				ACTUATOR LEAKING.						1	G	7	2 	3U				H1NE    					 
1999042300044	19990423	00044	NE  	1999	4	23	HEEA061632       	1	19990406	G	2913	7665009808101	PUMP            			SKRSKY	S76   	S76A        	8143006	NE  										HYDRAULIC SYS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545K					760047				HYDRAULIC PUMP FLUCTUATES 100 PSI.						1	G	7	2 	3U				H1NE    					 
1999042300045	19990423	00045	NE  	1999	4	23	HEEA061633       	1	19990406	G	2913	7665009808101	PUMP            			SKRSKY	S76   	S76A        	8143006	NE  										HYDRAULIC SYS	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	911MJ					760231				SEAL DRAIN LEAKING AT HYDRAULIC PUMP.						1	G	7	2 	3U				H1NE    					 
1999042300046	19990423	00046		1999	4	23	HEEA061634       	4	19990406	G	2210	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	792CH	7218 				760193				ACTUATOR INOPERATIVE.  INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND NR 2 POTENTIOMETER INDICATING ZERO VOLTAGE.						1	G	7	2 	3U				H1NE    					 
1999042300047	19990423	00047		1999	4	23	HEEA061635       	4	19990406	G	2210	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	CHATTERING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545K	10132				760047				AFCS ACTUATOR CHATTERING IN-FLIGHT.						1	G	7	2 	3U				H1NE    					 
1999042300048	19990423	00048		1999	4	23	HEEA061636       	4	19990406	G	2210	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31219	9275 				760230				AFCS ACTUATOR INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999042300049	19990423	00049		1999	4	23	HEEA061637       	4	19990406	G	2210	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4253S	10605				760035				AFCS INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999042300050	19990423	00050		1999	4	23	HEEA061638       	4	19990406	G	2210	7690001812102	BRAKE           			SKRSKY	S76   	S76A        	8143006	NE  										AUTOFLIGHT	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545K					760047				BRAKE SHAFT LOOSE.						1	G	7	2 	3U				H1NE    					 
1999042300051	19990423	00051		1999	4	23	HEEA061639       	4	19990406	G	2370	9806020023	VOICE RECORDER  			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22342					760096				CANNOT READ BEACON INFORMATION.  CVR REQUIRES EVALUATION.						1	G	7	2 	3U				H1NE    					 
1999042300052	19990423	00052	NE  	1999	4	23	HEEA061640       	1	19990406	G	2460	A1077B	RELAY           			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545K					760047				NR 2 GENERATOR LIGHT STAYS ON ALL OF THE TIME WITH GENERATOR ON-LINE.  ALSO, NUT STRIPPED PN TERMINAL NR 11.						1	G	7	2 	3U				H1NE    					 
1999042300053	19990423	00053	NE  	1999	4	23	HEEA061641       	1	19990406	G	3340	A413AHDACF1428	POWER SUPPLY    			SKRSKY	S76   	S76A        	8143006	NE  										STROBE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4253S					760035				POWER SUPPLY INOPERATIVE, NO OUTPUT, BURNT.						1	G	7	2 	3U				H1NE    					 
1999042300054	19990423	00054	NE  	1999	4	23	HEEA061642       	1	19990406	G	3340	A413AHDACF1428	POWER SUPPLY    			SKRSKY	S76   	S76A        	8143006	NE  										STROBE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5426U					760167				POWER SUPPLY INOPERATIVE, NO OUTPUT.						1	G	7	2 	3U				H1NE    					 
1999042300055	19990423	00055		1999	4	23	HEEA061643       	4	19990406	G	2340	AA25004	AUDIO CONTROL   			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	15460					760223				AUDIO CONTROL WOULD NOT TRANSMIT OUTSIDE OF AIRCRAFT ON FM 1, 2, 3, 4.						1	G	7	2 	3U				H1NE    					 
1999042300056	19990423	00056		1999	4	23	HEEA061644       	4	19990406	G	2562	ELP362D	PINGER          			SKRSKY	S76   	S76A        	8143006	NE  										LOCATOR BEACON	MISLABELED      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22342					760096				CANNOT READ UNIT INFORMATION ON STICKER.						1	G	7	2 	3U				H1NE    					 
1999042300057	19990423	00057		1999	4	23	HEEA061645       	4	19990407	G	3451	066106602	TRANSCEIVER     			SKRSKY	S76   	S76A        	8143006	NE  										DME	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1545K					760047				SENSITIVITY AND POWER LOW ON TRANSCEIVER..						1	G	7	2 	3U				H1NE    					 
1999042300058	19990423	00058	NE  	1999	4	23	HEEA061646       	1	19990408	G	2612	30326E7	AMPLIFIER       			SKRSKY	S76   	S76A        	8143006	NE  										FIRE DETECTOR	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1545K					760047				CONTROL AMPLIFIER LIGHT STAYS ON.						1	G	7	2 	3U				H1NE    					 
1999042300059	19990423	00059		1999	4	23	HEEA061647       	4	19990408	G	2312	4000106000	CONTROL UNIT    																	COCKPIT	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										UNIT INOPERATIVE.  SOMETHING LOOSE INSIDE.																			 
1999042300060	19990423	00060	NE  	1999	4	23	HEEA061648       	1	19990408	G	7720	7645001078101	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										ENGINE TEMP	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3122G					760232				ENGINE OIL INDICATOR HAD BUZZ WITH POWER TURNED ON.						1	G	7	2 	3U				H1NE    					 
1999042300061	19990423	00061	NE  	1999	4	23	HEEA061649       	1	19990408	G	2841	7645001078103	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										FUEL QUANTITY	STICKS          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1546K					760082				NR 2 NEEDLE STICKS ON FUEL QUANTITY INDICATOR.						1	G	7	2 	3U				H1NE    					 
1999042300062	19990423	00062	NE  	1999	4	23	HEEA061650       	1	19990408	G	2430	7655009005104	CONTROL UNIT    			SKRSKY	S76   	S76A        	8143006	NE  										GENERATOR	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1546K					760082				GENERATOR INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999042300063	19990423	00063	SW  	1999	4	23	HEEA061651       	1	19990405	G	3210	206323004	SKID            			BELL  	206   	206L3       	1182108	SW  										MLG	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251X					51552				MAJOR CRACKS ON BOTTOM OF SKID TUBE.  SCRAPPED TUBE.  REPLACED WITH SERVICEABLE TUBE.						1	G	7	1 	3U				H2SW    					 
1999042300064	19990423	00064	SW  	1999	4	23	HEEA061652       	1	19990405	G	3210	206324003	SKID            			BELL  	206   	206L3       	1182108	SW  										MLG	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251V					51404				LEFT SKID TUBE HAS CRACK NEAR 2ND SKID SHOE.  SCRAPPED TUBE.  REPLACED WITH SERVICEABLE TUBE.						1	G	7	1 	3U				H2SW    					 
1999042300065	19990423	00065	SW  	1999	4	23	HEEA061653       	1	19990405	G	3210	206324003	SKID            			BELL  	206   	206L1       	1182107	SW  										MLG	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2125M					45649				CRACKED IN SEVERAL AREAS ALONG SKID TUBE. SCRAPPED TUBE.  REPLACED WITH SERVICEABLE TUBE.						1	G	7	1 	3U				H2SW    					 
1999042300066	19990423	00066	SW  	1999	4	23	HEEA061654       	1	19990405	G	3210	206324003	SKID            			BELL  	206   	206L1       	1182107	SW  										MLG	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										CRACKED IN SEVERAL AREAS ALONG SKID TUBE. SCRAPPED TUBE.  REPLACED WITH SERVICEABLE TUBE.						1	G	7	1 	3U				H2SW    					 
1999042300067	19990423	00067	SW  	1999	4	23	HEEA061655       	1	19990405	G	3210	206324004	SKID            			BELL  	206   	206L1       	1182107	SW  										MLG	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										CRACKED IN SEVERAL AREAS ALONG SKID TUBE. SCRAPPED TUBE.  REPLACED WITH SERVICEABLE TUBE.						1	G	7	1 	3U				H2SW    					 
1999042300068	19990423	00068	SW  	1999	4	23	HEEA061656       	1	19990405	G	3210	206324004	SKID            			BELL  	206   	206L3       	1182108	SW  										MLG	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251V					51404				RIGHT SKID TUBE HAS CRACK BY THIRD SKID SHOE.  SCRAPPED TUBE.  REPLACED WITH SERVICEABLE TUBE.						1	G	7	1 	3U				H2SW    					 
1999042300069	19990423	00069	SW  	1999	4	23	HEEA061657       	1	19990405	G	3210	206324004	SKID            			BELL  	206   	206L1       	1182107	SW  										MLG	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2125M					45649				CRACKED IN SEVERAL AREAS ALONG TUBE.  SCRAPPED TUBE.  REPLACED WITH SERVICEABLE TUBE.						1	G	7	1 	3U				H2SW    					 
1999042300070	19990423	00070	SW  	1999	4	23	HEEA061658       	1	19990405	G	5210	209031816105	DOOR            			BELL  	412   	412         	1182202	SW  										CABIN	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	142PH					33150				DOOR ASSEMBLY DOESN'T FIT PROPERLY AND IS CHAFED AND BROKEN.						1	G	7	2 	4U				H4SW    					 
1999042300071	19990423	00071	SW  	1999	4	23	HEEA061659       	1	19990405	G	7712	212070160101	INDICATOR       			BELL  	212   	212         	1181420	SW  	PWA   	PT6T  	PT6T3       	52045	EA  					COCKPIT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3208H					31304				NR 1 INDICATION AND CURSOR POINTERS STICKING.						1	G	7	1 	4U	4	U		H4SW    	E22EA				 
1999042300072	19990423	00072	SW  	1999	4	23	HEEA061660       	1	19990405	G	3411	212070239101FM	FITTING         			BELL  	214   	214ST       	1182106	SW  										STATIC SYSTEM	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				STATIC SYSTEM FITTING BROKE UNDER PRESSURE DURING TEST (NEEDLE NOT ZERO).						2	G	7	2 	4U				H10SW   					 
1999042300073	19990423	00073	SW  	1999	4	23	HEEA061661       	1	19990405	G	7722	212075067105	INDICATOR       			BELL  	412   	412         	1182202	SW  										ITT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7128R					36007				ITT INDICATOR NEEDLE STICKS.						1	G	7	2 	4U				H4SW    					 
1999042300074	19990423	00074	SW  	1999	4	23	HEEA061662       	1	19990405	G	7722	212075067109	INDICATOR       			BELL  	412   	412         	1182202	SW  										ITT	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2261D					33076				ITT INDICATOR STICKS.						1	G	7	2 	4U				H4SW    					 
1999042300075	19990423	00075	SW  	1999	4	23	HEEA061663       	1	19990405	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										STEP ACTUATOR INOPERATIVE.  WILL NOT ACTUATE.						1	G	7	2 	4U				H4SW    					 
1999042300076	19990423	00076	SW  	1999	4	23	HEEA061664       	1	19990405	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S					33022				STEP ACTUATOR WILL NOT RAISE ON ITS OWN.						1	G	7	2 	4U				H4SW    					 
1999042300077	19990423	00077	SW  	1999	4	23	HEEA061665       	1	19990405	G	6730	212076005105	CYLINDER ASSY   			BELL  	412   	412         	1182202	SW  										M/R CONTROL	LEAKING         	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	141PH	3923 				33197				CYLINDER LEAKING.						1	G	7	2 	4U				H4SW    					 
1999042300078	19990423	00078	SW  	1999	4	23	HEEA061666       	1	19990405	G	2910	212076015001	VALVE           			BELL  	412   	412         	1182202	SW  										HYDRAULIC SYS	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	141PH					33197				VALVE LEAKING.						1	G	7	2 	4U				H4SW    					 
1999042300079	19990423	00079	SW  	1999	4	23	HEEA061667       	1	19990405	G	6710	214001970111	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										MAIN ROTOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ACTUATOR ASSEMBLY DISENGAGES.						2	G	7	2 	4U				H10SW   					 
1999042300080	19990423	00080	SW  	1999	4	23	HEEA061668       	1	19990405	G	6710	214001970111	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										MAIN ROTOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ASSEMBLY WILL NOT WORK WITH ANY ACTUATOR.						2	G	7	2 	4U				H10SW   					 
1999042300081	19990423	00081	SW  	1999	4	23	HEEA061669       	1	19990405	G	6210	214015300107	BLADE           			BELL  	214   	214ST       	1182106	SW  										MAIN ROTOR	WON'T TRACK     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y	2928 				28139				COULDN'T TRACK BLADE.						2	G	7	2 	4U				H10SW   					 
1999042300082	19990423	00082	SW  	1999	4	23	HEEA061670       	1	19990405	G	6330	214031614125	TORSION ARM     			BELL  	214   	214ST       	1182106	SW  										M/R TRANSMISSION	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				TORSION ARM ASSEMBLY HAD CRACKED BEARING.						2	G	7	2 	4U				H10SW   					 
1999042300083	19990423	00083	SW  	1999	4	23	HEEA061671       	1	19990405	G	2435	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										START/GENERATOR	WEAK            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				STARTER WEAK; WILL NOT START AIRCRAFT.						2	G	7	2 	4U				H10SW   					 
1999042300084	19990423	00084	SW  	1999	4	23	HEEA061672       	1	19990405	G	2435	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										START/GENERATOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805	585  				28141				NR 1 ENGINE WILL NOT GO INTO CROSS START FOR 20 SECONDS AND START.						2	G	7	2 	4U				H10SW   					 
1999042300085	19990423	00085		1999	4	23	HEEA061673       	4	19990405	G	3420	214074300107	CAUTION PANEL   			BELL  	214   	214ST       	1182106	SW  										AFCS	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										AFCS MASTER CAUTION PANEL DOES NOT ILLUMINATE.						2	G	7	2 	4U				H10SW   					 
1999042300086	19990423	00086		1999	4	23	HEEA061674       	4	19990405	G	3421	214075244001	GYRO            			BELL  	412   	412         	1182202	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	142PH					33150				TURN NEEDLE ON RATE GYRO INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999042300087	19990423	00087	SW  	1999	4	23	HEEA061675       	1	19990405	G	2913	214076334101	PUMP            			BELL  	214   	214ST       	1182106	SW  										HYDRAULIC SYS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				OIL COOLER FAN LIGHT STAYS ILLUMINATED.						2	G	7	2 	4U				H10SW   					 
1999042300088	19990423	00088	SW  	1999	4	23	HEEA061676       	1	19990405	G	3150	214175122107	CAUTION PANEL   			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				90 DEGREE CHIP AND NR 2 FUEL TRANSFER LIGHTS INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999042300089	19990423	00089	SW  	1999	4	23	HEEA061677       	1	19990405	G	7714	214175428101	PANEL ASSY      			BELL  	212   	212         	1181420	SW  										ENGINE GAUGE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	754H					35034				NR 2 ENGINE CLIMBED TO 105 PERCENT BEFORE MAXIMUM THROTTLE WAS REACHED.						1	G	7	1 	4U				H4SW    					 
1999042300090	19990423	00090	SW  	1999	4	23	HEEA061678       	1	19990405	G	2821	222366621101	FILTER          			BELL  	206   	206L3       	1182108	SW  										FUEL SYSTEM	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6748D					51106				BYPASS BUTTON MISSING ON FUEL FILTER.						1	G	7	1 	3U				H2SW    					 
1999042300091	19990423	00091		1999	4	23	HEEA061679       	4	19990405	G	3421	222375033107	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	PRECESSING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				ATTITUDE INDICATOR RECESSES CONSTANTLY.						2	G	7	2 	4U				H10SW   					 
1999042300092	19990423	00092	CE  	1999	4	23	HEEA061680       	1	19990405	G	2435	23048016	STARTER         			BEECH 	200   	200CBEECH   	1152926	CE  										START/GENERATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	500PH					BL29				STARTER/GENERATOR WILL NOT CRANK ENGINE.						1	L	7	2 	4T				A24CE   					 
1999042300093	19990423	00093		1999	4	23	HEEA061681       	4	19990405	G	2210	2593996333	TARSYN          			BELL  	212   	212         	1181420	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5010F					30936				UNIT DOES NOT SLAVE IN MAGNETIC COMPASS MODE.  UNIT FUNCTION GOOD ON SST BENCH.						1	G	7	1 	4U				H4SW    					 
1999042300094	19990423	00094		1999	4	23	HEEA061682       	4	19990405	G	2210	2593996333	TARSYN          			BELL  	212   	212         	1181420	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3208H					31304				TARSYN CAUSES CIRCUIT BREAKER TO TRIP.						1	G	7	1 	4U				H4SW    					 
1999042300095	19990423	00095	GL  	1999	4	23	HEEA061683       	2	19990405	G	7321	25490925N	FCU             			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	CP232	11118				45167				FUEL CONTROL CHANGED TO COMPLY WITH CEB-A-73-3102.   AIRCRAFT FLEW 6.5 HOURS AND THE AIRCRAFT EXPERIENCED A HANG START. 	 THE AIRCRAFT WAS TROUBLESHOT AND THE FUEL CONTROL WAS CHANGED.  COMPLIED WITH CEB-A-73-3102, NEW SPRING INSTALLED.  UPG	RADED UNIT.				1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999042300096	19990423	00096	SW  	1999	4	23	HEEA061684       	1	19990405	G	2611	302319	SMOKE DETECTOR  			BELL  	412   	412         	1182202	SW  										CABIN	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S					33022				SMOKE DETECTOR FAILED FUNCTION TEST.						1	G	7	2 	4U				H4SW    					 
1999042300097	19990423	00097	SW  	1999	4	23	HEEA061685       	1	19990405	G	7722	3030083	COMPENSATOR     			BELL  	212   	212         	1181420	SW  										ENGINE TIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1079U					31122				TRIM COMPENSATOR TURNED TO 100 DEGREES AND WILL NOT DROP TEMPS.  WITHIN RANGE.						1	G	7	1 	4U				H4SW    					 
1999042300098	19990423	00098		1999	4	23	HEEA061686       	4	19990405	G	2312	4000044000	TRANSCEIVER     			BELL  	212   	212         	1181420	SW  										COCKPIT VHF	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1082G					31109				VHF TRANSCEIVER WILL NOT TRANSMIT OR RECEIVE ON 119.70 THROUGH 131.57.						1	G	7	1 	4U				H4SW    					 
1999042300099	19990423	00099		1999	4	23	HEEA061687       	4	19990405	G	2312	4000044000	TRANSCEIVER     			BELL  	212   	212         	1181420	SW  										COCKPIT VHF	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1082G					31109				VHF TRANSCEIVER INOPERATIVE WHEN INSTALLED.						1	G	7	1 	4U				H4SW    					 
1999042300100	19990423	00100		1999	4	23	HEEA061688       	4	19990405	G	3442	40005040301	DRIVE ASSY      			BELL  	214   	214ST       	1182106	SW  										RADAR ANTENNA	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				RADAR DISH LOOSE AND PICTURE FUSSY AND JUMPS.						2	G	7	2 	4U				H10SW   					 
1999042300101	19990423	00101		1999	4	23	HEEA061689       	4	19990405	G	2312	40008310103	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				EXCESS CLUTTER ON HIGH RANGES.						2	G	7	2 	4U				H10SW   					 
1999042300102	19990423	00102		1999	4	23	HEEA061690       	4	19990405	G	2312	40008310103	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				R/T FAULT DISPLAY.						2	G	7	2 	4U				H10SW   					 
1999042300103	19990423	00103		1999	4	23	HEEA061691       	4	19990405	G	3442	40016702513	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										RADAR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				SCREEN GOES GREEN AFTER 20-30 MINUTES OF OPERATION.  FOUND DISPLAY SPIKES AND TURNS GREEN AFTER 20-30 MINUTES OF OPERATI	ON.					2	G	7	2 	4U				H10SW   					 
1999042300104	19990423	00104		1999	4	23	HEEA061692       	4	19990405	G	2210	4025008918	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				PITCH IS INOPERATIVE.  TIME SINCE REPAIR 37:20 HOURS.						1	G	7	2 	4U				H4SW    					 
1999042300105	19990423	00105		1999	4	23	HEEA061693       	4	19990405	G	2211	4033089901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	FAILS TEST      	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03										COMPUTER FAILS ALTITUDE HOLD TEST STEP 35.5 ON SST.						1	G	7	2 	4U				H4SW    					 
1999042300106	19990423	00106		1999	4	23	HEEA061694       	4	19990405	G	2211	4033089901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	FAILS TEST      	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03										COMPUTER FAILS ALTITUDE HOLD TEST STEP 35.7 AND .7.						1	G	7	2 	4U				H4SW    					 
1999042300107	19990423	00107	SW  	1999	4	23	HEEA061695       	1	19990405	G	6220	412010190103	SPINDLE         			BELL  	412   	412         	1182202	SW  										DAMPER	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T	5928 				33112				SPINDLE SEPARATION ON DAMPER BEARING.						1	G	7	2 	4U				H4SW    					 
1999042300108	19990423	00108	SW  	1999	4	23	HEEA061696       	1	19990405	G	6220	412010190103	SPINDLE         			BELL  	412   	412         	1182202	SW  										DAMPER	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T	5928 				33112				SPINDLE SEPARATION ON DAMPER BEARING.						1	G	7	2 	4U				H4SW    					 
1999042300109	19990423	00109	SW  	1999	4	23	HEEA061697       	1	19990405	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498	11744				36003				OUTBOARD LEADING EDGE STRIP ON BLADE HAD PIN HOLES THROUGH AND EROSION SHIELD TORN AT THE TIP END.						1	G	7	2 	4U				H4SW    					 
1999042300110	19990423	00110	SW  	1999	4	23	HEEA061698       	1	19990405	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	WON'T TRACK     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893L	9902 				33006				UNABLE TO TRACK AND BALANCE BLADE.						1	G	7	2 	4U				H4SW    					 
1999042300111	19990423	00111	SW  	1999	4	23	HEEA061699       	1	19990405	G	6210	412015300109	ABRASION STRIP  			BELL  	412   	412         	1182202	SW  										M/R BLADE	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008	3007 				36004				BOTH LEADING EDGE STRIPS ON BLADE SEPARATED AT THE SPLICE JOINT BEYOND LIMITS.						1	G	7	2 	4U				H4SW    					 
1999042300112	19990423	00112	SW  	1999	4	23	HEEA061700       	1	19990405	G	6210	412015300109	ABRASION STRIP  			BELL  	412   	412         	1182202	SW  										M/R BLADE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008	7102 				36004				OUTBOARD LEADING EDGE ABRASION STRIP ON BLADE CRACKED AT THE SPLICE JOINT.						1	G	7	2 	4U				H4SW    					 
1999042300113	19990423	00113	SW  	1999	4	23	HEEA061701       	1	19990405	G	6210	412015300109	ABRASION STRIP  			BELL  	412   	412         	1182202	SW  										M/R BLADE	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K	10389				33020				OUTBOARD ABRASION STRIP ON BLADE HAS PIN HOLE PENETRATED.						1	G	7	2 	4U				H4SW    					 
1999042300114	19990423	00114	SW  	1999	4	23	HEEA061702       	1	19990405	G	6210	412015300109	DOUBLER         			BELL  	412   	412         	1182202	SW  										M/R BLADE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893L	5754 				33006				TRAILING EDGE DOUBLER ON BLADE HAS THREE CRACKS.  THE LAST CRACK IS 10.75 INCHES FROM THE INBOARD END.						1	G	7	2 	4U				H4SW    					 
1999042300115	19990423	00115	SW  	1999	4	23	HEEA061703       	1	19990405	G	6210	412015300109	ABRASION STRIP  			BELL  	412   	412         	1182202	SW  										M/R BLADE	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K	7697 				33020				OUTBOARD ABRASION STRIP ON BLADE HAS PIN HOLE PENETRATED.						1	G	7	2 	4U				H4SW    					 
1999042300116	19990423	00116	SW  	1999	4	23	HEEA061704       	1	19990405	G	6210	412015300109	ABRASION STRIP  			BELL  	412   	412         	1182202	SW  										M/R BLADE	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K	7642 				33020				OUTBOARD ABRASION STRIP ON BLADE HAS PIN HOLE PENETRATED.						1	G	7	2 	4U				H4SW    					 
1999042300117	19990423	00117	SW  	1999	4	23	HEEA061705       	1	19990405	G	6210	412015300109	ABRASION STRIP  			BELL  	412   	412         	1182202	SW  										M/R BLADE	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K	4856 				33020				OUTBOARD ABRASION STRIP ON BLADE HAS PIN HOLE PENETRATED.						1	G	7	2 	4U				H4SW    					 
1999042300118	19990423	00118		1999	4	23	HEEA061706       	4	19990405	G	3453	4530103	LORAN           			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ARNAV 21 HAD VERY LOW SIGNAL STRENGTH.						1	G	7	1 	3U				H2SW    					 
1999042300119	19990423	00119	SW  	1999	4	23	HEEA061707       	1	19990405	G	2840	473203003	SIGNAL COND     			BELL  	412   	412         	1182202	SW  										FUEL SYSTEM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2149S					36002				LOW LEVEL LIGHT ILLUMINATING WITH 1500 POUNDS OF FUEL INDICATING.						1	G	7	2 	4U				H4SW    					 
1999042300120	19990423	00120	SW  	1999	4	23	HEEA061708       	1	19990405	G	2840	473203003	SIGNAL COND     			BELL  	412   	412         	1182202	SW  										FUEL SYSTEM	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	142PH					33150				SIGNAL CONDITIONER INOPERATIVE IN MID TANKS.						1	G	7	2 	4U				H4SW    					 
1999042300121	19990423	00121	SW  	1999	4	23	HEEA061709       	1	19990405	G	2840	473203003	SIGNAL COND     			BELL  	412   	412         	1182202	SW  										FUEL SYSTEM	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	21498					36003				FUEL LIGHT INTERMITTENT.						1	G	7	2 	4U				H4SW    					 
1999042300122	19990423	00122	SW  	1999	4	23	HEEA061710       	1	19990405	G	2840	473203003	SIGNAL COND     			BELL  	412   	412         	1182202	SW  										FUEL SYSTEM	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	21498					36003				FUEL LIGHT INTERMITTENT.						1	G	7	2 	4U				H4SW    					 
1999042300123	19990423	00123	SW  	1999	4	23	HEEA061711       	1	19990405	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22608					33075				SHOWS ONLY GENERATOR RESIDUAL VOLTAGE.  WILL NOT EXCITE THE GENERATOR FIELD.  CAUSES THE AIRCRAFT VOLTMETER TO BE DRIVEN	 DOWN BELOW ZERO WHEN THE GENERATOR SWITCH IS PLACED IN THE ON POSITION.					1	G	7	2 	4U				H4SW    					 
1999042300124	19990423	00124	SW  	1999	4	23	HEEA061712       	1	19990405	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T					33112				CONTROL UNIT WILL NOT ENGAGE BATTERY RELAY.						1	G	7	2 	4U				H4SW    					 
1999042300125	19990423	00125	SW  	1999	4	23	HEEA061713       	1	19990405	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S					33022				CONTROL UNIT ON BATTERY WILL NOT KICK OFF WHEN SECOND GENERATOR PUT ON LINE.  CANNOT ADJUST VOLTAGE.						1	G	7	2 	4U				H4SW    					 
1999042300126	19990423	00126	SW  	1999	4	23	HEEA061714       	1	19990405	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T					33112				NR 1 GENERATOR WILL NOT COME ON-LINE WHEN NR 2 GENERATOR ON-LINE FIRST.						1	G	7	2 	4U				H4SW    					 
1999042300127	19990423	00127	SW  	1999	4	23	HEEA061715       	1	19990405	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										CONTROL UNIT WILL NOT MAINTAIN VOLTAGE.  SETTING DROPS 2 VOLTS WITH SINGLE GENERATOR ON-LINE.						1	G	7	2 	4U				H4SW    					 
1999042300128	19990423	00128		1999	4	23	HEEA061716       	4	19990405	G	3416	5934D1	ALTIMETER       			BELL  	206   	206L3       	1182108	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251V					51404				ALTIMETER INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999042300129	19990423	00129		1999	4	23	HEEA061717       	4	19990405	G	3425	71252	GYRO            			BELL  	412   	412         	1182202	SW  										HSI	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22347					36005				GYRO INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999042300130	19990423	00130	SW  	1999	4	23	HEEA061718       	1	19990406	G	6320	206040004111	TRANSMISSION    			BELL  	206   	206L1       	1182107	SW  										MAIN ROTOR	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	CP232	18535				45167				DURING 600-HOUR TRANSMISSION OIL CHANGE, DISASSEMBLED FILTER ELEMENT AND NOTED EXCESSIVE AMOUNTS OF FINE METALLIC PARTIC	LES IN THE FIRST STAGE OF THE ELEMENT PAPER.  NO PARTICLES WERE NOTED IN THE FILTER BOWL.  REPLACED FILTER ELEMENT AND S	ERVICED TRANSMISSION WITH NEW OIL.  GROUND RAN AIRCRAFT FOR 30 MINUTES WITH PITCH.  DRAINED OIL AND CHECKED CHIP PLUGS -	 NO DEFECTS NOTED.  REMOVED TRANS FILTER BOWL AND INSPECTED - NO ABNORMALITIES NOTED.			1	G	7	1 	3U				H2SW    					 
1999042300131	19990423	00131	SW  	1999	4	23	HEEA061719       	1	19990406	G	3212	206050248113	FLOAT  ASSY     			BELL  	206   	206L3       	1182108	SW  										MLG	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	6603X					51412				FLOAT BAG HAS RESTRICTION AT INLET VALVE.  FLOAT DID NOT INFLATE FULLY WHEN ELECTRICAL INFLATION WAS PERFORMED.						1	G	7	1 	3U				H2SW    					 
1999042300132	19990423	00132	SW  	1999	4	23	HEEA061720       	1	19990406	G	2435	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										START/GENERATOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M					28102				FOUND DURING 250 HOUR INSPECTION, CLUTCH SLIPS AT ABOVE 500 HOUR INSPECTION AND HAD EXCESSIVE END PLAY.						2	G	7	2 	4U				H10SW   					 
1999042300133	19990423	00133	SW  	1999	4	23	HEEA061721       	1	19990406	G	3340	214175127103	POWER SUPPLY    			BELL  	214   	214ST       	1182106	SW  										STROBE	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	5748M					28102				POWER SUPPLY HAD LOOSE INTERNAL PART.  FLASH TUBE POWER SUPPLY WAS ONE OF THREE TO FAIL THE OPERATION OF ANTI-COLLISION 	SYSTEM.					2	G	7	2 	4U				H10SW   					 
1999042300134	19990423	00134	SW  	1999	4	23	HEEA061722       	1	19990406	G	2435	23046020	STARTER         			BELL  	412   	412         	1182202	SW  										START/GENERATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2149S	15205				36002				STARTER/GENERATOR DRAGS AND WILL NOT START ENGINE.						1	G	7	2 	4U				H4SW    					 
1999042300135	19990423	00135	SW  	1999	4	23	HEEA061723       	1	19990406	G	6220	406012102109	YOKE ASSEMBLY   		407012101105	BELL  	407   	407         		SW  										MAIN ROTORK	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	2255 			53038	53114				FOUND SUPPORT YIELD INDICATOR CLEARANCE DECREASED.  SCRAPPED YOKE ASSY.						1	G	7	1 	3U			O	H2SW    					 
1999042300136	19990423	00136	SW  	1999	4	23	HEEA061724       	1	19990406	G	6210	412015300106	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	WON'T TRACK     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3911L	8308 				33023				UNABLE TO TRACK AND BALANCE BLADE.						1	G	7	2 	4U				H4SW    					 
1999042300137	19990423	00137	SW  	1999	4	23	HEEA061725       	1	19990406	G	6210	412015300106	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	WON'T TRACK     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3911L	8333 				33023				UNABLE TO TRACK MAIN ROTOR BLADE.						1	G	7	2 	4U				H4SW    					 
1999042300138	19990423	00138	SW  	1999	4	23	HEEA061726       	1	19990406	G	6210	412015300106	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	WON'T TRACK     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3911L	5300 				33023				UNABLE TO TRACK MAIN ROTOR BLADE.						1	G	7	2 	4U				H4SW    					 
1999042300139	19990423	00139	SW  	1999	4	23	HEEA061727       	1	19990406	G	3340	6035571	POWER SUPPLY    			BELL  	214   	214ST       	1182106	SW  										STROBE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M					28102				POWER SUPPLY WILL ONLY POWER ONE STROBE LIGHT.   AIRCRAFT HAS TWO LIGHTS.  ONE CONNECTOR IS DEAD.  FLASH RATE IS VERY SL	OW.					2	G	7	2 	4U				H10SW   					 
1999042300140	19990423	00140	SW  	1999	4	23	HEEA061728       	1	19990406	G	6321	94501031	BRAKE ASSY      			BELL  	212   	212         	1181420	SW  										MAIN ROTOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5010F					30936				WHEN ROTOR BRAKE CALIPERS WERE INSTALLED, INBOARD MICROSWITCH CONTACTS ROTOR BRAKE QUILL HOUSING.  INBOARD MICROSWITCH W	AS INSTALLED DIFFERENT ON THIS CALIPER ASSY THAN THE ONE REMOVED.  SCRAPPED SWITCH ASSY ON INBOARD SIDE OF ROTOR BRAKE C	ALIPER.				1	G	7	1 	4U				H4SW    					 
1999042300141	19990423	00141		1999	4	23	HEEA061729       	4	19990406	G	3416	A30	ENCODER         			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50034					45169				WILL NOT GIVE ALT FOAM MILLED AROUND ANALOG BOARD.						1	G	7	1 	3U				H2SW    					 
1999042300142	19990423	00142		1999	4	23	HEEA061730       	4	19990406	G	3416	A30	ENCODER         			BELL  	206   	206B3       	1181506	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2269A					3608				ALTIMETER ENCODER NOT FUNCTIONING.						1	G	7	1 	3U				H2SW    					 
1999042300143	19990423	00143	SW  	1999	4	23	HEEA061731       	1	19990406	G	3340	A490ATSDF	POWER SUPPLY    			BELL  	206   	206L3       	1182108	SW  										STROBE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31073					51519				POWER SUPPLY INOPERATIVE.  LOOSE PARTS INSIDE.  UNIT WAS REPAIRED ON 2-11-98.						1	G	7	1 	3U				H2SW    					 
1999042300144	19990423	00144		1999	4	23	HEEA061732       	4	19990406	G	2350	AA34200	INTERFACE       			BELL  	212   	212         	1181420	SW  										COCKPIT	OUT OF ADJUST   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	27805					31106				UNABLE TO ADJUST SIDETONE.  PERFORMED PRELIMINARY INSPECTION.  FOUND 12VDC POWER SUPPLY BAD.						1	G	7	1 	4U				H4SW    					 
1999042300145	19990423	00145	SW  	1999	4	23	HEEA061733       	1	19990406	G	2430	MS24568D1	RELAY           			BELL  	412   	412         	1182202	SW  										DC SYSTEM	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893L					33006				RELAY ENGAGES INTERMITTENTLY.						1	G	7	2 	4U				H4SW    					 
1999042300146	19990423	00146	SW  	1999	4	23	HEEA061734       	1	19990407	G	2435	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										START/GENERATOR	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	59806					28140				STARTER WOULD NOT STAY ENGAGED.						2	G	7	2 	4U				H10SW   					 
1999042300147	19990423	00147		1999	4	23	HEEA061735       	4	19990407	G	2312	064100900	TRANSCEIVER     			BELL  	212   	212         	1181420	SW  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3131S					30953				CONTACT ON RF BNC BROKEN ON TRANSCEIVER.						1	G	7	1 	4U				H4SW    					 
1999042300148	19990423	00148		1999	4	23	HEEA061736       	4	19990407	G	2312	064102300	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	59805					28141				TRANSCEIVER RECEIVE IS NOISY AND INTERMITTENT, SUSPECT SQUELCH CIRCUIT.  PERFORMED PRELIMINARY INSPECTION AND FOUND TRAN	SMIT POWER SLOWLY DROPS.					2	G	7	2 	4U				H10SW   					 
1999042300149	19990423	00149		1999	4	23	HEEA061737       	4	19990407	G	2312	064102300	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	NOISY           	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	59805					28141				TRANSCEIVER RECEIVES NOISY.						2	G	7	2 	4U				H10SW   					 
1999042300150	19990423	00150		1999	4	23	HEEA061738       	4	19990407	G	3452	066104100	TRANSPONDER     			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2261D					33076				TRANSPONDER WORKED FOR TWO FLIGHTS, THEN WENT BELLY-UP.  NO MODE C, S, ETC.  REPLACED WITH SERVICEABLE PART.						1	G	7	2 	4U				H4SW    					 
1999042300151	19990423	00151		1999	4	23	HEEA061739       	4	19990407	G	2312	064105430	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6610Y					51419				TRANSCEIVER HAD CONSTANT SQUELCH.						1	G	7	1 	3U				H2SW    					 
1999042300152	19990423	00152		1999	4	23	HEEA061740       	4	19990407	G	3452	066106200	TRANSCEIVER     			BELL  	206   	206B3       	1181506	SW  										COCKPIT	BROKEN          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2753F					2729				TRANSCEIVER'S CIRCUIT RUN ON R 477 BROKEN AND RIGHT HAND SIDE RAIL BROKEN.						1	G	7	1 	3U				H2SW    					 
1999042300153	19990423	00153		1999	4	23	HEEA061741       	4	19990407	G	3452	066106200	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3207Q					51540				TRANSCEIVER'S REPLY LIGHT BLINKS CONSTANTLY.						1	G	7	1 	3U				H2SW    					 
1999042300154	19990423	00154		1999	4	23	HEEA061742       	4	19990407	G	3452	066106200	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5744Y					45465				ATC REPORTS WRONG NUMBERS BEING TRANSMITTED.   PERFORMED PRELIMINARY INSPECTION AND FOUND REPLY LIGHT BLINKING, ALT. COD	ING INFORMATION WRONG AND OFF FREQUENCY.					1	G	7	1 	3U				H2SW    					 
1999042300155	19990423	00155		1999	4	23	HEEA061743       	4	19990407	G	2312	066106600	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	33008					36004				POWER AND SENSITIVITY BAD ON HIGH END OF BAND.						1	G	7	2 	4U				H4SW    					 
1999042300156	19990423	00156		1999	4	23	HEEA061744       	4	19990407	G	3452	066107100	TRANSPONDER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6957Y					28139				TRANSPONDER TRANSMITS AND RECEIVES WEAK.						2	G	7	2 	4U				H10SW   					 
1999042300157	19990423	00157		1999	4	23	HEEA061745       	4	19990407	G	3431	066107800	RECEIVER        			BELL  	230   	230         	1182149	SW  										COCKPIT	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	230UN					23009				VHF NAVIGATOR RECEIVER INTERMITTENT.						1	G	7	2 	3U			NC	H9SW    					 
1999042300158	19990423	00158		1999	4	23	HEEA061746       	4	19990407	G	3444	066305401	ALTIMETER       			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	8591X					51495				NO INDICATION ABOVE 480 FEET.  PERFORMED PRELIMINARY INSPECTION AND FOUND BEZEL CRACKED.						1	G	7	1 	3U				H2SW    					 
1999042300159	19990423	00159	SW  	1999	4	23	HEEA061747       	1	19990408	G	6510	406340339103	BEARING         			BELL  	407   	407         		SW  										NR 1	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	382  				53114				TAIL ROTOR DRIVESHAFT HAD NR 1 BEARING FAILURE.  SERIAL NUMBERS REMOVED ARE K98-0778 AND K98-0786.  REPLACEMENT PART SER	IAL NUMBERS ARE H98-2271 AND H98-2327.					1	G	7	1 	3U			O	H2SW    					 
1999042300160	19990423	00160	SW  	1999	4	23	HEEA061748       	1	19990408	G	6510	406040320101	SHAFT           			BELL  	407   	407         		SW  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				FOUND OVERHEATING MARK ON BEARING JOURNAL.						1	G	7	1 	3U			O	H2SW    					 
1999042300161	19990423	00161	SW  	1999	4	23	HEEA061749       	1	19990408	G	6510	206061432117	BLOWER          			BELL  	407   	407         		SW  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				MECHANICAL DAMAGE DUE TO BALLS FROM BEARING STRIKING IMPELLER.						1	G	7	1 	3U			O	H2SW    					 
1999042300162	19990423	00162		1999	4	23	HEEA061750       	4	19990408	G	3454	066400702	RECEIVER        			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893S					33022				RMI WILL NOT ALIGN.						1	G	7	2 	4U				H4SW    					 
1999042300163	19990423	00163		1999	4	23	HEEA061751       	4	19990408	G	3444	071111401	ANTENNA         			BELL  	206   	206L3       	1182108	SW  										RADAR ALTIMETER	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8593X					51509				ANTENNA HAD CORROSION ON BASE AND WAS SWOLLEN.  UNIT SCRAPPED.						1	G	7	1 	3U				H2SW    					 
1999042300164	19990423	00164		1999	4	23	HEEA061752       	4	19990408	G	3442	071111401	WIRE            			BELL  	206   	206L1       	1182107	SW  										RADAR ANTENNA	MISSING         	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	5744Y					45465				ANTENNA DOESN'T HAVE CALIBRATED CABLE ATTACHED.  UNIT SCRAPPED.						1	G	7	1 	3U			 	H2SW    					 
1999042300165	19990423	00165	SW  	1999	4	23	HEEA061753       	1	19990408	G	5330	214021211113S	SKIN            			BELL  	214   	214ST       	1182106	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	6957Y					28139				PANEL MISMANUFACTURED.  FORWARD INBOARD EDGE OF PANEL IS TOO SHORT BY A MINIMUM OF .3750 INCH AND ADDED DOUBLER AT CENTE	R IS TOO SHORT; ALSO, AS MARKED ON PANEL.					2	G	7	2 	4U				H10SW   					 
1999042300166	19990423	00166	SW  	1999	4	23	HEEA061754       	1	19990408	G	2400	163404731	VOLT REGULATOR  			BELL  	206   	206L3       	1182108	SW  										DC SYSTEM	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3207Q					51540				VOLTAGE REGULATAOR DROPS OFF-LINE WHEN RADIO IS KEYED.						1	G	7	1 	3U				H2SW    					 
1999042300167	19990423	00167	SW  	1999	4	23	HEEA061755       	1	19990408	G	6510	206040370105	SHAFT           			BELL  	206   	206L3       	1182108	SW  										T/R DRIVE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	6603X	1873 				51412				LEFT AFT NUTPLATE ON AFT SIDE OF NR 2 SHAFT BLOWER HOUSING ASSY LOCATED IN WRONG POSITION.   OIL COOLER DUCT WILL NOT LI	NE UP.					1	G	7	1 	3U				H2SW    					 
1999042300168	19990423	00168	SW  	1999	4	23	HEEA061756       	1	19990408	G	6510	206040370105	SHAFT           			BELL  	206   	206L3       	1182108	SW  										T/R DRIVE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	6603X					51412				MOUNTING BRACKET IS LOCATED ABOUT .1250 OF AN INCH OFF THE AIRCRAFT MOUNTING INSERT.  THIS CAUSES THE HOUSING TO BE PUT 	UNDER A PRELOAD WHEN INSTALLED ON THIS AIRCRAFT.					1	G	7	1 	3U				H2SW    					 
1999042300169	19990423	00169	SW  	1999	4	23	HEEA061757       	1	19990408	G	7120	206062102013	LEG ASSY        			BELL  	206   	206B3       	1181506	SW  										ENGINE MOUNT	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	103PH					3000				LEG ASSEMBLY HAD CORROSION PITS BEYOND LIMITS.  REPLACED WITH SERVICEABLE PARTS.						1	G	7	1 	3U				H2SW    					 
1999042300170	19990423	00170	SW  	1999	4	23	HEEA061758       	1	19990408	G	3210	206324007	SKID            			BELL  	206   	206L3       	1182108	SW  										MLG	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251Y					51556				SKID TUBE HAD EXCESSIVE INTERGRANULAR CORROSION.  SCRAPPED AND REPLACED WITH SERVICEABLE SKID TUBE.						1	G	7	1 	3U				H2SW    					 
1999042300171	19990423	00171	SW  	1999	4	23	HEEA061759       	1	19990408	G	3210	206324008	SKID            			BELL  	206   	206L3       	1182108	SW  										MLG	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251Y					51556				SKID TUBE HAD EXCESSIVE INTERGRANULAR CORROSION.  SCRAPPED AND REPLACED WITH SERVICEABLE SKID TUBE.						1	G	7	1 	3U				H2SW    					 
1999042300172	19990423	00172	SW  	1999	4	23	HEEA061760       	1	19990408	G	7722	206375007103	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT TOT	STICKING        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5005B					45175				TOT INDICATION NEEDLE DOES NOT MOVE ON START.						1	G	7	1 	3U				H2SW    					 
1999042300173	19990423	00173	SW  	1999	4	23	HEEA061761       	1	19990408	G	5230	206513211	ACTUATOR        			BELL  	407   	407         		SW  										CARGO DOOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				ACTUATOR WILL NOT EXTEND.  SCRAPPED.						1	G	7	1 	3U			O	H2SW    					 
1999042300174	19990423	00174	SW  	1999	4	23	HEEA061762       	1	19990408	G	6730	212076005101	SERVO           			BELL  	412   	412         	1182202	SW  										CYCLIC	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893N	6547 				33010				WHILE INSTALLING ROD END ON SERVO, ROD END SEIZED UP, UNABLE TO REMOVE ROD END WITHOUT DAMAGING SERVO.  REPLACED WITH SE	RVICEABLE PART.					1	G	7	2 	4U				H4SW    					 
1999042300175	19990423	00175	SW  	1999	4	23	HEEA061763       	1	19990408	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										FLIGHT CONTROL	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	21498					36003				ROTARY ACTUATOR WILL NOT DISENGAGE.						1	G	7	2 	4U				H4SW    					 
1999042300176	19990423	00176	SW  	1999	4	23	HEEA061764       	1	19990408	G	3212	214073929107	VALVE           			BELL  	214   	214ST       	1182106	SW  										FLOAT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	824H					28119				SOLENOID VALVE OPENED WHILE SERVICING FLOAT BOTTLE.						2	G	7	2 	4U				H10SW   					 
1999042300177	19990423	00177	SW  	1999	4	23	HEEA061765       	1	19990408	G	3212	214073929107	VALVE           			BELL  	214   	214ST       	1182106	SW  										FLOAT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	824H					28119				SOLENOID VALVE OPENED WHILE SERVICING FLOAT BOTTLE.						2	G	7	2 	4U				H10SW   					 
1999042300178	19990423	00178	SW  	1999	4	23	HEEA061766       	1	19990408	G	2432	214175379103	BATTERY CHARGER 			BELL  	214   	214ST       	1182106	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	59805					28141				NR 2 BATTERY CHARGER MONITOR TRIPS OFF.						2	G	7	2 	4U				H10SW   					 
1999042300179	19990423	00179	GL  	1999	4	23	HEEA061767       	2	19990408	G	7320	23065805	HARNESS         			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					FADEC	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	407MM					53060				FADEC DEGRADE AND RESTART FAULT LIGHTS ON.  REPLACED WITH SERVICEABLE HARNESS.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999042300180	19990423	00180	GL  	1999	4	23	HEEA061768       	2	19990408	G	7320	23065805	HARNESS         			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					FADEC	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	722PH					53288				FADEC DEGRADE LIGHT ON AFTER SHUTDOWN.   COMPUTER SHOWED TORQUE TRANSMITTER PROBLEM FOUND IN FADEC HARNESS.   REPLACED W	ITH SERVICEABLE HARNESS.					1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999042300181	19990423	00181	GL  	1999	4	23	HEEA061769       	2	19990408	G	7320	23065805	HARNESS         			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					FADEC	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	408PH					53228				APPROXIMATELY 55 MINUTES INTO FLIGHT, FADEC HAD NPQ EXCEEDENCE.  ECU AND HMU REPLACED 9-13-98.  REPLACED WITH SERVICEABL	E HARNESS.					1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999042300182	19990423	00182	GL  	1999	4	23	HEEA061770       	2	19990408	G	7323	252469211	GOVERNOR        			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			CR	CRUISE         	1			SW	03	5005B	3791 				45175				AT CRUISE FLIGHT, 80 PERCENT TORQUE, TORQUE OSCILLATES 20 PERCENT, WITH A CORRESPONDING TOT OSCILLATION.  REPLACED WITH 	SERVICEABLE GOVERNOR.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999042300183	19990423	00183	GL  	1999	4	23	HEEA061771       	2	19990408	G	7321	252473834	FCU             			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	LEAKING         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2772A	14193				45311				FUEL CONTROL LEAKING OUT START DERICH SHAFT AND BYPASS COVER.  PERFORMED PRELIMINARY INSPECTION.  TEST START DERICH FUNC	TION AND FOUND NO LEAKAGE FROM THE SHAFT.  BENCH TEST AND FOUND NO LEAKAGE FROM BYPASS COVER OR START DERICH WHEN TESTED	 ON THE FLOW BENCH.   COULD NOT DUPLICATE PROBLEM AS STATED.				1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999042300184	19990423	00184	SW  	1999	4	23	HEEA061772       	1	19990408	G	2432	3055401C	BATTERY         			BELL  	206   	206L1       	1182107	SW  										BATTERY BOX	DISCHARGED      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5012V					45200				BATTERY WOULD NOT START AIRCRAFT, NOR WOULD IT TAKE CHARGE AFTER BEING STARTED.  REPLACED WITH SERVICEABLE BATTERY.						1	G	7	1 	3U				H2SW    					 
1999042300185	19990423	00185	GL  	1999	4	23	HEEA061773       	2	19990408	G	7314	3881005	PUMP            			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C20B     	03013	GL  					FUEL SYSTEM	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1076Y					45380				PERFORMED SPLINE INSPECTION AND FOUND WORN DRIVE SPLINES FUEL PUMP.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999042300186	19990423	00186		1999	4	23	HEEA061774       	4	19990408	G	2312	4000103000	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5744Y					45465				TRANSCEIVER HAD INTERMITTENT OPERATION, WILL NOT TRANSMIT OR RECEIVE INTERMITTENT.  PERFORMED PRELIMINARY INSPECTION AND	 FOUND MAIN R/T BOARD CHASIS BROKEN AND SIDETONE ERRATIC.					1	G	7	1 	3U				H2SW    					 
1999042300187	19990423	00187		1999	4	23	HEEA061775       	4	19990408	G	3442	40005040301	DRIVE ASSY      			BELL  	214   	214ST       	1182106	SW  										RADAR ANTENNA	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	59806					28140				DRIVE ASSEMBLY INOPERATIVE; SMOKED.						2	G	7	2 	4U				H10SW   					 
1999042300188	19990423	00188		1999	4	23	HEEA061776       	4	19990408	G	3442	40005040301	DRIVE ASSY      			BELL  	214   	214ST       	1182106	SW  										RADAR ANTENNA	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				ALLEN SCREWS LOOSE AND SHOCK MOUNTS NEED TO BE REPLACED.						2	G	7	2 	4U				H10SW   					 
1999042300189	19990423	00189		1999	4	23	HEEA061777       	4	19990408	G	3442	40008310105	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	59805					28141				RADAR SKIPPING.						2	G	7	2 	4U				H10SW   					 
1999042300190	19990423	00190		1999	4	23	HEEA061778       	4	19990408	G	2210	4025008918	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	OSCILLATES      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5759N					33002				COMPUTER PRODUCES OSCILLATION.						1	G	7	2 	4U				H4SW    					 
1999042300191	19990423	00191		1999	4	23	HEEA061779       	4	19990408	G	3460	5205160006	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	DAMAGED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	23023					33080				CSI HAD LOOSE INTERNAL PART.  TIGHTENED 3 EACH LOOSE SCREWS.  REPAIRED.  ALSO ADJUSTED RESOLVER AND VOR/LOC METER NEEDLE	 MOVEMENT.  BENCH CHECK GOOD.					1	G	7	2 	4U				H4SW    					 
1999042300192	19990423	00192	SW  	1999	4	23	HEEA061780       	1	19990408	G	3210	412050015109	SKID            			BELL  	412   	412         	1182202	SW  										MLG	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										SKID TUBE RIPPLED NEAR FORWARD SADDLE AT LOWER PART OF TUBE AT BEND.						1	G	7	2 	4U				H4SW    					 
1999042300193	19990423	00193	SW  	1999	4	23	HEEA061781       	1	19990408	G	5512	206023119151	SKIN            			BELL  	206   	206L3       	1182108	SW  										HORIZONTAL STAB	MISMANUFACTURED 	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31077					51520				STABILIZER MISMANUFACTURED.  COULD NOT INSTALL TAILBOOM SUPPORT PANELS DUE TO WHAT APPEARS TO BE A TWIST IN STABILIZER M	ANUFACTURE WITH ONE UPPER SIDE ATTACHED, OTHER SIDE BOLT HOLES APPROXIMATELY .50 INCH MISALIGNED ON ONE END.					1	G	7	1 	3U				H2SW    					 
1999042300194	19990423	00194	EU  	1999	4	23	HEEA061782       	1	19990405	G	2435	23032048	STARTER         			BOLKMS	105   	BO105S      	5626006	EU  										START/GENERATOR	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4302G					S853				STARTER/GENERATOR WILL NOT CRANK ENGINE.						1	G	7	2 	3U				H3EU    					 
1999042300195	19990423	00195	EU  	1999	4	23	HEEA061783       	1	19990405	G	2435	23032048	STARTER         			BOLKMS	105   	BO105S      	5626006	EU  										START/GENERATOR	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911HM	14310				S683				STARTER/GENERATOR HAD SLOW STARTS.						1	G	7	2 	3U				H3EU    					 
1999042300196	19990423	00196	EU  	1999	4	23	HEEA061784       	1	19990405	G	6420	350A33211904	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										T/R HEAD	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				HUB BEARINGS WORN.  CAUSED TAIL ROTOR TO BE OUT OF BALANCE.  REPLACED WITH SERVICEABLE TAIL ROTOR ASSY.						1	G	7	1 	3U				H9EU    					 
1999042300197	19990423	00197		1999	4	23	HEEA061785       	4	19990405	G	2312	4000106010	CONTROL         			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT VHF	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911PF					S718				RECEIVE/TRANSMIT SWITCH BROKEN ON CONTROL UNIT.						1	G	7	2 	3U				H3EU    					 
1999042300198	19990423	00198		1999	4	23	HEEA061786       	4	19990405	G	2312	4000106010	CONTROL         			BOLKMS	117   	BK117B2     	5626013	EU  										COCKPIT VHF	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	134AE					7237				DIGITS OF LED DISPLAY CHANGE WITH VIBRATION IF FACE PLATE IS PRESSED.  PERFORMED PRELIMINARY INSPECTION AND FOUND BROKEN	 WIRE, REPAIRED WIRE, CLEANED THUMBWHEEL NO HELP.  UNIT AUDIO CUTTING OUT ON ALL CHANNELS.					1	G	7	2 	3U			NC	H13EU   					 
1999042300199	19990423	00199		1999	4	23	HEEA061787       	4	19990405	G	2312	40001278500	TRANSCEIVER     			BOLKMS	117   	BK117B2     	5626013	EU  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	134AE					7237				TRANSCEIVER HAD INTERMITTENT OPERATION.  PERFORMED PRELIMINARY INSPECTION AND FOUND UNIT HAS NO TONE DEVIATION AND NO CT	CSS TONES.					1	G	7	2 	3U			NC	H13EU   					 
1999042300200	19990423	00200		1999	4	23	HEEA061788       	4	19990405	G	2312	40001452500	RECEIVER        			BOLKMS	105   	BO105CBS    	5626008	EU  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RS					S670				TRANSPONDER WILL NOT TRANSMIT OR RECEIVE.						1	G	7	2 	3U			NC	H3EU    					 
1999042300201	19990423	00201	EU  	1999	4	23	HEEA061789       	1	19990405	G	6520	4619002003	CASE            			BOLKMS	105   	BO105S      	5626006	EU  										T/R GEARBOX	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	135AE	2708 				S838				TAIL ROTOR GEARBOX CORRODED ON CASE ASSEMBLY.						1	G	7	2 	3U				H3EU    					 
1999042300202	19990423	00202		1999	4	23	HEEA061790       	4	19990405	G	3416	5035P2P42	ALTIMETER       			BOLKMS	117   	BK117A4     	5626017	EU  										COCKPIT	INACURATE       	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	8765J					7054				ALTITUDE INFO WAS INCORRECT ON 600 TEST SET.						1	G	7	2 	3U				H13EU   					 
1999042300203	19990423	00203	EU  	1999	4	23	HEEA061791       	1	19990406	G	6410	10531980	BLADE           		10531713    	BOLKMS	105   	BO105S      	5626006	EU  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8199J	2551 			050235	S826				TIP OF TAIL ROTOR BLADE DAMAGED.						1	G	7	2 	3U				H3EU    					 
1999042300204	19990423	00204		1999	4	23	HEEA061792       	4	19990406	G	2340	AA20030	AMPLIFIER       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5031U					S678				PA AMP INOPERATIVE.  NO OUTPUT.						1	G	7	2 	3U				H3EU    					 
1999042300205	19990423	00205	EU  	1999	4	23	HEEA061793       	1	19990406	G	3150	AA22110	CONTROL         			BOLKMS	105   	BO105S      	5626006	EU  										PA SIREN	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	137AE					S851				BROKEN VOLUME KNOB.						1	G	7	2 	3U				H3EU    					 
1999042300206	19990423	00206		1999	4	23	HEEA061794       	4	19990406	G	2350	AA95758	AUDIO CONTROL   			BOLKMS	105   	BO105CBS    	5626008	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RS					S670				AUDIO CONTROL AMPLIFIES NOISE IN HEADSETS.  PERFORMED PRELIMINARY INSPECTION.  FOUND UNIT TO DRAW EXCESSIVE CURRENT WHEN	 ALERTING IS TURNED ON.					1	G	7	2 	3U			NC	H3EU    					 
1999042300207	19990423	00207		1999	4	23	HEEA061795       	4	19990406	G	2340	ACS775SL	AUDIO CONTROL   			BOLKMS	117   	BK117A4     	5626017	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RZ					7092				AUDIO CONTROL HAD NO ICS VOLUME CONTROL.						1	G	7	2 	3U				H13EU   					 
1999042300208	19990423	00208		1999	4	23	HEEA061796       	4	19990406	G	2340	AMS41A	AUDIO CONTROL   			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	86CH					S557				NO RECEPTION ON HEADSETS.  PERFORMED PRELIMINARY INSPECTION AND FOUND SIDETONE LEVEL WEAK AND COULD NOT BE ADJUSTED TO M	FG SPECS.					1	G	7	2 	3U				H3EU    					 
1999042300209	19990423	00209	EU  	1999	4	23	HEEA061797       	1	19990406	G	2844	BSE206150G3	TRANSDUCER      			BOLKMS	105   	BO105S      	5626006	EU  										FUEL SYSTEM	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	624MB					S751				TRANSDUCER INDICATES HIGH OIL PRESSURE.						1	G	7	2 	3U				H3EU    					 
1999042300210	19990423	00210	EU  	1999	4	23	HEEA061798       	1	19990406	G	2822	D105102	BOOST PUMP      			BOLKMS	105   	BO105S      	5626006	EU  										FUEL SYSTEM	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3071K					S859				FUEL PUMP HAD INTERNAL LEAKAGE.						1	G	7	2 	3U				H3EU    					 
1999042300211	19990423	00211	EU  	1999	4	23	HEEA061799       	1	19990406	G	2822	D107318D1	BOOST PUMP      			BOLKMS	105   	BO105S      	5626006	EU  										FUEL SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6607K	4169 				S841				FUEL PUMP ASSY PUTS OUT LOW PRESSURE.						1	G	7	2 	3U				H3EU    					 
1999042300212	19990423	00212	EU  	1999	4	23	HEEA061800       	1	19990406	G	3212	D24762102	FLOAT           			BOLKMS	105   	BO105S      	5626006	EU  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	8199J					S826				FLOAT BAGS LEAKING.						1	G	7	2 	3U				H3EU    					 
1999042300213	19990423	00213	EU  	1999	4	23	HEEA061801       	1	19990406	G	7714	DL4044	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										TRIPLE TACH	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4302G					S853				NR 1 NEEDLE READS APPROXIMATELY 3 PERCENT HIGHER THAN NR 2 AND DOESN'T RETURN TO ZERO.  TIME SINCE REPAIR 0:00 HOURS.						1	G	7	2 	3U				H3EU    					 
1999042300214	19990423	00214	EU  	1999	4	23	HEEA061802       	1	19990406	G	7714	DL41239	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50293					S677				RPM INDICATION NEEDLES STICKING AND FLUCTUATING.						1	G	7	2 	3U				H3EU    					 
1999042300215	19990423	00215	EU  	1999	4	23	HEEA061803       	1	19990406	G	7712	DK50439	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										DUAL TORQUE	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3071K					S859				TORQUE INDICATOR'S NR 2 NEEDLE READING 4 PERCENT LOW.						1	G	7	2 	3U				H3EU    					 
1999042300216	19990423	00216		1999	4	23	HEEA061804       	4	19990406	G	2562	ELT910	ELT             			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6607K					S841				ELT ACTIVATES INTERMITTENTLY IN-FLIGHT.						1	G	7	2 	3U				H3EU    					 
1999042300217	19990423	00217		1999	4	23	HEEA061805       	4	19990407	G	2350	066105571	AUDIO PANEL     			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3071K					S859				COMM 3 POSITION HAS HOT MIKE.						1	G	7	2 	3U				H3EU    					 
1999042300218	19990423	00218		1999	4	23	HEEA061806       	4	19990407	G	3425	066304604	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4294R					S860				NAVIGATOR FLAG WOULD NOT STOW.						1	G	7	2 	3U				H3EU    					 
1999042300219	19990423	00219		1999	4	23	HEEA061807       	4	19990408	G	2312	069102525	NAV COMM        			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	8199J					S826				VOLUME CONTROL IS WEAK AND INTERMITTENT.						1	G	7	2 	3U				H3EU    					 
1999042300220	19990423	00220	EU  	1999	4	23	HEEA061808       	1	19990408	G	2930	1152014	SIGNAL COND     			BOLKMS	117   	BK117A4     	5626017	EU  										NR 2 HYD SYSTEM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	8765J					7054				COULD NOT ADJUST UP PRESSURE ON SIGNAL CONDITION, SYSTEM NR 2.						1	G	7	2 	3U				H13EU   					 
1999042300221	19990423	00221		1999	4	23	HEEA061809       	4	19990408	G	3457	13824120234	GPS RECEIVER    			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6097Z					2820				GPS RECEIVER WILL NOT COME ON WHEN POWER APPLIED.						1	G	7	1 	3U				H9EU    					 
1999042300222	19990423	00222		1999	4	23	HEEA061810       	4	19990408	G	2312	40001452500	RECEIVER        			BOLKMS	117   	BK117A3     	5626015	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911NC					7026				AFTER WARM-UP, THERE IS CONSTANT FEEDBACK.						1	G	7	2 	3U				H13EU   					 
1999042300223	19990423	00223	EU  	1999	4	23	HEEA061811       	1	19990408	G	2844	4021001	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										DUAL FUEL PRESS	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3071K					S859				FUEL PRESSURE INDICATION HAD ONLY 3 VOLTS OUTPUT ON PIN E.						1	G	7	2 	3U				H3EU    					 
1999042300224	19990423	00224	EU  	1999	4	23	HEEA061812       	1	19990408	G	2436	51565000R	REGULATOR       			BOLKMS	105   	BO105S      	5626006	EU  										DC SYSTEM	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	9190Y					S669				UNABLE TO ADJUST VOLTAGE ON VOLTAGE REGULATOR.						1	G	7	2 	3U				H3EU    					 
1999042300225	19990423	00225	EU  	1999	4	23	HEEA061813       	1	19990408	G	7714	AG44A202	TACH GENERATOR  			BOLKMS	105   	BO105S      	5626006	EU  										ENGINE	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	818SH					S753				NO RPM INDICATION.  TESTED TACHOMETER GENERATOR AND FOUND NO PROBLEM WITH UNIT.						1	G	7	2 	3U				H3EU    					 
1999042300226	19990423	00226	EU  	1999	4	23	HEEA061814       	1	19990408	G	6520	350A33020005	GEARBOX         			SNIAS 	350   	AS350B2     	8680813	EU  										T/R SPIDER	SEIZED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6095S	3462 				2777				TAIL ROTOR SPIDER BEARING SEIZED.   ASSEMBLY THEN BROKE AT PIPE.						1	G	7	1 	3U				H9EU    					 
1999050700208	19990507	00208	GL  	1999	5	7	HEEA061872       	2	19990423	G	7250	23031938	NOZZLE          		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					NR 1 ENGINE	CRACKED         	E			HEEA	E	A			ENGINE SHUTDOWN         	UNSCHED LANDING         			R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		CR	CRUISE         	1			SW	03	8197X				CAT33566	S808	CAE820965F			PILOT HEARD LOUD BANG WHILE IN CRUISE FLIGHT, SECURED NR 1 ENGINE AND MADE SINGLE ENGINE LANDING.  N1 AND N2 LOCKED DUE 	TO GP ROTOR FAILURE.  SUSPECTED CAUSE WAS NR 2 NOZZLE DIAPHRAGM CRACKED 360 DEGREES AROUND, MOVING FORWARD CONTACTING NR	 2 WHEEL CAUSING F.O.D. DAMAGE FROM NR 1 WHEEL TO EXHAUST COLLECTOR.  PART WAS OVERHAULED ON WORK ORDER NR LF3242.   NR 	2 NOZZLE, NR 1 NOZZLE, SHIELD, NR 1 AND NR 2 WHEELS SHIPPED FOR FAILURE INVESTIGATION.			1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999050700209	19990507	00209	GL  	1999	5	7	HEEA061873       	2	19990423	G	7261	23031461	PUMP            		23035179    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					SCAVENGER	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911MJ	5910 			CAG90525	760231	CAE890522S			ENGINE REMOVED DUE TO SUSPECTED SCAVENGE PUMP FAILURE.  OIL PUMP SCAVENGE BODY HAD EXCESSIVELY WORN GEAR WALLS.  O-RINGS	 WERE FLAT AND HARD, OIL PUMP GEARSHAFTS HAVE EXCESSIVE GROOVES AND WEAR CONTRIBUTING TO POOR SCAVENGE.  PART SCRAPPED.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999050700210	19990507	00210	SW  	1999	5	7	HEEA061874       	1	19990413	G	2434	214175150105	GENERATOR       			BELL  	214   	214ST       	1182106	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	824H					28119				GENERATOR WILL NOT HOLD VOLTAGE SETTING.						2	G	7	2 	4U				H10SW   					 
1999050700211	19990507	00211	SW  	1999	5	7	HEEA061875       	1	19990416	G	2435	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										START/GENERATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				ENGINE COG DISINTEGRATED.						2	G	7	2 	4U				H10SW   					 
1999050700212	19990507	00212	SW  	1999	5	7	HEEA061877       	1	19990423	G	2435	206062200113	STARTER         			BELL  	407   	407         		SW  										START/GENERATOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	722PH	575  				53288				FAILED 300 HOUR INSPECTION.  INSPECTED AND FOUND BRUSHES EXCESSIVELY WORN AND COMMUTATOR WAS GROOVED ON STARTER.						1	G	7	1 	3U			O	H2SW    					 
1999052100127	19990521	00127	GL  	1999	5	21	HEEA062135       	2	19990503	G	7261	23052360	PUMP            		23035179    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					ENGINE OIL	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	521AC				CAG90762	760261	CAE890754			NEW PART RECEIVING INSPECTION REVEALED OIL PUMP PRESSURE BODY CAGE HEIGHT BELOW SPECS.  REFERENCE:  AFA NR 41388A.						1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999052100128	19990521	00128	GL  	1999	5	21	HEEA062136       	2	19990503	G	7261	23052360	PUMP            		23035179    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					ENGINE OIL	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	1545K				CAG90472	760047	CAE890469S			IMPROPER CAGE INSTALLED IN OIL PUMP PRESSURE BODY.  REVEALED DURING RECEIVING INSPECTION.    REFERENCE:  AFA NR 41389A.						1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999052100129	19990521	00129	SW  	1999	5	21	HEEA062137       	1	19990429	G	6310	406040500123B	FREEWHEEL UNIT  			BELL  	407   	407         		SW  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	402PH	696  				53159				FREE WHEEL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999052100130	19990521	00130	SW  	1999	5	21	HEEA062138       	1	19990429	G	6310	406340102101	CARBON SEAL     		406040500123	BELL  	407   	407         		SW  										FREEWHEEL	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	447PH				A3277	53114				CARBON SEAL LEAKING.  PART SCRAPPED.						1	G	7	1 	3U			O	H2SW    					 
1999052100131	19990521	00131	SW  	1999	5	21	HEEA062139       	1	19990429	G	5320	206064902027	ANGLE           			BELL  	206   	206L3       	1182108	SW  										FIREWALL	MISMARKED       	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	31073					51519				MISIDENTIFIED.  AFT FIREWALL ANGLES:  FORWARD AND AFT ANGLE PART NUMBERS ARE SWITCHED.  IF THE FORWARD ANGLES ARE ORDERE	D, WILL RECEIVE THE AFT ANGLES.					1	G	7	1 	3U				H2SW    					 
1999052100132	19990521	00132	SW  	1999	5	21	HEEA062140       	1	19990429	G	5320	206064902028S	ANGLE           			BELL  	206   	206L3       	1182108	SW  										FIREWALL	MISMARKED       	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	31073					51519				MISIDENTIFIED.  AFT FIREWALL ANGLES:  FORWARD AND AFT ANGLE PART NUMBERS ARE SWITCHED.  IF FORWARD ANGLES ARE ORDERED, W	ILL RECEIVE THE AFT ANGLES.					1	G	7	1 	3U				H2SW    					 
1999052100133	19990521	00133	EU  	1999	5	21	HEEA062142       	1	19990430	G	6410	355A12004008	BLADE           			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	DAMAGED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4000L	2881 				2873				BONDING STRAP SEPARATED ON LEADING EDGE, LAMINATED BEARING HALF SEPARATED.						1	G	7	1 	3U				H9EU    					 
1999052100134	19990521	00134	EU  	1999	5	21	HEEA062143       	1	19990430	G	6410	355A12004008	BLADE           			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	40466	3120 				3004				HALF MOON BEARING PIN HOLE WORN ON SPAR MOUNTING FLANGE AND SPAR CRACKED ON OUTBOARD SIDE OF NON-TARGET BLADE.						1	G	7	1 	3U				H9EU    					 
1999052100135	19990521	00135	EU  	1999	5	21	HEEA062145       	1	19990430	G	2435	150SG122Q	STARTER         			SNIAS 	350   	AS350B2     	8680813	EU  										START/GENERATOR	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	60951					2771				STARTER/GENERATOR WOULD NOT START.						1	G	7	1 	3U				H9EU    					 
1999052100136	19990521	00136	EU  	1999	5	21	HEEA062147       	1	19990430	G	2435	150SG122Q	GENERATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										START/GENERATOR	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4000L					2873				INTERFERENCE IN FLEX COM FM RADIO.						1	G	7	1 	3U				H9EU    					 
1999052100137	19990521	00137	EU  	1999	5	21	HEEA062148       	1	19990505	G	7930	646600251	PROBE           			SNIAS 	350   	AS350B2     	8680813	EU  										OIL TEMPERATURE	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350BZ					2653				WHEN PROBE GETS HOT, TEMPERATURE GAUGE ENABLES, JUMPS AROUND.						1	G	7	1 	3U				H9EU    					 
1999052100138	19990521	00138	EU  	1999	5	21	HEEA062149       	1	19990505	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				PITCH ROD HAS WORN BEARINGS.						1	G	7	1 	3U				H9EU    					 
1999052100139	19990521	00139	EU  	1999	5	21	HEEA062150       	1	19990505	G	2510	504305401	INERTIA REEL    			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				INERTIA REEL WILL NOT LOCK.						1	G	7	1 	3U				H9EU    					 
1999052100140	19990521	00140	EU  	1999	5	21	HEEA062151       	1	19990505	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6100R					2862				PITCH ROD HAS WORN BEARING.						1	G	7	1 	3U				H9EU    					 
1999052100141	19990521	00141	EU  	1999	5	21	HEEA062152       	1	19990505	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z					2820				PITCH ROD HAS PLAY IN BEARINGS.						1	G	7	1 	3U				H9EU    					 
1999052100142	19990521	00142	EU  	1999	5	21	HEEA062153       	1	19990505	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z					2820				PITCH ROD HAS PLAY IN BEARINGS.						1	G	7	1 	3U				H9EU    					 
1999052100143	19990521	00143	EU  	1999	5	21	HEEA062154       	1	19990505	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				PITCH ROD HAS WORN BEARINGS.						1	G	7	1 	3U				H9EU    					 
1999052100144	19990521	00144	EU  	1999	5	21	HEEA062155       	1	19990505	G	7160	350A54108004	SUPPORT         			SNIAS 	350   	AS350B2     	8680813	EU  										INTAKE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				CRACK AROUND BOTTOM SUPPORT BOLT AREA.						1	G	7	1 	3U				H9EU    					 
1999052100145	19990521	00145	EU  	1999	5	21	HEEA062156       	1	19990505	G	3340	31031	LIGHT           			SNIAS 	350   	AS350B2     	8680813	EU  										FUSELAGE	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z					2820				MOUNTING SCREW HOLES ENLARGED, CAN'T SECURE LIGHT.						1	G	7	1 	3U				H9EU    					 
1999052100146	19990521	00146	EU  	1999	5	21	HEEA062157       	1	19990505	G	6420	350A33211905	HUB             			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				TAIL ROTOR HAS PLAY IN BEARINGS.						1	G	7	1 	3U				H9EU    					 
1999052100147	19990521	00147	EU  	1999	5	21	HEEA062158       	1	19990505	G	2435	645500071	GENERATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										START/GENERATOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				INTERFERENCE IN FLEX COMM FM RADIO.						1	G	7	1 	3U				H9EU    					 
1999052100148	19990521	00148	EU  	1999	5	21	HEEA062159       	1	19990505	G	7930	645500051	TRANSMITTER     			SNIAS 	350   	AS350B2     	8680813	EU  										ENGINE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				INTERFERENCE IN FLEX COMM FM RADIO.						1	G	7	1 	3U				H9EU    					 
1999062500533	19990625	00533	GL  	1999	6	25	HEEA062399       	2	19990519	G	7230	23056634	ADAPTER         		23051643    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					SPUR GEAR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	706AE	671  			CAC90549	760275	CAE890388S			ENGINE REMOVED DUE TO CYCLES.  UPON INSPECTION OF COMPRESSOR PARTS NOTED:  STEP WEAR BEYOND SERVICEABLE LIMITS ON SPUR G	EAR SHAFT AFT SPLINES FAILED NO-GO GAUGE.   INSTALLED A NEW SPUR GEAR SHAFT.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999062500534	19990625	00534	GL  	1999	6	25	HEEA062400       	2	19990519	G	7230	6887619	SEAL            		23051643    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					COMPRESSOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	706AE	671  			CAC90549	760275	CAE890388S			ENGINE REMOVED DUE TO CYCLES.  UPON INSPECTION OF COMPRESSOR PARTS NOTED:  WORN BEYOND SERVICEABLE LIMITS ON SEAL ASSY T	ANG SLOTS.  INSTALLED A NEW SEAL ASSY.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999062500535	19990625	00535	GL  	1999	6	25	HEEA062401       	2	19990519	G	7230	23056634	ADAPTER         		23033191    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					SPUR GEAR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5745S	805  			CAC70198	45491	CAE860782			ENGINE REMOVED DUE TO IMPELLER RETIREMENT.  UPON INSPECTION OF COMPRESSOR PARTS NOTED:  STEP WEAR BEYOND SERVICEABLE LIM	ITS ON SPUR GEAR SHAFT AFT SPLINES.  FAILED NO-GO GAUGE.  INSTALLED A NEW SPUR GEAR SHAFT.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999062500536	19990625	00536	GL  	1999	6	25	HEEA062402       	2	19990519	G	7230	23056634	ADAPTER         		23033191    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					SPUR GEAR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3905B	356  			CAC70524	45598	CAE860771			ENGINE REMOVED DUE TO CRACKED EXHAUST COLLECTOR.  COMPRESSOR REPAIRED DUE TO WHINE BETWEEN 10 PERCENT AND 35 PERCENT TOR	QUE.    INSPECTION OF COMPRESSOR PARTS REVEALED SPUR GEAR SHAFT AFT SPLINES FAILED NO-GO GAUGE CHECK.  INSTALLED A NEW S	PUR GEAR SHAFT.				1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999062500537	19990625	00537	GL  	1999	6	25	HEEA062403       	2	19990519	G	7230	23056634	ADAPTER         		23033193    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					SPUR GEAR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2133X	676  			CAC90149	45634	CAE860771			ENGINE REMOVED DUE TO CRACKED EXHAUST COLLECTOR.  COMPRESSOR REPAIRED DUE TO BROKEN VANE STUD.  INSPECTION OF COMPRESSOR	 PARTS REVEALED STEP WEAR IN EXCESS OF NO-GO GAUGE LIMITS ON AFT END SPLINES.  INSTALLED A NEW SPUR GEAR SHAFT.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999062500538	19990625	00538	GL  	1999	6	25	HEEA062404       	2	19990519	G	7313	47105	METER           								ALLSN 	250C  	250C*       		GL  					FUEL SYSTEM	MISMARKED       	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										RECEIVED PART FROM ALLISON AS P/N 47105 METER; BUT THE PART IN THE PACKAGE IS ACTUALLY P/N 47073 METER USED ON THE C-20 	FUEL NOZZLES.										3	U			E4CE				 
1999062500539	19990625	00539	GL  	1999	6	25	HEEA062405       	2	19990526	G	7250	23032345	COUPLING        		23035128    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					N1 SPLINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251V	104  			CAT97992	51404	CAE895529			ENGINE REMOVED DUE TO TURBINE OVERHAUL.  UPON INSPECTION OF TURBINE PARTS NOTED:  PITTED AND STEP WEAR BEYOND SERVICEABL	E LIMITS ON N1 COUPLING INNER SPLINES.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999062500540	19990625	00540	GL  	1999	6	25	HEEA062406       	2	19990526	G	7210	23059588	PTO GEAR        			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					GEARBOX	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	10814	4404 			CAG70015	45415	CAE860522			REMOVED DUE TO GROOVED SEAL JOURNALS.  P.T.O. GEAR INSTALLED IN ACCORDANCE WITH RFSE-250-93-1.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999062500541	19990625	00541	GL  	1999	6	25	HEEA062407       	2	19990526	G	7250	23032280	WHEEL           		23035128    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C30P     	03013	GL  					ADAPTER SPLINE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	3904L				CAT97895	45597	CAE895336			NEW PART ASSEMBLY INSPECTION REVEALED 19-24 SHOULDER TO SHAFT END DIMENSION APPROX:  .0025 INCH UNDERSIZED CAUSING ROTOR	 TO NOT MEET TRAVEL AT ASSEMBLY.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999062500542	19990625	00542	GL  	1999	6	25	HEEA062408       	2	19990601	G	7250	23062750	NOZZLE SHIELD   		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					NR 1 TURBINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911EB	984  			CAT37417	S812	CAE836073			ENGINE REMOVED DUE TO SMOKE ON SHUTDOWN.  UPON INSPECTION OF TURBINE PARTS NOTED:  CRACKED BEYOND SERVICEABLE LIMITS ON 	NR 1 NOZZLE SHIELD DOME AS MARKED.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999062500543	19990625	00543	GL  	1999	6	25	HEEA062409       	2	19990601	G	7250	6898764	SEAL            		23038160    						ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03					CAT15266		CAE295266			ENGINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL.  UPON INSPECTION OF TURBINE PARTS NOTED:  PITS BEYOND SERVICEABLE LIM	ITS ON CARBON SEAL MATING SURFACE.										3	U			E4CE				 
1999062500544	19990625	00544	GL  	1999	6	25	HEEA062410       	2	19990615	G	7250	6853279	WHEEL           			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					NR 4 TURBINE	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	967MB					S737	CAE836387			UPON ASSEMBLY OF P.T. ROTOR; UNABLE TO OBTAIN BALANCE.  REPLACEMENT OF NR 4 TURBINE WHEEL CURED PROBLEM.  INSTALLED NEW 	WHEEL.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999062500545	19990625	00545	NE  	1999	6	25	HEEA062411       	1	19990617	G	2421	7655009005110	GENERATOR       			SKRSKY	S76   	S76A        	8143006	NE  										AC SYSTEM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2743E					760155				A.C. GENERATOR BEARING LIGHT CAME ON IN-FLIGHT.   INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BEARINGS WERE ROUGH.						1	G	7	2 	3U				H1NE    					 
1999062500546	19990625	00546		1999	6	25	HEEA062412       	4	19990617	G	2215	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2743E	4635 				760155				ACTUATOR CHATTERS AND KICKS.						1	G	7	2 	3U				H1NE    					 
1999062500547	19990625	00547		1999	6	25	HEEA062413       	4	19990617	G	3434	066104400	BEACON          			SKRSKY	S76   	S76A        	8143006	NE  										FUSELAGE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2743E					760155				BEACON INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999062500548	19990625	00548	NE  	1999	6	25	HEEA062414       	1	19990618	G	2822	399A106	MOTOR           		769000180210	SKRSKY	S76   	S76A        	8143006	NE  										BOOST PUMP	WEAK            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	278X				8412577	760440				MOTOR IS VERY WEAK AND STICKS.   UNIT OVERHAULED ON 11-5-98.						1	G	7	2 	3U				H1NE    					 
1999062500549	19990625	00549	SW  	1999	6	25	HEEA062415       	1	19990519	G	6300	407340339103	BEARING         		PHIPBH40701 	BELL  	407   	407         		SW  										MAIN ROTOR	ROUGH           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH				AFS1141	53277				ROUGH BEARINGS.  SERIAL NUMBERS REMOVED ARE H98-2272 AND H98-2206.   REPLACEMENT PART SERIAL NUMBERS ARE M98-2111 AND M9	8-2284.					1	G	7	1 	3U			O	H2SW    					 
1999062500550	19990625	00550	SW  	1999	6	25	HEEA062418       	1	19990519	G	6420	406312100101	BEARING         		407012101105	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH	1255 			53230	53228				TAIL ROTOR  HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999062500551	19990625	00551	SW  	1999	6	25	HEEA062419       	1	19990519	G	7120	407060111101	BEARING         			BELL  	407   	407         		SW  										BIPOD MOUNT	ROUGH           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	427PH					53059				BIPOD MOUNT HAS ROUGH BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999062500552	19990625	00552	SW  	1999	6	25	HEEA062420       	1	19990519	G	7120	407060111101	BEARING         			BELL  	407   	407         		SW  										BIPOD MOUNT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	723PH					53283				BIPOD MOUNT HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999062500553	19990625	00553	SW  	1999	6	25	HEEA062421       	1	19990521	G	7120	407060111101	BEARING         			BELL  	407   	407         		SW  										BIPOD MOUNT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				WORN BEARING IN BIPOD MOUNT.						1	G	7	1 	3U			O	H2SW    					 
1999062500554	19990625	00554	SW  	1999	6	25	HEEA062422       	1	19990521	G	7120	407060111101	BEARING         			BELL  	407   	407         		SW  										BIPOD MOUNT	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				BIPOD MOUNT HAS LOOSE BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999062500555	19990625	00555	SW  	1999	6	25	HEEA062423       	1	19990521	G	7120	407060111101	BEARING         			BELL  	407   	407         		SW  										BIPOD MOUNT	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH					53278				BIPOD MOUNT HAS LOOSE BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999062500556	19990625	00556	SW  	1999	6	25	HEEA062424       	1	19990521	G	6330	407010206103B	ELASTOMERIC     			BELL  	407   	407         		SW  										XMSN MOUNT	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				ELASTOMER BEARING SEPARATED.						1	G	7	1 	3U			O	H2SW    					 
1999062500557	19990625	00557	SW  	1999	6	25	HEEA062425       	1	19990521	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN BEARING    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				LINK BEARINGS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999062500558	19990625	00558	SW  	1999	6	25	HEEA062426       	1	19990521	G	2435	206062200123	STARTER         			BELL  	407   	407         		SW  										START/GENERATOR	WORN BRUSHES    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416	1558 				53070				BRUSHES WORN ON STARTER/GENERATOR.						1	G	7	1 	3U			O	H2SW    					 
1999062500559	19990625	00559	SW  	1999	6	25	HEEA062427       	1	19990521	G	6510	407040303105A	HOUSING         			BELL  	407   	407         		SW  										BLOWER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH	1286 				53198				BELL SENT BLOWER HOUSING ASSY TO USE WHAT IS NEEDED SO ORIGINAL AIRCRAFT WOULD NOT BE GROUNDED.   PHI USED THE HOUSING B	ECAUSE THE ORIGINAL WAS CRACKED AND THE INSIDE SHAFT ASSY HAD ROUGH BEARINGS.					1	G	7	1 	3U			O	H2SW    					 
1999062500560	19990625	00560	SW  	1999	6	25	HEEA062428       	1	19990524	G	6300	406010413119	PITCH LINK      			BELL  	407   	407         		SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH	1264 				53198				SWAGED AREA OF PITCH LINK REMOVED.						1	G	7	1 	3U			O	H2SW    					 
1999062500561	19990625	00561	SW  	1999	6	25	HEEA062429       	1	19990524	G	6320	406010401115	SWASHPLATE      			BELL  	407   	407         		SW  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	612PH	812  				53199				EXCESSIVE GREASE LEAKING FROM UPPER TOP SEAL ON SWASHPLATE.						1	G	7	1 	3U			O	H2SW    					 
1999062500562	19990625	00562	SW  	1999	6	25	HEEA062430       	1	19990524	G	6220	407001528101	ELASTOMERIC     			BELL  	407   	407         		SW  										MAIN ROTOR	CONTAMINATED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	2160 				53114				ELASTOMER OIL SOAKED ON BELLCRANK.						1	G	7	1 	3U			O	H2SW    					 
1999062500563	19990625	00563	SW  	1999	6	25	HEEA062431       	1	19990524	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH	1137 				53228				UNIVERSAL BEARING HAS AXIAL PLAY.						1	G	7	1 	3U			O	H2SW    					 
1999062500564	19990625	00564	SW  	1999	6	25	HEEA062432       	1	19990524	G	6300	407010206103	BEARING         			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				ROD END BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999062500565	19990625	00565	SW  	1999	6	25	HEEA062433       	1	19990524	G	3212	206373901103	SOLENOID VALVE  			BELL  	407   	407         		SW  										MLG FLOAT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	447PH					53114				SOLENOID VALVE LEAKING OUT OF TOP SCREW, RIGHT SIDE.						1	G	7	1 	3U			O	H2SW    					 
1999062500566	19990625	00566	SW  	1999	6	25	HEEA062434       	1	19990524	G	7922	8A583000	THERMOVALVE     			BELL  	407   	407         		SW  										OIL TEMP	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	723PH	357  				53283				ENGINE OIL TEMPERATURE OVER 100 DEGREES.						1	G	7	1 	3U			O	H2SW    					 
1999062500567	19990625	00567	SW  	1999	6	25	HEEA062437       	1	19990524	G	6510	407340339103	BEARING         		PHIPBH40701 	BELL  	407   	407         		SW  										TAIL ROTOR	OVERHEATED      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH				AFS1138	53114				270 DEGREE HEAT TEMP TURNED BEARING BLACK.  SERIAL NUMBERS REMOVED ARE H98-2252 AND H98-2268.						1	G	7	1 	3U			O	H2SW    					 
1999062500568	19990625	00568	SW  	1999	6	25	HEEA062438       	1	19990524	G	3212	407350302101	FLOAT           			BELL  	407   	407         		SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	612PH					53199				FLOAT BAG LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999062500569	19990625	00569	SW  	1999	6	25	HEEA062439       	1	19990524	G	3212	206373901103	SOLENOID VALVE  			BELL  	407   	407         		SW  										MLG FLOAT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	407PH					53003				SOLENOID VALVE LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999062500570	19990625	00570	SW  	1999	6	25	HEEA062440       	1	19990524	G	6310	406040316101	ADAPTER         			BELL  	407   	407         		SW  										SPLINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH					53228				ADAPTER HAS SPLINE WEAR.						1	G	7	1 	3U			O	H2SW    					 
1999062500571	19990625	00571	SW  	1999	6	25	HEEA062442       	1	19990524	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				DISK COUPLING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999062500572	19990625	00572	SW  	1999	6	25	HEEA062443       	1	19990524	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				DISK COUPLING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999062500573	19990625	00573	SW  	1999	6	25	HEEA062444       	1	19990524	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				DISK COUPLING STRAINED AND STRESSED DUE TO BEARING FAILURE ON THE BLOWER SHAFT ASSY.						1	G	7	1 	3U			O	H2SW    					 
1999062500574	19990625	00574	SW  	1999	6	25	HEEA062445       	1	19990524	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				DISK COUPLING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999062500575	19990625	00575	SW  	1999	6	25	HEEA062446       	1	19990524	G	6510	406040340101	DISC PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				BLOWER HOUSING SHAFT ASSY HAD A BEARING FAILURE.  PART WAS STRESSED AND STRAINED.						1	G	7	1 	3U			O	H2SW    					 
1999062500576	19990625	00576	SW  	1999	6	25	HEEA062447       	1	19990524	G	7921	406040315111	BEARING         			BELL  	407   	407         		SW  										OIL COOLER	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	2262 				53114				FORWARD OIL COOLER BEARING FAILURE.						1	G	7	1 	3U			O	H2SW    					 
1999062500577	19990625	00577	SW  	1999	6	25	HEEA062448       	1	19990524	G	3212	206050247135	COVER           			BELL  	407   	407         		SW  										FLOAT ASSY	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				FLOAT COVER WORN AND TORN.						1	G	7	1 	3U			O	H2SW    					 
1999062500578	19990625	00578	SW  	1999	6	25	HEEA062450       	1	19990524	G	6510	206061432121	HOUSING         			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				OIL COOLER BLOWER HOUSING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999062500579	19990625	00579	SW  	1999	6	25	HEEA062451       	1	19990524	G	2510	407370721105	RESTRAINT       			BELL  	407   	407         		SW  										COCKPIT	CUT             	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				RESTRAINT ASSEMBLY FRAYED/CUT.						1	G	7	1 	3U			O	H2SW    					 
1999062500580	19990625	00580	SW  	1999	6	25	HEEA062452       	1	19990524	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM	2547 				53060				UNIVERSAL HAS WORN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999062500581	19990625	00581	SW  	1999	6	25	HEEA062453       	1	19990524	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	ROUGH           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	2076 				53159				UNIVERSAL HAS ROUGH BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999062500582	19990625	00582	SW  	1999	6	25	HEEA062454       	1	19990524	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	722  				53114				UNIVERSAL HAS WORN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999062500583	19990625	00583	SW  	1999	6	25	HEEA062455       	1	19990524	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH	1578 				53207				UNIVERSAL HAS WORN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999062500584	19990625	00584	SW  	1999	6	25	HEEA062456       	1	19990524	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	723PH	444  				53283				UNIVERSAL HAS WORN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999062500585	19990625	00585	SW  	1999	6	25	HEEA062457       	1	19990524	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH	926  				53003				UNIVERSAL HAS WORN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999062500586	19990625	00586	SW  	1999	6	25	HEEA062458       	1	19990524	G	7921	407062021101	DUCT            			BELL  	407   	407         		SW  										OIL COOLER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				OIL COOLER DUCT ASSY CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999062500587	19990625	00587	SW  	1999	6	25	HEEA062459       	1	19990524	G	7921	407062021101	DUCT            			BELL  	407   	407         		SW  										OIL COOLER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				DUCT CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999062500588	19990625	00588	SW  	1999	6	25	HEEA062460       	1	19990524	G	7921	407062021101	DUCT            			BELL  	407   	407         		SW  										OIL COOLER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				DUCT CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999062500589	19990625	00589	SW  	1999	6	25	HEEA062461       	1	19990524	G	6510	407040316101	FLYWHEEL        			BELL  	407   	407         		SW  										TAIL ROTOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				BEARING FAILURE ON FLYWHEEL.						1	G	7	1 	3U			O	H2SW    					 
1999062500590	19990625	00590	SW  	1999	6	25	HEEA062462       	1	19990524	G	6510	407040316101	FLYWHEEL        			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH					53228				FLYWHEEL HAS WORN SPLINES.						1	G	7	1 	3U			O	H2SW    					 
1999062500592	19990625	00592	SW  	1999	6	25	HEEA062464       	1	19990524	G	6510	206061432116	HOUSING         			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				BLOWER HOUSING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999062500593	19990625	00593	SW  	1999	6	25	HEEA062465       	1	19990525	G	6510	206061432116	HOUSING         			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				BLOWER HOUSING HAS A CRACK AT LEFT OUTLET CORNER AND RIVETS LOOSE.						1	G	7	1 	3U			O	H2SW    					 
1999062500594	19990625	00594	SW  	1999	6	25	HEEA062466       	1	19990525	G	2435	206062200113	STARTER         			BELL  	407   	407         		SW  										START/GENERATOR	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	437PH					53072				STARTER/GENERATOR HAS WORN BRUSHES.  INSPECTED  AND FOUND BRUSHES EXCESSIVELY WORN, DAMPENER PLATE WAS PITTED, AND FRICT	ION RING WAS GROOVED.					1	G	7	1 	3U			O	H2SW    					 
1999062500595	19990625	00595	SW  	1999	6	25	HEEA062468       	1	19990526	G	6510	206061432121	HOUSING         			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	722PH					53288				CRACK AT LEFT OUTLET CORNER AND LOOSE RIVETS.						1	G	7	1 	3U			O	H2SW    					 
1999062500596	19990625	00596	SW  	1999	6	25	HEEA062470       	1	19990526	G	6510	406040320101	SHAFT           		PHIPBH40701 	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH				AFS1016	53209				SHAFT WORN BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999062500597	19990625	00597	SW  	1999	6	25	HEEA062471       	1	19990526	G	6510	407340339103	BEARING         		PHIPBH40701 	BELL  	407   	407         		SW  										TAIL ROTOR	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	723PH	3    			AFS1124	53283				UNABLE TO BALANCE O/C FAN SHAFT ASSY FLYWHEEL BELOW 3 IPS.  CLEANED BEARINGS WITH DRY RAG TO REMOVE EXCESS GREASE.   RE-	INSTALLED BEARINGS TO SHAFT.  UPON PURGING BEARINGS WITH ROYCO 13 GREASE, WATER WAS NOTICED SQUIRTING FROM SEAL AREA ON 	BEARINGS.  SERIAL NUMBERS REMOVED ARE K98-0775 AND J98-1859.				1	G	7	1 	3U			O	H2SW    					 
1999062500598	19990625	00598	SW  	1999	6	25	HEEA062474       	1	19990526	G	6510	406040320101	SHAFT           		PHIPBH40701 	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH				AFS883	53142				SHAFT SPLINES WORN, EXCEEDING PROPER LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999062500599	19990625	00599	SW  	1999	6	25	HEEA062478       	1	19990526	G	6420	406312100101	BEARING         		407012101105	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH				53207	53207				BEARINGS WORN BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999062500600	19990625	00600	SW  	1999	6	25	HEEA062479       	1	19990526	G	6420	407312100101	BEARING         		407012101105	BELL  	407   	407         		SW  										TAIL ROTOR	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH	865  			53200	53199				SPLINES PITTED.						1	G	7	1 	3U			O	H2SW    					 
1999062500601	19990625	00601	SW  	1999	6	25	HEEA062480       	1	19990526	G	6420	406312100101	BEARING         		407012101105	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH	865  			53200	53199				BEARING WORN BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999062500602	19990625	00602	SW  	1999	6	25	HEEA062481       	1	19990526	G	6320	214040806003	SWITCH          			BELL  	407   	407         		SW  										TRANSMISSION OIL	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	719PH					53266				TRANS. OIL PRESSURE SEGMENT WOULD NOT COME ON.  (LIGHT DOES NOT TURN ON).						1	G	7	1 	3U			O	H2SW    					 
1999062500603	19990625	00603	SW  	1999	6	25	HEEA062482       	1	19990526	G	2844	407362013101	SWITCH          			BELL  	407   	407         		SW  										FUEL PRESSURE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	427PH					53059				PUMP LIGHT WON'T COME ON.						1	G	7	1 	3U			O	H2SW    					 
1999062500604	19990625	00604	SW  	1999	6	25	HEEA062483       	1	19990526	G	2844	407362013101	SWITCH          			BELL  	407   	407         		SW  										FUEL PRESSURE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	427PH	2112 				53059				LOW LEVEL FUEL LIGHT STAYS ON WHEN BATTERY SWITCH IS ON WITH 600 POUNDS OF FUEL.						1	G	7	1 	3U			O	H2SW    					 
1999062500605	19990625	00605	SW  	1999	6	25	HEEA062484       	1	19990526	G	2840	407362005103	SWITCH          			BELL  	407   	407         		SW  										FUEL SYSTEM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	612PH					53199				FUEL LOW LIGHT STAYS ON.						1	G	7	1 	3U			O	H2SW    					 
1999062500606	19990625	00606	SW  	1999	6	25	HEEA062485       	1	19990526	G	2840	407362005103	SWITCH          			BELL  	407   	407         		SW  										FUEL SYSTEM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	406PH					53198				LOW LIGHT WOULDN'T GO OUT.						1	G	7	1 	3U			O	H2SW    					 
1999062500607	19990625	00607	SW  	1999	6	25	HEEA062486       	1	19990526	G	7930	407375004101	INDICATOR       			BELL  	407   	407         		SW  										OIL SYSTEM	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	407MM					53060				OIL TEMPERATURE INTERMITTENT.						1	G	7	1 	3U			O	H2SW    					 
1999062500608	19990625	00608	SW  	1999	6	25	HEEA062487       	1	19990526	G	6710	406010429101	PIN             			BELL  	407   	407         		SW  										CYCLIC STICK	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	407PH					53003				PIN WORN.						1	G	7	1 	3U			O	H2SW    					 
1999062500609	19990625	00609	SW  	1999	6	25	HEEA062488       	1	19990526	G	6710	406010421103	SPACER          			BELL  	407   	407         		SW  										CYCLIC STICK	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	407PH					53003				SPACERS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999062500610	19990625	00610	SW  	1999	6	25	HEEA062489       	1	19990526	G	2840	407375007103	INDICATOR       			BELL  	407   	407         		SW  										FUEL PRESSURE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	723PH	446  				53283				FUEL PRESSURE TRANSMISSION INDICATOR INDICATES 5 POUNDS ALL THE TIME EVEN WHEN PUMP IS SECURE.						1	G	7	1 	3U			O	H2SW    					 
1999062500611	19990625	00611	SW  	1999	6	25	HEEA062492       	1	19990526	G	3212	8226003	FUSIBLE PLUG    			BELL  	407   	407         		SW  										FLOAT	LEAKING         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	721PH	773  				53278				PLUG LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999062500612	19990625	00612	SW  	1999	6	25	HEEA062493       	1	19990526	G	6510	407040302103	SHAFT           			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	723PH	441  				53283				TAIL ROTOR DRIVE SHAFT HAS WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999062500613	19990625	00613	SW  	1999	6	25	HEEA062494       	1	19990526	G	6420	206011728001	TRUNNION        			BELL  	407   	407         		SW  										T/R HUB	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH	865  				53199				TRUNNION BEARINGS WORN BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999062500614	19990625	00614	SW  	1999	6	25	HEEA062495       	1	19990526	G	6420	206011728001	TRUNNION        			BELL  	407   	407         		SW  										T/R HUB	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH	1629 				53207				SPLINES WORN BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999062500615	19990625	00615	SW  	1999	6	25	HEEA062497       	1	19990526	G	3212	212073905001	PRESSURE GAUGE  			BELL  	407   	407         		SW  										FLOAT	DAMAGED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	457PH					53147				FACE SPINS ON GAUGE PRESSURE.						1	G	7	1 	3U			O	H2SW    					 
1999062500616	19990625	00616	SW  	1999	6	25	HEEA062498       	1	19990526	G	6510	206061432121	HOUSING         			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416	275  				53070				BLOWER HOUSING CRACKED AT UPPER OUTLET CORNER LEFT, AND OTHER PLACES, AND LOOSE RIVETS.						1	G	7	1 	3U			O	H2SW    					 
1999062500617	19990625	00617	SW  	1999	6	25	HEEA062500       	1	19990526	G	6310	407010206103A	SPRING          			BELL  	407   	407         		SW  										TRANSMISSION	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				RUBBER WORN.						1	G	7	1 	3U			O	H2SW    					 
1999062500618	19990625	00618	SW  	1999	6	25	HEEA062501       	1	19990526	G	6230	406010427109	GIMBAL RING     			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH	3791 				53003				BUSHING ON GIMBAL RING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999062500619	19990625	00619	SW  	1999	6	25	HEEA062502       	1	19990526	G	6230	406010425107	LEVER ASSY      			BELL  	407   	407         		SW  										PYLON	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH	438  				53003				LEVER ASSEMBLY BUSHING WORN.  SERIAL NUMBERS REMOVED ARE A-2487 AND A-2485.						1	G	7	1 	3U			O	H2SW    					 
1999062500620	19990625	00620	SW  	1999	6	25	HEEA062503       	1	19990526	G	6520	406040400115	GEARBOX         			BELL  	407   	407         		SW  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH	865  				53199				TAIL ROTOR ASSEMBLY RUSTED TO SPLINES ON T/R GEARBOX.						1	G	7	1 	3U			O	H2SW    					 
1999062500621	19990625	00621	SW  	1999	6	25	HEEA062504       	1	19990526	G	6320	407375005101	INDICATOR       			BELL  	407   	407         		SW  										M/R GEARBOX	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				LCD DISPLAY IS VERY DIM ON INDICATOR.						1	G	7	1 	3U			O	H2SW    					 
1999062500622	19990625	00622	SW  	1999	6	25	HEEA062505       	1	19990526	G	2913	206076030111	PUMP            			BELL  	407   	407         		SW  										HYDRAULIC SYS	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	4999	310  				53323				PUMP LEAKING FROM SHAFT AREA.  REMOVED FROM AIRCRAFT.						1	G	7	1 	3U			O	H2SW    					 
1999062500623	19990625	00623		1999	6	25	HEEA062506       	4	19990526	G	2210	214074305105	AMPLIFIER ASSY  			BELL  	214   	214ST       	1182106	SW  										AUTO PILOT	WON'T TEST      	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03										AMPLIFIER ASSEMBLY UNIT WAS INSTALLED AND WOULD NOT PASS AARS MONITOR TEST.						2	G	7	2 	4U				H10SW   					 
1999062500624	19990625	00624	SW  	1999	6	25	HEEA062525       	1	19990526	G	6520	406040400115	GEARBOX         			BELL  	407   	407         		SW  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH	1629 				53207				TAIL ROTOR GEARBOX HAS EXCESSIVE CORROSION ON OUTPUT SHAFT SPLINES.						1	G	7	1 	3U			O	H2SW    					 
1999062500625	19990625	00625	SW  	1999	6	25	HEEA062526       	1	19990526	G	6310	406040500123B	FREEWHEEL UNIT  			BELL  	407   	407         		SW  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	447PH	1337 				53114				FORWARD SEAL LEAKING ON FREEWHEEL ASSEMBLY.						1	G	7	1 	3U			O	H2SW    					 
1999062500626	19990625	00626	SW  	1999	6	25	HEEA062528       	1	19990528	G	3340	900601	LIGHT           			BELL  	230   	230         	1182149	SW  										FUSELAGE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RC	312  				23037				INOPERATIVE, NO MOVEMENT BUT LIGHT WORKS.						1	G	7	2 	3U			NC	H9SW    					 
1999062500627	19990625	00627	SW  	1999	6	25	HEEA062530       	1	19990601	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	DRAGGING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M	751  				28102				STARTER DRAGS BADLY DURING START - SOMETIMES WORKS INTERMITTENTY.						2	G	7	2 	4U				H10SW   					 
1999062500628	19990625	00628	SW  	1999	6	25	HEEA062531       	1	19990601	G	6710	214001540117	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										SCAS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										SCAS YAW CHANNEL KICKS OFF IN-FLIGHT.						2	G	7	2 	4U				H10SW   					 
1999062500629	19990625	00629	SW  	1999	6	25	HEEA062532       	1	19990607	G	3150	214175122105	CAUTION PANEL   			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				CAUTION PANEL HAS INTERNAL SHORT.  NR 1 FUEL PRESSURE LIGHT STAYS ON.						2	G	7	2 	4U				H10SW   					 
1999062500630	19990625	00630	SW  	1999	6	25	HEEA062533       	1	19990607	G	2841	214066212103	PROBE           			BELL  	214   	214ST       	1182106	SW  										FUEL QUANTITY	FAILED TEST     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				PROBE DID NOT PASS CALIBRATION CHECK PER M&O.						2	G	7	2 	4U				H10SW   					 
1999062500631	19990625	00631		1999	6	25	HEEA062534       	4	19990607	G	3100	222375010111	LENS            			BELL  	214   	214ST       	1182106	SW  										SIGNAL ASSY	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										SIGNAL ASSEMBLY HAS BROKEN LENS.						2	G	7	2 	4U				H10SW   					 
1999062500632	19990625	00632	SW  	1999	6	25	HEEA062535       	1	19990609	G	6710	206001020101	TUBE ASSY       			BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				TUBE ASSEMBLY CORRODED BEYOND LIMITS.  SCRAPPED AND REPLACED WITH SERVICEABLE TUBE.						1	G	7	1 	3U				H2SW    					 
1999062500633	19990625	00633	SW  	1999	6	25	HEEA062536       	1	19990609	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	FAILED          	E			HEEA	K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			SW	03	5748M					28102				UNABLE TO GET ABOVE 30 PERCENT ON BATTERY. OR CROSS START.  STARTS HAVE STRONG BURNT ODOR.						2	G	7	2 	4U				H10SW   					 
1999062500634	19990625	00634	SW  	1999	6	25	HEEA062537       	1	19990609	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y	2379 				28139				TROUBLESHOOTING, NR 2 ENGINE WILL NOT START OFF AIRCRAFT BATTERIES.						2	G	7	2 	4U				H10SW   					 
1999062500635	19990625	00635	SW  	1999	6	25	HEEA062538       	1	19990609	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				STARTER WILL NOT DISENGAGE.						2	G	7	2 	4U				H10SW   					 
1999062500636	19990625	00636	SW  	1999	6	25	HEEA062539       	1	19990609	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				STARTER DOES NOT DISENGAGE.						2	G	7	2 	4U				H10SW   					 
1999062500637	19990625	00637	SW  	1999	6	25	HEEA062540       	1	19990609	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N	2439 				28106				STARTER HAS SLOW START.						2	G	7	2 	4U				H10SW   					 
1999062500638	19990625	00638	SW  	1999	6	25	HEEA062541       	1	19990609	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH	1578 				53207				UNIVERSAL WORN.						1	G	7	1 	3U			O	H2SW    					 
1999062500639	19990625	00639	SW  	1999	6	25	HEEA062542       	1	19990609	G	6220	407010105101	STUD            			BELL  	407   	407         		SW  										DROOP STOP	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	2496 				53114				DROOP STOP REMOVED DURING OVERHAUL AND NDT PROCEDURE.  CRACKS WERE FOUND.						1	G	7	1 	3U			O	H2SW    					 
1999062500640	19990625	00640	SW  	1999	6	25	HEEA062543       	1	19990609	G	6220	406010107105	ADAPTER         			BELL  	407   	407         		SW  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	2496 				53114				REMOVED DURING OVERHAUL AND NDT PROCEDURE.  CRACKS WERE FOUND.  SERIAL NUMBERS REMOVED ARE A2855, A2844, A2882, AND A288	4.   REPLACEMENT PART SERIAL NUMBERS ARE A3311, A3592, A3615, AND A3591.					1	G	7	1 	3U			O	H2SW    					 
1999062500641	19990625	00641		1999	6	25	HEEA062547       	4	19990609	G	3414	214074152101	TRANSPONDER     			BELL  	214   	214ST       	1182106	SW  										AIRSPEED	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	824H					28119				AIRSPEED TRANSCEIVER CAUSES ELEVATION SYSTEM TO DROP OFFLINE IN-FLIGHT.						2	G	7	2 	4U				H10SW   					 
1999062500642	19990625	00642	SW  	1999	6	25	HEEA062548       	1	19990617	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	DRAGGING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M	1054 				28102				STARTER DRAGS DURING START CAUSING GENERATOR TO KICK OFF.   ALSO EMITS STRONG BURNT SMELL AFTER STARTING.						2	G	7	2 	4U				H10SW   					 
1999062500643	19990625	00643	SW  	1999	6	25	HEEA062549       	1	19990618	G	3212	206373901103	SOLENOID VALVE  			BELL  	407   	407         		SW  										FLOAT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	402PH					53159				SEEPING FROM SOLENOID VALVE HEAD.						1	G	7	1 	3U			O	H2SW    					 
1999062500644	19990625	00644	SW  	1999	6	25	HEEA062550       	1	19990618	G	3212	407350301101	FLOAT           			BELL  	407   	407         		SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	402PH					53159				LEFT FLOAT BAG SEEPING FROM SEAM IN FORWARD AS MARKED.						1	G	7	1 	3U			O	H2SW    					 
1999062500645	19990625	00645		1999	6	25	HEEA062553       	1	19990618	G	2620	RTA600	EXTINGUISHER    																	EMERGENCY EQUIP	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										FIRE EXTINGUISHER BELOW MINIMUM WEIGHT.  ORIGINAL FACTORY INSTALLED EQUIPMENT ON 11-26-98.																			 
1999062500646	19990625	00646	SW  	1999	6	25	HEEA062554       	1	19990618	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										STEP ACTUATOR IN THE EXTENDED POSITION, MOTOR WILL NOT RETRACT WITH A CORD ON IT, INTERMITTENT.						1	G	7	2 	4U				H4SW    					 
1999062500647	19990625	00647	SW  	1999	6	25	HEEA062555       	1	19990618	G	3150	214175122105	CAUTION PANEL   			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5748M					28102				CAUTION PANEL - AFCS AND AUTOPILOTS ON VERY DIM AND ANTI-ICE SEGMENTS INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999062500648	19990625	00648		1999	6	25	HEEA062556       	4	19990618	G	2310	214074303115	AMPLIFIER ASSY  			BELL  	214   	214ST       	1182106	SW  										AUTO FLIGHT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5748M					28102				PITCH WILL NOT STAY ON-LINE.						2	G	7	2 	4U				H10SW   					 
1999062500649	19990625	00649	SW  	1999	6	25	HEEA062557       	1	19990618	G	3242	204001376103	BRAKE ASSY      			BELL  	212   	212         	1181420	SW  										MLG	LOCKED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										BRAKE ASSEMBLY LOCKED-UP.						1	G	7	1 	4U				H4SW    					 
1999062500650	19990625	00650	EU  	1999	6	25	HEEA062558       	1	19990525	G	7921	420800001	BLOWER          			SNIAS 	350   	AS350B2     	8680813	EU  										OIL COOLER	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6095S					2777				BLOWER HAS BROKEN BRUSH PLUG.						1	G	7	1 	3U				H9EU    					 
1999071600145	19990716	00145	SW  	1999	7	16	HEEA062730       	1	19990708	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										START/GENERATOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	1842 				53159				STARTER/GENERATOR BRUSHES WERE EXCESSIVELY WORN AND COMMUTATOR WAS GROOVED.						1	G	7	1 	3U			O	H2SW    					 
1999071600146	19990716	00146	SW  	1999	7	16	HEEA062732       	1	19990708	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										START/GENERATOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	723PH	576  				53283				STARTER/GENERATOR BRUSHES WERE EXCESSIVELY WORN.						1	G	7	1 	3U			O	H2SW    					 
1999071600147	19990716	00147		1999	7	16	HEEA062733       	4	19990708	G	2210	214074303115	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										AUTOFLIGHT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5748M					28102				AARS WILL NOT STAY ENGAGED IN-FLIGHT AFTER 30 MINUTES.  TIME SINCE REPAIR 18:55 HOURS.						2	G	7	2 	4U				H10SW   					 
1999071600148	19990716	00148	SW  	1999	7	16	HEEA062734       	1	19990708	G	3212	206050247138	COVER           			BELL  	407   	407         		SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				FLOAT COVER WORN.   REFERENCE:   DMR NR 686161.						1	G	7	1 	3U			O	H2SW    					 
1999071600149	19990716	00149	SW  	1999	7	16	HEEA062735       	1	19990708	G	3212	206050247138	COVER           			BELL  	407   	407         		SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				FLOAT COVER WORN.   REF:  DMR NR 686159.						1	G	7	1 	3U			O	H2SW    					 
1999071600150	19990716	00150	SW  	1999	7	16	HEEA062736       	1	19990708	G	3212	206050247131	COVER           			BELL  	407   	407         		SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				FLOAT COVER WORN.   REFERENCE:  DMR NR 686160.						1	G	7	1 	3U			O	H2SW    					 
1999071600151	19990716	00151	SW  	1999	7	16	HEEA062738       	1	19990708	G	6300	206362002103	CAP SEAL        			BELL  	407   	407         		SW  										M/R DRIVE	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH					53228				CAP LEAKING.   REFERENCE:   DMR NR 686163.						1	G	7	1 	3U			O	H2SW    					 
1999071600152	19990716	00152	SW  	1999	7	16	HEEA062739       	1	19990708	G	5210	407070620137	PANEL           			BELL  	407   	407         		SW  										PASSENGER DOOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				DOOR CRACKED.   REFERENCE:  DMR NR 686168.						1	G	7	1 	3U			O	H2SW    					 
1999071600153	19990716	00153	SW  	1999	7	16	HEEA062740       	1	19990708	G	5210	407070620138	PANEL           			BELL  	407   	407         		SW  										PASSENGER DOOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				DOOR CRACKED.   REFERENCE:  DMR NR 686169.						1	G	7	1 	3U			O	H2SW    					 
1999071600155	19990716	00155	SW  	1999	7	16	HEEA062742       	1	19990708	G	2822	1C2710	CARTRIDGE       			BELL  	407   	407         		SW  										FUEL PUMP	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	722PH					53288				CARTRIDGE INOPERATIVE.   REFERENCE:  DMR NR 686155.						1	G	7	1 	3U			O	H2SW    					 
1999071600156	19990716	00156	EU  	1999	7	16	HEEA062744       	1	19990708	G	6240	58137000011	TACHOMETER      			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	INACCURATE      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6097Z					2820				TACHOMETER NEEDLES OUT OF ALIGNMENT.   REF:  RMA NR R020261.						1	G	7	1 	3U				H9EU    					 
1999071600157	19990716	00157	EU  	1999	7	16	HEEA062746       	1	19990708	G	7921	420800001	BLOWER          			SNIAS 	350   	AS350B2     	8680813	EU  										OIL COOLER	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	350BZ					2653				BLOWER INOPERATIVE.    REFERENCE:  RMA NR R020408.						1	G	7	1 	3U				H9EU    					 
1999071600158	19990716	00158	EU  	1999	7	16	HEEA062747       	1	19990708	G	2822	P94B12209	PUMP            			SNIAS 	350   	AS350B2     	8680813	EU  										FUEL SYSTEM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	40466					3004				FUEL PUMP NOT MAKING PRESSURE.   REF:  MA NR R020528.						1	G	7	1 	3U				H9EU    					 
1999071600159	19990716	00159	EU  	1999	7	16	HEEA062748       	1	19990708	G	7931	642790041	TRANSMITTER     			SNIAS 	350   	AS350B2     	8680813	EU  										OIL PRESSURE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6097Z					2820				OIL PRESSURE GAUGE STAYS PEGGED OUT.   REFERENCE:  RMA NR R020186.						1	G	7	1 	3U				H9EU    					 
1999071600160	19990716	00160		1999	7	16	HEEA062749       	4	19990708	G	2312	374GC01Y	RADIO           			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4000L					2873				UNABLE TO TRANSMIT TR138 WHEN GENERATOR IS IN THE ON POSITION.   REFERENCE:  RMA NR R019532.						1	G	7	1 	3U				H9EU    					 
1999071600161	19990716	00161	EU  	1999	7	16	HEEA062750       	1	19990708	G	6520	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				CRACKED BUSHING.    REFERENCE:  RMA NR R020074.						1	G	7	1 	3U				H9EU    					 
1999071600162	19990716	00162	EU  	1999	7	16	HEEA062751       	1	19990708	G	6410	355A12004008	BLADE           			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	NOISY           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951	1280 				2771				SPAR NOISE IN AREA OF TAIL ROTOR BLADES.    REFERENCE:   RMA NR R019946.						1	G	7	1 	3U				H9EU    					 
1999071600163	19990716	00163	EU  	1999	7	16	HEEA062752       	1	19990708	G	7712	305731365	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										TORQUE	READS HIGH      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4000L					2873				TORQUE INDICATOR READS HIGH AND IS STICKING.   REFERENCE:  MA NR R019826.						1	G	7	1 	3U				H9EU    					 
1999071600164	19990716	00164	EU  	1999	7	16	HEEA062753       	1	19990708	G	7712	305731365	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										TORQUE	READS HIGH      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4000L					2873				TORQUE INDICATOR GAUGE READS HIGH THEN STUCK AT 90 PERCENT.   REFERENCE:  RMA NR R019905.						1	G	7	1 	3U				H9EU    					 
1999071600165	19990716	00165	EU  	1999	7	16	HEEA062755       	1	19990708	G	6520	350A33200405	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										T/R SPIDER	ROUGH           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				BEARING ROUGH WHEN ROTATING.    REFERENCE:  MA NR R019985.						1	G	7	1 	3U				H9EU    					 
1999072300327	19990723	00327	NE  	1999	7	23	HEEA062777       	1	19990712	G	2460	A1077B	RELAY           			SKRSKY	S76   	S76A        	8143006	NE  										FLT COMPARTMENT	SHORTED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911MJ					760231				RELAY HAS OPEN CONNECTION BETWEEN B3 AND B2.						1	G	7	2 	3U				H1NE    					 
1999072300328	19990723	00328		1999	7	23	HEEA062778       	4	19990712	G	3421	40016702511	GYRO            																	COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										INDICATOR GETS R/T FLAG.																			 
1999072300329	19990723	00329	NE  	1999	7	23	HEEA062779       	2	19990712	G	7323	25249994	GOVERNOR        			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					ENGINE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z					33077				GOVERNOR CAUSING SURGING ON ENGINE.						1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999072300330	19990723	00330	NE  	1999	7	23	HEEA062780       	1	19990712	G	6210	7615009043050	TIP CAP         			SKRSKY	S76   	S76A        	8143006	NE  										M/R BLADE	WEAK            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122G					760232				TRAILING EDGE WEAK ON CAP.						1	G	7	2 	3U				H1NE    					 
1999072300331	19990723	00331	NE  	1999	7	23	HEEA062781       	1	19990712	G	6210	7615009043050	TIP CAP         			SKRSKY	S76   	S76A        	8143006	NE  										M/R BLADE	ERODED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545X					760050				END CAP IS ERRODED THROUGH.						1	G	7	2 	3U				H1NE    					 
1999072300332	19990723	00332		1999	7	23	HEEA062782       	4	19990712	G	3431	066400700	RECEIVER        																	COCKPIT VOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										BAD SUPER FLAG DRIVER ON MAN. VOR CONV.																			 
1999072300333	19990723	00333		1999	7	23	HEEA062783       	4	19990712	G	2350	AMS44	AUDIO SELECTOR  																	DUAL CHANNEL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										NO MICROPHONE, OUT.																			 
1999072300334	19990723	00334		1999	7	23	HEEA062784       	4	19990712	G	2312	4000106010	CONTROL UNIT    																	THUMB WHEEL	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TONE INOPERATIVE ON CONTROL UNIT.																			 
1999072300335	19990723	00335	NE  	1999	7	23	HEEA062785       	1	19990712	G	2841	7645001078103	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										FUEL QUANTITY	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911MJ					760231				NR 1 NEEDLE STUCK AT ZERO ON FUEL QUANTITY INDICATOR.						1	G	7	2 	3U				H1NE    					 
1999072300336	19990723	00336	NE  	1999	7	23	HEEA062786       	1	19990713	G	2841	7645001078103	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										FUEL QUANTITY	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911MJ					760231				NR 1 NEEDLE STICKS AT ZERO INTERMITTENTLY ON FUEL QUANTITY INDICATOR.						1	G	7	2 	3U				H1NE    					 
1999072300337	19990723	00337		1999	7	23	HEEA062787       	1	19990713	G	2822	D10731814	ROTOR           																	BOOST PUMP	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										BOOST PUMP KICKED CIRCUIT BREAKER.   ARMATURE WAS FOUND TO BE BURNT.																			 
1999072300338	19990723	00338		1999	7	23	HEEA062788       	4	19990713	G	2200	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122G					760232				AFCS ACTUATOR KICKS.						1	G	7	2 	3U				H1NE    					 
1999072300339	19990723	00339		1999	7	23	HEEA062789       	4	19990713	G	3455	066104701	RECEIVER        			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5426U					760167				ADF NEEDLE DOES NOT POINT, ROTATES CONTINUOUSLY.						1	G	7	2 	3U				H1NE    					 
1999072300340	19990723	00340		1999	7	23	HEEA062790       	4	19990713	G	3434	066104400	RECEIVER        			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31219					760230				NO MARKER BEACON LIGHTS ON INDICATOR.						1	G	7	2 	3U				H1NE    					 
1999072300341	19990723	00341		1999	7	23	HEEA062791       	4	19990713	G	3434	066104400	RECEIVER        			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31219					760230				NO MARKER BEACON LIGHTS ON INDICATOR.						1	G	7	2 	3U				H1NE    					 
1999072300342	19990723	00342	NE  	1999	7	23	HEEA062792       	1	19990713	G	2430	A1077D	RELAY           			SKRSKY	S76   	S76A        	8143006	NE  										DC SYSTEM	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	15460					760223				GENERATOR WANTED TO COME ON-LINE DURING START SEQUENCE.   INTERMITTENT PROBLEM.						1	G	7	2 	3U				H1NE    					 
1999072300343	19990723	00343		1999	7	23	HEEA062793       	4	19990713	G	2340	AA25004	AUDIO CONTROL   			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	15460					760223				AUDIBLE NOISE HEARD FROM BOX AT DIFFERENT ENGINE LEVER POWER SETTINGS INTERMITTENTLY.  CAN HEAR IT ON ALL COMM AND FM CH	ANNELS THROUGHOUT ALL HEADSETS.					1	G	7	2 	3U				H1NE    					 
1999072300344	19990723	00344	NE  	1999	7	23	HEEA062794       	1	19990713	G	7921	7630807902106	BLOWER          			SKRSKY	S76   	S76A        	8143006	NE  										ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22342	11405				760096				CHAFE MARKS ON BLOWER HOUSING AND WEAR.   CORROSION ON SHAFT.						1	G	7	2 	3U				H1NE    					 
1999072300345	19990723	00345		1999	7	23	HEEA062795       	4	19990713	G	3457	8144002241B	GPS             			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				GPS LOCKS UP WHEN WPT BUTTON IS PUSHED.						1	G	7	2 	3U				H1NE    					 
1999072300346	19990723	00346		1999	7	23	HEEA062796       	4	19990713	G	3434	066104400	RECEIVER        																	COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										NO LIGHTS ON INDICATOR AND AUDIO DISTORTED.																			 
1999072300347	19990723	00347		1999	7	23	HEEA062797       	4	19990713	G	3457	8143902240B	GPS             			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31217					760229				GPS FAILED FREEZE UP AFTER TWO MINUTES OF BEING TURNED ON.  BENCH CHECK GOOD.						1	G	7	2 	3U				H1NE    					 
1999072300348	19990723	00348	GL  	1999	7	23	HEEA062798       	2	19990716	G	7230	23007208	DIFFUSER VANE   		23033191    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					ENGINE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	2761X	63   			CAC70781	45283	CAE860611			ENGINE REMOVED DUE TO LOW POWER.  COMPRESSOR DISASSEMBLED,TROUBLESHOOTING LOW POWER.   REPLACED VANE ASSY.  CURED POWER.	  VANE TRIED ON SEVERAL COMPRESSORS; ALL WERE LOW POWER.   REPLACED VANE.  INSTALLED A SERVICEABLE VANE ASSY.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999072300349	19990723	00349		1999	7	23	HEEA062799       	4	19990712	G	2312	064101900	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8592X					51508				TRANSCEIVER HAD STATIC AND BACKGROUND NOISE.						1	G	7	1 	3U				H2SW    					 
1999072300350	19990723	00350		1999	7	23	HEEA062800       	4	19990712	G	2312	064102300	VHF COMM        			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141PH					33197				TRANSCEIVER STAYS ON TRANSMIT ALL THE TIME.						1	G	7	2 	4U				H4SW    					 
1999072300351	19990723	00351		1999	7	23	HEEA062801       	4	19990712	G	2312	064105430	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	49EA					51507				TRANSCEIVER HAD INTERMITTENT SQUELCH.						1	G	7	1 	3U				H2SW    					 
1999072300352	19990723	00352		1999	7	23	HEEA062802       	4	19990712	G	3416	066106103	ALTIMETER       			BELL  	407   	407         		SW  										COCKPIT	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				RADAR ALTIMETER HAD INACCURATE READINGS AND FRAME PLATE BROKEN.						1	G	7	1 	3U			O	H2SW    					 
1999072300353	19990723	00353		1999	7	23	HEEA062803       	4	19990712	G	3451	066106602	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										DME	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893P					33012				TRANSCEIVER DOES NOT RECEIVE.						1	G	7	2 	4U				H4SW    					 
1999072300354	19990723	00354		1999	7	23	HEEA062804       	4	19990712	G	2312	071121540	COMM CONTROL    			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				DIGITAL SCREEN GOES BLANK AFTER A FEW MINUTES.						2	G	7	2 	4U				H10SW   					 
1999072300355	19990723	00355		1999	7	23	HEEA062805       	4	19990712	G	3457	13824120234	GPS RECEIVER    			BELL  	212   	212         	1181420	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1079U					31122				GPS RECEIVER FAILED ON SHORT FINAL.						1	G	7	1 	4U				H4SW    					 
1999072300356	19990723	00356	SW  	1999	7	23	HEEA062806       	1	19990712	G	6420	206010795105	BEARING         			BELL  	206   	206L3       	1182108	SW  										PITCH LINK	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31073					51519				MECHANICAL DAMAGE AROUND BEARING MORE THAN .010 INCH AND IN TWO PLACES.   REPLACED T/R P/C LINKS WITH SERVICEABLE PARTS.						1	G	7	1 	3U				H2SW    					 
1999072300357	19990723	00357		1999	7	23	HEEA062807       	4	19990712	G	3421	206075607103	GYRO            			BELL  	206   	206L1       	1182107	SW  										ATTITUDE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ATTITUDE GYRO HAD NO DEGREE TILT MARKED ON UNIT.						1	G	7	1 	3U				H2SW    					 
1999072300358	19990723	00358	SW  	1999	7	23	HEEA062808       	1	19990712	G	6240	206075681117	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										DUAL TACH	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8588X					51486				ROTOR TACHOMETER SLOW TO REACH 100 PERCENT.						1	G	7	1 	3U				H2SW    					 
1999072300359	19990723	00359	SW  	1999	7	23	HEEA062809       	1	19990712	G	6730	206076062003	SERVO           			BELL  	206   	206L3       	1182108	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	6603X					51412				LEAKING FROM FORWARD AND AFT SEALS.						1	G	7	1 	3U				H2SW    					 
1999072300360	19990723	00360	SW  	1999	7	23	HEEA062810       	1	19990712	G	6730	206076062003	SERVO           			BELL  	206   	206L3       	1182108	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	6603X					51412				LEAKING FROM FORWARD AND AFT SEALS.						1	G	7	1 	3U				H2SW    					 
1999072300361	19990723	00361	SW  	1999	7	23	HEEA062811       	1	19990712	G	2913	214076334101	SHAFT           			BELL  	214   	214ST       	1182106	SW  										HYDRAULIC PUMP	SHEARED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M					28102				HYDRAULIC PUMP SHEARED THE SHAFT.						2	G	7	2 	4U				H10SW   					 
1999072300362	19990723	00362		1999	7	23	HEEA062812       	4	19990712	G	3414	214175299107	CONNECTOR       			BELL  	214   	214ST       	1182106	SW  										MACH INDICATOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				CANNON PLUG OUT OF ROUND.  TIME SINCE REPAIR 0:00 HOURS.						2	G	7	2 	4U				H10SW   					 
1999072300363	19990723	00363		1999	7	23	HEEA062813       	4	19990712	G	3421	258719343	GYRO            			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				COPILOT'S HSI WOULD NOT SLAVE.  TIME SINCE REPAIR 101:25 HOURS.						2	G	7	2 	4U				H10SW   					 
1999072300364	19990723	00364		1999	7	23	HEEA062814       	4	19990712	G	3453	4530103	RECEIVER        			BELL  	206   	206L3       	1182108	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3108E					51498				ARNAV 21 INOPERATIVE.  NAV FLAG ON.						1	G	7	1 	3U				H2SW    					 
1999072300365	19990723	00365	SW  	1999	7	23	HEEA062815       	1	19990712	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC SYSTEM	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				CONTROL UNIT NOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999072300366	19990723	00366		1999	7	23	HEEA062816       	4	19990712	G	3457	80415100611	GPS             			BELL  	206   	206L4       	1182110	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	CFVEF					52071				NAV COMPUTER FAILED.						1	G	7	1 	3U			NC	H2SW    					 
1999072300367	19990723	00367		1999	7	23	HEEA062817       	4	19990712	G	3457	8143902240B	GPS             			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893N					33010				GPS WILL NOT TURN ON.						1	G	7	2 	4U				H4SW    					 
1999072300368	19990723	00368		1999	7	23	HEEA062818       	4	19990712	G	2370	9806020023	CVR             			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z					33077				CVR DOES NOT TEST.						1	G	7	2 	4U				H4SW    					 
1999072300369	19990723	00369		1999	7	23	HEEA062819       	4	19990712	G	2370	9806020023	CVR             			BELL  	212   	212         	1181420	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5736D					31135				CVR WILL NOT TEST.						1	G	7	1 	4U				H4SW    					 
1999072300370	19990723	00370		1999	7	23	HEEA062820       	4	19990712	G	2562	ELT910	TRANSMITTER     			BELL  	206   	206L1       	1182107	SW  										ELT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2772A					45311				ELT UNIT ON WHEN SWITCHED TO ARM.  TIME SINCE REPAIR 0:00 HOURS.						1	G	7	1 	3U				H2SW    					 
1999072300371	19990723	00371		1999	7	23	HEEA062821       	4	19990712	G	3442	MI5852013	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T					33112				POWERS UP THEN SHUTS DOWN.						1	G	7	2 	4U				H4SW    					 
1999072300372	19990723	00372		1999	7	23	HEEA062822       	4	19990712	G	3421	1113034	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893P					33012				ATTITUDE INDICATOR WILL NOT ADJUST,  ERRATIC IN FLIGHT.						1	G	7	2 	4U				H4SW    					 
1999072300373	19990723	00373		1999	7	23	HEEA062823       	4	19990712	G	3421	1113034	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	PRECESSING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				ATTITUDE INDICATOR PRECESSES AND HORIZONTAL CONTROL KNOB CAUSES BALL TO REACT IN A SKIPPING MOTION.						1	G	7	2 	4U				H4SW    					 
1999072300374	19990723	00374		1999	7	23	HEEA062824       	4	19990712	G	2210	7000299901	CONTROLLER      			BELL  	412   	412         	1182202	SW  										AUTOPILOT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3911L					33023				SAS LIGHT INOPERATIVE ON AUTOPILOT CONTROL.  SEGMENT LABEL MISSING.						1	G	7	2 	4U				H4SW    					 
1999072300375	19990723	00375		1999	7	23	HEEA062825       	4	19990712	G	2312	066106200	TRANSPONER      			BELL  	206   	206L4       	1182110	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7074W					52033				TRANSCEIVER OUT OF FREQUENCY.   PERFORMED PRELIMINARY INSPECTION AND FOUND FREQUENCY SLIGHTLY OUT OF LIMITS.  REPLACED V	101 CAVITY.  ADJUSTED POWER FREQUENCY, AND UNIT BENCH CHECK GOOD.					1	G	7	1 	3U			NC	H2SW    					 
1999072300376	19990723	00376	SW  	1999	7	23	HEEA062826       	1	19990712	G	5313	206031314073A	LONGERON        			BELL  	206   	206L4       	1182110	SW  										TAIL BOOM	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7074W					52033				LONGERON CRACKED AT MOST FORWARD OUTBOARD RIVET HOLE AT TAILBOOM MOUNT.  REPLACED WITH SERVICEABLE LONGERON.						1	G	7	1 	3U			NC	H2SW    					 
1999072300377	19990723	00377	SW  	1999	7	23	HEEA062827       	1	19990712	G	3246	206053184102	TUBE            			BELL  	206   	206L3       	1182108	SW  										SKID	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	129MR					51129				SKID TUBE CORRODED BEYOND LIMITS.   REPLACED WITH SERVICEABLE SKID TUBE.						1	G	7	1 	3U				H2SW    					 
1999072300378	19990723	00378	SW  	1999	7	23	HEEA062828       	1	19990712	G	3246	206323002	CROSSTUBE       			BELL  	206   	206L3       	1182108	SW  										SKID	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	129MR					51129				CROSSTUBE CORRODED BEYOND LIMITS UNDER SUPPORT PAD.  REPLACED WITH SERVICEABLE CROSSTUBE.						1	G	7	1 	3U				H2SW    					 
1999072300379	19990723	00379	SW  	1999	7	23	HEEA062829       	1	19990712	G	3246	206324007	TUBE            			BELL  	206   	206L1       	1182107	SW  										SKID	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	83MT					45492				CORROSION BEYOND LIMITS AT SKID SHOES UNDER CROSSTUBE ATTACH POINTS.  REPLACED WITH SERVICEABLE SKID TUBE.						1	G	7	1 	3U				H2SW    					 
1999072300380	19990723	00380	SW  	1999	7	23	HEEA062830       	1	19990712	G	6310	PHI206052	MAGNETIC SEAL   			BELL  	206   	206L3       	1182108	SW  										M/R GEARBOX	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	49EA					51507				MAGNETIC SEAL LEAKING FLUID.   REPLACED WITH SERVICEABLE SEAL ASSY.						1	G	7	1 	3U				H2SW    					 
1999072300381	19990723	00381	SW  	1999	7	23	HEEA062831       	1	19990712	G	6520	212040004009	GEARBOX         			BELL  	412   	412         	1182202	SW  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22347	2484 				36005				COULD NOT MOUNT GEARBOX - FOUND STUDS BENT.   REPLACED WITH SERVICEABLE ASSY.						1	G	7	2 	4U				H4SW    					 
1999072300382	19990723	00382	SW  	1999	7	23	HEEA062832       	1	19990712	G	6220	412010182101	BEARING         			BELL  	412   	412         	1182202	SW  										PITCH LINK	BINDING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893N	2315 				33010				BINDING IN CYCLIC WITH HYDRAULIC POWER ON.  REPLACED WITH SERVICEABLE ASSY.						1	G	7	2 	4U				H4SW    					 
1999072300383	19990723	00383	SW  	1999	7	23	HEEA062833       	1	19990712	G	2460	MS2414202	RELAY           			BELL  	412   	412         	1182202	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T					33112				RELAY WILL NOT LET GENERATOR COME ON LINE.  REPLACED WITH SERVICEABLE ASSY.						1	G	7	2 	4U				H4SW    					 
1999072300384	19990723	00384	GL  	1999	7	23	HEEA062834       	2	19990712	G	7321	23054164	SENSOR          			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					FADEC	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				N2 SENSOR CAUSING FADEC DEGRADE LIGHT.   REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999072300385	19990723	00385	SW  	1999	7	23	HEEA062835       	1	19990712	G	3010	23007827F	VALVE           			BELL  	407   	407         		SW  										ANTI-ICE	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				ENGINE ANTI-ICE ON WARNING LIGHT COMES ON INTERMITTENTLY.  REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U			O	H2SW    					 
1999072300386	19990723	00386	GL  	1999	7	23	HEEA062836       	2	19990712	G	7320	23056914	TRANSDUCER      			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				TRANSDUCER CAUSED FADEC DEGRADE LIGHT TO ILLUMINATE.   REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999072300387	19990723	00387	GL  	1999	7	23	HEEA062837       	2	19990712	G	7261	23063144	FILTER          			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE	CLOGGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724PH					53327				ENGINE OIL FILTER BYPASS BUTTON POPPED AFTER RESETTING TWICE.  REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999072300388	19990723	00388	GL  	1999	7	23	HEEA062838       	2	19990712	G	7261	23063144	FILTER          			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE	CLOGGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				ENGINE OIL FILTER BYPASS BUTTON POPPED.  REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999072300389	19990723	00389	GL  	1999	7	23	HEEA062839       	2	19990712	G	7261	23063144	FILTER          			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE	CLOGGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH					53209				ENGINE OIL FILTER BYPASS INDICATOR EXTENDED. REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999072300390	19990723	00390	GL  	1999	7	23	HEEA062840       	2	19990712	G	7261	23063144	FILTER          			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE	CLOGGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				ENGINE OIL FILTER BYPASS INDICATOR EXTENDED. REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999072300391	19990723	00391	GL  	1999	7	23	HEEA062841       	2	19990712	G	7412	23064130	IGNITOR BOX     			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				DIFFICULT TO START ENGINE.  REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999072300392	19990723	00392	GL  	1999	7	23	HEEA062842       	2	19990712	G	7320	23065805	HARNESS         			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				HARNESS CAUSING FADEC DEGRADE AND RESTART FAULT LIGHTS.  REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999072300393	19990723	00393		1999	7	23	HEEA062843       	4	19990712	G	2350	AMS44	AUDIO SELECTOR  			BELL  	407   	407         		SW  										DUAL CHANNEL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				COPILOT'S TRANSMIT LIGHT IS ALWAYS ON AND THE HEADSET IS DEAD.						1	G	7	1 	3U			O	H2SW    					 
1999072300394	19990723	00394		1999	7	23	HEEA062844       	4	19990712	G	2312	064101902	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	206LS					51070				DIGITS FADE OUT AFTER 30 MINUTES OF USE.						1	G	7	1 	3U				H2SW    					 
1999072300395	19990723	00395		1999	7	23	HEEA062845       	4	19990712	G	2350	066105571	AUDIO PANEL     			BELL  	206   	206L4       	1182110	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7074W					52033				CAN'T TRANSMIT OFF FM CHANNEL FROM COPILOT'S SIDE.						1	G	7	1 	3U			NC	H2SW    					 
1999072300396	19990723	00396		1999	7	23	HEEA062846       	4	19990712	G	2312	066106200	TRANSPONDER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251Y					51556				TRANSCEIVER INOPERATIVE.  DOES NOT TURN ON.						1	G	7	1 	3U				H2SW    					 
1999072300397	19990723	00397	SW  	1999	7	23	HEEA062847       	1	19990712	G	7810	206064300005	EXHAUST STACK   			BELL  	206   	206L3       	1182108	SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				MOUNTING FLANGE IS WARPED BEYOND USE, CRACK WAS NOTED AT REPAIR AREA.						1	G	7	1 	3U				H2SW    					 
1999072300398	19990723	00398	SW  	1999	7	23	HEEA062848       	1	19990712	G	2430	206075447007	REGULATOR       			BELL  	206   	206L3       	1182108	SW  										DC SYSTEM	FLUCTUATING     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251Y					51556				VOLTAGE REGULATOR FLUCTUATING.						1	G	7	1 	3U				H2SW    					 
1999072300399	19990723	00399	SW  	1999	7	23	HEEA062849       	1	19990712	G	2430	206075447007	REGULATOR       			BELL  	206   	206L3       	1182108	SW  										DC SYSTEM	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251Y					51556				VOLTAGE REGULATOR INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999072300400	19990723	00400	SW  	1999	7	23	HEEA062850       	1	19990712	G	6710	206076062003	SERVO           			BELL  	206   	206L3       	1182108	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251Y	18809				51556				CYLINDER LEAKING EXCESSIVELY AT AFT END OF PISTON, AND SERVO VALVE HAS HIGH INPUT FORCE AT LEVERS.						1	G	7	1 	3U				H2SW    					 
1999072300401	19990723	00401	GL  	1999	7	23	HEEA062851       	2	19990712	G	7314	3881005	PUMP            			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					FUEL SYSTEM	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2133X	17053				45634				FUEL PUMP SUCKING AIR.  PERFORMED SPLINE INSPECTION AND FOUND DRIVE SPLINES TO BE PITTED.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999072300402	19990723	00402		1999	7	23	HEEA062852       	4	19990712	G	3453	4530093	RECEIVER        			BELL  	206   	206L3       	1182108	SW  										LORAN	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	205FC					51130				RECEIVER HAD ERRATIC OPERATION.						1	G	7	1 	3U				H2SW    					 
1999072300403	19990723	00403		1999	7	23	HEEA062853       	4	19990712	G	3422	5050031904	GYRO            			BELL  	407   	407         		SW  										COCKPIT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724PH					53327				WHEN DIRECTIONAL GYRO UNIT IS MOVED, LOOSE PARTS ARE HEARD INSIDE CAN.						1	G	7	1 	3U			O	H2SW    					 
1999072300404	19990723	00404	SW  	1999	7	23	HEEA062854       	1	19990712	G	5321	205030280141	DECK            			BELL  	412   	412         	1182202	SW  										SERVICE DECK	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				SERVICE DECK SEPARATED BEYOND ALLOWABLE REPAIR.						1	G	7	2 	4U				H4SW    					 
1999072300405	19990723	00405	SW  	1999	7	23	HEEA062855       	1	19990712	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	WON'T TRACK     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K	3011 				33020				BLADE WILL NOT TRACK.						1	G	7	2 	4U				H4SW    					 
1999072300406	19990723	00406		1999	7	23	HEEA062856       	4	19990712	G	3444	066104802	RADAR ALTIMETER 			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7128R					36007				RADAR ALTIMETER WILL NOT INDICATE ALTITUDE.						1	G	7	2 	4U				H4SW    					 
1999072300407	19990723	00407		1999	7	23	HEEA062857       	4	19990712	G	3444	066106103	RADAR ALTIMETER 			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2772A					45311				RADAR ALTIMETER POWER OUT BELOW 25 MILLIWATTS.						1	G	7	1 	3U				H2SW    					 
1999072300408	19990723	00408		1999	7	23	HEEA062858       	4	19990712	G	3444	066305401	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										RADIO ALTIMETER	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2772A					45311				BROKEN AND BENT GEARS, CAUSING IT HARD TO TURN SHAFT.						1	G	7	1 	3U				H2SW    					 
1999072300409	19990723	00409	SW  	1999	7	23	HEEA062859       	1	19990712	G	5260	206331119	STEP            			BELL  	206   	206L3       	1182108	SW  										FUSELAGE	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	129MR					51129				LEFT AND RIGHT CABIN STEPS CORRODED BEYOND LIMITS.						1	G	7	1 	3U				H2SW    					 
1999072300410	19990723	00410	SW  	1999	7	23	HEEA062860       	1	19990712	G	5260	206331120	STEP            			BELL  	206   	206L3       	1182108	SW  										FUSELAGE	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	129MR					51129				LEFT AND RIGHT CABIN STEPS CORRODED BEYOND LIMITS.						1	G	7	1 	3U				H2SW    					 
1999072300411	19990723	00411	SW  	1999	7	23	HEEA062861       	1	19990712	G	2435	23032048	GENERATOR       			BELL  	206   	206B3       	1181506	SW  										START/GENERATOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3181J	8792 				3771				STARTER/GENERATOR HAD HIGH FREQUENCY VIBRATION.						1	G	7	1 	3U				H2SW    					 
1999072300412	19990723	00412	SW  	1999	7	23	HEEA062862       	1	19990712	G	6320	206040530001	MAIN CASE       			BELL  	206   	206L1       	1182107	SW  										M/R GEARBOX	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1073W					45386				MAIN CASE ASSEMBLY LINERS WORN AND CORRODED.						1	G	7	1 	3U				H2SW    					 
1999072300413	19990723	00413	SW  	1999	7	23	HEEA062863       	1	19990712	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	HEAVY           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K	6248 				33020				BLADE CLIMBS EXCESSIVELY IN FLIGHT AND IS HEAVY.						1	G	7	2 	4U				H4SW    					 
1999072300414	19990723	00414	SW  	1999	7	23	HEEA062864       	1	19990712	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K	6913 				33020				BLADE CLIMBS EXCESSIVELY.						1	G	7	2 	4U				H4SW    					 
1999072300415	19990723	00415	SW  	1999	7	23	HEEA062865       	1	19990712	G	6730	206076062003	SERVO           			BELL  	206   	206L3       	1182108	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	8594X	19926				51531				STATIC LEAK EXCESSIVE AT SERVO VALVE, BOOT TORN AND DETERIORATED.						1	G	7	1 	3U				H2SW    					 
1999072300416	19990723	00416	SW  	1999	7	23	HEEA062866       	1	19990712	G	6420	212010750105	BLADE           		212011701101	BELL  	412   	412         	1182202	SW  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008	1578 			TR112096	36004				F.O.D. HOLE IN LEADING EDGE OF BLADE.						1	G	7	2 	4U				H4SW    					 
1999072300417	19990723	00417	SW  	1999	7	23	HEEA062867       	1	19990712	G	2435	23081018	STARTER         			BELL  	206   	206L3       	1182108	SW  										START/GENERATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31073	15603				51519				STARTER/GENERATOR DOES NOT ENGAGE.						1	G	7	1 	3U				H2SW    					 
1999072300418	19990723	00418		1999	7	23	HEEA062869       	4	19990713	G	3442	40005040301	DRIVE ASSY      			BELL  	214   	214ST       	1182106	SW  										RADAR ANNTENA	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				TILT INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999072300419	19990723	00419	SW  	1999	7	23	HEEA062870       	1	19990713	G	3246	206323018	CROSSTUBE       			BELL  	206   	206L1       	1182107	SW  										SKID	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	83MT					45492				CORROSION BEYOND LIMITS IN ZONE 1.						1	G	7	1 	3U				H2SW    					 
1999072300420	19990723	00420		1999	7	23	HEEA062871       	4	19990713	G	3442	40008310105	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				TRANSCEIVER WILL NOT PAINT TARGETS, FOUND R/T FAULT.						2	G	7	2 	4U				H10SW   					 
1999072300421	19990723	00421		1999	7	23	HEEA062872       	4	19990713	G	2312	066107800	RECEIVER        			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2149S					36002				VHF NAV RECEIVER UNRELIABLE.						1	G	7	2 	4U				H4SW    					 
1999072300422	19990723	00422		1999	7	23	HEEA062873       	4	19990713	G	3457	1624811	ANTENNA         			BELL  	412   	412         	1182202	SW  										GPS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023					33080				GPS SIGNAL INTERMITTENT.						1	G	7	2 	4U				H4SW    					 
1999072300423	19990723	00423	SW  	1999	7	23	HEEA062874       	1	19990713	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L3       	1182108	SW  										DROOP COMPART	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8594X					51531				NE RPM WILL NOT RETURN TO THE SAME SETTING EVERY TIME BY ABOUT 4 PERCENT.  ACTUATOR IS JUMPING A GEARTOOTH.						1	G	7	1 	3U				H2SW    					 
1999072300424	19990723	00424		1999	7	23	HEEA062875       	4	19990713	G	3453	069102439	VHF COMM        			BELL  	206   	206L4       	1182110	SW  										LORAN	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	CFVEF					52071				VHF COMM NAV UNIT WILL NOT TURN OFF.						1	G	7	1 	3U			NC	H2SW    					 
1999072300425	19990723	00425		1999	7	23	HEEA062876       	4	19990713	G	3422	2891ESR	GYRO            			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2124Z					45646				DIRECTIONAL GYRO HAS NO SLAVE OUTPUT.  TIME SINCE REPAIR 75:30 HOURS.						1	G	7	1 	3U				H2SW    					 
1999072300426	19990723	00426	SW  	1999	7	23	HEEA062877       	1	19990713	G	2822	9A1746	PUMP            			BELL  	214   	214ST       	1182106	SW  										ENGINE FUEL	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				BOLT HOLES TOO LARGE FOR REQUIRED BOLTS.						2	G	7	2 	4U				H10SW   					 
1999072300427	19990723	00427	GL  	1999	7	23	HEEA062878       	2	19990713	G	7314	3881005	SPLINES         			BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					FUEL PUMP	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6160Y	4089 				51609				FUEL PUMP HAD WORN DRIVE SHAFT SPLINES AND GEAR SPLINES.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999072300428	19990723	00428		1999	7	23	HEEA062879       	4	19990713	G	3442	MI5852013	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K					33020				INDICATOR HAS NO DISPLAY.						1	G	7	2 	4U				H4SW    					 
1999072300429	19990723	00429		1999	7	23	HEEA062880       	4	19990713	G	3452	066106200	TRANSPONDER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6160Z					51610				TRANSCEIVER IDENT LIGHT STAYS ON.						1	G	7	1 	3U				H2SW    					 
1999072300430	19990723	00430		1999	7	23	HEEA062881       	4	19990713	G	3457	8143902240B	GPS             			BELL  	412   	412         	1182202	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7128R					36007				GPS INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999072300431	19990723	00431		1999	7	23	HEEA062882       	4	19990713	G	2312	071121525	CONTROL UNIT    			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				CONTROL UNIT NOT CHANNELING CORRECTLY AND DISPLAY HAD HOT SPOTS.						2	G	7	2 	4U				H10SW   					 
1999072300432	19990723	00432		1999	7	23	HEEA062883       	4	19990713	G	2312	064102300	VHF COMM        			BELL  	412   	412         	1182202	SW  										COCKPIT	WEAK            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	800Y					33134				TRANSMITS AND RECEIVES WEAK AND BREAKS SQUELCH INTERMITTENTLY.						1	G	7	2 	4U				H4SW    					 
1999072300433	19990723	00433		1999	7	23	HEEA062884       	4	19990713	G	2210	214074305105	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										FBW ELEVATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	824H					28119				ELEVATOR AMPLIFIER WILL NOT ENGAGE.						2	G	7	2 	4U				H10SW   					 
1999072300434	19990723	00434		1999	7	23	HEEA062885       	4	19990713	G	2210	214074305105	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										FBW ELEVATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	824H					28119				ELEVATOR AMPLIFIER WILL NOT MONITOR TEST CORRECTLY.						2	G	7	2 	4U				H10SW   					 
1999072300435	19990723	00435		1999	7	23	HEEA062886       	4	19990713	G	2210	214074303115	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										AUTOFLIGHT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	824H					28119				DURING TESTING THE AARS DRIFTS IN PITCH AND ROLL.  ALSO AARS WILL NOT ALIGN PROPERLY.						2	G	7	2 	4U				H10SW   					 
1999072300436	19990723	00436	GL  	1999	7	23	HEEA062887       	2	19990713	G	7320	23069551	HMU             			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				RESTART FAULT AND FADEC DEGRADE LIGHTS ILLUMINATED ON SHUTDOWN. REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999072300437	19990723	00437	GL  	1999	7	23	HEEA062888       	2	19990713	G	7320	23069551	HMU             			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				HMU FAILED DRIVE SHAFT BACKLASH CHECK.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999072300438	19990723	00438		1999	7	23	HEEA062889       	1	19990715	G	3020	NAS1375A12SA022	DUCT            																	ANTI-ICE SYSTEM	MISMARKED       	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										DUCT HOSE MISIDENTIFIED.  THE PICK TICKET AND PART DO NOT MATCH.																			 
1999072300439	19990723	00439	SW  	1999	7	23	HEEA062890       	1	19990715	G	5347	412030100123	SEAT TRACK      			BELL  	412   	412         	1182202	SW  										COCKPIT	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										TRACK ASSY MISMANUFACTURED.  OUTBOUND HOLES DO NOT LINE UP, MISDRILLED.						1	G	7	2 	4U				H4SW    					 
1999072300440	19990723	00440	SW  	1999	7	23	HEEA062891       	1	19990716	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										START/GENERATOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724PH	574  				53327				STARTER/GENERATOR HAD WORN BRUSHES.						1	G	7	1 	3U			O	H2SW    					 
1999072300441	19990723	00441	SW  	1999	7	23	HEEA062892       	1	19990716	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										START/GENERATOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8595X	1573 				53267				FAILED 300 HOUR BRUSH INSPECTION.  INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES WERE EXCESSIVELY WORN.						1	G	7	1 	3U			O	H2SW    					 
1999072300442	19990723	00442	SW  	1999	7	23	HEEA062893       	1	19990716	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	INOPERATIVE     	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	23023					33080				STEP ACTUATOR RECEIVED INOPERATIVE.  ACTUATOR WILL NOT RETRACT.						1	G	7	2 	4U				H4SW    					 
1999072300443	19990723	00443	SW  	1999	7	23	HEEA062894       	1	19990716	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										STEP ACTUATOR WOULD NOT RAISE STEP TO FULL UP POSITION.						1	G	7	2 	4U				H4SW    					 
1999072300444	19990723	00444	SW  	1999	7	23	HEEA062895       	1	19990716	G	2435	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										START/GENERATOR	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	8045T					28101				STARTER KICKED OFF LINE AT 10 PERCENT NG.						2	G	7	2 	4U				H10SW   					 
1999072300445	19990723	00445	SW  	1999	7	23	HEEA062896       	1	19990716	G	6210	407015001107	BLADE           			BELL  	407   	407         		SW  										MAIN ROTOR	PEELING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	2327 				53016				MAIN ROTOR BLADE PAINT PEELING.						1	G	7	1 	3U			O	H2SW    					 
1999072300446	19990723	00446	SW  	1999	7	23	HEEA062897       	1	19990716	G	6210	407015001107	BLADE           			BELL  	407   	407         		SW  										MAIN ROTOR	PEELING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	2327 				53016				MAIN ROTOR PAINT PEELING.						1	G	7	1 	3U			O	H2SW    					 
1999072300447	19990723	00447	EU  	1999	7	23	HEEA062898       	1	19990712	G	2612	0301017690	LEAD            			SNIAS 	350   	AS350B2     	8680813	EU  										THERMOCOUPLE	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				LEADS ON THERMOCOUPLE BROKEN.   REPLACED WITH SERVICEABLE HARNESS.						1	G	7	1 	3U				H9EU    					 
1999072300448	19990723	00448		1999	7	23	HEEA062899       	4	19990712	G	2312	064101900	TRANSCEIVER     			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4573B					S673				INOPERATIVE.  WILL NOT COME ON. PERFORMED PRELIMINARY INSPECTION.  FOUND UNIT TO BE DRAWING CURRENT, BUT ALL POWER SUPPL	Y VOLTAGES ARE LOW.					1	G	7	2 	3U				H3EU    					 
1999072300449	19990723	00449		1999	7	23	HEEA062900       	4	19990712	G	2312	064101902	TRANSCEIVER     			BOLKMS	105   	BO105CBS    	5626008	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RS					S670				DOES NOT RECEIVE OR TRANSMIT. PERFORMED PRELIMINARY INSPECTION AND FOUND C627 ON TRANSMITTER BOARD BURNT.						1	G	7	2 	3U			NC	H3EU    					 
1999072300450	19990723	00450		1999	7	23	HEEA062901       	4	19990712	G	2312	069102505	TRANSCEIVER NAV 			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4294R					S860				NAV TRANSCEIVER SQUELCH CONSTANTLY BREAKS.						1	G	7	2 	3U				H3EU    					 
1999072300451	19990723	00451		1999	7	23	HEEA062902       	4	19990712	G	2312	4000106010	CONTROL UNIT    			BOLKMS	105   	BO105S      	5626006	EU  										THUMBWHEEL	MISMARKED       	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	911DD					S830				THUMBWHEEL NOT CORRESPONDING TO DIGITAL READOUTS.						1	G	7	2 	3U				H3EU    					 
1999072300452	19990723	00452		1999	7	23	HEEA062903       	4	19990712	G	2312	4000106000	CONTROL UNIT    			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				CONTROL UNIT INOPERATIVE.  WILL NOT TRANSMIT OR RECEIVE.						1	G	7	1 	3U				H9EU    					 
1999072300453	19990723	00453		1999	7	23	HEEA062904       	4	19990712	G	2312	4000106010	CONTROL UNIT    			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911HM					S683				NUMBERS ON CONTROL UNIT INTERMITTENTLY CHANGING.						1	G	7	2 	3U				H3EU    					 
1999072300454	19990723	00454		1999	7	23	HEEA062905       	4	19990712	G	2312	40001452502	TRANSCEIVER     			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				TRANSMIT LIGHT FLASHES AND RADIO TRANSMIT IS BROKEN WHEN AIRCRAFT GENERATOR IS TURNED ON.						1	G	7	1 	3U				H9EU    					 
1999072300455	19990723	00455	EU  	1999	7	23	HEEA062906       	1	19990712	G	6520	4619003003	TRANSMISSION    			BOLKMS	105   	BO105S      	5626006	EU  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03		5499 								TAIL ROTOR TRANS HAD CRACKED MAIN CASE.  REPLACED WITH SERVICEABLE PART.						1	G	7	2 	3U				H3EU    					 
1999072300456	19990723	00456	EU  	1999	7	23	HEEA062907       	1	19990712	G	6520	4619210902	BEVEL GEAR SET  			BOLKMS	105   	BO105CBS    	5626008	EU  										M/R GEARBOX	SPALLED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RS	7    				S670				BEVEL GEAR SET SPALLING.						1	G	7	2 	3U			NC	H3EU    					 
1999072300457	19990723	00457	EU  	1999	7	23	HEEA062908       	1	19990712	G	6720	741C000005	ACTUATOR        			BOLKMS	117   	BK117A4     	5626017	EU  										TAIL ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	8765J					7054				TAIL ROTOR ACTUATOR LEAKS.						1	G	7	2 	3U				H13EU   					 
1999072300458	19990723	00458		1999	7	23	HEEA062909       	4	19990712	G	2350	AMS44	AUDIO SELECTOR  			BOLKMS	105   	BO105S      	5626006	EU  										DUAL CHANNEL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8199J					S826				CABIN ICS SYSTEM HAS BACKGROUND NOISE WHILE IN-FLIGHT AND AFTER START WITH VOX OFF.						1	G	7	2 	3U				H3EU    					 
1999072300459	19990723	00459		1999	7	23	HEEA062910       	4	19990712	G	2312	4000106010	CONTROL UNIT    			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911HM					S683				FREQUENCY DISPLAY INTERMITTENT ON CONTROL UNIT.						1	G	7	2 	3U				H3EU    					 
1999072300460	19990723	00460	EU  	1999	7	23	HEEA062911       	1	19990712	G	6410	10531980	BLADE           			BOLKMS	105   	BO105S      	5626006	EU  										TAIL ROTOR	PEELING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721MB	2744 				S752				PAINT PEELING FROM BLADES.						1	G	7	2 	3U				H3EU    					 
1999072300461	19990723	00461		1999	7	23	HEEA062912       	4	19990712	G	2312	40001452500	TRANSCEIVER     			BOLKMS	117   	BK117A4     	5626017	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8765J					7054				AIRCRAFT WILL NOT TRANSMIT OR RECEIVE ON 154.250 PL32, 155.865, 154.295, 155.340, PL06, TRANSMITS ON 463.150 PL32 OR REC	EIVE ON 468.150 PL32.					1	G	7	2 	3U				H13EU   					 
1999072300462	19990723	00462		1999	7	23	HEEA062913       	4	19990713	G	3451	066107001	TRANSCEIVER     			BOLKMS	117   	BK117B1     	5626012	EU  										DME	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	217UC					7152				DME INOPERATIVE.						1	G	7	2 	3U				H13EU   					 
1999072300463	19990723	00463		1999	7	23	HEEA062914       	4	19990713	G	3457	0845000000	GPS             			BOLKMS	117   	BK117B2     	5626013	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	134AE					7237				BENCH CHECK REQUIRED.  FOUND SELECTOR KNOBS INTERMITTENT WHEN TURNED.						1	G	7	2 	3U			NC	H13EU   					 
1999072300464	19990723	00464		1999	7	23	HEEA062915       	4	19990713	G	2340	AA95759	AUDIO CONTROL   			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	135AE					S838				AUDIO CONTROL CAUSED LOUD SQUEAL IN HEADSETS.						1	G	7	2 	3U				H3EU    					 
1999072300465	19990723	00465		1999	7	23	HEEA062916       	4	19990713	G	3451	066107001	TRANCEIVER      			BOLKMS	105   	BO105S      	5626006	EU  										DME	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	205UC					S668				NO POWER TO DME INDICATOR.						1	G	7	2 	3U				H3EU    					 
1999072300466	19990723	00466	EU  	1999	7	23	HEEA062917       	1	19990713	G	3320	3014C	POWER SUPPLY    			BOLKMS	105   	BO105S      	5626006	EU  										CABIN	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	624MB					S751				POWER UNIT BLOWS FUSE.						1	G	7	2 	3U				H3EU    					 
1999072300467	19990723	00467	EU  	1999	7	23	HEEA062918       	1	19990713	G	7712	30802012	INDICATOR       			BOLKMS	117   	BK117B2     	5626013	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	136AE					7234				NR 1 AND NR 2 NEEDLES WOULD NOT CORRECT FOR THE ZERO SCALE.  SLOPE ADJUST WAS WORKING NORMALLY.  LOW READINGS STAYED AT 	OR ABOVE 26 PERCENT.					1	G	7	2 	3U			NC	H13EU   					 
1999072300468	19990723	00468		1999	7	23	HEEA062919       	4	19990713	G	2350	066105571	AUDIO PANEL     			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3071K					S859				RETAINING RING HAS SNAP RING AND WASHER MISSING FROM BACK OF UNIT.  SCREW PULLS OUT OF THE BACK OF UNIT.						1	G	7	2 	3U				H3EU    					 
1999072300469	19990723	00469	EU  	1999	7	23	HEEA062920       	1	19990713	G	2431	BD63	CONNECTOR       			BOLKMS	105   	BO105S      	5626006	EU  										BATTERY	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721MB					S752				POSITIVE RECEPTACLE FAILED PIN TEST WITH TOOL P/N  PHI10420.   REPLACED WITH SERVICEABLE PART.						1	G	7	2 	3U				H3EU    					 
1999073000133	19990730	00133	GL  	1999	7	30	HEEA062968       	2	19990719	G	7230	23004513	CARBON SEAL     		23051643    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30P     	03013	GL  					NR 1 BEARING	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545X	169  			CAC90185	760050	CAE890397S			ENGINE REMOVED DUE TO NR 1 SEAL LEAK.  UPON INSPECTION, FOUND SLOT WEAR IN CARBON SEAL RING.  PART SCRAPPED.						1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999073000134	19990730	00134	GL  	1999	7	30	HEEA062969       	2	19990723	G	7230	23064593	DIFFUSER        		23051643    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30P     	03013	GL  					NR 2 BEARING	LEAKING         	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	1545X				CAC90185	760050	CAE890397S			ENGINE REMOVED DUE TO METAL IN OIL.  FOUND REAR SUPPORT MAJOR SEAL LIFTING AND CHROME FITTING FLAKING IN NR 2 BEARING BO	RE.  REPLACED WITH SERVICEABLE REAR DIFFUSER.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999073000135	19990730	00135	GL  	1999	7	30	HEEA062970       	2	19990723	G	7260	6893672	PINION GEAR     		23035179    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					GEARBOX	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545X				CAG90833	760050	CAE890825S			ENGINE REMOVED DUE TO METAL IN OIL.  FOUND CAUSE:  PICKOUT IN GEAR TEETH.   REPLACED WITH SERVICEABLE GEAR.  SCRAPPED GE	AR.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999073000136	19990730	00136	SW  	1999	7	30	HEEA062971       	1	19990719	G	6710	214001423109	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										MAIN ROTOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ACTUATOR WILL NOT ACTUATE.  BHT FUNCTION TEST ACCEPTANCE DATED 08-04-99.  GLOBE MOTORS ACCEPTANCE STAMPED 07-28-98.						2	G	7	2 	4U				H10SW   					 
1999073000137	19990730	00137	SW  	1999	7	30	HEEA062972       	1	19990721	G	6310	406340102101	CARBON SEAL     			BELL  	407   	407         		SW  										M/R DRIVE	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	467PH					53142				CARBON SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999073000138	19990730	00138	SW  	1999	7	30	HEEA062973       	1	19990721	G	6310	406340102101	CARBON SEAL     			BELL  	407   	407         		SW  										M/R DRIVE	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	8595X					53267				CARBON SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999073000139	19990730	00139		1999	7	30	HEEA062974       	4	19990722	G	2210	214074303115	AMPLIFIER ASSY  			BELL  	214   	214ST       	1182106	SW  										AUTOFLIGHT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5748M					28102				AMPLIFIER WILL NOT TEST OR STAY ON-LINE.						2	G	7	2 	4U				H10SW   					 
1999073000140	19990730	00140	SW  	1999	7	30	HEEA062979       	1	19990723	G	6220	407010103101	PITCH HORN      			BELL  	407   	407         		SW  										MAIN ROTOR	CORRODED        	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	447PH	2496 				53114				PITCH HORN HAS CORROSION DUE TO NO PREVENTIVE MAINTENANCE.						1	G	7	1 	3U			O	H2SW    					 
1999073000141	19990730	00141	SW  	1999	7	30	HEEA062980       	1	19990723	G	6230	406010126107	DRIVE RING      			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				SPLINE WORN BEYOND LIMITS ON DRIVE RING SET.						1	G	7	1 	3U			O	H2SW    					 
1999073000142	19990730	00142	SW  	1999	7	30	HEEA062981       	1	19990723	G	6220	407010107103	BEARING         			BELL  	407   	407         		SW  										MAIN ROTOR	PEELING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	1255 				53114				BEARING  HAS BLUE EPOXY PEELING.						1	G	7	1 	3U			O	H2SW    					 
1999073000143	19990730	00143	SW  	1999	7	30	HEEA062982       	1	19990723	G	6220	407310100103	DAMPER          			BELL  	407   	407         		SW  										MAIN ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	2496 				53114				CORROSION DUE TO NO PREVENTIVE MAINTENANCE.						1	G	7	1 	3U			O	H2SW    					 
1999073000144	19990730	00144	SW  	1999	7	30	HEEA062983       	1	19990723	G	2435	206062200113	START/GENERATOR 			BELL  	407   	407         		SW  										ENGINE	DAMAGED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	409PH					53059				PROTECTIVE SCREEN CAME LOOSE AND SHREDDED THROUGH STARTER/GENERATOR.						1	G	7	1 	3U			O	H2SW    					 
1999073000145	19990730	00145	SW  	1999	7	30	HEEA062986       	1	19990723	G	7712	407375003107	INDICATOR       			BELL  	407   	407         		SW  										ENGINE TORQUE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				TORQUE INDICATOR WILL NOT READ AT ALL.						1	G	7	1 	3U			O	H2SW    					 
1999073000146	19990730	00146	SW  	1999	7	30	HEEA062987       	1	19990723	G	7700	407375016103	SIGNAL COND     			BELL  	407   	407         		SW  										ENGINE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	723PH					53283				FUEL LOW LIGHT WILL NOT EXTINGUISH.						1	G	7	1 	3U			O	H2SW    					 
1999073000147	19990730	00147	SW  	1999	7	30	HEEA062988       	1	19990723	G	6230	406010428109	HUB BUSHING     			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH	1570 				53142				WORN BEARINGS ON HUB.						1	G	7	1 	3U			O	H2SW    					 
1999073000148	19990730	00148	SW  	1999	7	30	HEEA062989       	1	19990723	G	2435	206062200113	STARTER         			BELL  	407   	407         		SW  										START/GENERATOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM	961  				53060				STARTER/GENERATOR HAS WORN SPLINES.						1	G	7	1 	3U			O	H2SW    					 
1999073000149	19990730	00149	SW  	1999	7	30	HEEA062990       	1	19990723	G	2435	206062200113	STARTER         			BELL  	407   	407         		SW  										START/GENERATOR	MISMARKED       	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	467PH	3    				53142				STARTER/GENERATOR'S DATA TAG INCORRECT.						1	G	7	1 	3U			O	H2SW    					 
1999073000150	19990730	00150	SW  	1999	7	30	HEEA062992       	1	19990723	G	6300	406010426101	LINK ASSEMBLY   			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	1156 				53016				LINK ASSEMBLY HAS WORN BUSHING.  SERIAL NUMBERS REMOVED ARE AFS-1223 AND AFS-1219.  REFERENCE:  DMR NR 686246.  REPLACEM	ENT PART SERIAL NUMBERS ARE AFS-2131 AND AFS-2134.					1	G	7	1 	3U			O	H2SW    					 
1999073000151	19990730	00151	SW  	1999	7	30	HEEA062995       	1	19990723	G	7930	407375004101	INDICATOR       			BELL  	407   	407         		SW  										ENGINE OIL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				BACK LIGHTING DIM ON ENGINE OIL INDICATOR.   REFERENCE:  DMR NR 686216.						1	G	7	1 	3U			O	H2SW    					 
1999073000152	19990730	00152	SW  	1999	7	30	HEEA062996       	1	19990723	G	6300	406010425107	LEVER ASSEMBLY  			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	141MA	1156 				53016				LEVER ASSY HAS WORN BUSHING.  SERIAL NUMBERS REMOVED ARE A-2083 AND A-2074.  DMR NR 686195.  REPLACEMENT PART SERIAL NUM	BERS ARE A-2523 AND A-2525.					1	G	7	1 	3U			O	H2SW    					 
1999073000153	19990730	00153	SW  	1999	7	30	HEEA062997       	1	19990723	G	3212	407350302101	FLOAT BAG       			BELL  	407   	407         		SW  										FLOAT	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	57416					53070				FLOAT BAG LEAKING.   REFERENCE:  DMR NR 686204.						1	G	7	1 	3U			O	H2SW    					 
1999073000154	19990730	00154	SW  	1999	7	30	HEEA062998       	1	19990723	G	3212	407350302101	FLOAT BAG       			BELL  	407   	407         		SW  										FLOAT	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	57416					53070				FLOAT BAG LEAKING.   REFERENCE:  DMR NR 686199.						1	G	7	1 	3U			O	H2SW    					 
1999073000155	19990730	00155	SW  	1999	7	30	HEEA062999       	1	19990723	G	6520	406040400115	GEARBOX         			BELL  	407   	407         		SW  										TAIL ROTOR	MAKING METAL    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	447PH					53114				TAIL ROTOR GEARBOX MAKING METAL.  REFERENCE:  DMR NR 686197.						1	G	7	1 	3U			O	H2SW    					 
1999073000156	19990730	00156	SW  	1999	7	30	HEEA063000       	1	19990723	G	3212	407350301101	FLOAT BAG       			BELL  	407   	407         		SW  										FLOAT	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	417PH					53038				LEFT FLOAT BAG LEAKING AT STEM.   REFERENCE:  DMR NR 686183.						1	G	7	1 	3U			O	H2SW    					 
1999073000157	19990730	00157	SW  	1999	7	30	HEEA063001       	1	19990723	G	3212	407350301101	FLOAT BAG       			BELL  	407   	407         		SW  										FLOAT	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	57416					53070				LEFT FLOAT BAG LEAKING.   REFERENCE:  DMR NR 686198.						1	G	7	1 	3U			O	H2SW    					 
1999073000158	19990730	00158	SW  	1999	7	30	HEEA063002       	1	19990723	G	6220	407010150103	FRAHM ASSY      			BELL  	407   	407         		SW  										MAIN ROTOR	UNBONDED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457PH					53147				RUBBER UNBONDED ON FRAM ASSEMBLY.  REFERENCE:  DMR NR 686200.						1	G	7	1 	3U			O	H2SW    					 
1999073000159	19990730	00159	SW  	1999	7	30	HEEA063003       	1	19990723	G	3212	407350300101	FLOAT BAG       			BELL  	407   	407         		SW  										FLOAT	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	417PH					53038				FLOAT BAG LEAKING AROUND RELIEF VALVE.  REFERENCE:  DMR NR 686182.						1	G	7	1 	3U			O	H2SW    					 
1999073000160	19990730	00160	SW  	1999	7	30	HEEA063004       	1	19990723	G	3110	407375001105	INDICATOR       			BELL  	407   	407         		SW  										M/R DRIVE	ERRATIC         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	404PH					53188				MGT INDICATOR ERRATIC AND INTERMITTENT.  REFERENCE:  DMR NR 686109.						1	G	7	1 	3U			O	H2SW    					 
1999073000161	19990730	00161	EU  	1999	7	30	HEEA063007       	1	19990719	G	6220	1051410130	STRAP           			BOLKMS	105   	BO105S      	5626006	EU  										MAIN ROTOR	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										STRAP MISMANUFACTURED.  THICKNESS DIAMETER 6.4 MM; SHOULD BE 6 MM.						1	G	7	2 	3U				H3EU    					 
1999073000162	19990730	00162	EU  	1999	7	30	HEEA063008       	1	19990722	G	6520	350A33215001	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				BALL END BEARINGS WORN.						1	G	7	1 	3U				H9EU    					 
1999073000163	19990730	00163	EU  	1999	7	30	HEEA063009       	1	19990722	G	2822	P94B12209	PUMP            			SNIAS 	350   	AS350B2     	8680813	EU  										FUEL BOOST	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L	576  				2873				FUEL PUMP INOPERATIVE.						1	G	7	1 	3U				H9EU    					 
1999073000164	19990730	00164		1999	7	30	HEEA063010       	4	19990722	G	3414	3839949002	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT AIRSPEED	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				AIRSPEED INDICATOR INACCURATE.						1	G	7	1 	3U				H9EU    					 
1999073000165	19990730	00165	EU  	1999	7	30	HEEA063011       	1	19990722	G	7712	305731365	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										ENGINE TORQUE	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				TORQUE INDICATOR READS LOW AND STICKS HIGH, INTERMITTENTLLY.						1	G	7	1 	3U				H9EU    					 
1999073000166	19990730	00166	EU  	1999	7	30	HEEA063012       	1	19990722	G	6220	704A33633208	SPHERICAL STOP  			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR HEAD	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				SPHERIAL STOP SEPARATED.  SERIAL NUMBERS REMOVED ARE LK2082, LK2147, AND LK2192.						1	G	7	1 	3U				H9EU    					 
1999082000448	19990820	00448	GL  	1999	8	20	HEEA063030       	2	19990728	G	7260	230595681	BEARING         		23053349    						ALLSN 	250C  	250C30P     	03013	GL  					GEARBOX	CORRODED        	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03					CAG95316		CAE895311			RECEIVING INSPECTION REVEALED PART NOT PRESERVED AT TIME OF MANUFACTURE AND EXHIBITS RUST.											3	U			E1GL				 
1999082000449	19990820	00449	NE  	1999	8	20	HEEA063031       	1	19990729	G	6320	400047610R	CALIPER         			SKRSKY	S76   	S76A        	8143006	NE  										ROTOR BRAKE	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	792CH					760193				ROTOR BRAKE CALIPER BEGAN LEAKING AROUND AFT PISTON SEAL.  REPLACED WITH SERVICEABLE PART.						1	G	7	2 	3U				H1NE    					 
1999082000450	19990820	00450		1999	8	20	HEEA063032       	1	19990729	G	2824	L88010491	VALVE           																	FUEL SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										FUEL VALVE CYCLES.																			 
1999082000451	19990820	00451	NE  	1999	8	20	HEEA063033       	1	19990729	G	7921	7636209203102	OIL COOLER      			SKRSKY	S76   	S76A        	8143006	NE  										ENGINE OIL	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	5128					760181				OIL COOLER LEAKING.						1	G	7	2 	3U				H1NE    					 
1999082000452	19990820	00452	NE  	1999	8	20	HEEA063034       	1	19990729	G	2913	7665009808101	PUMP            			SKRSKY	S76   	S76A        	8143006	NE  										HYDRAULIC SYSTEM	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	1546K					760082				HYDRAULIC PUMP LEAKING EXTERNALLY.  TIME SINCE REPAIR 0:00 HOURS.						1	G	7	2 	3U				H1NE    					 
1999082000453	19990820	00453		1999	8	20	HEEA063035       	4	19990729	G	3416	5035P2P44	ENCODER         			SKRSKY	S76   	S76A        	8143006	NE  										ALTIMETER	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122G					760232				ALTIMETER SHOWS 100 FOOT DIFFERENCE FROM PILOT'S.						1	G	7	2 	3U				H1NE    					 
1999082000454	19990820	00454		1999	8	20	HEEA063036       	4	19990729	G	3421	7660002113103	VERTICAL GYRO   			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	PRECESSES       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1546G					760076				VERTICAL GYRO PRECESSES.						1	G	7	2 	3U				H1NE    					 
1999082000455	19990820	00455		1999	8	20	HEEA063037       	4	19990729	G	3421	7660002113103	VERTICAL GYRO   			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5426U					760167				ATTITUDE INDICATOR FAILED IN-FLIGHT.						1	G	7	2 	3U				H1NE    					 
1999082000456	19990820	00456		1999	8	20	HEEA063038       	4	19990729	G	3421	7660002113103	VERTICAL GYRO   			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	CHATTERS        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545K					760047				ROLL CHATTERS IN-FLIGHT.						1	G	7	2 	3U				H1NE    					 
1999082000457	19990820	00457		1999	8	20	HEEA063039       	4	19990729	G	3421	7660002113103	VERTICAL GYRO   			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	KICKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1546G					760076				NR 1 PITCH CHANGE KICKING ON VERTICAL GYRO.						1	G	7	2 	3U				H1NE    					 
1999082000458	19990820	00458		1999	8	20	HEEA063040       	4	19990729	G	3421	7660002113103	VERTICAL GYRO   			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	PRECESSES       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5435V					760158				ADI PRECESSING AND CAUSING AFCS KICK INTERMITTENTLY.						1	G	7	2 	3U				H1NE    					 
1999082000459	19990820	00459		1999	8	20	HEEA063041       	4	19990729	G	3421	7660002113103	VERTICAL GYRO   			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	KICKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545K					760047				NR 1 PITCH KICKING ON VERTICAL GYRO.						1	G	7	2 	3U				H1NE    					 
1999082000460	19990820	00460		1999	8	20	HEEA063044       	4	19990806	G	3120	M877R28GMTLTFTET	CLOCK           			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5128					760181				FIRST NUMBER ON CLOCK DOESN'T LIGHT UP.						1	G	7	2 	3U				H1NE    					 
1999082000461	19990820	00461	NE  	1999	8	20	HEEA063045       	1	19990806	G	2611	30231R7B	SMOKE DETECTOR  			SKRSKY	S76   	S76A        	8143006	NE  										CABIN	WON'T TEST      	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	3122G					760232				SMOKE DETECTOR WILL NOT TEST.						1	G	7	2 	3U				H1NE    					 
1999082000462	19990820	00462		1999	8	20	HEEA063046       	4	19990806	G	2210	7690001805101	SWITCH          			SKRSKY	S76   	S76A        	8143006	NE  										AIRSPEED	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5128					760181				AUTOFLIGHT SWITCH INTERMITTENT.						1	G	7	2 	3U				H1NE    					 
1999082000463	19990820	00463	NE  	1999	8	20	HEEA063047       	1	19990809	G	2931	7645001078104	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2743E					760155				NR 2 NEEDLE INOPERATIVE ON HYDRAULIC PRESSURE INDICATOR.						1	G	7	2 	3U				H1NE    					 
1999082000464	19990820	00464	NE  	1999	8	20	HEEA063048       	1	19990809	G	7720	7645001078101	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										ENGINE TEMP	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	706AE					760275				PRESSURE SIDE INOPERATIVE ON ENGINE OIL INDICATOR.						1	G	7	2 	3U				H1NE    					 
1999082000465	19990820	00465		1999	8	20	HEEA063049       	4	19990809	G	3421	7000466915	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	792CH					760193				AH FLAG INTERMITTENTLY DISPLAYS SLOW TO ERECT.						1	G	7	2 	3U				H1NE    					 
1999082000466	19990820	00466		1999	8	20	HEEA063050       	4	19990809	G	2562	ELT910	TRANSMITTER     			SKRSKY	S76   	S76A        	8143006	NE  										ELT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4253S					760035				ELT WILL NOT SHUT OFF.   HAD TO DISCONNECT THE BATTERY.						1	G	7	2 	3U				H1NE    					 
1999082000467	19990820	00467		1999	8	20	HEEA063051       	4	19990809	G	3451	6221233001	DME             																	COCKPIT	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										NO READOUT.  INOPERATIVE.																			 
1999082000468	19990820	00468		1999	8	20	HEEA063052       	1	19990809	G	3340	ACR4F	RESCUE LIGHT    																	FUSELAGE	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										RESCUE LIGHT INTERMITTENT.																			 
1999082000469	19990820	00469	GL  	1999	8	20	HEEA063053       	2	19990809	G	7314	3944001	FUEL PUMP       			SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					ENGINE	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5435V	11132				760158				FUEL PUMP INOPERABLE.  DOES NOT PUMP FUEL.						1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999082000470	19990820	00470		1999	8	20	HEEA063054       	4	19990809	G	3420	1113034	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										ADI	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1545X					760050				TURN INDICATOR OFF TO RIGHT.						1	G	7	2 	3U				H1NE    					 
1999082000471	19990820	00471		1999	8	20	HEEA063055       	4	19990809	G	3451	066106602	TRANSCEIVER     																	COCKPIT DME	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										TRANSCEIVER WILL NOT TRANSMIT.  TIME SINCE REPAIR 0:00 HOURS.																			 
1999082000472	19990820	00472	NE  	1999	8	20	HEEA063057       	2	19990809	G	7321	324473513	FCU             			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					ENGINE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893N					33010				AUTOFUEL CONTROL CAUSING TORQUE SURGES.						1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999082000473	19990820	00473	GL  	1999	8	20	HEEA063058       	2	19990810	G	7314	3944001	FUEL PUMP       			SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122G	685  				760232				FUEL PUMP HAD WORN AND PITTED SPLINES.						1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999082000474	19990820	00474	NE  	1999	8	20	HEEA063059       	1	19990810	G	6410	7610105101041	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	15460	7806 				760223				TAIL ROTOR PADDLE HAS A HOLE AT THE TIP END.						1	G	7	2 	3U				H1NE    					 
1999082000475	19990820	00475	NE  	1999	8	20	HEEA063060       	1	19990810	G	6210	7615009043054	TIP CAP         			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	SPLIT           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4253S					760035				TRAILING EDGE SPLIT OPEN NEAR THE TIP LEADING EDGE.  ABRASION STRIP CRACKED TOP AND BOTTOM.						1	G	7	2 	3U				H1NE    					 
1999082000476	19990820	00476	NE  	1999	8	20	HEEA063061       	1	19990812	G	2430	51530006A	DC CONTROL      			SKRSKY	S76   	S76A        	8143006	NE  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2743E					760155				DC CONTROL COULD NOT RESET AFTER TEST.						1	G	7	2 	3U				H1NE    					 
1999082000477	19990820	00477		1999	8	20	HEEA063062       	4	19990812	G	2210	7690001804103	YAW INDICATOR   			SKRSKY	S76   	S76A        	8143006	NE  										ROLL PITCH	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5128					760181				NEEDLE AT CH. 1 NOT SET CENTER ON YAW INDICATOR.						1	G	7	2 	3U				H1NE    					 
1999082000478	19990820	00478	NE  	1999	8	20	HEEA063063       	1	19990812	G	7712	7645001078106	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										DUAL TORQUE	STICKS          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1546G					760076				DUAL TORQUE INDICATOR STICKS.						1	G	7	2 	3U				H1NE    					 
1999082000479	19990820	00479		1999	8	20	HEEA063064       	1	19990812	G	6121	6852920	SYNCROPHASER    																	PROPELLER	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										PROPELLER SYNC ERRATIC.																			 
1999082000480	19990820	00480		1999	8	20	HEEA063065       	1	19990812	G	2460	A1077B	RELAY           																	FLT COMPARTMENT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										RELAY TRIPPED CIRCUIT BREAKER.																			 
1999082000481	19990820	00481		1999	8	20	HEEA063066       	2	19990812	G	7510	1092T1002W	SERVOMOTOR      																	ENGINE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										SERVO MOTOR INOPERATIVE.																			 
1999082000482	19990820	00482	NE  	1999	8	20	HEEA063067       	1	19990812	G	2611	30326E7	CONTROL AMP     			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5128					760181				BAGGAGE SMOKE DETECTOR LIGHT STAYS ON CONTINUOUSLY.						1	G	7	2 	3U				H1NE    					 
1999082000483	19990820	00483	GL  	1999	8	20	HEEA063068       	2	19990813	G	7250	23008064	NOZZLE          		23035128    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					1ST STAGE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122G	685  			CAT95381	760232	CAE890547S			ENGINE REMOVED DUE TO CYCLED TURBINE WHEELS.   UPON INSPECTION OF TURBINE PARTS NOTED CRACKS BEYOND SERVICEABLE LIMITS O	N 1ST STAGE NOZZLE LEADING AND TRAILING EDGE VANES.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999082000484	19990820	00484	GL  	1999	8	20	HEEA063069       	2	19990813	G	7250	23066744	WHEEL           		23035128    						ALLSN 	250C  	250C30P     	03013	GL  					TURBINE SECTION	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03					CAT97745		CAE895185			NEW NR 4 WHEEL BALANCE INSPECTION FOUND RIM TO HAVE EXCESSIVE RUNOUT.  ROTOR COULD NOT BE BALANCED.  INSTALLED A NEW NR 	4 WHEEL.										3	U			E1GL				 
1999082000485	19990820	00485	GL  	1999	8	20	HEEA063070       	2	19990813	G	7250	23008064	NOZZLE          		23035128    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					1ST STAGE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545X	709  			CAT90143	760050	CAE890670S			ENGINE REMOVED DUE TO TURBINE OVERHAUL.  UPON INSPECTION OF TURBINE PARTS NOTED CRACKS BEYOND SERVICEABLE LIMITS ON 1ST 	STAGE NOZZLE VANES.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999082000486	19990820	00486	GL  	1999	8	20	HEEA063071       	2	19990813	G	7250	23008064	NOZZLE          		23035128    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					1ST STAGE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5128	637  			CAT97610	760181	CAE890463S			ENGINE REMOVED DUE TO TURBINE OVERHAUL.  UPON INSPECTION OF TURBINE PARTS NOTED VANE CRACKS BEYOND SERVICEABLE LIMITS ON	 1ST STAGE NOZZLE.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999082000487	19990820	00487	NE  	1999	8	20	HEEA063072       	1	19990813	G	7930	7645001076105	REPEATER        			SKRSKY	S76   	S76A        	8143006	NE  										ENGINE OIL	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	31219					760230				LIGHTS INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999082000488	19990820	00488	NE  	1999	8	20	HEEA063073       	1	19990813	G	7714	7645001076103	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										TRIPLE TACH	READS LOW       	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	706AE					760275				N1 READS LOW ON TRIPLE TACHOMETER.						1	G	7	2 	3U				H1NE    					 
1999082000489	19990820	00489		1999	8	20	HEEA063074       	1	19990813	G	7712	967741818427	TRANSMITTER     																	TORQUE	STUCK           	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										NEEDLE STUCK ON 50 PERCENT ON BOTH THE PILOT AND COPILOT TORQUE GAUGES.																			 
1999082000490	19990820	00490		1999	8	20	HEEA063075       	4	19990813	G	2312	7001840913	TRANSCEIVER     																	COCKPIT	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										AUDIO/VIDEO BRIEF SYSTEM WILL NOT COME ON-LINE.																			 
1999082000491	19990820	00491		1999	8	20	HEEA063076       	4	19990813	G	2370	9906000000	MONITOR         																	AUDIO/VIDEO	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										SYSTEM WILL NOT COME ON.																			 
1999082000492	19990820	00492		1999	8	20	HEEA063077       	1	19990813	G	7603	2539149	SHAFT           																	COCKPIT	MISREPAIRED     	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										THROTTLE SHAFT REPLATED AND WAS PLATED TOO FAR OVER TOWARDS THE THROTTLE SHAFT LEVER PIN HOLE, SO THE THROTTLE SHAFT LEV	ER PINS CANNOT BE INSTALLED.																		 
1999082000493	19990820	00493	SW  	1999	8	20	HEEA063081       	1	19990726	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										STEP ACTUATOR NOPERATIVE.  TIME SINCE REPAIR 0:00 HOURS.						1	G	7	2 	4U				H4SW    					 
1999082000494	19990820	00494	SW  	1999	8	20	HEEA063082       	1	19990727	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T					33112				STEP ACTUATOR ONLY FUNCTIONS WHEN IT HAS NO LOAD.  UNIT WILL NOT EXTEND AND RETRACT, AND WILL NOT RAISE THE WEIGHT OF TH	E STEP.  SUBMITTER STATED THIRD FAULT FOUND WITH THIS UNIT.					1	G	7	2 	4U				H4SW    					 
1999082000495	19990820	00495	SW  	1999	8	20	HEEA063083       	1	19990728	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP COMP	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										ACTUATOR WILL NOT BEEP UP OR DOWN.						1	G	7	1 	3U				H2SW    					 
1999082000496	19990820	00496		1999	8	20	HEEA063084       	2	19990728	G	7510	23007827	VALVE           			BELL  	407   	407         		SW  										ANTI-ICE	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	720PH					53277				VALVE ASSY LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999082000497	19990820	00497	SW  	1999	8	20	HEEA063085       	1	19990728	G	3212	206050247132	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	409PH					53059				FLOAT COVER TORN.						1	G	7	1 	3U			O	H2SW    					 
1999082000498	19990820	00498	SW  	1999	8	20	HEEA063086       	1	19990728	G	3212	206050247135	COVER           			BELL  	407   	407         		SW  										FLOAT	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	447PH					53114				FLOAT COVER WORN.  END CAP MISSING.						1	G	7	1 	3U			O	H2SW    					 
1999082000499	19990820	00499	SW  	1999	8	20	HEEA063087       	1	19990728	G	3212	206050247135	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	407PH					53003				FLOAT COVER HAD TORN END CAP.						1	G	7	1 	3U			O	H2SW    					 
1999082000500	19990820	00500	SW  	1999	8	20	HEEA063088       	1	19990728	G	3212	206050247135	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	447PH					53114				FLOAT COVER TORN.						1	G	7	1 	3U			O	H2SW    					 
1999082000501	19990820	00501	SW  	1999	8	20	HEEA063089       	1	19990728	G	3212	206050247132	COVER           			BELL  	407   	407         		SW  										FLOAT	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	402PH					53159				FLOAT COVER WORN.						1	G	7	1 	3U			O	H2SW    					 
1999082000502	19990820	00502	SW  	1999	8	20	HEEA063090       	1	19990728	G	3212	206050247137	COVER           			BELL  	407   	407         		SW  										FLOAT	LOOSE           	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	409PH					53059				END VELCRO LOOSE ON FLOAT COVER.						1	G	7	1 	3U			O	H2SW    					 
1999082000503	19990820	00503	SW  	1999	8	20	HEEA063091       	1	19990728	G	3212	206050247138	COVER           			BELL  	407   	407         		SW  										FLOAT	DETERIORATED    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	409PH					53059				FLOAT COVER DETERIORATED.						1	G	7	1 	3U			O	H2SW    					 
1999082000504	19990820	00504	SW  	1999	8	20	HEEA063092       	1	19990728	G	3212	206050247138	COVER           			BELL  	407   	407         		SW  										FLOAT	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	457PH					53147				VELCRO STITCHING MISSING ON AFT CAP, FRONT WORN ON FLOAT COVER.						1	G	7	1 	3U			O	H2SW    					 
1999082000505	19990820	00505	SW  	1999	8	20	HEEA063093       	1	19990728	G	3212	206050247137	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	612PH					53199				FLOAT COVER WORN AND TORN.						1	G	7	1 	3U			O	H2SW    					 
1999082000506	19990820	00506	SW  	1999	8	20	HEEA063094       	1	19990728	G	3212	206050247135	COVER           			BELL  	407   	407         		SW  										FLOAT	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	402PH					53159				FLOAT COVER WORN.						1	G	7	1 	3U			O	H2SW    					 
1999082000507	19990820	00507	SW  	1999	8	20	HEEA063095       	1	19990728	G	3212	206050247132	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	437PH					53072				TORN FLAP, LOOSE VELCRO ON FLOAT COVER.						1	G	7	1 	3U			O	H2SW    					 
1999082000508	19990820	00508	SW  	1999	8	20	HEEA063097       	1	19990728	G	6520	406040453101	SEAL            			BELL  	407   	407         		SW  										T/R GEARBOX	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	402PH					53159				SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999082000509	19990820	00509	SW  	1999	8	20	HEEA063098       	1	19990728	G	6510	407340340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	447PH					53114				DISC PACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999082000510	19990820	00510	SW  	1999	8	20	HEEA063099       	1	19990728	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	721PH					53278				UNIVERSAL HAD WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999082000511	19990820	00511	SW  	1999	8	20	HEEA063100       	1	19990728	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	510PH					53209				UNIVERSAL WORN (UNSTAKED).						1	G	7	1 	3U			O	H2SW    					 
1999082000512	19990820	00512	SW  	1999	8	20	HEEA063101       	1	19990728	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	720PH					53277				UNIVERSAL WORN.						1	G	7	1 	3U			O	H2SW    					 
1999082000513	19990820	00513	SW  	1999	8	20	HEEA063102       	1	19990728	G	6320	407040006107	TRANSMISSION    			BELL  	407   	407         		SW  										MAIN ROTOR	MAKING METAL    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	404PH	1645 				53188				TRANSMISSION ASSY MAKING METAL.						1	G	7	1 	3U			O	H2SW    					 
1999082000514	19990820	00514	SW  	1999	8	20	HEEA063104       	1	19990728	G	7921	407062021101	DUCT            			BELL  	407   	407         		SW  										EXHAUST	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	141MA					53016				DUCT CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999082000515	19990820	00515	SW  	1999	8	20	HEEA063105       	1	19990728	G	6720	406012129101	LINK ASSY       			BELL  	407   	407         		SW  										PITCH CONTROL	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	719PH					53266				LINK ASSY HAD WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999082000516	19990820	00516	SW  	1999	8	20	HEEA063106       	1	19990728	G	2913	206076030111	PUMP            			BELL  	407   	407         		SW  										HYDRAULIC SYSTEM	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	447PH					53114				ADAPTER SHAFT AND CLIP WORN ON PUMP.						1	G	7	1 	3U			O	H2SW    					 
1999082000517	19990820	00517	SW  	1999	8	20	HEEA063107       	1	19990728	G	6321	406010429101	PIN             			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	467PH					53142				PIN WORN, PLAY IN DRIVE LINK.						1	G	7	1 	3U			O	H2SW    					 
1999082000518	19990820	00518	SW  	1999	8	20	HEEA063108       	1	19990728	G	6240	222375077119	TRANSMITTER     			BELL  	407   	407         		SW  										TORQUE	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	722PH					53288				TRANSMITTER HAD NO TORQUE INDICATIONS.						1	G	7	1 	3U			O	H2SW    					 
1999082000519	19990820	00519	SW  	1999	8	20	HEEA063109       	1	19990728	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	457PH					53147				LINK HAD WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999082000520	19990820	00520	SW  	1999	8	20	HEEA063110       	1	19990728	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	457PH					53147				LINK HAD WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999082000521	19990820	00521	SW  	1999	8	20	HEEA063111       	1	19990728	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	720PH					53277				UNIVERSAL HAD WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999082000522	19990820	00522	SW  	1999	8	20	HEEA063112       	1	19990728	G	2910	70079H000Y150	HOSE ASSY       			BELL  	407   	407         		SW  										HYDRAULIC SYSTEM	KINKED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	141MA					53016				HOSE KINKED.						1	G	7	1 	3U			O	H2SW    					 
1999082000523	19990820	00523	SW  	1999	8	20	HEEA063113       	1	19990728	G	6510	206061432116	HOUSING         			BELL  	407   	407         		SW  										BLOWER	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	141MA					53016				BLOWER HOUSING CRACKED, UPPER LEFT CORNER.						1	G	7	1 	3U			O	H2SW    					 
1999082000524	19990820	00524	SW  	1999	8	20	HEEA063114       	1	19990728	G	6510	206061432121	HOUSING         			BELL  	407   	407         		SW  										BLOWER	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	437PH					53072				BLOWER HOUSING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999082000525	19990820	00525	SW  	1999	8	20	HEEA063115       	1	19990728	G	6720	406012129101	LINK ASSY       			BELL  	407   	407         		SW  										PITCH CONTROL	BINDING         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	408PH					53228				LINK ASSY BEARINGS BINDING.						1	G	7	1 	3U			O	H2SW    					 
1999082000526	19990820	00526	SW  	1999	8	20	HEEA063116       	1	19990728	G	6510	407040316101	FLYWHEEL        			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	141MA					53016				SPLINES WORN BEYOND LIMITS ON FLYWHEEL.						1	G	7	1 	3U			O	H2SW    					 
1999082000527	19990820	00527	SW  	1999	8	20	HEEA063118       	1	19990728	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	719PH					53266				UNIVERSAL HAD WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999082000528	19990820	00528	SW  	1999	8	20	HEEA063119       	1	19990728	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	722PH					53288				UNIVERSAL WORN AXIALLY.						1	G	7	1 	3U			O	H2SW    					 
1999082000529	19990820	00529	SW  	1999	8	20	HEEA063120       	1	19990728	G	3212	8226003	FUSIBLE PLUG    			BELL  	407   	407         		SW  										FLOAT	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	612PH					53199				PLUG LEAKS.						1	G	7	1 	3U			O	H2SW    					 
1999082000530	19990820	00530	SW  	1999	8	20	HEEA063121       	1	19990728	G	6510	407340340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	724PH					53327				DISC PACK CRACKED AND BROKEN.						1	G	7	1 	3U			O	H2SW    					 
1999082000531	19990820	00531	SW  	1999	8	20	HEEA063122       	1	19990728	G	6510	407340340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	720PH					53277				DISC PACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999082000532	19990820	00532	SW  	1999	8	20	HEEA063123       	1	19990728	G	6720	206011728001	TRUNNION        			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	408PH					53228				WORN TRUNNION GEAR.						1	G	7	1 	3U			O	H2SW    					 
1999082000533	19990820	00533	SW  	1999	8	20	HEEA063124       	1	19990728	G	6321	206076047101	CYLINDER        			BELL  	407   	407         		SW  										ROTOR BRAKE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	720PH					53277				PRESSURE BINDING ON UP AND DOWN STROKE ON CYLINDER ASSY.						1	G	7	1 	3U			O	H2SW    					 
1999082000534	19990820	00534	SW  	1999	8	20	HEEA063125       	1	19990728	G	6520	406040453101	SEAL            			BELL  	407   	407         		SW  										T/R GEARBOX	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	8595X					53267				SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999082000535	19990820	00535	SW  	1999	8	20	HEEA063126       	1	19990728	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										STEP ACTUATOR INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999082000536	19990820	00536	SW  	1999	8	20	HEEA063128       	1	19990729	G	6330	206033542003	MOUNT           			BELL  	206   	206L1       	1182107	SW  										TRANSMISSON	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										BUSHING HOLE ELONGATED ON MOUNT ASSY.						1	G	7	1 	3U				H2SW    					 
1999082000537	19990820	00537		1999	8	20	HEEA063129       	4	19990729	G	2200	2593996333	TARSYN 333      			BELL  	412   	412         	1182202	SW  										FLIGHT CONTROL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023					33080				UNABLE TO DRIVE HSI WITH COMPASS CONTROL SPEX.  EXP. DATE 1-19-99.						1	G	7	2 	4U				H4SW    					 
1999082000538	19990820	00538		1999	8	20	HEEA063130       	4	19990729	G	2200	2593996333	TARSYN 333      			BELL  	412   	412         	1182202	SW  										FLIGHT CONTROL	PRECESSES       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141PH					33197				TARSYN PRECESSING MOSTLY IN PITCH.						1	G	7	2 	4U				H4SW    					 
1999082000539	19990820	00539		1999	8	20	HEEA063131       	4	19990729	G	2200	2593996333	TARSYN 333      			BELL  	412   	412         	1182202	SW  										FLIGHT CONTROL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893N					33010				HSI UNRELIABLE.						1	G	7	2 	4U				H4SW    					 
1999082000540	19990820	00540		1999	8	20	HEEA063132       	4	19990729	G	2200	2593996333	TARSYN 333      			BELL  	412   	412         	1182202	SW  										FLIGHT CONTROL	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5759N					33002				TARSYN 333 CAUSES PITCH ROLL OSCILLATION IN AIRCRAFT.						1	G	7	2 	4U				H4SW    					 
1999082000541	19990820	00541		1999	8	20	HEEA063133       	4	19990729	G	2200	4020936903	TARSYN 333      			BELL  	412   	412         	1182202	SW  										FLIGHT CONTROL	RATCHETS        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	21498					36003				INDICATOR RATCHETS 7-8 DEGREES IN A TURN.						1	G	7	2 	4U				H4SW    					 
1999082000542	19990820	00542	SW  	1999	8	20	HEEA063134       	1	19990729	G	6730	206076062003	CYLINDER        			BELL  	206   	206L1       	1182107	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2772A	7123 				45311				CYLINDER LEAKING.						1	G	7	1 	3U				H2SW    					 
1999082000543	19990820	00543	SW  	1999	8	20	HEEA063135       	1	19990729	G	6730	206076062003	CYLINDER        			BELL  	206   	206L1       	1182107	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2772A	7117 				45311				CYLINDER LEAKING.						1	G	7	1 	3U				H2SW    					 
1999082000544	19990820	00544		1999	8	20	HEEA063136       	1	19990729	G	2822	9A1746	CARTRIDGE       																	FUEL PUMP	NOISY           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										EXTREMELY NOISY AND ROUGH SOUNDING.																			 
1999082000545	19990820	00545		1999	8	20	HEEA063137       	4	19990729	G	3420	5050010902	GYRO            			BELL  	206   	206L1       	1182107	SW  										COCKPIT	PRECESSES       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21240					45647				GYRO PRECESSES 45 DEGREES THEN LOCKS UP.						1	G	7	1 	3U				H2SW    					 
1999082000546	19990820	00546		1999	8	20	HEEA063138       	4	19990729	G	3421	214075244001	GYRO            			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	142PH					33150				RT FLAG WILL NOT PULL ON RATE GYRO.						1	G	7	2 	4U				H4SW    					 
1999082000547	19990820	00547		1999	8	20	HEEA063139       	4	19990729	G	3420	1113034	INDICATOR       			BELL  	412   	412         	1182202	SW  										ATTITUDE	RATCHETS        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				ATTITUDE INDICATOR RATCHETY.						1	G	7	2 	4U				H4SW    					 
1999082000548	19990820	00548		1999	8	20	HEEA063140       	4	19990729	G	3414	412075009105	INDICATOR       			BELL  	412   	412         	1182202	SW  										AIRSPEED	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	800Y					33134				AIRSPEED INDICATOR GAUGE STICKS AT 10 KNOTS WHEN STATIC.						1	G	7	2 	4U				H4SW    					 
1999082000549	19990820	00549	SW  	1999	8	20	HEEA063141       	1	19990729	G	2913	206076022101	PUMP            			BELL  	206   	206B3       	1181506	SW  										HYDRAULIC SYSTEM	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	103PH	12944				3000				LEAKS ABOVE SIGHT GLASS.						1	G	7	1 	3U				H2SW    					 
1999082000550	19990820	00550		1999	8	20	HEEA063142       	4	19990729	G	3417	214175421101	COMPUTER        			BELL  	214   	214ST       	1182106	SW  										AIR DATA	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M					28102				COMPUTER WILL NOT READ POWER ASSURANCE.						2	G	7	2 	4U				H10SW   					 
1999082000551	19990820	00551		1999	8	20	HEEA063143       	4	19990729	G	3416	120120461210	ALTIMETER       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	INCORRECT       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2251A					45755				ALTIMETER READS INCORRECT.						1	G	7	1 	3U				H2SW    					 
1999082000552	19990820	00552		1999	8	20	HEEA063144       	4	19990729	G	3416	212070238007	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141PH					33197				INDICATOR SLOW TO REACT, LAGS BEHIND OTHER ALTIMETER.						1	G	7	2 	4U				H4SW    					 
1999082000553	19990820	00553		1999	8	20	HEEA063145       	4	19990729	G	3444	7000839901	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										RADIO ALTIMETER	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806	786  				28140				INDICATOR READS 200 FEET HIGH.						2	G	7	2 	4U				H10SW   					 
1999082000554	19990820	00554		1999	8	20	HEEA063146       	4	19990729	G	3416	8800T	ENCODER         			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023					33080				ENCODER WILL NOT READ ALTITUDE.						1	G	7	2 	4U				H4SW    					 
1999082000555	19990820	00555	SW  	1999	8	20	HEEA063147       	1	19990729	G	6220	206011100105	HUB             			BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	OVERSERVICED    	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	31073	4670 				51519				MAIN ROTOR HUB SLINGING GREASE.						1	G	7	1 	3U				H2SW    					 
1999082000556	19990820	00556	SW  	1999	8	20	HEEA063148       	1	19990729	G	3212	206050248117	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	FAILED TEST     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41128					51465				FLOAT BAG FAILED 6 MONTH FLOAT INSPECTION.  PRESSURE CHECK.   LEAKING FROM FORWARD LOWER RIGHT END.						1	G	7	1 	3U				H2SW    					 
1999082000557	19990820	00557	SW  	1999	8	20	HEEA063149       	1	19990729	G	3212	206050248111	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	31821					51076				FLOAT BAG LEAKING.						1	G	7	1 	3U				H2SW    					 
1999082000558	19990820	00558	SW  	1999	8	20	HEEA063150       	1	19990729	G	2435	23046020	STARTER         			BELL  	412   	412         	1182202	SW  										STARTER/GEN	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893P	12956				33012				STARTER/GENERATOR WOULD NOT TURN OVER.						1	G	7	2 	4U				H4SW    					 
1999082000559	19990820	00559		1999	8	20	HEEA063151       	4	19990729	G	3444	7001840903	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S					33022				RECEIVER/TRANSMITTER QUITS AFTER 5 SECONDS.						1	G	7	2 	4U				H4SW    					 
1999082000560	19990820	00560	SW  	1999	8	20	HEEA063152       	1	19990729	G	2822	164A199	BOOST PUMP      			BELL  	206   	206L1       	1182107	SW  										FUEL SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										LEFT HAND BOOST PUMP LIGHT ILLUMINATED.						1	G	7	1 	3U				H2SW    					 
1999082000561	19990820	00561	SW  	1999	8	20	HEEA063153       	1	19990729	G	6730	206076062003	CYLINDER        			BELL  	206   	206L3       	1182108	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6160Y	17274				51609				CYLINDER LEAKING.						1	G	7	1 	3U				H2SW    					 
1999082000562	19990820	00562	SW  	1999	8	20	HEEA063154       	1	19990729	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										STEP ACTUATOR INOPERATIVE.  PEGS OUT AMPMETER ON SAM TEST KIT.						1	G	7	2 	4U				H4SW    					 
1999082000563	19990820	00563	SW  	1999	8	20	HEEA063155       	1	19990729	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										STEP ACTUATOR WORKS INTERMITTENTLY.						1	G	7	2 	4U				H4SW    					 
1999082000564	19990820	00564	SW  	1999	8	20	HEEA063156       	1	19990729	G	3212	206050248111	FLOAT           			BELL  	206   	206L1       	1182107	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03										FLOAT BAG LEAKING AT INTERNAL BAFFLE DURING 6 MONTH INSPECTION.						1	G	7	1 	3U				H2SW    					 
1999082000565	19990820	00565	SW  	1999	8	20	HEEA063157       	1	19990729	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ISTEP ACTUATOR INOPERATIVE.  PEGS OUT AMPMETER ON SAPA TEST KIT.						1	G	7	2 	4U				H4SW    					 
1999082000566	19990820	00566	SW  	1999	8	20	HEEA063158       	1	19990729	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										STEP ACTUATOR INOPERATIVE.  PEGS OUT AMPMETER.						1	G	7	2 	4U				H4SW    					 
1999082000567	19990820	00567	SW  	1999	8	20	HEEA063159       	1	19990729	G	3212	212050207012	FLOAT           			BELL  	212   	212         	1181420	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3131S	2350 				30953				FLOAT BAG LEAKING.						1	G	7	1 	4U				H4SW    					 
1999082000568	19990820	00568	SW  	1999	8	20	HEEA063160       	1	19990729	G	2435	23081018	STARTER         			BELL  	206   	206L1       	1182107	SW  										STARTER/GEN	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2253E	10403				45758				STARTER/GENERATOR WILL NOT ROTATE.						1	G	7	1 	3U				H2SW    					 
1999082000569	19990820	00569	SW  	1999	8	20	HEEA063161       	1	19990729	G	6730	206076062003	CYLINDER        			BELL  	206   	206L1       	1182107	SW  										CYCLIC	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1072T	21960				45385				CYLINDER HAD WORN BEARING.						1	G	7	1 	3U				H2SW    					 
1999082000570	19990820	00570	SW  	1999	8	20	HEEA063162       	1	19990729	G	2823	L88010501	VALVE           			BELL  	412   	412         	1182202	SW  										NR 2 ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										NR 2 ENGINE IN ASH LIGHT WILL NOT COME ON AFTER ENGINE IS SHUT POWER.						1	G	7	2 	4U				H4SW    					 
1999082000571	19990820	00571	SW  	1999	8	20	HEEA063163       	1	19990802	G	6220	206011105001	TRUNNION        			BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										BEARING MISMANUFACTURED.  INCORRECT POSITION OF GREASE INLET RELATIVE TO BOLT CUT-OUTS ON BARREL (GREASE INLET ON BOTTOM	 OF BARREL WHEN INSTALLED).  UNABLE TO INJECT GREASE INTO BARREL WHEN INSTALLED.					1	G	7	1 	3U				H2SW    					 
1999082000572	19990820	00572		1999	8	20	HEEA063164       	4	19990802	G	2210	214074303115	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										AUTOFLIGHT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	59805					28141				PITCH CHANNEL DROPS OFF WHEN BEEPING FORE AND AFT.  ATTEMPTED ALIGNMENT.  DID NOT CURE PROBLEM.						2	G	7	2 	4U				H10SW   					 
1999082000573	19990820	00573	SW  	1999	8	20	HEEA063165       	1	19990802	G	6710	214001970111	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										MAIN ROTOR	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6957Y					28139				BRAKE WILL NOT RELEASE.  SUBMITTER STATED THIS IS A RECURRING PROBLEM WITH THIS UNIT.						2	G	7	2 	4U				H10SW   					 
1999082000574	19990820	00574	SW  	1999	8	20	HEEA063166       	1	19990802	G	3210	400052015101	RUBBER          			BELL  	407   	407         		SW  										MLG	MISSING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8595X					53267				RUBBER MISSING ON AFT LANDING GEAR.						1	G	7	1 	3U			O	H2SW    					 
1999082000575	19990820	00575	SW  	1999	8	20	HEEA063167       	1	19990802	G	3212	406015043101	COVER           			BELL  	407   	407         		SW  										FLOAT	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				COVER HAD CORROSION.						1	G	7	1 	3U			O	H2SW    					 
1999082000576	19990820	00576	SW  	1999	8	20	HEEA063168       	1	19990802	G	6220	407010150103	FRAHM ASSY      			BELL  	407   	407         		SW  										MAIN ROTOR	MAKING METAL    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	407PH					53003				FRAM ASSY MAKING METAL.						1	G	7	1 	3U			O	H2SW    					 
1999082000577	19990820	00577	SW  	1999	8	20	HEEA063169       	1	19990803	G	5340	204030403001S	FITTING         			BELL  	212   	212         	1181420	SW  										FUSELAGE	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										CORROSION ON BOTTOM SIDE OF FITTING.						1	G	7	1 	4U				H4SW    					 
1999082000578	19990820	00578	SW  	1999	8	20	HEEA063170       	1	19990803	G	5320	206031314083S	CHANNEL         			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										CHANNEL MISMANUFACTURED.  NO EDGE DISTANCE FOR .1562 INCH RIVET AT TOP FORWARD JOGGLED AREA OF LONGERON.						1	G	7	1 	3U				H2SW    					 
1999082000579	19990820	00579	SW  	1999	8	20	HEEA063171       	1	19990803	G	5313	206031314037S	LONGERON        			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										LONGERON MISMANUFACTURED.  DEFECTS ON UPPER FLANGE.  FLANGE IS WARPED AND HAS GOUGES ON AFT END.  THE PART IS BOWED.						1	G	7	1 	3U				H2SW    					 
1999082000580	19990820	00580	SW  	1999	8	20	HEEA063172       	1	19990803	G	5320	209031314125S	CHANNEL         			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										CHANNEL MISMANUFACTURED.  NO EDGE DISTANCE ON EXISTING RIVET HOLES - LONGERON TOO SHORT.						1	G	7	1 	3U				H2SW    					 
1999082000581	19990820	00581	SW  	1999	8	20	HEEA063173       	1	19990803	G	6410	214011819101	BEARING         		214011801117	BELL  	214   	214ST       	1182106	SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N	432  			A761	28106				BEARING WORN BEYOND LIMITS. SCRAPPED BEARINGS.						2	G	7	2 	4U				H10SW   					 
1999082000582	19990820	00582	SW  	1999	8	20	HEEA063174       	1	19990803	G	5320	212030121015S	WEB             			BELL  	212   	212         	1181420	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										WEB MISMANUFACTURED.  WEB HAS A .005 INCH DEEP MACHINE MARK RUNNING ON THE FORWARD, RT SIDE OF PART, DOWN APPROXIMATELY 	6 INCHES FROM TOP END OF WEB.  THIS MARK IS APPROXIMATELY .3750 INCH TO .50 INCH IN FROM EDGE OF PART.  THIS WOULD PUT R	IGHT IN LINE WITH THE RIVET ROW FOR THE RT CAP ANGLE.  THE WEB ALSO HAS A BOWED AREA ON THE TOP END WHICH PREVENTS THE C	AP ANGLE FROM HAVING A FLAT SURFACE TO ATTACH TO.			1	G	7	1 	4U				H4SW    					 
1999082000583	19990820	00583	SW  	1999	8	20	HEEA063175       	1	19990803	G	6320	206040052105	HOUSING         			BELL  	206   	206L1       	1182107	SW  										M/R GEARBOX	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										HOUSING MISMANUFACTURED.  SMALL HOLE IN HOUSING.						1	G	7	1 	3U				H2SW    					 
1999082000584	19990820	00584	SW  	1999	8	20	HEEA063176       	1	19990806	G	2841	393008047	INDICATOR       			BELL  	412   	412         	1182202	SW  										FUEL QUANTITY	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K					33020				INDICATOR IS PEGGED PAST ZERO.						1	G	7	2 	4U				H4SW    					 
1999082000585	19990820	00585		1999	8	20	HEEA063177       	4	19990806	G	3420	5050010902	GYRO            			BELL  	206   	206L1       	1182107	SW  										COCKPIT	PRECESSES       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50046					45173				GYRO PRECESSES EXCESSIVELY.						1	G	7	1 	3U				H2SW    					 
1999082000586	19990820	00586		1999	8	20	HEEA063178       	4	19990806	G	3417	214175421101	COMPUTER        			BELL  	214   	214ST       	1182106	SW  										AIR DATA	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M					28102				GROSS WT LIGHT HAS 2ND DIGIT OUT.						2	G	7	2 	4U				H10SW   					 
1999082000587	19990820	00587		1999	8	20	HEEA063179       	4	19990806	G	3420	258719343	GYRO            			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				GYRO DOES NOT SPOOL UP.  OFF FLAG NOT PULLING ON HSI.						2	G	7	2 	4U				H10SW   					 
1999082000588	19990820	00588		1999	8	20	HEEA063180       	4	19990806	G	3120	206070275005	CLOCK           			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610E					51424				CLOCK NOT WORKING.						1	G	7	1 	3U				H2SW    					 
1999082000589	19990820	00589		1999	8	20	HEEA063181       	4	19990806	G	2562	ELT10	ELT             			BELL  	206   	206L3       	1182108	SW  										CABIN	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251V					51404				ANTENNA CONNECTOR LOOSE.						1	G	7	1 	3U				H2SW    					 
1999082000590	19990820	00590		1999	8	20	HEEA063182       	4	19990806	G	2562	ELT10	ELT             			BELL  	206   	206L3       	1182108	SW  										CABIN	WON'T TEST      	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	21497					51518				ELT WILL NOT TEST.						1	G	7	1 	3U				H2SW    					 
1999082000591	19990820	00591		1999	8	20	HEEA063183       	4	19990806	G	2562	ELT910	SWITCH          			BELL  	206   	206L3       	1182108	SW  										ELT	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8589X					51487				SWITCH STUCK ON DURING MONTHLY CHECK, BATTERY DISCONNECTED.						1	G	7	1 	3U				H2SW    					 
1999082000592	19990820	00592	SW  	1999	8	20	HEEA063184       	1	19990806	G	6340	214074280107	DETECTOR        			BELL  	412   	412         	1182202	SW  										RPM LIMIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				CYCLIC LIGHT STAYS ON.						1	G	7	2 	4U				H4SW    					 
1999082000593	19990820	00593	SW  	1999	8	20	HEEA063185       	1	19990806	G	7722	212075067105	INDICATOR       			BELL  	412   	412         	1182202	SW  										ITT	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S					33022				ITT INDICATOR STUCK AT 500 DEGREES.						1	G	7	2 	4U				H4SW    					 
1999082000594	19990820	00594	SW  	1999	8	20	HEEA063186       	1	19990806	G	7722	212075067105	INDICATOR       			BELL  	412   	412         	1182202	SW  										ITT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	142PH					33150				ITT INDICATION GOES TO ZERO AFTER SHORT TIME.						1	G	7	2 	4U				H4SW    					 
1999082000595	19990820	00595		1999	8	20	HEEA063187       	4	19990806	G	3417	214175421101	COMPUTER        			BELL  	214   	214ST       	1182106	SW  										AIR DATA	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				COMPUTER SHOWS FAIL 5.						2	G	7	2 	4U				H10SW   					 
1999082000596	19990820	00596	SW  	1999	8	20	HEEA063188       	1	19990806	G	7810	206064300005	STACK           			BELL  	206   	206L3       	1182108	SW  										EXHAUST SYSTEM	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	205FC					51130				CRACK NEXT TO VOID ON AFT LOWER RIGHT SIDE OF EXHAUST ASSEMBLY.						1	G	7	1 	3U				H2SW    					 
1999082000597	19990820	00597	GL  	1999	8	20	HEEA063189       	2	19990806	G	7314	3881005	FUEL PUMP       			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3905B	11247				45598				FUEL PUMP HAD EXCESSIVE STEP WEAR ON SPLINE.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999082000598	19990820	00598		1999	8	20	HEEA063190       	4	19990806	G	3420	5050010902	GYRO            			BELL  	206   	206L3       	1182108	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6603X					51412				GYRO INOPERATIVE.  MANUAL SLAVE ROD DOESN'T WORK.						1	G	7	1 	3U				H2SW    					 
1999082000599	19990820	00599	SW  	1999	8	20	HEEA063191       	1	19990806	G	7722	206375006101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5742N					45477				TOT INDICATOR HAD SOMETHING LOOSE INSIDE.						1	G	7	1 	3U				H2SW    					 
1999082000600	19990820	00600		1999	8	20	HEEA063192       	4	19990806	G	3420	5050010902	GYRO            			BELL  	206   	206L4       	1182110	SW  										COCKPIT	PRECESSES       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										GYRO PRECESSING.						1	G	7	1 	3U			NC	H2SW    					 
1999082000601	19990820	00601	SW  	1999	8	20	HEEA063201       	1	19990809	G	2430	206075447007	VOLT REGULATOR  			BELL  	206   	206L1       	1182107	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3904L					45597				GENERATOR DROPS OFF LINE.						1	G	7	1 	3U				H2SW    					 
1999082000602	19990820	00602	SW  	1999	8	20	HEEA063202       	1	19990809	G	7722	9429100115	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	31073					51519				BACK LIGHT INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999082000603	19990820	00603		1999	8	20	HEEA063203       	4	19990809	G	3451	6223670001	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										DME	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	515KA					51048				DME INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999082000604	19990820	00604	SW  	1999	8	20	HEEA063204       	1	19990809	G	2840	212070122009	INDICATOR       			BELL  	212   	212         	1181420	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3131S					30953				INDICATOR HAD SLOW RESPONSE.						1	G	7	1 	4U				H4SW    					 
1999082000605	19990820	00605	SW  	1999	8	20	HEEA063205       	1	19990809	G	6340	214074280107	DETECTOR        			BELL  	412   	412         	1182202	SW  										RPM LIMIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K					33020				RPM LIMIT DETECTOR INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999082000606	19990820	00606	SW  	1999	8	20	HEEA063206       	1	19990809	G	2822	205060606003	PUMP            			BELL  	412   	412         	1182202	SW  										FUEL BOOST	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2148K					36001				PUMP INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999082000607	19990820	00607	SW  	1999	8	20	HEEA063207       	1	19990809	G	7931	206075187003	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										ENGINE OIL	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251Y					51556				ENGINE OIL AND TEMPERATURE INDICATIONS HAD NO LIGHT.						1	G	7	1 	3U				H2SW    					 
1999082000608	19990820	00608	SW  	1999	8	20	HEEA063208       	1	19990809	G	2822	205060606003	PUMP            			BELL  	412   	412         	1182202	SW  										FUEL BOOST	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7128R					36007				TRANSFER DISPLAY LIGHT COMES ON IN-FLIGHT.						1	G	7	2 	4U				H4SW    					 
1999082000609	19990820	00609		1999	8	20	HEEA063209       	4	19990809	G	3422	206075606103	GYRO            			BELL  	206   	206L1       	1182107	SW  										COCKPIT	PRECESSES       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3178K					45765				DIRECTIONAL GYRO PRECESSES EXCESSIVELY.						1	G	7	1 	3U				H2SW    					 
1999082000610	19990820	00610	SW  	1999	8	20	HEEA063210       	1	19990809	G	6730	206076062003	CYLINDER        			BELL  	206   	206L1       	1182107	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	45RP	6651 				45521				CYLINDER LEAKING.						1	G	7	1 	3U				H2SW    					 
1999082000611	19990820	00611		1999	8	20	HEEA063211       	4	19990809	G	3455	6222362001	RECEIVER        			BELL  	412   	412         	1182202	SW  										ADF	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1202T					33112				RECEIVER WILL NOT RECEIVE.						1	G	7	2 	4U				H4SW    					 
1999082000612	19990820	00612		1999	8	20	HEEA063212       	4	19990809	G	3413	212070239001	INDICATOR       			BELL  	212   	212         	1181420	SW  										RATE OF CLIMB	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5736D					31135				INDICATOR STICKING.						1	G	7	1 	4U				H4SW    					 
1999082000613	19990820	00613		1999	8	20	HEEA063213       	4	19990809	G	3414	8000	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										AIRSPEED	ERRATIC         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5745N					45489				AIRSPEED INDICATOR HAD ERRATIC READINGS.						1	G	7	1 	3U				H2SW    					 
1999082000614	19990820	00614	SW  	1999	8	20	HEEA063214       	1	19990809	G	7722	206375007103	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TOT INDICATOR FAILED TO OPERATE.						1	G	7	1 	3U				H2SW    					 
1999082000615	19990820	00615	SW  	1999	8	20	HEEA063215       	1	19990809	G	2435	23046020	STARTER         			BELL  	412   	412         	1182202	SW  										STARTER/GEN	VIBRATING       	E			HEEA	O				OTHER                   				E			VIBRATION/BUFFET          			NR	NOT REPORTED   	1			SW	03	3893S	12754				33022				HIGH FREQUENCY VIBRATION FELT IN AIRFRAME WITH GENERATOR TURNED ON.						1	G	7	2 	4U				H4SW    					 
1999082000616	19990820	00616	SW  	1999	8	20	HEEA063216       	1	19990809	G	7722	206375006101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2758N					45267				TOT INDICATOR INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999082000617	19990820	00617		1999	8	20	HEEA063217       	1	19990809	G	7722	206375007103	INDICATOR       																	TOT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	CFVEF					52071				TOT INDICATOR STICKS ON ZERO ON START.																			 
1999082000618	19990820	00618		1999	8	20	HEEA063218       	4	19990809	G	3420	1113034	INDICATOR       			BELL  	212   	212         	1181420	SW  										ATTITUDE	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5010F					30936				INDICATOR OPERATES INTERMITTENTLY.						1	G	7	1 	4U				H4SW    					 
1999082000619	19990820	00619	SW  	1999	8	20	HEEA063219       	1	19990809	G	2430	206075447007	VOLT REGULATOR  			BELL  	206   	206L1       	1182107	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2758N					45267				GENERATOR WILL NOT COME ON-LINE.						1	G	7	1 	3U				H2SW    					 
1999082000620	19990820	00620	SW  	1999	8	20	HEEA063220       	1	19990809	G	8011	2CM272B1	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				STARTER/GENERATOR BURNED UP.						2	G	7	2 	4U				H10SW   					 
1999082000621	19990820	00621	SW  	1999	8	20	HEEA063221       	1	19990809	G	3212	412050013113	BAG             			BELL  	412   	412         	1182202	SW  										FLOAT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3911L					33023				FLOAT BAG LEAKING.						1	G	7	2 	4U				H4SW    					 
1999082000622	19990820	00622	SW  	1999	8	20	HEEA063222       	1	19990809	G	3212	D24922117	BAG             			BELL  	412   	412         	1182202	SW  										FLOAT	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	2148K	1664 				36001				FLOAT BAG LEAKING FROM CHECK VALVE.						1	G	7	2 	4U				H4SW    					 
1999082000623	19990820	00623	SW  	1999	8	20	HEEA063223       	1	19990809	G	3212	412050013117	BAG             			BELL  	412   	412         	1182202	SW  										FLOAT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3911L					33023				FLOAT BAG LEAKING.						1	G	7	2 	4U				H4SW    					 
1999082000624	19990820	00624	SW  	1999	8	20	HEEA063224       	1	19990809	G	3212	D24921115	BAG             			BELL  	412   	412         	1182202	SW  										FLOAT	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	3911L					33023				FORWARD CELL ON FLOAT BAG LEAKING.						1	G	7	2 	4U				H4SW    					 
1999082000625	19990820	00625	SW  	1999	8	20	HEEA063225       	1	19990809	G	3212	206050248117	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	8591X					51495				FLOAT BAG LEAKING AT VENT ATTACHING.						1	G	7	1 	3U				H2SW    					 
1999082000626	19990820	00626		1999	8	20	HEEA063226       	4	19990809	G	3414	412075009105	INDICATOR       			BELL  	412   	412         	1182202	SW  										AIRSPEED	STICKING        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893L					33006				AIRSPEED INDICATOR HANGS UP AT 45 KNOTS.						1	G	7	2 	4U				H4SW    					 
1999082000627	19990820	00627	SW  	1999	8	20	HEEA063227       	1	19990809	G	3212	412050013119	BAG             			BELL  	412   	412         	1182202	SW  										FLOAT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	800Y	487  				33134				CHAFED HOLE ON TWO ENDS OF FLOAT.						1	G	7	2 	4U				H4SW    					 
1999082000628	19990820	00628		1999	8	20	HEEA063228       	4	19990809	G	3414	412075009105	INDICATOR       			BELL  	412   	412         	1182202	SW  										AIRSPEED	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	293CA					33005				RED LINES HAVE FADED TO ORANGE ON AIRSPEED INDICATOR.						1	G	7	2 	4U				H4SW    					 
1999082000629	19990820	00629	SW  	1999	8	20	HEEA063229       	1	19990809	G	2823	L88010501	VALVE           			BELL  	412   	412         	1182202	SW  										FUEL SYSTEM	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										VALVE WILL NOT CLOSE.						1	G	7	2 	4U				H4SW    					 
1999082000630	19990820	00630	SW  	1999	8	20	HEEA063230       	1	19990809	G	7722	206375007103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TOT	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251Y					51556				TOT INDICATOR STUCK AT 300 DEGREES.						1	G	7	1 	3U				H2SW    					 
1999082000631	19990820	00631	SW  	1999	8	20	HEEA063231       	1	19990809	G	7722	206375007103	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TOT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TOT GAUGE RISES 30 DEGREES WHEN VHF IS KEYED.						1	G	7	1 	3U				H2SW    					 
1999082000632	19990820	00632		1999	8	20	HEEA063232       	4	19990809	G	3457	0110005400	GPS             			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	41128					51465				GPS 150 LOSES WAY POINTS.						1	G	7	1 	3U				H2SW    					 
1999082000633	19990820	00633	SW  	1999	8	20	HEEA063233       	1	19990809	G	2822	164A199	BOOST PUMP      			BELL  	206   	206L1       	1182107	SW  										FUEL SYSTEM	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	10778					45391				VENDOR INSERT THAT HOLDS LOW LEVEL IS NO GOOD ON BOOST PUMP.  APPEARS TO BE A DOUBLE INSERT.  STUD CANNOT CATCH THREADS.						1	G	7	1 	3U				H2SW    					 
1999082000634	19990820	00634	SW  	1999	8	20	HEEA063234       	1	19990809	G	3212	V80500113	SOLENOID VALVE  			BELL  	214   	214ST       	1182106	SW  										VACUUM SYSTEM	MALFUNCITONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	8045T					28101				SOLENOID VALVE ACTIVATED AND PREMATURELY INFLATED FLOATS.						2	G	7	2 	4U				H10SW   					 
1999082000635	19990820	00635		1999	8	20	HEEA063235       	4	19990809	G	3416	5035P2P44	ENCODER         			BELL  	412   	412         	1182202	SW  										ALTIMETER	OUT OF ADJUST   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2149S					36002				ENCODING OFF 115 DEGREES ON ALTIMETER.						1	G	7	2 	4U				H4SW    					 
1999082000636	19990820	00636		1999	8	20	HEEA063236       	4	19990809	G	2312	40008310103	TRANSCEIVER,RT14			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	59806					28140				TRANSCEIVER TRIPS CIRCUIT BREAKER AFTER WARM UP.						2	G	7	2 	4U				H10SW   					 
1999082000637	19990820	00637		1999	8	20	HEEA063237       	4	19990809	G	3422	2891ESR	GYRO            			BELL  	206   	206L3       	1182108	SW  										COCKPIT DG	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	31801					51074				DIRECTIONAL GYRO WILL NOT SLAVE PLUS OR MINUS 5 VOLTS.						1	G	7	1 	3U				H2SW    					 
1999082000638	19990820	00638		1999	8	20	HEEA063238       	4	19990809	G	2312	064100900	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										VHF COMM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893S					33022				TRANSMITS GARBLED.  TIME SINCE REPAIR 316:50. HOURS.						1	G	7	2 	4U				H4SW    					 
1999082000639	19990820	00639	SW  	1999	8	20	HEEA063239       	1	19990809	G	3212	206050248117	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	129MR					51129				AFT FLOAT BAG COMPARTMENT HAS A LEAK.  DATE OF MFG 11-94.						1	G	7	1 	3U				H2SW    					 
1999082000640	19990820	00640		1999	8	20	HEEA063240       	4	19990809	G	3457	13824120234	GPS RECEIVER    			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6603X					51412				RECEIVER TRIPS CIRCUIT BREAKER.  TIME SINCE REPAIR 132:45 HOURS.						1	G	7	1 	3U				H2SW    					 
1999082000641	19990820	00641		1999	8	20	HEEA063241       	4	19990809	G	3457	0845000000	GPS             			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	81671					51301				GPS WILL NOT UPDATE.						1	G	7	1 	3U				H2SW    					 
1999082000642	19990820	00642		1999	8	20	HEEA063242       	4	19990809	G	3457	0845000000	GPS             			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2777D					45299				GPS WILL NOT UPDATE, STUCK IN ONE POSITION.						1	G	7	1 	3U				H2SW    					 
1999082000643	19990820	00643		1999	8	20	HEEA063243       	4	19990809	G	3457	0845000000	GPS             			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5007N					45184				SOME BUTTONS ON GPS INOPERATIVE AND CANNOT SCROLL WITH KNOBS.						1	G	7	1 	3U				H2SW    					 
1999082000644	19990820	00644		1999	8	20	HEEA063244       	4	19990809	G	2312	064100900	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										VHF COMM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	22608					33075				TRANSCEIVER TRANSMITS MUFFLED SIGNAL.  TIME SINCE REPAIR 3:15 HOURS.						1	G	7	2 	4U				H4SW    					 
1999082000645	19990820	00645		1999	8	20	HEEA063245       	4	19990809	G	2312	066106600	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	8045T					28101				DME DISPLAYS DASHES.						2	G	7	2 	4U				H10SW   					 
1999082000646	19990820	00646		1999	8	20	HEEA063246       	4	19990809	G	3457	8143902240B	GPS             			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	22608					33075				RECEIVER FAILED.						1	G	7	2 	4U				H4SW    					 
1999082000647	19990820	00647		1999	8	20	HEEA063247       	4	19990809	G	3457	13824120234	GPS RECEIVER    			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6161A					51611				GPS RECEIVER - BUSS FAILURE NR 10, BUSS FAILURE NR 8.						1	G	7	1 	3U				H2SW    					 
1999082000648	19990820	00648		1999	8	20	HEEA063248       	4	19990809	G	3444	071111400	ANTENNA         			BELL  	407   	407         		SW  										RADAR ALTIMETER	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	720PH					53277				RADAR ALTIMETER ERRATIC IN-FLIGHT.						1	G	7	1 	3U			O	H2SW    					 
1999082000649	19990820	00649	SW  	1999	8	20	HEEA063249       	1	19990809	G	2430	A1077V	RELAY           			BELL  	206   	206L3       	1182108	SW  										COCKPIT	STICKING        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	8588X					51486				CONTACTOR STICKING.						1	G	7	1 	3U				H2SW    					 
1999082000650	19990820	00650	SW  	1999	8	20	HEEA063250       	1	19990809	G	2435	23081018	STARTER         			BELL  	206   	206L1       	1182107	SW  										STARTER/GEN	MISOVERHAULED   	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	5745S	15164				45491				STARTER/GENERATOR INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND THE WRONG TYPE BRUSHES WERE INSTALLED BY THE VENDOR AT 	OVERHAUL.  THESE HAVE THE HARD INSERTS AND GROOVED THE COMMUTATOR.					1	G	7	1 	3U				H2SW    					 
1999082000651	19990820	00651		1999	8	20	HEEA063251       	4	19990809	G	3421	5040017901	INDICATOR       			BELL  	412   	412         	1182202	SW  										ATTITUDE	WON'T CAGE      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5759N					33002				ATTITUDE INDICATOR WILL NOT CAGE.						1	G	7	2 	4U				H4SW    					 
1999082000652	19990820	00652	GL  	1999	8	20	HEEA063252       	2	19990809	G	7314	3881005	FUEL PUMP       			BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2759U	16442				45272				FOUND EXCESSIVE STEP WEAR AND PITTING ON INNER SPLINES AND DRIVE SHAFT ON FUEL PUMP.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999082000653	19990820	00653	SW  	1999	8	20	HEEA063253       	1	19990809	G	2436	163404731	VOLT REGULATOR  			BELL  	206   	206L3       	1182108	SW  										DC SYSTEM	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6251Y					51556				GENERATOR FALLS OFF-LINE, WILL NOT RESET.						1	G	7	1 	3U				H2SW    					 
1999082000654	19990820	00654		1999	8	20	HEEA063254       	4	19990809	G	3452	066106200	TRANSPONDER     			BELL  	206   	206L1       	1182107	SW  										ATC PANEL	WEAK            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1077A					45382				TRANSCEIVER'S NR 4 DIGIT KNOB BROKEN.  PERFORMED PRELIMINARY INSPECTION AND REPLACED BROKEN KNOB ON FACEPLATE.  FOUND FR	EQUENCY OUT OF TOLERANCE, ADJUSTED V101 AND FOUND RECEIVER SENSITIVITY WEAK.					1	G	7	1 	3U				H2SW    					 
1999082000655	19990820	00655		1999	8	20	HEEA063255       	4	19990810	G	2312	064105430	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										VHF COMM	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3904L					45597				TRANSCEIVER BLINKS OFF INTERMITTENTLY ON LED SCREEN.  PERFORMED PRELIMINARY INSPECTION.   REPLACED DISPLAY BOARD AND 3 H	EADERS.  DISPLAY STILL BAD.					1	G	7	1 	3U				H2SW    					 
1999082000656	19990820	00656		1999	8	20	HEEA063256       	4	19990810	G	2312	064105430	TRANSCEIVER     			BELL  	206   	206L4       	1182110	SW  										VHF COMM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7074W					52033				RECEIVING BLEEDOVER ON 123.00 AND 129.77.  PERFORMED PRELIMINARY INSPECTION.  FOUND UNIT TRANSMITTING WEAK INTERMITTENTL	Y AND ALSO RECEIVER HAS CONSTANT STATIC.					1	G	7	1 	3U			NC	H2SW    					 
1999082000657	19990820	00657		1999	8	20	HEEA063257       	4	19990810	G	2312	069102505	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COMMUNICATIONS	WEAK            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	92MT					51175				WEAK RECEIVE AND TRANSMIT.  PERFORMED PRELIMINARY INSPECTION.  FOUND RECEIVER SENSITIVITY VERY LOW.						1	G	7	1 	3U				H2SW    					 
1999082000658	19990820	00658		1999	8	20	HEEA063258       	4	19990810	G	3457	13824120234	GPS RECEIVER    			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED TEST     	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	4282Z					51499				WARNING FLAG ON ALL THE TIME.  PERFORMED PRELIMINARY INSPECTION.  FOUND UNIT TO FAIL GPS TEST.						1	G	7	1 	3U				H2SW    					 
1999082000659	19990820	00659	SW  	1999	8	20	HEEA063259       	1	19990810	G	6210	206010200133	BLADE           			BELL  	206   	206B3       	1181506	SW  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	206JB	840  				4398				SEVERAL AREAS OF CORROSION ON TRAILING EDGE OF BLADES.						1	G	7	1 	3U				H2SW    					 
1999082000660	19990820	00660	SW  	1999	8	20	HEEA063260       	1	19990810	G	6320	206040530001	CASE ASSY       		206040004111	BELL  	206   	206L1       	1182107	SW  										M/R GEARBOX	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2250U					45754				FOUND CORROSION BEHIND INPUT LINER ON MAIN CASE ASSY.  (OIL FILTER CORROSION) REPLACED WITH SERVICEABLE ASSY.						1	G	7	1 	3U				H2SW    					 
1999082000661	19990820	00661	SW  	1999	8	20	HEEA063261       	1	19990810	G	6730	206076062003	CYLINDER        			BELL  	206   	206L1       	1182107	SW  										CYCLIC	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	5019F	20449				45244				BLED ALL AIR FROM SERVO WITH AUXILIARY GROUND HYDRAULIC UNIT AND SHUT OFF HYDRAULIC POWER.   FOUND SERVO STATIC LEAKING 	WITH NO PRESSURE AT FORWARD PISTON.   ALSO FOUND BOOT DETERIORATED.					1	G	7	1 	3U				H2SW    					 
1999082000662	19990820	00662	GL  	1999	8	20	HEEA063262       	2	19990810	G	7321	25490923	FCU             			BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					ENGINE	FLUCTUATING     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31073	1038 				51519				TORQUE AND TOT FLUCTUATIONS IN-FLIGHT AFTER POWER CHANGES.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999082000663	19990820	00663		1999	8	20	HEEA063263       	4	19990810	G	3422	2891ESR	GYRO            			BELL  	206   	206L1       	1182107	SW  										COCKPIT DG	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5742N					45477				UNIT WILL NOT SLAVE.  TIME SINCE REPAIR 0:00 HOURS.						1	G	7	1 	3U				H2SW    					 
1999082000664	19990820	00664		1999	8	20	HEEA063264       	4	19990810	G	3420	5050010902	GYRO            			BELL  	206   	206L3       	1182108	SW  										COCKPIT	PRECESSES       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6748D					51106				FLAG WILL NOT PULL AND PRECESSES.						1	G	7	1 	3U				H2SW    					 
1999082000665	19990820	00665	SW  	1999	8	20	HEEA063265       	1	19990810	G	6710	C4264215	SLIDE AND SLEEVE			BELL  	206   	206L3       	1182108	SW  										M/R CONTROL	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03										LEAKING AFTER BLEEDING AIR FROM SERVO VALVE PRIMARY SPOOL WITH NO PRESSURE.  TIME SINCE REPAIR 0:00 HOURS.						1	G	7	1 	3U				H2SW    					 
1999082000666	19990820	00666		1999	8	20	HEEA063266       	4	19990810	G	3452	066107100	TRANSPONDER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			SW	03	59805					28141				TRANSPONDER INOPERATIVE.  SMELLS BURNT.  PERFORMED PRELIMINARY INSPECTION.  FOUND EXCESSIVE CORROSION AND POWER SUPPLY B	AD.					2	G	7	2 	4U				H10SW   					 
1999082000667	19990820	00667		1999	8	20	HEEA063267       	4	19990810	G	2312	064102300	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										VHF COMM	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2148K					36001				TRANSCEIVER NTERMITTENT AND SCRATCHY.  PERFORMED PRELIMINARY INSPECTION.  FOUND CORROSION IN UNIT AND TRANSMIT POWER OUT	 LOW AT SOME FREQUENCIES.					1	G	7	2 	4U				H4SW    					 
1999082000668	19990820	00668		1999	8	20	HEEA063268       	4	19990810	G	3431	066107800	HEADER          			BELL  	214   	214ST       	1182106	SW  										COCKPIT NAV	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				2 YEAR INSPECTION.  FOUND EXCESSIVE CORROSION UNDER HEADER P102 AND J101. REMOVED HEADER AND PLUG AND CLEANED CORROSION.	  REPLACED P102 AND J101.  UNIT WILL NOT TURN ON.					2	G	7	2 	4U				H10SW   					 
1999082000669	19990820	00669	SW  	1999	8	20	HEEA063269       	1	19990810	G	6420	214011802111	YOKE            		214011801117	BELL  	214   	214ST       	1182106	SW  										TAIL ROTOR	BENT            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N	2229 			A761	28106				FLAPPING STOP EAR BENT.  SCRAPPED YOKE AND REPLACED WITH SERVICEABLE PART.						2	G	7	2 	4U				H10SW   					 
1999082000670	19990820	00670	SW  	1999	8	20	HEEA063270       	1	19990810	G	6210	214015300107	BLADE           			BELL  	214   	214ST       	1182106	SW  										MAIN ROTOR	DEBONDED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N	8187 				28106				TOP METAL EROSION SHIELD IS DEBONDING.						2	G	7	2 	4U				H10SW   					 
1999082000671	19990820	00671	SW  	1999	8	20	HEEA063271       	1	19990810	G	6520	214040404101	SHAFT           		214040011119	BELL  	214   	214ST       	1182106	SW  										T/R GEARBOX	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N	3869 				28106				GEARBOX REMOVED DUE TO CORROSION AND WEAR ON SPLINES.  FOUND 1 EACH SPLINE BROKEN.  REPLACED WITH SERVICEABLE OUTPUT SHA	FT.					2	G	7	2 	4U				H10SW   					 
1999082000672	19990820	00672	SW  	1999	8	20	HEEA063273       	1	19990810	G	6520	214040404101	SHAFT           		214040011119	BELL  	214   	214ST       	1182106	SW  										T/R GEARBOX	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T	1248 			A610	28101				FAILURE IN THREAD AREA OF OUTPUT SHAFT.  REPLACED WITH SERVICEABLE OUTPUT SHAFT.						2	G	7	2 	4U				H10SW   					 
1999082000673	19990820	00673	SW  	1999	8	20	HEEA063274       	1	19990810	G	6520	214040408101	GEAR            		214040011119	BELL  	214   	214ST       	1182106	SW  										T/R GEARBOX	SCORED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				BEARING SEAT SCORED.  REPLACED WITH SERVICEABLE GEAR ASSY.						2	G	7	2 	4U				H10SW   					 
1999082000674	19990820	00674	SW  	1999	8	20	HEEA063275       	1	19990810	G	6300	214040844109	RETAINER ASSY   		214040013109	BELL  	214   	214ST       	1182106	SW  										M/R DRIVE	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805	2498 			A12	28141				RETAINER ASSY HAD EXCESSIVE PITTING.  REPLACED WITH SERVICEABLE PART.						2	G	7	2 	4U				H10SW   					 
1999082000675	19990820	00675	SW  	1999	8	20	HEEA063276       	1	19990810	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T	2556 				28101				STARTER INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999082000676	19990820	00676	SW  	1999	8	20	HEEA063277       	1	19990810	G	2435	36B510954G2	CLUTCH          		214060056103	BELL  	214   	214ST       	1182106	SW  										STARTER/GEN	SLIPPAGE        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806				88D0440	28140				CLUTCH FAILED SLIPPAGE TORQUE TEST.  IT EXCEEDED MAXIMUM LIMITS.  REPLACED CLUTCH AND RETURNED STARTER TO SERVICE.						2	G	7	2 	4U				H10SW   					 
1999082000677	19990820	00677		1999	8	20	HEEA063278       	4	19990810	G	3442	40008310105	TRANSCEIVER     			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				TRANSERVER DISPLAYS R/T FAULT IN 1 AND 2 MODES WHEN IN SEARCH.						2	G	7	2 	4U				H10SW   					 
1999082000678	19990820	00678		1999	8	20	HEEA063279       	4	19990810	G	2312	064105430	TRANSCEIVER     			BELL  	407   	407         		SW  										VHF COMM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	723PH					53283				STAND-BY SIDE WILL NOT RETAIN FREQUENCY MEMORY.						1	G	7	1 	3U			O	H2SW    					 
1999082000679	19990820	00679	SW  	1999	8	20	HEEA063280       	1	19990810	G	2435	23081018	STARTER         			BELL  	407   	407         		SW  										STARTER/GEN	MISOVERHAULED   	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	141MA	15177				53016				STARTER/GENERATOR INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND THE WRONG TYPE BRUSHES WERE INSTALLED BY THE VENDOR AT 	OVERHAUL.  THESE HAVE THE HARD INSERTS AND GROOVED THE COMMUTATOR.					1	G	7	1 	3U			O	H2SW    					 
1999082000680	19990820	00680	SW  	1999	8	20	HEEA063281       	1	19990810	G	5200	3226201	LEVER           		20898411    	BELL  	407   	407         		SW  										PAX  DOOR	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA				NA	53016				LEVER BROKE ON LEFT FORWARD DOOR WHICH PREVENTED THE OUTSIDE DOOR HANDLE FROM OPENING THE DOOR.						1	G	7	1 	3U			O	H2SW    					 
1999082000681	19990820	00681	SW  	1999	8	20	HEEA063282       	1	19990810	G	6320	NAS6606H23	BOLT            		407040006103	BELL  	407   	407         		SW  										M/R GEARBOX	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA				A16	53016				BOLT WORN .011 INCH.  REPLACED WITH SERVICEABLE BOLT.						1	G	7	1 	3U			O	H2SW    					 
1999082000682	19990820	00682	SW  	1999	8	20	HEEA063283       	1	19990810	G	3340	01077028521	STROBE          			BELL  	412   	412         	1182202	SW  										FUSELAGE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K					33020				STROBE LIGHT DOES NOT FLASH, INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999082000683	19990820	00683	SW  	1999	8	20	HEEA063284       	1	19990810	G	3340	01077028521	STROBE          			BELL  	412   	412         	1182202	SW  										FUSELAGE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				STROBE LIGHT INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999082000684	19990820	00684		1999	8	20	HEEA063285       	4	19990810	G	3444	066104802	RADAR ALTIMETER 			BELL  	412   	412         	1182202	SW  										RT UNIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2261D					33076				SYSTEM INDICATOR SURGES FROM ZERO TO FULL SCALE CONTINUOUSLY ABOVE 3,000 FEET ALTITUDE.  PERFORMED PRELIMINARY INSPECTIO	N.   FOUND UNIT OFF FREQUENCY, ADJUSTED TO SPECS WHILE TESTING NEEDLE WOULD BECOME ERRATIC.					1	G	7	2 	4U				H4SW    					 
1999082000685	19990820	00685	SW  	1999	8	20	HEEA063286       	1	19990810	G	2844	124044	INDICATOR       			BELL  	412   	412         	1182202	SW  										FUEL PRESSURE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	107X					33113				NEEDLE MOVES WHEN POTENTIOMETER IS VARIED.						1	G	7	2 	4U				H4SW    					 
1999082000686	19990820	00686	SW  	1999	8	20	HEEA063287       	1	19990810	G	7931	209070262101	INDICATOR       			BELL  	412   	412         	1182202	SW  										ENGINE OIL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893L					33006				ENGINE OIL TEMPERATURE SIDE DROPS TO ZERO AND COMES BACK UP.  ALSO, THE PRESSURE SIDE IS INDICATING LOW BY 10 PSI.						1	G	7	2 	4U				H4SW    					 
1999082000687	19990820	00687	SW  	1999	8	20	HEEA063288       	1	19990810	G	7931	209070262101	INDICATOR       			BELL  	412   	412         	1182202	SW  										ENGINE OIL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893L					33006				THE PRESSURE SIDE DOES NOT INDICATE AT ALL.  THE RANGE MARKINGS ARE NOT CORRECT FOR THE TEMPERATURE OR THE PRESSURE SIDE	 OF THIS INDICATOR.					1	G	7	2 	4U				H4SW    					 
1999082000688	19990820	00688	SW  	1999	8	20	HEEA063289       	1	19990810	G	6410	212010750105	BLADE           			BELL  	412   	412         	1182202	SW  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008	3690 				36004				F.O.D. HOLE IN LEADING EDGE OF BLADE.						1	G	7	2 	4U				H4SW    					 
1999082000689	19990820	00689	SW  	1999	8	20	HEEA063290       	1	19990810	G	2435	23046020	STARTER         			BELL  	412   	412         	1182202	SW  										STARTER/GEN	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7128R	16208				36007				STARTER/GENERATOR DRAGGING DURING START.						1	G	7	2 	4U				H4SW    					 
1999082000690	19990820	00690	SW  	1999	8	20	HEEA063291       	1	19990810	G	6710	41001687	LEVER           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										FLANGED BUSHING OF LEVER ASSY TOO LARGE FOR YOKE ASSY.  TIME SINCE REPAIR 0:00 HOURS.						1	G	7	2 	4U				H4SW    					 
1999082000691	19990820	00691	SW  	1999	8	20	HEEA063292       	1	19990810	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22347	13212				36005				BLADE HAD SEVERAL PIN HOLES IN THE OUTBOARD LEADING EDGE STRIP.  THE INBOARD TRIM TAB WAS CRACKED.						1	G	7	2 	4U				H4SW    					 
1999082000692	19990820	00692	SW  	1999	8	20	HEEA063293       	1	19990810	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22347	10805				36005				SEVERAL PIN HOLES IN THE OUTBOARD LEADING EDGE STRIP.  THE INBOARD TAB AND CENTER TAB HAD SOME SEPARATION.						1	G	7	2 	4U				H4SW    					 
1999082000693	19990820	00693	SW  	1999	8	20	HEEA063294       	1	19990810	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	DEBONDED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3911L	5053 				33023				SKIN AT SPLICE JOINT AREA UNBONDED.						1	G	7	2 	4U				H4SW    					 
1999082000694	19990820	00694	SW  	1999	8	20	HEEA063295       	1	19990810	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893L	5951 				33006				INBOARD ABRASION STRIP CRACKED NEAR THE SPLICE COVER ON THE UPPER SURFACE.  FIBERGLASS CRACKED AROUND THE INBOARD AND MI	D-SPAN TAB.					1	G	7	2 	4U				H4SW    					 
1999082000695	19990820	00695	SW  	1999	8	20	HEEA063296       	1	19990810	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONTROL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	293CA					33005				NR 1 GENERATOR WILL NOT COME ON-LINE.						1	G	7	2 	4U				H4SW    					 
1999082000696	19990820	00696		1999	8	20	HEEA063297       	4	19990810	G	3460	5205160006	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	WON'T TEST      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023					33080				TO FLAG COMES WITH POWER AND NO FROM FLAG WHEN TEST WITH NAV 401 TEST SET.  PERFORMED PRELIMINARY INSPECTION AND UNIT FU	NCTION TEST GOOD.					1	G	7	2 	4U				H4SW    					 
1999082000697	19990820	00697	SW  	1999	8	20	HEEA063298       	1	19990810	G	7931	206075678103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										ENGINE OIL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8593X					51509				INDICATOR'S TEMPERATURE NEEDLE WILL NOT MOVE.						1	G	7	1 	3U				H2SW    					 
1999082000698	19990820	00698		1999	8	20	HEEA063299       	4	19990810	G	2210	214074305105	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										FBW ELEVATOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				A/S 3 LIGHT DIM WHEN ELEVATOR IS TESTED.						2	G	7	2 	4U				H10SW   					 
1999082000699	19990820	00699		1999	8	20	HEEA063300       	4	19990810	G	3420	1113025	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT HSI	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	108X					33115				INDICATOR'S ADF NEEDLE OFF 30-60 PERCENT.						1	G	7	2 	4U				H4SW    					 
1999082000700	19990820	00700	SW  	1999	8	20	HEEA063301       	1	19990810	G	6322	214076333107	MOTOR           			BELL  	214   	214ST       	1182106	SW  										BLOWER	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				OIL COOLER LIGHT STAYS ON.						2	G	7	2 	4U				H10SW   					 
1999082000701	19990820	00701	SW  	1999	8	20	HEEA063302       	1	19990810	G	7712	412075008111	INDICATOR       			BELL  	412   	412         	1182202	SW  										DUAL TORQUE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893N					33010				TORQUE INDICATOR TRIPS CIRCUIT BREAKER.						1	G	7	2 	4U				H4SW    					 
1999082000702	19990820	00702	SW  	1999	8	20	HEEA063303       	1	19990810	G	7712	412075008111	INDICATOR       			BELL  	412   	412         	1182202	SW  										DUAL TORQUE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2148K					36001				TORQUE INDICATOR TRIPS BREAKER.						1	G	7	2 	4U				H4SW    					 
1999082000703	19990820	00703	SW  	1999	8	20	HEEA063304       	1	19990811	G	7810	407063001101	STACK           			BELL  	407   	407         		SW  										EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				EXHAUST STACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999082000704	19990820	00704	SW  	1999	8	20	HEEA063311       	1	19990811	G	6510	407340340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				DISC PACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999082000705	19990820	00705	SW  	1999	8	20	HEEA063313       	1	19990811	G	5320	204030959002A	SUPPORT         			BELL  	212   	212         	1181420	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										SUPPORT MISMANUFACTURED.  RIGHT AFT VOR ANTENNA MOUNTS RECEIVED WITH PILOT HOLES.   SEVERAL OF THESE PILOT HOLES DO NOT 	HAVE SUFFICIENT EDGE DISTANCE FOR INSTALLATION OF .1250 INCH OR .1562 INCH RIVETS, WHICH ARE REQUIRED FOR INSTALLATION O	F THE FITTING.				1	G	7	1 	4U				H4SW    					 
1999082000706	19990820	00706		1999	8	20	HEEA063314       	4	19990812	G	3431	066107800	RECEIVER        			BELL  	412   	412         	1182202	SW  										COCKPIT NAV	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008					36004				VBR INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999082000707	19990820	00707	SW  	1999	8	20	HEEA063315       	1	19990812	G	2820	205060612003	VALVE ASSY      			BELL  	412   	412         	1182202	SW  										FUEL SYSTEM	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893L					33006				GAUGE SHOWS PRESSURE WHEN PUMP IS TURNED ON WITH VALVE SHUT OFF.						1	G	7	2 	4U				H4SW    					 
1999082000708	19990820	00708	SW  	1999	8	20	HEEA063316       	1	19990812	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										ROTARY	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893N					33010				LATERAL MAG BRAKE STICKING.						1	G	7	2 	4U				H4SW    					 
1999082000709	19990820	00709		1999	8	20	HEEA063317       	4	19990812	G	2312	064101902	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1081T					45411				LED'S TOO DIM TO READ FREQUENCY.						1	G	7	1 	3U				H2SW    					 
1999082000710	19990820	00710		1999	8	20	HEEA063318       	4	19990812	G	3455	066104701	RECEIVER        			BELL  	212   	212         	1181420	SW  										ADF	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3131S					30953				TRANSCEIVER WILL NOT COME ON.						1	G	7	1 	4U				H4SW    					 
1999082000711	19990820	00711		1999	8	20	HEEA063319       	4	19990812	G	3421	222375033107	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				GAUGE KNOB WILL NOT RESET.						2	G	7	2 	4U				H10SW   					 
1999082000712	19990820	00712	SW  	1999	8	20	HEEA063320       	1	19990812	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONTROL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	293CA					33005				CONTROL UNIT WOULD NOT COME ON-LINE.						1	G	7	2 	4U				H4SW    					 
1999082000713	19990820	00713	SW  	1999	8	20	HEEA063321       	1	19990812	G	2437	214175250103	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				INDICATOR'S NR 2 NEEDLE STICKS.						2	G	7	2 	4U				H10SW   					 
1999082000714	19990820	00714		1999	8	20	HEEA063322       	4	19990812	G	2211	4033089901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AUTO FLIGHT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	800Y					33134				COMPUTER INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999082000715	19990820	00715		1999	8	20	HEEA063323       	4	19990812	G	3420	1113025	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT HSI	INACCURATE      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893N					33010				PILOT REPORTS THAT COURSE NUMBER READS DIFFERENT FROM COMPASS NUMBER.						1	G	7	2 	4U				H4SW    					 
1999082000716	19990820	00716	SW  	1999	8	20	HEEA063324       	1	19990812	G	6710	206062721113	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP COMP	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ACTUATOR WILL NOT BEEP.						1	G	7	1 	3U				H2SW    					 
1999082000717	19990820	00717	SW  	1999	8	20	HEEA063325       	1	19990812	G	3212	214073936104	BAG             			BELL  	214   	214ST       	1182106	SW  										FLOAT	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805	725  				28141				FLOAT BAG LEAKING.						2	G	7	2 	4U				H10SW   					 
1999082000718	19990820	00718	SW  	1999	8	20	HEEA063326       	1	19990812	G	6240	206075681003	INDICATOR       			BELL  	206   	206B3       	1181506	SW  										DUAL TACH	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	103PH					3000				ROTOR NEEDLE LAGGED AND FLUCTUATES ON DUAL TACHOMETER INDICATOR.						1	G	7	1 	3U				H2SW    					 
1999082000719	19990820	00719		1999	8	20	HEEA063327       	4	19990812	G	3444	066104800	RADAR ALTIMETER 			BELL  	412   	412         	1182202	SW  										RT UNIT	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				ALTIMETER INDICATOR FLUCTUATES INTERMITTENTLY.						1	G	7	2 	4U				H4SW    					 
1999082000720	19990820	00720		1999	8	20	HEEA063328       	4	19990812	G	2312	7001840913	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008					36004				RECEIVER/TRANSMITTER INDICATOR NEEDLE FLUCTUATES.						1	G	7	2 	4U				H4SW    					 
1999082000721	19990820	00721	SW  	1999	8	20	HEEA063329       	1	19990812	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP COMP	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5007Q					45187				ACTUATOR HAD EXCESSIVE PLAY ON ROD END.						1	G	7	1 	3U				H2SW    					 
1999082000722	19990820	00722		1999	8	20	HEEA063330       	4	19990812	G	3457	81439000232	RECEIVER        			BELL  	214   	214ST       	1182106	SW  										GPS SYSTEM	MISINSTALLED    	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	59806					28140				GPS RECEIVER'S BEARING 180 DEGREES OFF.						2	G	7	2 	4U				H10SW   					 
1999082000723	19990820	00723	SW  	1999	8	20	HEEA063331       	1	19990812	G	6720	214001540117	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										T/R CONTROL	WON'T TEST      	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	5748M					28102				LIGHT IN SCAS TEST WILL NOT WORK.						2	G	7	2 	4U				H10SW   					 
1999082000724	19990820	00724	SW  	1999	8	20	HEEA063332       	1	19990812	G	2913	206076030111	PUMP            			BELL  	206   	206L1       	1182107	SW  										HYDRAULIC SYSTEM	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5007N					45184				PUMP'S RESERVOIR HOT AND BLADES HARD TO TURN.						1	G	7	1 	3U				H2SW    					 
1999082000725	19990820	00725		1999	8	20	HEEA063333       	4	19990812	G	2312	7001840913	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3116L					51529				RECEIVER/TRANSMITTER INDICATES 100 TO 150 FEET AT ALL TIMES.						1	G	7	1 	3U				H2SW    					 
1999082000726	19990820	00726		1999	8	20	HEEA063334       	4	19990812	G	3421	500DCBELL5	HORIZON         			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	10761					45381				HORIZONTAL GYRO UNRELIABLE.						1	G	7	1 	3U				H2SW    					 
1999082000727	19990820	00727		1999	8	20	HEEA063335       	4	19990812	G	2200	4030182901	ALTITUDE SENSOR 			BELL  	412   	412         	1182202	SW  										AUTO FLIGHT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	142PH					33150				AUTOFLIGHT MAKES AIRCRAFT PORPOISE.						1	G	7	2 	4U				H4SW    					 
1999082000728	19990820	00728		1999	8	20	HEEA063336       	4	19990812	G	2211	4033089901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AUTO FLIGHT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	800Y					33134				FLIGHT DIRECTOR WILL NOT HOLD PITCH.						1	G	7	2 	4U				H4SW    					 
1999082000729	19990820	00729		1999	8	20	HEEA063337       	4	19990812	G	3140	MI5852013	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141PH					33197				INDICATOR GOES FROM WORKING MODE TO WAIT MODE THEN DROPS OFF-LINE.						1	G	7	2 	4U				H4SW    					 
1999082000730	19990820	00730	SW  	1999	8	20	HEEA063338       	1	19990812	G	6510	206040370105	SHAFT           			BELL  	206   	206L1       	1182107	SW  										T/R DRIVE	BEARING ROUGH   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5742N					45477				ROUGH BEARING.						1	G	7	1 	3U				H2SW    					 
1999082000731	19990820	00731	SW  	1999	8	20	HEEA063339       	1	19990812	G	6320	212040054105	CASE ASSY       			BELL  	212   	212         	1181420	SW  										M/R GEARBOX	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										CASE ASSEMBLY HAD CORROSION AROUND STUD HOLE, LOWER MAST LINER WORN, MOUNTING FACE CORROSION.						1	G	7	1 	4U				H4SW    					 
1999082000732	19990820	00732		1999	8	20	HEEA063340       	4	19990812	G	3425	71252	GYRO            			BELL  	412   	412         	1182202	SW  										HSI	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5759N					33002				GYRO FAILED.						1	G	7	2 	4U				H4SW    					 
1999082000733	19990820	00733		1999	8	20	HEEA063341       	4	19990812	G	2210	4025008918	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7128R					36007				YAW INDICATION ON AIRCRAFT IS REVERSED.						1	G	7	2 	4U				H4SW    					 
1999082000734	19990820	00734		1999	8	20	HEEA063342       	4	19990812	G	2210	4025008918	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	KICKS           	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6559Z					36019				KICK IN YAW CHANNEL.						1	G	7	2 	4U				H4SW    					 
1999082000735	19990820	00735		1999	8	20	HEEA063343       	4	19990812	G	3444	066104800	RADAR ALTIMETER 			BELL  	412   	412         	1182202	SW  										RT UNIT	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2261D					33076				ALTIMETER INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999082000736	19990820	00736	SW  	1999	8	20	HEEA063344       	1	19990812	G	7714	206070266009	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2124Z					45646				INDICATOR STICKING.						1	G	7	1 	3U				H2SW    					 
1999082000737	19990820	00737	SW  	1999	8	20	HEEA063345       	1	19990812	G	6240	206076373001	TACH GENERATOR  			BELL  	206   	206L1       	1182107	SW  										RPM WARNING	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TACHOMETER GENERATOR'S RPM WARNING LIGHT WILL FLICKER AT ROLLER.						1	G	7	1 	3U				H2SW    					 
1999082000738	19990820	00738		1999	8	20	HEEA063346       	4	19990812	G	2312	064105430	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										VHF COMM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				TRANSCEIVER HAD CONSTANT SQUELCH.						1	G	7	1 	3U				H2SW    					 
1999082000739	19990820	00739	SW  	1999	8	20	HEEA063347       	1	19990812	G	6240	206076373001	TACH GENERATOR  			BELL  	206   	206L1       	1182107	SW  										ROTOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TACHOMETER GENERATOR'S CAUTION HORN WILL NOT STOP.						1	G	7	1 	3U				H2SW    					 
1999082000740	19990820	00740	SW  	1999	8	20	HEEA063348       	1	19990812	G	6240	206076373001	TACH GENERATOR  			BELL  	206   	206L1       	1182107	SW  										ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TACHOMETER GENERATOR'S SPLINE GROOVES ARE WORN.						1	G	7	1 	3U				H2SW    					 
1999082000741	19990820	00741		1999	8	20	HEEA063349       	4	19990812	G	3100	206076373001	TACH GENERATOR  			BELL  	206   	206L1       	1182107	SW  										ROTOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5006F					45181				TACHOMETER GENERATOR'S ROTOR WARNING LIGHT FLICKERS AT LOW RPM.						1	G	7	1 	3U				H2SW    					 
1999082000742	19990820	00742	SW  	1999	8	20	HEEA063350       	1	19990812	G	2430	51539002N	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										GENERATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T					33112				DC GENERATOR WILL NOT COME ON-LINE.						1	G	7	2 	4U				H4SW    					 
1999082000743	19990820	00743	SW  	1999	8	20	HEEA063351       	1	19990812	G	6240	412075010109	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				READING 2 PERCENT LOWER THAN PILOT'S TACHOMETER.						1	G	7	2 	4U				H4SW    					 
1999082000744	19990820	00744	SW  	1999	8	20	HEEA063352       	1	19990812	G	7712	206075185101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	10814					45415				TORQUEMETER HAD CRACKED GLASS AND FADED RED LINE.						1	G	7	1 	3U				H2SW    					 
1999082000745	19990820	00745	SW  	1999	8	20	HEEA063353       	1	19990812	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP COMP	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										CORROSION/STROKE ADJ. SCREW BROKEN. S						1	G	7	1 	3U				H2SW    					 
1999082000746	19990820	00746	SW  	1999	8	20	HEEA063354       	1	19990812	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONTROL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S					33022				VM PEGGED OUT, THEN DIED.						1	G	7	2 	4U				H4SW    					 
1999082000747	19990820	00747	SW  	1999	8	20	HEEA063355       	1	19990812	G	6710	206062721109	ACTUATOR        			BELL  	206   	206L1       	1182107	SW  										DROOP COMP	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ACTUATOR INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999082000748	19990820	00748	SW  	1999	8	20	HEEA063356       	1	19990812	G	2425	209070263003	INDICATOR       			BELL  	412   	412         	1182202	SW  										DUAL VOLT	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	107X					33113				D.C. NEEDLE IS STUCK.						1	G	7	2 	4U				H4SW    					 
1999082000749	19990820	00749	SW  	1999	8	20	HEEA063357       	1	19990813	G	7714	206070266009	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	CONTAMINATED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										INDICATOR HAD GLASS DIRTY INSIDE, INSTALLATION LIGHT CRACKED.						1	G	7	1 	3U				H2SW    					 
1999082000750	19990820	00750	SW  	1999	8	20	HEEA063358       	1	19990813	G	7712	412075008111	INDICATOR       			BELL  	412   	412         	1182202	SW  										DUAL TORQUE	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893S					33022				TORQUE INDICATOR'S LIGHTS INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999082000751	19990820	00751		1999	8	20	HEEA063359       	4	19990813	G	3420	1113025	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT HSI	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893P					33012				VOR/GPS FLAG INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999082000752	19990820	00752	SW  	1999	8	20	HEEA063360       	1	19990813	G	6240	412075010111	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008					36004				TRIPLE TACHOMETER INDICATOR HAD INACCURATE READINGS.						1	G	7	2 	4U				H4SW    					 
1999082000753	19990820	00753		1999	8	20	HEEA063361       	4	19990813	G	2312	7001840913	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	ERRATIC         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3911L					33023				RECEIVER/TRANSMITTER HAD ERRATIC INDICATION.						1	G	7	2 	4U				H4SW    					 
1999082000754	19990820	00754		1999	8	20	HEEA063362       	4	19990813	G	2312	7001840913	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3911L					33023				RECEIVER/TRANSMITTER INTERMITTENT.						1	G	7	2 	4U				H4SW    					 
1999082000755	19990820	00755		1999	8	20	HEEA063363       	4	19990813	G	3420	1113025	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT HSI	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893P					33012				YELLOW NEEDLE OFF FLAG WILL NOT PULL.						1	G	7	2 	4U				H4SW    					 
1999082000756	19990820	00756		1999	8	20	HEEA063364       	4	19990813	G	2210	7000298901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	7128R					36007				TRIPS NR 1 AFCS CIRCUIT BREAKER.						1	G	7	2 	4U				H4SW    					 
1999082000757	19990820	00757		1999	8	20	HEEA063365       	4	19990813	G	3453	4530103	RECEIVER        			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2253E					45758				LORAN LOCKED UP ON WAY POINT MODE.						1	G	7	1 	3U				H2SW    					 
1999082000758	19990820	00758	SW  	1999	8	20	HEEA063366       	1	19990813	G	7722	212070116007	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2148K					36001				OIL INDICATOR INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999082000759	19990820	00759	SW  	1999	8	20	HEEA063367       	1	19990813	G	6240	39433339002	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008					36004				TRIPLE TACHOMETER'S ROTOR NEEDLE READS HIGH.						1	G	7	2 	4U				H4SW    					 
1999082000760	19990820	00760	SW  	1999	8	20	HEEA063368       	1	19990813	G	2437	214175255103	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										INDICATOR PEGS OUT DURING OPERATION OF AIRCRAFT.   IT ALSO FLUCTUATES.						2	G	7	2 	4U				H10SW   					 
1999082000761	19990820	00761	SW  	1999	8	20	HEEA063369       	1	19990813	G	6240	39433339002	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22347					36005				TRIPLE TACHOMETER READS 2 PERCENT LOWER THAN PILOT'S.						1	G	7	2 	4U				H4SW    					 
1999082000762	19990820	00762	SW  	1999	8	20	HEEA063370       	1	19990813	G	7714	206070266009	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1076Y					45380				INDICATOR STICKS DURING STARTING, GLASS FOGGED IN-FLIGHT.						1	G	7	1 	3U				H2SW    					 
1999082000763	19990820	00763	SW  	1999	8	20	HEEA063371       	1	19990813	G	7714	206070266009	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3905B					45598				INDICATOR NEEDLE STICKING.						1	G	7	1 	3U				H2SW    					 
1999082000764	19990820	00764	SW  	1999	8	20	HEEA063372       	1	19990813	G	6240	212070108007	INDICATOR       			BELL  	212   	212         	1181420	SW  										TRIPLE TACH	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1082G					31109				ROTOR PORTION OF TACHOMETER INOPERATIVE.						1	G	7	1 	4U				H4SW    					 
1999082000765	19990820	00765	SW  	1999	8	20	HEEA063373       	1	19990813	G	6240	412075010111	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893P					33012				TRIPLE TACHOMETER INDICATOR'S NR 1 NEEDLE READS 30 PERCENT LOW AT FULL THROTTLE.						1	G	7	2 	4U				H4SW    					 
1999082000766	19990820	00766		1999	8	20	HEEA063374       	4	19990813	G	2210	7000298901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893P					33012				BOTH SAS AND ATT LIGHTS COME ON TOGETHER INTERMITTENTLY.						1	G	7	2 	4U				H4SW    					 
1999082000767	19990820	00767		1999	8	20	HEEA063375       	1	19990813	G	2840	473203003	SIGNAL COND     																	FUEL SYSTEM	MALFUNCITONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										LOW FUEL LIGHT COMES ON WITH FULL FUEL IN-FLIGHT.																			 
1999082000768	19990820	00768		1999	8	20	HEEA063376       	4	19990813	G	2312	7001840913	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	FLUCTUATES      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	33008					36004				RECEIVER/TRANSMITTER FLUCTUATES IN-FLIGHT.						1	G	7	2 	4U				H4SW    					 
1999082000769	19990820	00769	SW  	1999	8	20	HEEA063377       	1	19990813	G	7722	3030083A	TRIM COMPENSATOR			BELL  	212   	212         	1181420	SW  										ENGINE TIT	OUT OF ADJUST   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5736J					31140				TRIM COMPENSATOR OUT OF ADJUSTMENT.  (INCREASE).						1	G	7	1 	4U				H4SW    					 
1999082000770	19990820	00770	SW  	1999	8	20	HEEA063378       	1	19990813	G	7714	206070266009	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3905B					45598				INDICATOR STICKING BELOW 10 PERCENT.						1	G	7	1 	3U				H2SW    					 
1999082000771	19990820	00771	SW  	1999	8	20	HEEA063379       	1	19990813	G	6240	412075010111	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008					36004				TRIPLE TACHOMETER INDICATOR'S NR 1 NEEDLE INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999082000772	19990820	00772		1999	8	20	HEEA063380       	4	19990813	G	3457	0845000000	GPS             			BELL  	212   	212         	1181420	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3131S					30953				WHEN THE SMALL KNOB IS TOUCHED TO MOVE THE CURSOR, THE CURSOR STARTS MOVING ALL OVER THE SCREEN; HAVE TO WAIT FOR IT TO 	STOP MOVING BEFORE ADJUSTMENT CAN BE MADE.					1	G	7	1 	4U				H4SW    					 
1999082000773	19990820	00773		1999	8	20	HEEA063381       	4	19990813	G	2210	7000298901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	108X					33115				BEEP TRIM GOES FULL TRAVEL WITH SMALL INPUT.						1	G	7	2 	4U				H4SW    					 
1999082000774	19990820	00774	SW  	1999	8	20	HEEA063382       	1	19990813	G	6420	205012710001	BEARING         		212011701003	BELL  	412   	412         	1182202	SW  										T/R BLADE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911AR				A714	33111				TAIL ROTOR BEARINGS WORN, TWO EACH RACES AND BEARINGS BRINELLED.						1	G	7	2 	4U				H4SW    					 
1999082000775	19990820	00775	SW  	1999	8	20	HEEA063383       	1	19990813	G	6220	412010424103	BEARING         		412010405107	BELL  	412   	412         	1182202	SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911FD	1956 			A323	33056				BEARINGS WORN.						1	G	7	2 	4U				H4SW    					 
1999082000776	19990820	00776	SW  	1999	8	20	HEEA063384       	1	19990813	G	6220	412010424103	BEARING         		412010405109	BELL  	412   	412         	1182202	SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911FD	1070 			A658	33056				BEARINGS WORN.						1	G	7	2 	4U				H4SW    					 
1999082000777	19990820	00777	SW  	1999	8	20	HEEA063385       	1	19990813	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										ROTARY	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893N					33010				ROTARY ACTUATOR FREQUENTLY DOES NOT RELEASE.						1	G	7	2 	4U				H4SW    					 
1999082000778	19990820	00778		1999	8	20	HEEA063386       	4	19990813	G	3420	1113025	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT HSI	RATCHETS        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	33008					36004				RATCHETS IN A TURN IS NOT SMOOTH.						1	G	7	2 	4U				H4SW    					 
1999082000779	19990820	00779	SW  	1999	8	20	HEEA063387       	1	19990813	G	7714	206075682107	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										GAS PRODUCER	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251V					51404				GUAGE INDICATOR LIGHT IS OUT.						1	G	7	1 	3U				H2SW    					 
1999082000780	19990820	00780		1999	8	20	HEEA063388       	4	19990813	G	2200	4020936903	GYRO            			BELL  	412   	412         	1182202	SW  										TARSYN	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	293CA					33005				FLAG CIRCUIT NOT PULLING HSI.						1	G	7	2 	4U				H4SW    					 
1999082000781	19990820	00781	SW  	1999	8	20	HEEA063389       	1	19990813	G	7931	206075187003	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										ENGINE OIL	DETERIORATED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4180F					51469				CASE SEAL DETERIORATED.						1	G	7	1 	3U				H2SW    					 
1999082000782	19990820	00782	SW  	1999	8	20	HEEA063390       	1	19990813	G	6240	412075010109	INDICATOR       			BELL  	212   	212         	1181420	SW  										TRIPLE TACH	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1082G					31109				TRIPLE TACHOMETER INDICATOR READS 3 PERCENT LOW.						1	G	7	1 	4U				H4SW    					 
1999082000783	19990820	00783	SW  	1999	8	20	HEEA063391       	1	19990813	G	6240	412075010109	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				COPILOT'S TRIPLE TACHOMETER READS 5 PERCENT HIGHER THAN PILOT'S ON ROTOR NEEDLE. S						1	G	7	2 	4U				H4SW    					 
1999082000784	19990820	00784	SW  	1999	8	20	HEEA063392       	1	19990813	G	7712	206075185101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5019F					45244				NEEDLE STICKS, GLASS FOGGY AND CRACKED.						1	G	7	1 	3U				H2SW    					 
1999082000785	19990820	00785	SW  	1999	8	20	HEEA063393       	1	19990813	G	7712	206075739103	TORQUEMETER     			BELL  	206   	206L3       	1182108	SW  										ENGINE	FRICTION ERROR  	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251Y					51556				TORQUEMETER HAS EXCESSIVE FRICTION ERROR, GLASS FOGGY AND NEEDLE STICKS.						1	G	7	1 	3U				H2SW    					 
1999082000786	19990820	00786	SW  	1999	8	20	HEEA063394       	1	19990813	G	2430	51539002N	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										GENERATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T					33112				CONTROL UNIT WILL NOT LET GENERATOR COME ON-LINE.						1	G	7	2 	4U				H4SW    					 
1999082000787	19990820	00787		1999	8	20	HEEA063395       	4	19990813	G	3452	071119218	DISPLAY         			BELL  	214   	214ST       	1182106	SW  										XPONDER CONTROL	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6957Y					28139				BAD PHOTO CELL WILL NOT GO BRIGHT.						2	G	7	2 	4U				H10SW   					 
1999082000788	19990820	00788		1999	8	20	HEEA063396       	4	19990813	G	2200	2593996333	TARSYN 333      			BELL  	412   	412         	1182202	SW  										PITCH	PRECESSES       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z					33077				RMI AND HSI PRECESSING.						1	G	7	2 	4U				H4SW    					 
1999082000789	19990820	00789	SW  	1999	8	20	HEEA063397       	1	19990813	G	7714	214175249101	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				INDICATOR WILL NOT SPIN UP.						2	G	7	2 	4U				H10SW   					 
1999082000790	19990820	00790	SW  	1999	8	20	HEEA063398       	1	19990813	G	6240	412075010109	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				TRIPLE TACHOMETER INDICATOR'S NR 2 NEEDLE STUCK.						1	G	7	2 	4U				H4SW    					 
1999082000791	19990820	00791	EU  	1999	8	20	HEEA063399       	1	19990729	G	6220	350A31185421	SCREW           			SNIAS 	350   	AS350B2     	8680813	EU  										M/R HEAD	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	40466					3004				SCREW WORN.  REPLACED WITH SERVICEABLE BOLTS.						1	G	7	1 	3U				H9EU    					 
1999082000792	19990820	00792	EU  	1999	8	20	HEEA063400       	1	19990729	G	6220	350A31187320	SCREW           			SNIAS 	350   	AS350B2     	8680813	EU  										M/R HEAD	CORRODED        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	40466					3004				CORROSION ON RED BLADE UPPER PC LINK ATTACH BOLT.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U				H9EU    					 
1999082000793	19990820	00793	EU  	1999	8	20	HEEA063401       	1	19990729	G	6220	350A37124420	SCREW           			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	CORRODED        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	40466					3004				CORROSION ON M/R HUB SCREW.  REPLACED WITH SERVICEABLE PARTS.						1	G	7	1 	3U				H9EU    					 
1999082000794	19990820	00794	EU  	1999	8	20	HEEA063402       	1	19990729	G	6230	350A37114820	PITCH LINK      			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	CORRODED        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6097Z					2820				P/C LINK CORRODED BEYOND LIMITS.  REPLACED WITH SERVICEABLE PARTS.						1	G	7	1 	3U				H9EU    					 
1999082000795	19990820	00795	EU  	1999	8	20	HEEA063403       	1	19990729	G	3241	350A4110161063	PAD             			SNIAS 	350   	AS350B2     	8680813	EU  										BRAKE	CORRODED        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6100R					2862				PAD CORRODED BEYOND LIMITS.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U				H9EU    					 
1999082000796	19990820	00796	EU  	1999	8	20	HEEA063404       	1	19990729	G	3241	350A4110161063	PAD             			SNIAS 	350   	AS350B2     	8680813	EU  										BRAKE	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6097Z					2820				PAD CRACKED AND CORRODED.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U				H9EU    					 
1999082000797	19990820	00797	EU  	1999	8	20	HEEA063405       	1	19990729	G	3241	350A4110161163	PAD             			SNIAS 	350   	AS350B2     	8680813	EU  										BRAKE	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6097Z					2820				PAD CRACKED AND CORRODED.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U				H9EU    					 
1999082000798	19990820	00798	EU  	1999	8	20	HEEA063406       	1	19990729	G	3241	350A4110161163	PAD             			SNIAS 	350   	AS350B2     	8680813	EU  										BRAKE	CORRODED        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6100R					2862				RIGHT PAD ASSEMBLY HAD CORROSION BEYOND LIMITS.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U				H9EU    					 
1999082000799	19990820	00799	EU  	1999	8	20	HEEA063407       	1	19990729	G	7110	350A58164301	BRACE           			SNIAS 	350   	AS350B2     	8680813	EU  										COWL	BENT            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	40466					3004				ENGINE COWLING BRACE BENT.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U				H9EU    					 
1999082000800	19990820	00800	EU  	1999	8	20	HEEA063408       	1	19990729	G	6220	704A33633151	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	40466					3004				MAIN ROTOR BEARING WORN BEYOND LIMITS.  REPLACED WITH SERVICEABLE PARTS.						1	G	7	1 	3U				H9EU    					 
1999082000801	19990820	00801	EU  	1999	8	20	HEEA063409       	1	19990729	G	6220	704A33633153	MEMBER          			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR HEAD	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	40466					3004				STOP LAMINATES WORN BEYOND LIMITS.						1	G	7	1 	3U				H9EU    					 
1999082000802	19990820	00802	NE  	1999	8	20	HEEA063410       	2	19990729	G	7421	9550166670	IGNITER PLUG    			SNIAS 	350   	AS350B2     	8680813	EU  	TMECA 	ARRIEL	ARRIEL1D    		NE  					ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				IGNITER SHOWS WEAR, BURNED, AND SIGNS OF ARCING.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U	3	U		H9EU    	E19EU				 
1999082000803	19990820	00803	NE  	1999	8	20	HEEA063411       	2	19990729	G	7421	9550168770	IGNITER         			SNIAS 	350   	AS350B2     	8680813	EU  	TMECA 	ARRIEL	ARRIEL1D    		NE  					ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				TIP OF IGNITER WORN.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U	3	U		H9EU    	E19EU				 
1999082000804	19990820	00804	EU  	1999	8	20	HEEA063412       	1	19990729	G	2460	9550168600	HARNESS         			SNIAS 	350   	AS350B2     	8680813	EU  										DC SYSTEM	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				CABLE HAS SIGNS OF ARCING.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U				H9EU    					 
1999082000805	19990820	00805	EU  	1999	8	20	HEEA063413       	1	19990729	G	6730	SC5084	SERVO           			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z	145  				2820				SERVO LEAKING.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U				H9EU    					 
1999082000806	19990820	00806	EU  	1999	8	20	HEEA063414       	1	19990729	G	7120	TL100AXE10LL50	FASTENER        			SNIAS 	350   	AS350B2     	8680813	EU  										ENGINE MOUNT	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				RIGHT FORWARD LATCH BROKEN.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U				H9EU    					 
1999082000807	19990820	00807	EU  	1999	8	20	HEEA063415       	1	19990729	G	7120	TL100AXE10LL50	FASTENER        			SNIAS 	350   	AS350B2     	8680813	EU  										ENGINE MOUNT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				FASTENER WORN.  REPLACED WITH SERVICEABLE PART.						1	G	7	1 	3U				H9EU    					 
1999082000808	19990820	00808		1999	8	20	HEEA063416       	4	19990729	G	3452	066106200	TRANSPONDER     			BOLKMS	105   	BO105S      	5626006	EU  										ATC PANEL	FAILED TEST     	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	7136H					S833				TRANSCEIVER FAILS ALL TESTS.  REPLACED 2 EACH BACKLIGHTING BULBS.  ALIGNED RECEIVER AND ADJUSTED FREQUENCY AND POWER OUT	.  BENCH CHECK GOOD.					1	G	7	2 	3U				H3EU    					 
1999082000809	19990820	00809	EU  	1999	8	20	HEEA063417       	1	19990729	G	6520	4619211901	HOUSING         		4619003003  	BOLKMS	105   	BO105S      	5626006	EU  										T/R GEARBOX	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5031U	1261 			1325	S678				HOUSING CRACKED AT MOUNTING EAR.  REPLACED WITH SERVICEABLE PART.						1	G	7	2 	3U				H3EU    					 
1999082000810	19990820	00810	EU  	1999	8	20	HEEA063418       	1	19990729	G	2435	23032048	STARTER         			BOLKMS	105   	BO105S      	5626006	EU  										STARTER/GEN	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	50293	6979 				S677				UNABLE TO OBTAIN STARTING RPM. SENT TO CORPORATE SERVICE SUPPLY, INC. FOR OVERHAUL.						1	G	7	2 	3U				H3EU    					 
1999082000811	19990820	00811	EU  	1999	8	20	HEEA063419       	1	19990729	G	2435	23032048	STARTER         			BOLKMS	105   	BO105S      	5626006	EU  										STARTER/GEN	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721MB					S752				STARTER/GENERATOR WOULD NOT START OR COME ON-LINE.  START OPPOSITE ENGINE THEN IT WOULD WORK AND COME ON LINE AT 100 PER	CENT ONLY.					1	G	7	2 	3U				H3EU    					 
1999082000812	19990820	00812	EU  	1999	8	20	HEEA063420       	1	19990729	G	2822	D105102	BOOST PUMP      			BOLKMS	105   	BO105S      	5626006	EU  										FUEL SYSTEM	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3071K					S859				FUEL POOST PUMP LEAKING FROM SEAL DRAIN.						1	G	7	2 	3U				H3EU    					 
1999082000813	19990820	00813	EU  	1999	8	20	HEEA063421       	1	19990729	G	2822	D107318E	PUMP            			BOLKMS	105   	BO105S      	5626006	EU  										FUEL BOOST	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	137AE	3313 				S851				FUEL PUMP HAD ERRATIC FUNCTION.						1	G	7	2 	3U				H3EU    					 
1999082000814	19990820	00814	EU  	1999	8	20	HEEA063422       	1	19990729	G	2822	D107318E	PUMP            			BOLKMS	105   	BO105S      	5626006	EU  										FUEL BOOST	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	135AE	3523 				S838				MOTOR FLANGE SEEP/STATIC LEAK.						1	G	7	2 	3U				H3EU    					 
1999082000815	19990820	00815	EU  	1999	8	20	HEEA063423       	1	19990729	G	6410	10531980	BLADE           			BOLKMS	105   	BO105S      	5626006	EU  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81832	1163 				S828				RUBBER COATING ON TAIL ROTOR BLADE CHIPPED OFF AT BLADE TIPS.						1	G	7	2 	3U				H3EU    					 
1999082000816	19990820	00816	EU  	1999	8	20	HEEA063424       	1	19990729	G	6410	10531980	BLADE           			BOLKMS	105   	BO105S      	5626006	EU  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81832	1163 				S828				RUBBER COATING ON TAIL ROTOR BLADE CHIPPED OFF AT BLADE TIPS.						1	G	7	2 	3U				H3EU    					 
1999082000817	19990820	00817	EU  	1999	8	20	HEEA063425       	1	19990802	G	7712	305731365	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										ENGINE TORQUE	READS HIGH      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6095S					2777				TORQUE INDICATOR READS HIGH.						1	G	7	1 	3U				H9EU    					 
1999082000818	19990820	00818	EU  	1999	8	20	HEEA063426       	1	19990806	G	2435	23032048	STARTER         			BOLKMS	105   	BO105S      	5626006	EU  										STARTER/GEN	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4302G	15521				S853				STARTER/GENERATOR WILL NOT START ENGINE.						1	G	7	2 	3U				H3EU    					 
1999082000819	19990820	00819	EU  	1999	8	20	HEEA063427       	1	19990806	G	7722	TM42739	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										TOT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	86CH					S557				GAUGE READS NEGATIVE WHEN AIRCRAFT RUNNING.						1	G	7	2 	3U				H3EU    					 
1999082000820	19990820	00820	EU  	1999	8	20	HEEA063428       	1	19990806	G	6240	2202A1002	WARNING BOX     			BOLKMS	105   	BO105S      	5626006	EU  										RPM WARNING	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911EB					S812				RPM WARNING BOX MALFUNCTION CAUSES RPM LIGHT TO CONTINUOUSLY BLINK.						1	G	7	2 	3U				H3EU    					 
1999082000821	19990820	00821	EU  	1999	8	20	HEEA063429       	1	19990806	G	6240	2202A1002	WARNING BOX     			BOLKMS	105   	BO105S      	5626006	EU  										RPM WARNING	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81832					S828				RPM WARNING HORN WILL NOT GO OUT WHEN AT FULL RPM.						1	G	7	2 	3U				H3EU    					 
1999082000822	19990820	00822	EU  	1999	8	20	HEEA063430       	1	19990806	G	6240	2202A1002	WARNING BOX     			BOLKMS	105   	BO105S      	5626006	EU  										RPM WARNING	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81982					S818				RPM LIGHT AND HORN COME ON WHEN VHF IS KEYED.						1	G	7	2 	3U				H3EU    					 
1999082000823	19990820	00823	EU  	1999	8	20	HEEA063431       	1	19990809	G	2430	51565000R	VOLT REGULATOR  			BOLKMS	105   	BO105S      	5626006	EU  										DC SYSTEM	OUT OF ADJUST   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4302G					S853				UNABLE TO ADJUST VOLTAGE.						1	G	7	2 	3U				H3EU    					 
1999082000824	19990820	00824	EU  	1999	8	20	HEEA063432       	1	19990809	G	2436	51530001EI	REGULATOR       			BOLKMS	117   	BK117A4     	5626017	EU  										DC SYSTEM	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911RZ					7092				VOLTAGE REGULATOR WOULD NOT SHARE LOAD.						1	G	7	2 	3U				H13EU   					 
1999082000825	19990820	00825	EU  	1999	8	20	HEEA063433       	1	19990809	G	7714	KDW021	WARNING BOX     			BOLKMS	105   	BO105S      	5626006	EU  										ROTOR RPM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	721MB					S752				RPM WILL NOT CANCEL, STAYS ON ALL THE TIME.						1	G	7	2 	3U				H3EU    					 
1999082000826	19990820	00826		1999	8	20	HEEA063434       	4	19990809	G	3120	JB15307	CLOCK           			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	DAMAGED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	8199J					S826				CLOCK HARD TO WIND.						1	G	7	2 	3U				H3EU    					 
1999082000827	19990820	00827	EU  	1999	8	20	HEEA063435       	1	19990809	G	7714	DL41239	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	818SH					S753				VERY LITTLE NEEDLE RESPONSE AT LOW RPM.						1	G	7	2 	3U				H3EU    					 
1999082000828	19990820	00828		1999	8	20	HEEA063436       	4	19990809	G	3421	40205773	GYRO            			BOLKMS	117   	BK117B1     	5626012	EU  										COCKPIT	PRECESSES       	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911TL					7198				DIRECTIONAL GYRO PRECESSING.						1	G	7	2 	3U				H13EU   					 
1999082000829	19990820	00829		1999	8	20	HEEA063437       	4	19990809	G	3424	5090004910	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										TURN AND BANK	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5421E					S806				TURN AND SLIP INDICATOR INOPERATIVE.						1	G	7	2 	3U				H3EU    					 
1999082000830	19990820	00830	EU  	1999	8	20	HEEA063438       	1	19990809	G	7714	DL41239	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	READS HIGH      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	133AE					S800				CANNON PLUG BROKEN.  SMALL NEEDLE READS 5 PERCENT HIGHER THAN BIG NEEDLE.						1	G	7	2 	3U				H3EU    					 
1999082000831	19990820	00831	EU  	1999	8	20	HEEA063439       	1	19990809	G	2430	51565000R	VOLT REGULATOR  			BOLKMS	105   	BO105CBS    	5626008	EU  										DC SYSTEM	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911RS					S670				GENERATOR WENT OFF-LINE.  VOLTAGE CANNOT BE ADJUSTED BELOW 33.1 VOLTS.						1	G	7	2 	3U			NC	H3EU    					 
1999082000832	19990820	00832		1999	8	20	HEEA063440       	4	19990809	G	3421	40205773	GYRO            			BOLKMS	117   	BK117B1     	5626012	EU  										COCKPIT	INACCURATE      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911TL					7198				DIRECTIONAL GYRO READING 30 - 60 DEGREES OFF.						1	G	7	2 	3U				H13EU   					 
1999082000833	19990820	00833		1999	8	20	HEEA063441       	4	19990809	G	3457	0110005400	BATTERY         			BOLKMS	105   	BO105S      	5626006	EU  										GPS	DISCHARGED      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	133AE					S800				BATTERY LOW.  FOUND BATTERY DEAD AND ENT BUTTON UNREADABLE.						1	G	7	2 	3U				H3EU    					 
1999082000834	19990820	00834	EU  	1999	8	20	HEEA063442       	1	19990809	G	7714	DL43638	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	READS HIGH      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	8199J					S826				RPM INDICATOR'S NR 1 NEEDLE 3 PERCENT HIGHER THAN THE OTHER TWO THROUGHOUT RANGE ALL THE TIME.						1	G	7	2 	3U				H3EU    					 
1999082000835	19990820	00835		1999	8	20	HEEA063443       	4	19990809	G	2312	069102525	TRANSCEIVER     			SNIAS 	350   	AS350B2     	8680813	EU  										COMMUNICATIONS	WEAK            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	350BZ					2653				WEAK TRANSMIT.						1	G	7	1 	3U				H9EU    					 
1999082000836	19990820	00836	EU  	1999	8	20	HEEA063444       	1	19990809	G	6700	10545028	HYD PACK        			BOLKMS	105   	BO105S      	5626006	EU  										FLIGHT CONTROL	FAILED          	E			HEEA	A				UNSCHED LANDING         				J			WARNING INDICATION        			CR	CRUISE         	1			SW	03	8197X	5569 				S808				DURING CRUISE FLIGHT, NOSE TUCKED 15 DEGREES- COULD NOT RECOVER WITH CYCLIC UNTIL RECOVERED BY ITSELF.  RPM AND HYD BLOC	K LIGHTS FLASHED.					1	G	7	2 	3U				H3EU    					 
1999082000837	19990820	00837		1999	8	20	HEEA063445       	4	19990809	G	2312	064105430	TRANSCEIVER     			SNIAS 	350   	AS350B2     	8680813	EU  										VHF COMM	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6097Z					2820				TRANSCEIVER WILL NOT TRANSMIT.						1	G	7	1 	3U				H9EU    					 
1999082000838	19990820	00838		1999	8	20	HEEA063446       	4	19990809	G	2312	40001452502	TRANSCEIVER     			BOLKMS	117   	BK117B2     	5626013	EU  										COCKPIT VHF	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	136AE					7234				UNSERVICEABLE.  PERFORMED PRELIMINARY INSPECTIONS AND CLEANED CORROSION FROM UNIT.   FOUND GUARD RECEIVER WEAK.  ALIGNED	 GUARD RECEIVER.  FOUND MAIN RECEIVER AND TRANSMITTER NOT TRANSMITTING AND RECEIVING OVER 150 MHZ.					1	G	7	2 	3U			NC	H13EU   					 
1999082000839	19990820	00839	EU  	1999	8	20	HEEA063447       	1	19990809	G	7714	KDW021	WARNING BOX     			BOLKMS	105   	BO105S      	5626006	EU  										ROTOR RPM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911DD					S830				RPM WARNING LIGHT COMES ON DURING FLIGHT.						1	G	7	2 	3U				H3EU    					 
1999082000840	19990820	00840		1999	8	20	HEEA063448       	4	19990810	G	2312	069102505	TRANSCEIVER     			SNIAS 	350   	AS350B2     	8680813	EU  										COMMUNICATIONS	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4000L					2873				VOR INTERMITTENTLY INOPERATIVE.  PERFORMED PRELIMINARY INSPECTION.  FOUND VOR BEARING ERRORS AND WOULD INTERMITTENTLY LO	SE VOR SIGNAL.					1	G	7	1 	3U				H9EU    					 
1999082000841	19990820	00841	EU  	1999	8	20	HEEA063449       	1	19990810	G	6210	10515141	BLADE           			BOLKMS	105   	BO105S      	5626006	EU  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911BR	9263 				S719				THE NR 1 INBOARD ABRASION STRIP HAS SEPARATION ON THE OUTBOARD END OF THE STRIP.						1	G	7	2 	3U				H3EU    					 
1999082000842	19990820	00842	EU  	1999	8	20	HEEA063450       	1	19990810	G	6210	10515141	BLADE           			BOLKMS	105   	BO105S      	5626006	EU  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911PF	3256 				S718				EROSION HOLE THROUGH THE OUTBOARD ABRASION STRIP ON MAIN ROTOR BLADE.						1	G	7	2 	3U				H3EU    					 
1999082000843	19990820	00843	EU  	1999	8	20	HEEA063451       	1	19990810	G	6210	10515150	BLADE           			BOLKMS	117   	BK117A4     	5626017	EU  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RZ	3909 				7092				ROTOR BLADE HAD SEPARATION ON THE INBOARD ABRASION STRIP ON THE OUTER END.  THE ABRASION STRIP AT THE TIP HAD EROSION HO	LES.					1	G	7	2 	3U				H13EU   					 
1999082000844	19990820	00844	EU  	1999	8	20	HEEA063452       	1	19990810	G	6210	10515150	BLADE           			BOLKMS	105   	BO105CBS    	5626008	EU  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RS	3909 				S670				INBOARD ABRASION STRIP HAD SEPARATION ON THE OUTBOARD END OF THE STRIP.						1	G	7	2 	3U			NC	H3EU    					 
1999082000845	19990820	00845	EU  	1999	8	20	HEEA063453       	1	19990810	G	6220	116488P	BEARING         			BOLKMS	105   	BO105S      	5626006	EU  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4302G					S853				BEARING UNSTAKED.  REPLACED WITH SERVICEABLE PART.						1	G	7	2 	3U				H3EU    					 
1999082000846	19990820	00846		1999	8	20	HEEA063454       	4	19990810	G	3457	13824120234	GPS RECEIVER    			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7136H					S833				ADJUSTER KNOB ON FRONT SKIPS WHEN DIALING BY PILOT.						1	G	7	2 	3U				H3EU    					 
1999082000847	19990820	00847	EU  	1999	8	20	HEEA063455       	1	19990810	G	2844	BSE206150G3	TRANSDUCER      			BOLKMS	105   	BO105S      	5626006	EU  										FUEL SYSTEM	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	135AE					S838				TRANSDUCER INOPERATIVE.						1	G	7	2 	3U				H3EU    					 
1999082000848	19990820	00848	EU  	1999	8	20	HEEA063456       	1	19990812	G	3310	1179203903	BATTERY         			BOLKMS	117   	BK117B2     	5626013	EU  										LIGHTS	DISCHARGED      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911LK					7168				BATTERY POWER LOW.						1	G	7	2 	3U			NC	H13EU   					 
1999082000849	19990820	00849		1999	8	20	HEEA063457       	4	19990812	G	2312	069102505	TRANSCEIVER     			BOLKMS	105   	BO105S      	5626006	EU  										COMMUNICATIONS	DAMAGED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	133AE					S800				LED LIGHTS ARE HARD TO READ.						1	G	7	2 	3U				H3EU    					 
1999082000850	19990820	00850	EU  	1999	8	20	HEEA063458       	1	19990812	G	2150	20475591	TURBINE         			BOLKMS	105   	BO105S      	5626006	EU  										ECU	SEIZED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724MB					S756				TURBINE SEIZED.						1	G	7	2 	3U				H3EU    					 
1999082000851	19990820	00851	EU  	1999	8	20	HEEA063459       	1	19990812	G	2840	BSE20660G1	TRANSMITTER     			BOLKMS	105   	BO105S      	5626006	EU  										FUEL PRESSURE	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	133AE					S800				FUEL PRESSURE GAUGE READS ERRATIC.						1	G	7	2 	3U				H3EU    					 
1999082000852	19990820	00852	EU  	1999	8	20	HEEA063460       	1	19990812	G	2422	SS120	STATIC INVERTER 			BOLKMS	117   	BK117B1     	5626012	EU  										AC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	217UC					7152				INVERTER NOT WORKING WITH AIRCRAFT POWER.						1	G	7	2 	3U				H13EU   					 
1999082000853	19990820	00853	EU  	1999	8	20	HEEA063461       	1	19990812	G	3310	1179203103	CONTROL UNIT    			BOLKMS	117   	BK117B1     	5626012	EU  										LIGHTS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	217UC					7152				CENTER PANEL INSTRUMENT LIGHTS INOPERATIVE.						1	G	7	2 	3U				H13EU   					 
1999082000854	19990820	00854		1999	8	20	HEEA063462       	4	19990812	G	3421	4021541671	HORIZON         			BOLKMS	117   	BK117B2     	5626013	EU  										COCKPIT	FOGGED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	134AE					7237				ARTIFICIAL HORIZON HAS FOGGED GLASS.						1	G	7	2 	3U			NC	H13EU   					 
1999082000855	19990820	00855		1999	8	20	HEEA063463       	4	19990812	G	2312	4000106010	CONTROL UNIT    			BOLKMS	105   	BO105S      	5626006	EU  										COMMUNICATIONS	WEAK            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	137AE					S851				AUDIO WEAK.						1	G	7	2 	3U				H3EU    					 
1999082000856	19990820	00856	EU  	1999	8	20	HEEA063464       	1	19990812	G	7933	TM41039	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										TRIPLE OIL TEMP	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5031U					S678				NR 2 TEMP FLUCTUATES.						1	G	7	2 	3U				H3EU    					 
1999082000857	19990820	00857	EU  	1999	8	20	HEEA063465       	1	19990812	G	7714	DL40440	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										TRIPLE TACH	LAGGING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8199J					S826				TRIPLE RPM INDICATOR'S NR 1 NEEDLE LAGGING.						1	G	7	2 	3U				H3EU    					 
1999082000858	19990820	00858	EU  	1999	8	20	HEEA063466       	1	19990812	G	7712	DK50445	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										TORQUE	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	137AE					S851				TORQUE INDICATOR'S NR 2 NEEDLE STICKS AT 35-40 PERCENT WHEN IT SHOULD INDICATE 15-20 PERCENT.						1	G	7	2 	3U				H3EU    					 
1999082000859	19990820	00859		1999	8	20	HEEA063467       	4	19990813	G	3425	066304605	HSI CONTROL     			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	ERRATIC         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	137AE					S851				HSI CONTROL HAD ERRATIC ACTION.  NEW HEADING RESULTS IN INDICATOR ROTATING.  TIME SINCE REPAIR 80:15 HOURS.						1	G	7	2 	3U				H3EU    					 
1999082000860	19990820	00860		1999	8	20	HEEA063468       	4	19990813	G	3425	066304605	HSI CONTROL     			BOLKMS	105   	BO105CBS    	5626008	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911RS					S670				READING FLAG NOT STICKING TO THE CARD.						1	G	7	2 	3U			NC	H3EU    					 
1999091500003	19990915	00003	EU  	1999	9	15	HEEA063469       	1	19990813	G	6240	1179405303	INDICATOR       			BOLKMS	117   	BK117B2     	5626013	EU  										TRIPLE TACH	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911LK					7168				ROTOR TACHOMETER NEEDLE DROPS TO 50 OR SO, TAP GAUGE AND CUU GO BACK TO 100 PERCENT.						1	G	7	2 	3U			NC	H13EU   					 
1999082000861	19990820	00861	EU  	1999	8	20	HEEA063470       	1	19990813	G	7714	4011001	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										TRIPLE TACH	FLUCTUATES      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4302G					S853				INDICATOR'S NR 2 OIL PRESSURE FLUCTUATES AND DROPS TO ZERO.						1	G	7	2 	3U				H3EU    					 
1999082000862	19990820	00862	EU  	1999	8	20	HEEA063471       	1	19990813	G	6240	1179405303	INDICATOR       			BOLKMS	117   	BK117B2     	5626013	EU  										TRIPLE TACH	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911LK					7168				NR 2 N2 INTERMITTENTLY DROPS TO ZERO IN-FLIGHT AND RETURNS TO 100 PERCENT.						1	G	7	2 	3U			NC	H13EU   					 
1999082000863	19990820	00863	EU  	1999	8	20	HEEA063472       	1	19990813	G	6240	10594564	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										MAST MOMENT	WON'T CALIBRATE 	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8197X					S808				MAST MOMENT INDICATOR WILL NOT CALIBRATE.						1	G	7	2 	3U				H3EU    					 
1999082000864	19990820	00864	EU  	1999	8	20	HEEA063473       	1	19990813	G	6340	10594575	TRANSMITTER     			BOLKMS	105   	BO105S      	5626006	EU  										MAST MOMENT	WON'T CALIBRATE 	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8197X					S808				TORQUE TRANSMITTER WILL NOT CALIBRATE.						1	G	7	2 	3U				H3EU    					 
1999090300092	19990903	00092	GL  	1999	9	3	HEEA063665       	2	19990817	G	7250	68777362	BEARING CAGE    		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE SECTION	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4302G				CAT25464	S853	CAE834470			NEW PART ASSEMBLY INSPECTION REVEALED EXCESSIVE BEARING BORE RUN-OUT ON NR 8 BEARING CAGE INSTALLED IN SUPPORT AND UNINS	TALLED.  INSTALLED NEW BEARING CAGE.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999090300093	19990903	00093	GL  	1999	9	3	HEEA063666       	2	19990817	G	7230	23056634	GEARSHAFT       		23033191    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					SPUR ADAPTER	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3178K	661  			CAC70762	45765	CAE860357			ENGINE REMOVED DUE TO 1,500 HOUR INSPECTION.  UPON INSPECTION OF COMPRESSOR PARTS NOTED:  STEP WEAR BEYOND LIMITS ON SPU	R GEAR AFT END SPLINES.  INSTALLED NEW SPUR GEARSHAFT.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999090300094	19990903	00094	GL  	1999	9	3	HEEA063667       	2	19990817	G	7230	23056634	GEARSHAFT       		23051643    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					SPUR ADAPTER	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122G	685  			CAC91631	760232	CAE890547S			ENGINE REMOVED DUE TO 2,000 HOUR INSPECTION.  UPON INSPECTION OF COMPRESSOR PARTS NOTED:  STEP WEAR BEYOND LIMITS ON SPU	R GEAR AFT END SPLINES.  INSTALLED NEW SPUR GEARSHAFT.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999090300095	19990903	00095	GL  	1999	9	3	HEEA063668       	2	19990817	G	7250	6898764	SEAL            		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					OIL BELLOWS	CHIPPED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5421E	978  			CAT33588	S806	CAE834699			ENGINE REMOVED DUE TO  TURBINE OVERHAUL.  UPON INSPECTION OF TURBINE PARTS NOTED:  PITS AND CHIPPING ON CARBON SEAL MATI	NG SURFACE.  INSTALLED NEW CARBON SEAL.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999090300096	19990903	00096	GL  	1999	9	3	HEEA063669       	2	19990817	G	7230	23056634	GEARSHAFT       		23033191    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					SPUR ADAPTER	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5745S	805  			CAC70198	45491	CAE860782			ENGINE REMOVED DUE TO HIGH TIME IMPELLER.  UPON INSPECTION OF COMPRESSOR PARTS NOTED:  STEP WEAR BEYOND LIMITS ON SPUR G	EAR AFT END SPLINES. INSTALLED NEW SPUR GEARSHAFT.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999090300097	19990903	00097	GL  	1999	9	3	HEEA063670       	2	19990817	G	7230	23056634	GEARSHAFT       		23051643    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					SPUR ADAPTER	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	792CH	855  			CAC90538	760193	CAE890532S			ENGINE REMOVED DUE TO SMOKING AND BURNING OIL.   UPON INSPECTION OF COMPRESSOR PARTS NOTED:  STEP WEAR BEYOND LIMITS ON 	SPUR GEAR AFT END SPLINES. INSTALLED NEW SPUR GEARSHAFT.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999090300098	19990903	00098	SW  	1999	9	3	HEEA063719       	1	19990817	G	6220	407010101101	YOKE            		407010100111	BELL  	407   	407         		SW  										MAIN ROTOR	MISREPAIRED     	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	510PH	1569 			A226	53209				QUESTIONABLE REPAIR AREAS FROM VENDOR. SENT TO BELL HELICOPTER TEXTRON FOR EVALUATION AND POSSIBLE REPAIR.						1	G	7	1 	3U			O	H2SW    					 
1999090300099	19990903	00099	SW  	1999	9	3	HEEA063720       	1	19990818	G	5313	206031314037S	LONGERON        			BELL  	206   	206L3       	1182108	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										MISMANUFACTURED.  PART HAS A BOW AND TWIST AND WILL NOT MATCH UP TO AIRFRAME PROPERLY. SENT TO BELL HELICOPTER TEXTRON F	OR CREDIT AGAINST ORIGINAL PURCHASE.					1	G	7	1 	3U				H2SW    					 
1999090300100	19990903	00100	SW  	1999	9	3	HEEA063721       	1	19990818	G	5313	206031314037S	LONGERON        			BELL  	206   	206L3       	1182108	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										MISMANUFACTURED.  PART HAS A BOW AND TWIST AND WILL NOT MATCH UP TO AIRFRAME PROPERLY. SENT TO BELL HELICOPTER TEXTRON F	OR CREDIT AGAINST ORIGINAL PURCHASE.					1	G	7	1 	3U				H2SW    					 
1999090300101	19990903	00101	SW  	1999	9	3	HEEA063722       	1	19990818	G	5313	206031314037S	LONGERON        			BELL  	206   	206L3       	1182108	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										MISMANUFACTURED.  DEFECTS ON UPPER FLANGE.  FLANGE IS WARPED AND HAS GOUGES ON AFT END.  THE PART IS BOWED. SENT TO BELL	 HELICOPTER TEXTRON FOR CREDIT AGAINST ORIGINAL PURCHASE.					1	G	7	1 	3U				H2SW    					 
1999090300102	19990903	00102	SW  	1999	9	3	HEEA063723       	1	19990818	G	5313	206031314037S	LONGERON        			BELL  	206   	206L3       	1182108	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										MISMANUFACTURED.  CHANNEL HAS A 5 DEGREE STYLE TWIST.  WILL NOT MATCH UP TO AIRFRAME. SENT TO BELL HELICOPTER TEXTRON FO	R CREDIT AGAINST ORIGINAL PURCHASE.					1	G	7	1 	3U				H2SW    					 
1999090300356	19990903	00356	SW  	1999	9	3	HEEA063747       	1	19990823	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GEN	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	1518 				53114				BRUSHES FAILED 300 HOUR INSPECTION.  INSPECTED BY ACCESSORY SHOP AND FOUND BRUSHES WERE EXCESSIVELY WORN.						1	G	7	1 	3U			O	H2SW    					 
1999090300343	19990903	00343	SW  	1999	9	3	HEEA063751       	1	19990825	G	6210	407015001117	BLADE           			BELL  	407   	407         		SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH	2344 				53038				LOWER POCKET WEIGHT CORROSION, VOID AT STATION 197 ON LOWER SURFACE, HOLE AT STATION 197 ON LOWER.  SERIAL NUMBERS REMOV	ED ARE A285, A341 AND A263.  REPLACEMENT PART SERIAL NUMBERS ARE A754, A650 AND A596.  REFERENCE:  DMR NR 686294.					1	G	7	1 	3U			O	H2SW    					 
1999090300344	19990903	00344		1999	9	3	HEEA063752       	4	19990825	G	3417	214175421101	COMPUTER        			BELL  	214   	214ST       	1182106	SW  										AIR DATA	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				AIR DATA COMPUTER WILL NOT COUNT DOWN.						2	G	7	2 	4U				H10SW   					 
1999090300345	19990903	00345	SW  	1999	9	3	HEEA063753       	1	19990826	G	3246	407050202101	CROSSTUBE       			BELL  	407   	407         		SW  										MLG	CORRODED        	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	141MA					53016				CROSSTUBE CORRODED DUE TO INADEQUATE DISSIMILAR METAL PROTECTION FROM T-BOLT CLAMP.  REFERENCE:  DMR NR 686353.						1	G	7	1 	3U			O	H2SW    					 
1999090300346	19990903	00346	SW  	1999	9	3	HEEA063754       	1	19990826	G	3246	407050202101	CROSSTUBE       			BELL  	407   	407         		SW  										MLG	CORRODED        	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	510PH					53209				CROSSTUBE CORRODED DUE TO INADEQUATE DISSIMILAR METAL PROTECTION FROM T-BOLT CLAMP.  REFERENCE:  DMR NR 686354.						1	G	7	1 	3U			O	H2SW    					 
1999090300347	19990903	00347	SW  	1999	9	3	HEEA063755       	1	19990826	G	3246	407050201101	CROSSTUBE       			BELL  	407   	407         		SW  										MLG	CORRODED        	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	141MA					53016				CROSSTUBE CORRODED DUE TO INADEQUATE DISSIMILAR METAL PROTECTION FROM T-BOLT CLAMP.   REFERENCE:  DMR NR 686353.						1	G	7	1 	3U			O	H2SW    					 
1999090300348	19990903	00348	SW  	1999	9	3	HEEA063756       	1	19990827	G	6210	407015001117	BLADE           			BELL  	407   	407         		SW  										MAIN ROTOR	BLISTERED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM	3029 				53060				SMALL VOID ON UNDERSIDE OF BLADE NEAR TIP.  BLISTER NOTED ON DAILY INSPECTION.  REFERENCE:  DMR NR 686382.						1	G	7	1 	3U			O	H2SW    					 
1999090300349	19990903	00349	EU  	1999	9	3	HEEA063759       	1	19990825	G	2435	150SG122Q	GENERATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										STARTER/GEN	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L	1152 				2873				GENERATOR ARCING AND SLOW TURN.  REFERENCE:  RMA NR R021037.						1	G	7	1 	3U				H9EU    					 
1999090300350	19990903	00350	EU  	1999	9	3	HEEA063760       	1	19990825	G	6310	350A35105901	COUPLING        			SNIAS 	350   	AS350B2     	8680813	EU  										ENG/TRANSMISSION	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6095S					2777				COUPLING CRACKED.  REFERENCE:  RMA NR R020829.						1	G	7	1 	3U				H9EU    					 
1999090300351	19990903	00351	EU  	1999	9	3	HEEA063761       	1	19990825	G	6720	350A33214501	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				PLAY IN BEARINGS.  REFERENCE:  RMA NR R020609.						1	G	7	1 	3U				H9EU    					 
1999090300352	19990903	00352	EU  	1999	9	3	HEEA063762       	1	19990825	G	6720	350A33214501	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350BZ					2653				WORN BEARINGS.  SERIAL NUMBERS REMOVED ARE 2873 AND 2240.  REFERENCE:  RMA NR R020608.						1	G	7	1 	3U				H9EU    					 
1999090300353	19990903	00353	EU  	1999	9	3	HEEA063763       	1	19990825	G	6220	704A33633109	THRUST BEARING  			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z	464  				2820				BEARINGS WORN.  REFERENCE:  RMA NR  R021033.						1	G	7	1 	3U				H9EU    					 
1999090300354	19990903	00354	EU  	1999	9	3	HEEA063764       	1	19990825	G	6220	704A3363310951	STOP ASSY       			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z	1744 				2820				STOP ASSEMBLY WORN.  SERIAL NUMBERS REMOVED ARE 12494 AND 12563.  REFERENCE:  RMA NR  R021033.						1	G	7	1 	3U				H9EU    					 
1999090300355	19990903	00355	EU  	1999	9	3	HEEA063766       	1	19990825	G	3340	704A46814049	LIGHT           			SNIAS 	350   	AS350B2     	8680813	EU  										FUSELAGE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				NR 1 SIDE LIGHT SYSTEM WILL NOT COME ON.  REFERENCE:  RMA NR R021136.						1	G	7	1 	3U				H9EU    					 
1999091700425	19990917	00425	GL  	1999	9	17	HEEA063854       	2	19990831	G	7250	23008054	NOZZLE          		23033185    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					NR 1	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5007Y	614  			CAT70531	45192	CAE860100			ENGINE REMOVED DUE TO CRACKED EXHAUST COLLECTOR.  UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING:  CRACKED VANES O	N NR 1 NOZZLE.   INSTALLED NEW PART.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999091700426	19990917	00426	GL  	1999	9	17	HEEA063855       	2	19990831	G	7250	23062753	NOZZLE          		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					NR 1	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4573B	403  			CAT30507F	S673	CAE836418			ENGINE REMOVED DUE TO 3,500 HOUR OVERHAUL.  UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING:  CRACKED VANES ON NR 1	 NOZZLE.  INSTALLED NEW PART.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999091700427	19990917	00427	GL  	1999	9	17	HEEA063856       	2	19990831	G	7250	23062750	NOZZLE SHIELD   		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					NR 1	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	967MB	584  			CAT40104	S737	CAE836387			ENGINE REMOVED DUE TO N1 DRAG.  UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING:  CRACKED DOME ON NR 1 NOZZLE SHIEL	D.  INSTALLED NEW PART.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999091700428	19990917	00428	GL  	1999	9	17	HEEA063857       	2	19990831	G	7250	23062750	NOZZLE SHIELD   		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					NR 1	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	137AE	663  			CAT20425F	S851	CAE835939			ENGINE REMOVED DUE TO 1,750 HOUR INSPECTION.  UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING:  CRACKED DOME ON NR 	1 NOZZLE SHIELD.  INSTALLED NEW PART.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999091700429	19990917	00429	GL  	1999	9	17	HEEA063858       	2	19990831	G	7260	230595681	BEARING         								ALLSN 	250C  	250C30P     	03013	GL  					GEARBOX	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										RECEIVING INSPECTION PER BOOK FAX 99 AMC043 REVEALED CORROSION ON BEARING.											3	U			E1GL				 
1999091700430	19990917	00430		1999	9	17	HEEA063861       	4	19990831	G	3421	5040045904	INDICATOR       			BELL  	407   	407         		SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	57416					53070				INDICATOR SHOWS TILT IN LEVEL FLIGHT.   REFERENCE:  DMR NR 686221.						1	G	7	1 	3U			O	H2SW    					 
1999091700431	19990917	00431	SW  	1999	9	17	HEEA063862       	1	19990831	G	6320	407040050101	MAIN CASE       			BELL  	407   	407         		SW  										GEARBOX	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	2329 				53016				INPUT BEARING LINER WORN DUE TO APPLICATION OF SEALANT TO INPUT FLANGE AREA CAUSING IMPROPER PINCH FIT ON TRIPLEX BEARIN	G.   REFERENCE:  DMR NR 686308.					1	G	7	1 	3U			O	H2SW    					 
1999091700432	19990917	00432	SW  	1999	9	17	HEEA063863       	1	19990831	G	6310	406040500123	FREEWHEEL UNIT  			BELL  	407   	407         		SW  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	721PH	1020 				53278				LEAKING FORWARD SEAL.   REFERENCE:  DMR NR 686304.						1	G	7	1 	3U			O	H2SW    					 
1999091700433	19990917	00433	SW  	1999	9	17	HEEA063866       	1	19990902	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GENERATO	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH	1766 				53278				STARTER/GENERATOR FAILED 300-HOUR INSPECTION.						1	G	7	1 	3U			O	H2SW    					 
1999091700434	19990917	00434	SW  	1999	9	17	HEEA063868       	1	19990902	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GENERATO	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	722PH	1566 				53288				STARTER/GENERATOR FAILED 300-HOUR INSPECTION.   BRUSHES HAD LESS THAT 1/4 LIFE.						1	G	7	1 	3U			O	H2SW    					 
1999091700435	19990917	00435	SW  	1999	9	17	HEEA063870       	1	19990902	G	2435	206062200113	GENERATOR       			BELL  	407   	407         		SW  										STARTER/GENERATO	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH	1150 				53059				GENERATOR DROPS OFF-LINE.						1	G	7	1 	3U			O	H2SW    					 
1999091700436	19990917	00436	EU  	1999	9	17	HEEA063871       	1	19990831	G	2150	6AS35039	EVAPORATOR      			SNIAS 	350   	AS350B2     	8680813	EU  										FORWARD	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350BZ					2653				FAN AND SHAFT SEPARATED.  FAN NOT BEING DRIVEN.  REFERENCE:  RMA NR  R021215.						1	G	7	1 	3U				H9EU    					 
1999092400076	19990924	00076	SW  	1999	9	24	HEEA064287       	1	19990907	G	7712	407375003107	INDICATOR       			BELL  	407   	407         		SW  										TORQUE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH					53278				DROPPED TO ZERO IN-FLIGHT.  REFERENCE:  DMR NR 686242.						1	G	7	1 	3U			O	H2SW    					 
1999092400077	19990924	00077	SW  	1999	9	24	HEEA064291       	1	19990907	G	7714	407375008101	INDICATOR       			BELL  	407   	407         		SW  										DUAL TACHOMETER	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457PH					53147				ROTOR PORTION OF INDICATOR INOPERATIVE.  REFERENCE:  DMR NR 686380.						1	G	7	1 	3U			O	H2SW    					 
1999092400078	19990924	00078	SW  	1999	9	24	HEEA064292       	1	19990907	G	7714	407375008101	INDICATOR       			BELL  	407   	407         		SW  										DUAL TACHOMETER	LOCKED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				ROTOR NEEDLE LOCKED AT 110 PERCENT.   REFERENCE:  DMR NR 686329.						1	G	7	1 	3U			O	H2SW    					 
1999092400079	19990924	00079	SW  	1999	9	24	HEEA064293       	1	19990907	G	6300	407010206103	BEARING         			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	2329 				53016				WORN BEARINGS.  REFERENCE:  DMR NR 686345.						1	G	7	1 	3U			O	H2SW    					 
1999092400080	19990924	00080	SW  	1999	9	24	HEEA064294       	1	19990907	G	6300	407010206103	BEARING         			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	2329 				53016				WORN BEARINGS.   REFERENCE:  DMR NR 686345.						1	G	7	1 	3U			O	H2SW    					 
1999092400081	19990924	00081	SW  	1999	9	24	HEEA064295       	1	19990907	G	2822	1C2710	CARTRIDGE       			BELL  	407   	407         		SW  										FUEL PUMP	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				INOPERATIVE WITH INTERMITTENT GRINDING NOISE.  REFERENCE:  DMR NR 686402.						1	G	7	1 	3U			O	H2SW    					 
1999092400082	19990924	00082	SW  	1999	9	24	HEEA064296       	1	19990907	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				WORN BEARING.   REFERENCE:  DMR NR 686272.						1	G	7	1 	3U			O	H2SW    					 
1999092400083	19990924	00083	SW  	1999	9	24	HEEA064297       	1	19990907	G	6420	406312100101	BEARING         		407012101111	BELL  	407   	407         		SW  										TAIL ROTOR BLADE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	1086 			53114	53114				WORN BEARINGS.  REFERENCE:  DMR NR 686384.						1	G	7	1 	3U			O	H2SW    					 
1999092400084	19990924	00084	SW  	1999	9	24	HEEA064298       	1	19990907	G	6420	406312100101	BEARING         		407012101111	BELL  	407   	407         		SW  										TAIL ROTOR BLADE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH	675  			53006	53003				WORN BEARINGS.  REFERENCE:  DMR NR 686224.						1	G	7	1 	3U			O	H2SW    					 
1999092400085	19990924	00085	SW  	1999	9	24	HEEA064299       	1	19990907	G	6420	406312100101	BEARING         		407012101111	BELL  	407   	407         		SW  										TAIL ROTOR BLADE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM	407  			53207	53060				WORN BEARINGS.   REFERENCE:  DMR NR 686206.						1	G	7	1 	3U			O	H2SW    					 
1999092400086	19990924	00086	SW  	1999	9	24	HEEA064300       	1	19990907	G	6420	406312100101	BEARING         		407012101111	BELL  	407   	407         		SW  										TAIL ROTOR BLADE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	838  			53057	53016				WORN BEARINGS.  REFERENCE:  DMR NR 686421.						1	G	7	1 	3U			O	H2SW    					 
1999092400087	19990924	00087	SW  	1999	9	24	HEEA064301       	1	19990907	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				LINK HAD WORN BEARINGS.  REFERENCE:  DMR NR 686281.						1	G	7	1 	3U			O	H2SW    					 
1999092400088	19990924	00088	SW  	1999	9	24	HEEA064302       	1	19990907	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T	123  				28101				STARTER KICKS OFF AROUND 5 SECONDS DURING FIRST START ATTEMPT.						2	G	7	2 	4U				H10SW   					 
1999092400089	19990924	00089	SW  	1999	9	24	HEEA064303       	1	19990907	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				LINK HAD WORN BEARINGS.  SERIAL NUMBERS REMOVED ARE NHFS-3297 AND NHFS-2170.   REFERENCE:  DMR NR 686273.  REPLACEMENT P	ART SERIAL NUMBERS ARE NHFS-4516 AND NHFS-4526.					1	G	7	1 	3U			O	H2SW    					 
1999092400090	19990924	00090	SW  	1999	9	24	HEEA064304       	1	19990907	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				LINK HAD WORN BEARINGS.  REFERENCE:  DMR NR 686279.  REPLACEMENT PART SERIAL NUMBERS ARE NHFS-4311 AND NHFS-4459.						1	G	7	1 	3U			O	H2SW    					 
1999092400091	19990924	00091	SW  	1999	9	24	HEEA064305       	1	19990907	G	6220	407010107103	BEARING         			BELL  	407   	407         		SW  										MAIN ROTOR	FLAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	1092 				53016				SEAT HAD BLUE EPOXY COATING FLAKING.  REFERENCE:  DMR NR 686291.						1	G	7	1 	3U			O	H2SW    					 
1999092400092	19990924	00092	SW  	1999	9	24	HEEA064306       	1	19990907	G	5311	206032308121S	FRAME           			BELL  	407   	407         		SW  										FUSELAGE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	2491 				53159				FRAME CRACKED ABOVE RT TAILBOOM MOUNT BOLT HOLE.  REFERENCE:  DMR NR 686286.						1	G	7	1 	3U			O	H2SW    					 
1999092400093	19990924	00093	SW  	1999	9	24	HEEA064307       	1	19990907	G	2420	SM20ACD300A21	RELAY           			BELL  	407   	407         		SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				RELAY CAUSES FADEC DEGRADE LIGHT.  REFERENCE:  DMR  NR 686288.						1	G	7	1 	3U			O	H2SW    					 
1999092400094	19990924	00094	SW  	1999	9	24	HEEA064308       	1	19990907	G	6720	406012129101	LINK ASSEMBLY   			BELL  	407   	407         		SW  										TAIL ROTOR	FROZEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	723PH					53283				BEARING FROZEN ON LINK ASSY.   REFERENCE:  DMR NR 686265.						1	G	7	1 	3U			O	H2SW    					 
1999092400095	19990924	00095	SW  	1999	9	24	HEEA064309       	1	19990907	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	2843 				53114				UNIVERSAL HAD UNSTAKED BEARING.  REFERENCE:  DMR NR 686330.						1	G	7	1 	3U			O	H2SW    					 
1999092400096	19990924	00096	SW  	1999	9	24	HEEA064310       	1	19990907	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										MAIN ROTOR	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH	1474 				53072				UNIVERSAL HAD EXCESSIVE PLAY.   REFERENCE:  DMR NR 686219.						1	G	7	1 	3U			O	H2SW    					 
1999092400097	19990924	00097	SW  	1999	9	24	HEEA064311       	1	19990907	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	723PH					53283				LINK HAD WORN BEARINGS.  SERIAL NUMBERS REMOVED ARE NHFS-3225 AND NHFS-3288.   DMR NR 686263.  REPLACED WITH SERIAL NUMB	ERS NHFS-4384 AND NHFS-4412.					1	G	7	1 	3U			O	H2SW    					 
1999092400098	19990924	00098	SW  	1999	9	24	HEEA064312       	1	19990907	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH					53228				LINK HAD WORN BEARINGS.  SERIAL NUMBERS REMOVED ARE NHFS-3151 AND NHFS-3155.  DMR NR 686262.  REPLACED WITH SERIAL NUMBE	RS NHFS-4552 AND NHFS-4335.					1	G	7	1 	3U			O	H2SW    					 
1999092400099	19990924	00099	SW  	1999	9	24	HEEA064313       	1	19990907	G	6230	406010126107	DRIVE RING      			BELL  	407   	407         		SW  										MAIN ROTOR	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	510PH					53209				BLUE EPOXY COATING MISSING FROM DRIVE RING SET.  TOTAL RINS 4101.  REFERENCE:  DMR NR 686422.						1	G	7	1 	3U			O	H2SW    					 
1999092400100	19990924	00100	SW  	1999	9	24	HEEA064314       	1	19990907	G	6220	407010107103	BEARING         			BELL  	407   	407         		SW  										MAIN ROTOR	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	510PH	1569 				53209				SEAT HAD BLUE EPOXY COATING MISSING.   REFERENCE:  DMR NR 686423.						1	G	7	1 	3U			O	H2SW    					 
1999092400101	19990924	00101	SW  	1999	9	24	HEEA064315       	1	19990907	G	6220	407010104109	LOWER CONE      			BELL  	407   	407         		SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				LOWER CONE HAD DAMAGED TEFLON.  REFERENCE:  DMR NR 686212.						1	G	7	1 	3U			O	H2SW    					 
1999092400102	19990924	00102	SW  	1999	9	24	HEEA064316       	1	19990907	G	3212	206050247132	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				FLOAT COVER'S END FLAP TORN OFF.   REFERENCE:  DMR NR 686214.						1	G	7	1 	3U			O	H2SW    					 
1999092400103	19990924	00103	SW  	1999	9	24	HEEA064317       	1	19990907	G	3212	206050247135	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				FLOAT COVER'S END FLAP TORN OFF.   REFERENCE:  DMR NR 686243.						1	G	7	1 	3U			O	H2SW    					 
1999092400104	19990924	00104	SW  	1999	9	24	HEEA064318       	1	19990907	G	3212	206050247135	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				FLOAT COVER TORN AND DETERIORATED.  REFERENCE:  DMR NR 686290.						1	G	7	1 	3U			O	H2SW    					 
1999092400105	19990924	00105	SW  	1999	9	24	HEEA064319       	1	19990907	G	3212	206050247135	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				END FLAP TORN OFF ON FLOAT COVER.  REFERENCE:  DMR NR 686213.						1	G	7	1 	3U			O	H2SW    					 
1999092400106	19990924	00106	SW  	1999	9	24	HEEA064320       	1	19990907	G	3212	206050247135	COVER           			BELL  	407   	407         		SW  										FLOAT	DETERIORATED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				FLOAT COVER DETERIORATED.  REFERENCE:  DMR NR 686318.						1	G	7	1 	3U			O	H2SW    					 
1999092400107	19990924	00107	SW  	1999	9	24	HEEA064321       	1	19990907	G	3212	206050247137	COVER           			BELL  	407   	407         		SW  										FLOAT	DETERIORATED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				FLOAT COVER DETERIORATED.  REFERENCE:  DMR NR 686287.						1	G	7	1 	3U			O	H2SW    					 
1999092400108	19990924	00108	SW  	1999	9	24	HEEA064322       	1	19990907	G	6230	406010126107	DRIVE RING      			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	2329 				53016				SPLINES WORN BEYOND LIMITS.  REFERENCE:  DMR NR 68627101.						1	G	7	1 	3U			O	H2SW    					 
1999092400109	19990924	00109	SW  	1999	9	24	HEEA064323       	1	19990907	G	6230	406010428109	HUB SET         			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	2329 				53016				TEFLON ON BUSHINGS WORN.  REFERENCE:  DMR NR 686264.						1	G	7	1 	3U			O	H2SW    					 
1999092400110	19990924	00110	SW  	1999	9	24	HEEA064324       	1	19990907	G	3246	206053184122	SKID TUBE       			BELL  	407   	407         		SW  										MLG	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				SKID TUBE ASSY WORN ON BOTTOM.  REFERENCE:  DMR NR 686116.						1	G	7	1 	3U			O	H2SW    					 
1999092400111	19990924	00111	SW  	1999	9	24	HEEA064325       	1	19990907	G	3246	206053184121	SKID TUBE       			BELL  	407   	407         		SW  										MLG	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				SKID TUBE ASSY WORN ON BOTTOM.  REFERENCE:  DMR NR 686115.						1	G	7	1 	3U			O	H2SW    					 
1999092400112	19990924	00112	SW  	1999	9	24	HEEA064326       	1	19990907	G	7931	MS280343	TEMP BULB       			BELL  	407   	407         		SW  										OIL TEMP	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH					53198				HIGH TEMP INDICATIONS.  REFERENCE:  DMR NR 686425.						1	G	7	1 	3U			O	H2SW    					 
1999092400113	19990924	00113	SW  	1999	9	24	HEEA064327       	1	19990907	G	6240	222375077119	TRANSMITTER     			BELL  	407   	407         		SW  										TORQUE	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				ERRATIC READING ON TORQUE GAUGE.   REFERENCE:  DMR NR 686170.						1	G	7	1 	3U			O	H2SW    					 
1999092400114	19990924	00114	SW  	1999	9	24	HEEA064328       	1	19990907	G	6510	406040340101	DISK PACK       			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				DISC COUPLING CRACKED.  REFERENCE:  DMR NR 686433.						1	G	7	1 	3U			O	H2SW    					 
1999092400115	19990924	00115	SW  	1999	9	24	HEEA064329       	1	19990907	G	6230	406010428109	HUB SET         			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	2491 				53159				WORN BEARING SURFACE.   REFERENCE:  DMR NR 686211.						1	G	7	1 	3U			O	H2SW    					 
1999092400116	19990924	00116	SW  	1999	9	24	HEEA064330       	1	19990907	G	6230	406010427109	GIMBAL RING     			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	2492 				53159				GIMBAL HAS WORN PIVOT BUSHING.  REFERENCE:  DMR NR 686210.						1	G	7	1 	3U			O	H2SW    					 
1999092400117	19990924	00117	SW  	1999	9	24	HEEA064331       	1	19990907	G	6322	206061432121	HOUSING         			BELL  	407   	407         		SW  										BLOWER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				BLOWER HOUSING CRACKED.   REFERENCE:  DMR NR 686371.						1	G	7	1 	3U			O	H2SW    					 
1999092400118	19990924	00118	SW  	1999	9	24	HEEA064332       	1	19990907	G	7810	407062021101	DUCT            			BELL  	407   	407         		SW  										EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				DUCT CRACKED.  REFERENCE:  DMR NR 686295.						1	G	7	1 	3U			O	H2SW    					 
1999092400119	19990924	00119	SW  	1999	9	24	HEEA064333       	1	19990907	G	6320	222375077113	TRANSMITTER     			BELL  	407   	407         		SW  										TRANSMISSION	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724PH					53327				PRESSURE FLUCTUATES 15 PSI.   REFERENCE:  DMR NR 686312.						1	G	7	1 	3U			O	H2SW    					 
1999092400120	19990924	00120	SW  	1999	9	24	HEEA064334       	1	19990907	G	6510	406340340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH					53207				CRACK FOUND AT NR 6 DISC PACK ASSY.   REFERENCE:  DMR NR 686435.						1	G	7	1 	3U			O	H2SW    					 
1999092400121	19990924	00121	SW  	1999	9	24	HEEA064335       	1	19990907	G	6520	406040453101	SEAL            			BELL  	407   	407         		SW  										T/R GEARBOX	PITTED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH					53209				SEAL PITTED.   REFERENCE:  DMR NR 686436.						1	G	7	1 	3U			O	H2SW    					 
1999092400122	19990924	00122	GL  	1999	9	24	HEEA064336       	2	19990907	G	7320	407076503109	CONNECTOR       			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					FADEC	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				SEVERAL PINHOLES ON CONNECTOR ARE CHIPPED AND ELONGATED.  REFERENCE:  DMR NR 686305.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999092400123	19990924	00123	SW  	1999	9	24	HEEA064338       	1	19990907	G	3230	70079K000Y310	LINE            			BELL  	407   	407         		SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	722PH					53288				HOSE ASSY LEAKING FROM FITTING.  REFERENCE:  DMR NR 686355.						1	G	7	1 	3U			O	H2SW    					 
1999092400124	19990924	00124	SW  	1999	9	24	HEEA064339       	1	19990907	G	6320	406040074101	COLLECTOR PAN   			BELL  	407   	407         		SW  										M/R GEARBOX	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	141MA	2329 				53016				COLLECTOR PAN NOT CONCENTRIC.   REFERENCE:  DMR NR 686332.						1	G	7	1 	3U			O	H2SW    					 
1999092400125	19990924	00125	SW  	1999	9	24	HEEA064340       	1	19990907	G	6320	406040030107	BEARING         			BELL  	407   	407         		SW  										M/R GEARBOX	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	2329 				53016				OUTER DIAMETER WORN BELOW LIMITS.  REFERENCE:  DMR NR 686316.						1	G	7	1 	3U			O	H2SW    					 
1999092400126	19990924	00126	SW  	1999	9	24	HEEA064341       	1	19990907	G	6710	406010425107	BUSHING         			BELL  	407   	407         		SW  										CONTROL LEVER	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH	1662 				53142				BUSHINGS WORN ON LEVER ASSY.  SERIAL NUMBERS REMOVED ARE A-2028 AND A-2037.  REFERENCE:  DMR NR 686315.  REPLACEMENT PAR	T SERIAL NUMBERS ARE A-2636 AND A-2627.					1	G	7	1 	3U			O	H2SW    					 
1999092400127	19990924	00127	SW  	1999	9	24	HEEA064342       	1	19990907	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH	599  				53266				UNIVERSAL HAD WORN BEARINGS.  REFERENCE:  DMR NR 686205.						1	G	7	1 	3U			O	H2SW    					 
1999092400128	19990924	00128	SW  	1999	9	24	HEEA064344       	1	19990907	G	2434	214175150105	GENERATOR       			BELL  	214   	214ST       	1182106	SW  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M					28102				GENERATOR HOT LIGHT INTERMITTENT.						2	G	7	2 	4U				H10SW   					 
1999092400129	19990924	00129	SW  	1999	9	24	HEEA064345       	1	19990908	G	5313	206031314037S	LONGERON        			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										LONGERON MISMANUFACTURED.  WHEN CHANNEL IS DRILLED UNABLE TO OBTAIN PROPER RIVET EDGE DISTANCE PER BELL MANUAL.  CHANNEL	 LIP TOO SHORT.   REFERENCE:  DMR NR 681232.					1	G	7	1 	3U				H2SW    					 
1999092400130	19990924	00130	SW  	1999	9	24	HEEA064346       	1	19990908	G	5313	206031314037S	LONGERON        			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										LONGERON MISMANUFACTURED.  CHANNEL HAS BOW AND WILL NOT FIT AIRFRAME PROPERLY.  DREFERENCE:  DMR NR 681233.						1	G	7	1 	3U				H2SW    					 
1999092400131	19990924	00131	SW  	1999	9	24	HEEA064347       	1	19990910	G	6220	407010101101	YOKE            		407010100111	BELL  	407   	407         		SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH	2492 			A63	53059				YOKE HAD MECHANICAL DAMAGE OF INNER WEB EDGES - UNABLE TO DETERMINE CAUSE OF DAMAGES.						1	G	7	1 	3U			O	H2SW    					 
1999100100269	19991001	00269	GL  	1999	10	1	HEEA064376       	2	19990915	G	7260	6896437	GEARSHAFT       		6894171     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					GEARBOX	SPALLED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911PF	127  			CAG38015F	S718	CAE836333			ENGINE REMOVED DUE TO METAL IN OIL.  UPON INSPECTION OF GEARBOX PARTS NOTED:  SPALLING ON FUEL CONTROL/OIL PUMP GEAR TEE	TH.  INSTALLED NEW PARTS.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999100100270	19991001	00270	GL  	1999	10	1	HEEA064377       	2	19990915	G	7260	6893672	PINION GEAR     		23035179    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30P     	03013	GL  					GEARBOX	SPALLED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545X	213  			CAG90400	760050	CAE890397S			ENGINE REMOVED DUE TO METAL IN OIL.  UPON INSPECTION OF GEARBOX PARTS NOTED:  SPALLING OF GEAR TEETH.  INSTALLED NEW PAR	TS.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999100100271	19991001	00271	GL  	1999	10	1	HEEA064378       	2	19990915	G	7260	6893673	GEAR            		23035179    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30P     	03013	GL  					GEARBOX	SPALLED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545X	213  			CAG90400	760050	CAE890397S			ENGINE REMOVED DUE TO METAL IN OIL.  UPON INSPECTION OF GEARBOX PARTS NOTED:  SPALLING OF GEAR TEETH.  INSTALLED NEW PAR	TS.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999100100272	19991001	00272	GL  	1999	10	1	HEEA064379       	2	19990922	G	7230	23004513	CARBON SEAL     		6890550     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911PF	790  			CAC33537	S718	CAE836333			ENGINE REMOVED DUE TO METAL IN OIL.  UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING:  GROOVED BEYOND SERVICEABL	E LIMITS ON CARBON SEAL ASSY TANGS AND SLOTS.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999100100273	19991001	00273	GL  	1999	10	1	HEEA064380       	2	19990922	G	7230	23039791	SPLINE ADAPTER  		6890550     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911PF	791  			CAC33537	S718	CAE836333			ENGINE REMOVED DUE TO METAL IN OIL.  UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING:  FRETTING AND WORN BEYOND 	OVERHAUL MANUAL LIMITS ON SPLINE ADAPTER OUTSIDE DIAMETER AND RETAINING RING GROOVE.  INSTALLED NEW PART.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999100100274	19991001	00274	GL  	1999	10	1	HEEA064381       	2	19990922	G	7250	23062750	NOZZLE SHIELD   		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					NR 1	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	133AE	825  			CAT34269	S800	CAE833901			ENGINE REMOVED DUE TO TURBINE RUBBING ON SHUTDOWN.  UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING:  CRACKED AND S	EPARATED FROM INNER BAND BEYOND OVERHAUL MANUAL LIMITS ON NR 1 NOZZLE SHIELD DOME.  INSTALLED NEW PART.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999100100275	19991001	00275	GL  	1999	10	1	HEEA064382       	2	19990922	G	7261	6876925	TUBE            		6894171     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE OIL	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	8199J	2607 			CAG23059	S826	CAE836370			FAILED DIMENSIONAL REQUIREMENTS OF CEB1307 ON OIL FILTER INLET TUBE ASSY.  INSTALLED NEW PART.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999100100276	19991001	00276	GL  	1999	10	1	HEEA064389       	2	19990923	G	7250	23008020	TIE BOLT        		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE SECTION	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	91070				CAT31355F	S145	CAE835824			TIE BOLT INSPECTION REVEALED FREE LENGTH OVER MAX LIMITS AT 6.888 INCHES.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999100100277	19991001	00277	GL  	1999	10	1	HEEA064390       	2	19990923	G	7250	23008020	TIE BOLT        		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE SECTION	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	4294R				CAT31653F	S860	CAE836450			TIE BOLT INSPECTION REVEALED FREE LENGTH OVER MAX LIMITS AT 6.888 INCHES.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999100100278	19991001	00278	GL  	1999	10	1	HEEA064391       	2	19990923	G	7230	23004513	CARBON SEAL     		23033191    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					COMPRESSOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	5006F				CAC70541	45181	CAE860545			CARBON SEAL INSPECTION REVEALED LEAKS DURING PRESSURE TEST.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999100100279	19991001	00279	GL  	1999	10	1	HEEA064392       	2	19990923	G	7260	6896437	GEARSHAFT       		6894171     	BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					GEARBOX	SPALLED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2753F	313  			CAG23058	2729	CAE820957F			ENGINE REMOVED DUE TO MAKING METAL.  UPON INSPECTION OF GEARBOX NOTED THE FOLLOWING:  SPALLING BEYOND SERVICEABLE LIMITS	 ON F/C O/P GEAR TEETH.  INSTALLED NEW PART.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999100100280	19991001	00280	GL  	1999	10	1	HEEA064393       	2	19990923	G	7250	6898764	SEAL            		23035128    						ALLSN 	250C  	250C20B     	03013	GL  					TURBINE SECTION	CORRODED        	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03					CAT95503					SEAL ASSEMBLY INSPECTION REVEALED PITTED MATING SURFACE.											3	U			E4CE				 
1999100100281	19991001	00281	GL  	1999	10	1	HEEA064394       	2	19990923	G	7250	23062753	NOZZLE          		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					NR 1	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	133AE	825  			CAT34269	S800	CAE833901			ENGINE REMOVED DUE TO TURBINE RUBBING ON SHUTDOWN.  UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING:  CRACKED BEYON	D SERVICEABLE LIMITS ON NR 1 NOZZLE VANES.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999100100282	19991001	00282	GL  	1999	10	1	HEEA064397       	2	19990923	G	7250	23062750	NOZZLE SHIELD   		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					NR 1	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5031U	1196 			CAT34156F	S678				TURBINE REPAIR DUE TO HIGH CYCLES.  UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING:  CRACKED BEYOND REPAIRABLE LIM	ITS ON NR 1 NOZZLE SHIELD DOME.  REPLACED WITH SERVICEABLE PARTS.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999100100283	19991001	00283	SW  	1999	10	1	HEEA064398       	1	19990917	G	2435	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806	179  				28140				WILL NOT MOTOR ENGINE PAST 25 PERCENT.						2	G	7	2 	4U				H10SW   					 
1999100100284	19991001	00284		1999	10	1	HEEA064399       	4	19990920	G	3417	214175421101	COMPUTER        			BELL  	214   	214ST       	1182106	SW  										AIR DATA	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				WILL NOT COUNT DOWN.						2	G	7	2 	4U				H10SW   					 
1999100100285	19991001	00285	SW  	1999	10	1	HEEA064401       	1	19990920	G	6310	406340102101	CARBON SEAL     		406040500123	BELL  	407   	407         		SW  										TRANSMISSION	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	724PH	493  			A4539	53327				SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999100100286	19991001	00286	SW  	1999	10	1	HEEA064403       	1	19990920	G	6420	407012101111	HUB             			BELL  	407   	407         		SW  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH	2534 				53072				ONE OF THE TAIL ROTOR BLADES IS SEPARATED ON THE TRAILING EDGE.						1	G	7	1 	3U			O	H2SW    					 
1999100100287	19991001	00287	SW  	1999	10	1	HEEA064404       	1	19990920	G	6310	406040500119	SEAL            			BELL  	407   	407         		SW  										TRANSMISSION	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	721PH	1020 				53278				SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999100100288	19991001	00288	SW  	1999	10	1	HEEA064405       	1	19990922	G	3212	206373901103	SOLENOID VALVE  			BELL  	407   	407         		SW  										MLG FLOAT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	408PH	1727 				53228				RELIEF VALVE LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999100100289	19991001	00289	SW  	1999	10	1	HEEA064406       	1	19990922	G	6310	406040500123	FREEWHEEL UNIT  			BELL  	407   	407         		SW  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	437PH	3775 				53072				LEAKING FROM FRONT SEAL.						1	G	7	1 	3U			O	H2SW    					 
1999100100290	19991001	00290	SW  	1999	10	1	HEEA064407       	1	19990922	G	6320	407375005101	INDICATOR       			BELL  	407   	407         		SW  										TRANSMISSION OIL	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				TEMPERATURE WENT TO ZERO DEGREES DURING RUN.						1	G	7	1 	3U			O	H2SW    					 
1999100100291	19991001	00291	SW  	1999	10	1	HEEA064408       	1	19990922	G	6230	406010427109	GIMBAL RING     			BELL  	407   	407         		SW  										MAIN ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH	2496 				53228				BUSHING PITTED AND CORRODED.						1	G	7	1 	3U			O	H2SW    					 
1999100100292	19991001	00292	SW  	1999	10	1	HEEA064409       	1	19990922	G	6220	407010103101	HORN            			BELL  	407   	407         		SW  										M/R HUB	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	2496 				53114				CORROSION, UNABLE TO DETECT DURING VISUAL INSPECTION DUE TO LOCATION OF CORROSION.						1	G	7	1 	3U			O	H2SW    					 
1999100100293	19991001	00293	SW  	1999	10	1	HEEA064410       	1	19990922	G	6220	407310100103	DAMPER          			BELL  	407   	407         		SW  										MAIN ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	2496 				53114				DAMPER HAS CORROSION, UNABLE TO DETECT DURING VISUAL INSPECTION DUE TO LOCATION OF CORROSION.						1	G	7	1 	3U			O	H2SW    					 
1999100100294	19991001	00294		1999	10	1	HEEA064411       	4	19990922	G	3416	5934D3	ALTIMETER       			BELL  	407   	407         		SW  										COCKPIT	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457PH					53147				ALTIMETER READS 90 FEET LOW.						1	G	7	1 	3U			O	H2SW    					 
1999100100295	19991001	00295	SW  	1999	10	1	HEEA064413       	1	19990922	G	7714	407375008101	INDICATOR       			BELL  	407   	407         		SW  										DUAL TACH	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				NP NEEDLE IS INTERMITTENT.						1	G	7	1 	3U			O	H2SW    					 
1999100100296	19991001	00296	SW  	1999	10	1	HEEA064414       	1	19990922	G	7714	407375008101	INDICATOR       			BELL  	407   	407         		SW  										DUAL TACH	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH					53209				ROTOR NEEDLE COMES ON-LINE THEN DROPS OFF.						1	G	7	1 	3U			O	H2SW    					 
1999100100297	19991001	00297	SW  	1999	10	1	HEEA064415       	1	19990922	G	7714	407375008101	INDICATOR       			BELL  	407   	407         		SW  										DUAL TACH	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH					53209				TURBINE NEEDLE FAILED.						1	G	7	1 	3U			O	H2SW    					 
1999100100298	19991001	00298	SW  	1999	10	1	HEEA064416       	1	19990922	G	7714	407375002103	INDICATOR       			BELL  	407   	407         		SW  										ENGINE NG	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				NG INDICATOR WENT BLANK ON GROUND RUN.						1	G	7	1 	3U			O	H2SW    					 
1999100100299	19991001	00299	SW  	1999	10	1	HEEA064417       	1	19990922	G	3246	206053184121	SKID TUBE       			BELL  	407   	407         		SW  										MLG	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH					53207				SKID TUBE WORN AT AFT TIP.						1	G	7	1 	3U			O	H2SW    					 
1999100100300	19991001	00300	SW  	1999	10	1	HEEA064418       	1	19990922	G	3246	206053184122	SKID TUBE       			BELL  	407   	407         		SW  										MLG	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH					53207				SKID TUBE WORN AT AFT TIP.						1	G	7	1 	3U			O	H2SW    					 
1999100100301	19991001	00301	SW  	1999	10	1	HEEA064419       	1	19990922	G	6320	407040050101	MAIN CASE       			BELL  	407   	407         		SW  										GEARBOX	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH	1569 				53209				INPUT BORE WORN BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999100100302	19991001	00302	SW  	1999	10	1	HEEA064420       	1	19990922	G	6220	407010150103	FRAHM ASSY      			BELL  	407   	407         		SW  										MAIN ROTOR	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				AIRCRAFT EXPERIENCES SHUTTER IN TRANSITION TO CRUISE FLIGHT.  RUBBER CUSHION ON PAD ASSY GONE.						1	G	7	1 	3U			O	H2SW    					 
1999100100303	19991001	00303	SW  	1999	10	1	HEEA064424       	1	19990922	G	7921	406360500101	COOLER          			BELL  	407   	407         		SW  										ENGINE OIL	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	510PH					53209				COOLER LEAKS.						1	G	7	1 	3U			O	H2SW    					 
1999100100304	19991001	00304		1999	10	1	HEEA064429       	4	19990922	G	3442	40005040301	DRIVE ASSY      			BELL  	214   	214ST       	1182106	SW  										RADAR ANTENNA	DEFECTIVE       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	824H					28119				CANNOT ADJUST PITCH POTENTIOMETER.						2	G	7	2 	4U				H10SW   					 
1999100100305	19991001	00305		1999	10	1	HEEA064430       	4	19990922	G	3442	40005040301	DRIVE ASSY      			BELL  	214   	214ST       	1182106	SW  										RADAR ANTENNA	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				STABILIZATION INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999100100306	19991001	00306		1999	10	1	HEEA064431       	4	19990922	G	3442	40005040301	DRIVE ASSY      			BELL  	214   	214ST       	1182106	SW  										ANTENNA	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ANTENNA FAULT INDICATION.						2	G	7	2 	4U				H10SW   					 
1999100100307	19991001	00307		1999	10	1	HEEA064432       	4	19990922	G	3442	40005040301	DRIVE ASSY      			BELL  	214   	214ST       	1182106	SW  										RADAR ANTENNA	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				WILL NOT TILT UP.						2	G	7	2 	4U				H10SW   					 
1999100100308	19991001	00308		1999	10	1	HEEA064433       	4	19990922	G	3442	40005040301	DRIVE ASSY      			BELL  	214   	214ST       	1182106	SW  										RADAR ANTENNA	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				STOPS SWEEPING WHEN WARMED UP.						2	G	7	2 	4U				H10SW   					 
1999100100309	19991001	00309		1999	10	1	HEEA064434       	4	19990922	G	3442	40005040301	DRIVE ASSY      			BELL  	214   	214ST       	1182106	SW  										RADAR ANTENNA	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				RADAR WILL NOT PAINT TARGETS.						2	G	7	2 	4U				H10SW   					 
1999100100310	19991001	00310		1999	10	1	HEEA064435       	4	19990922	G	3442	40005040301	DRIVE ASSY      			BELL  	214   	214ST       	1182106	SW  										RADAR ANTENNA	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				WILL NOT TILT.  SHAFT SHEARED.						2	G	7	2 	4U				H10SW   					 
1999100100311	19991001	00311	SW  	1999	10	1	HEEA064436       	1	19990922	G	7712	407375003107	INDICATOR       			BELL  	407   	407         		SW  										ENGINE TORQUE	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH					53278				INDICATOR INTERMITTENTLY GOES INTO INITIAL TEST.						1	G	7	1 	3U			O	H2SW    					 
1999100100312	19991001	00312	SW  	1999	10	1	HEEA064437       	1	19990923	G	7712	407375003107	INDICATOR       			BELL  	407   	407         		SW  										ENGINE TORQUE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				TWO LED SEGMENTS BETWEEN 95 PERCENT AND 100 PERCENT VERY DIM.						1	G	7	1 	3U			O	H2SW    					 
1999100100313	19991001	00313	SW  	1999	10	1	HEEA064438       	1	19990923	G	7712	407375003107	INDICATOR       			BELL  	407   	407         		SW  										ENGINE TORQUE	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH					53266				TORQUE FLUCTUATES.						1	G	7	1 	3U			O	H2SW    					 
1999100100314	19991001	00314	SW  	1999	10	1	HEEA064445       	1	19990924	G	5210	20898411	LATCH           			BELL  	407   	407         		SW  										MAIN DOOR	BROKE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				LEVER P/N 3226-201 BROKE ON LT FORWARD DOOR.  THE LEVER WAS NON-PROCURABLE FROM BELL.  LATCH ASSY P/N 20898-411 WAS ORDE	RED AND THE LEVER WAS SCRAPPED LOCALLY.					1	G	7	1 	3U			O	H2SW    					 
1999100100315	19991001	00315	EU  	1999	10	1	HEEA064447       	1	19990916	G	6710	SC5083	SERVO           			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z	2277 				2820				SERVO LEAKING AT PILOT VALVE.						1	G	7	1 	3U				H9EU    					 
1999100100316	19991001	00316	EU  	1999	10	1	HEEA064448       	1	19990916	G	7712	305731365	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										ENGINE TORQUE	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z					2820				TORQUE INDICATOR FLUCTUATES IN-FLIGHT.  DROPS OR RISES 8-12 PERCENT  WITH NO CHANGE IN COLLECTIVE OR OTHER ENGINE PARAME	TERS.					1	G	7	1 	3U				H9EU    					 
1999100100317	19991001	00317	EU  	1999	10	1	HEEA064449       	1	19990916	G	6410	355A12004008	BLADE           			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WON'T BALANCE   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z	3742 				2820				CAUSING VIBRATION AT MID-RANGE, WILL NOT BALANCE AT LOW SPEED.						1	G	7	1 	3U				H9EU    					 
1999100100318	19991001	00318	EU  	1999	10	1	HEEA064452       	1	19990916	G	2822	P94B12209	PUMP            			SNIAS 	350   	AS350B2     	8680813	EU  										FUEL BOOST	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				BLOW FUSES. SENT TO AMERICAN EUROCOPTER CORP. FOR CREDIT AGAINST REPLACEMENT PART PURCHASED.  REFERENCE:  RMA# R021689.						1	G	7	1 	3U				H9EU    					 
1999100100319	19991001	00319	EU  	1999	10	1	HEEA064453       	1	19990916	G	5302	350A1400210401	RIVETS          			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL BOOM	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z					2820				STABILIZER ASSEMBLY HAS WORKING RIVETS, ALREADY OVERSIZED.						1	G	7	1 	3U				H9EU    					 
1999100100320	19991001	00320	EU  	1999	10	1	HEEA064454       	1	19990916	G	6520	350A33020005	GEARBOX         			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z	2191 				2820				GEARBOX MAKING METAL.						1	G	7	1 	3U				H9EU    					 
1999100100321	19991001	00321	EU  	1999	10	1	HEEA064455       	1	19990917	G	2800	MS5750V01	MOTOR           			SNIAS 	350   	AS350B2     	8680813	EU  										FUEL SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				BLOWN 50-AMP CIRCUIT BREAKER.						1	G	7	1 	3U				H9EU    					 
1999100100322	19991001	00322	EU  	1999	10	1	HEEA064456       	1	19990917	G	6520	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				PITCH ROD BEARINGS WORN.  REPLACED WITH SERIAL NUMBERS S3672 AND S3739.						1	G	7	1 	3U				H9EU    					 
1999100100323	19991001	00323	EU  	1999	10	1	HEEA064457       	1	19990917	G	6520	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				PITCH ROD BEARINGS WORN.   REPLACED WITH SERIAL NUMBERS S3613 AND S3845.						1	G	7	1 	3U				H9EU    					 
1999100100324	19991001	00324	EU  	1999	10	1	HEEA064458       	1	19990917	G	6520	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH CONTROL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350BZ					2653				PITCH ROD BEARINGS WORN.  SERIAL NUMBERS REMOVED ARE S2863 AND S2250.  REPLACED WITH SERIAL NUMBERS S3693 AND S3624.						1	G	7	1 	3U				H9EU    					 
1999100800132	19991008	00132	GL  	1999	10	8	HEEA064463       	2	19990927	G	7250	23007202	BEARING         		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	SCORED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	133AE	224  			CAT33140	S800	CAE800850F			ENGINE REMOVED DUE TO TURBINE RUBBING.  UPON INSPECTION OF PARTS NOTED:  SCORING BEYOND O/H MANUAL LIMITS ON NR 6 AND NR	 7 BEARING ROLLERS.    SERIAL NUMBERS REMOVED ARE MP42920 AND MP42909. NEW PARTS INSTALLED.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999100800133	19991008	00133	GL  	1999	10	8	HEEA064464       	2	19990927	G	7230	23004513	CARBON SEAL     		23033191    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					ENGINE	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	5006F	667  			CAC70541	45181	CAE860545			ENGINE REMOVED DUE TO NR 1 BEARING OIL LEAK.  UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING:  GROOVED SLOTS AN	D TANGS BEYOND SERVICEABLE LIMITS ON CARBON SEAL ASSY.  NEW PART INSTALLED.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999100800134	19991008	00134	GL  	1999	10	8	HEEA064465       	2	19990927	G	7230	23004513	CARBON SEAL     		23033193    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					ENGINE	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	53119	102  			CAC91057	51575	CAE895160			ENGINE REMOVED DUE TO SMOKE AT 100 PERCENT TO IDLE.  UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING:  GROOVED S	LOTS AND TANGS BEYOND SERVICEABLE LIMITS ON CARBON SEAL ASSY.  NEW PART INSTALLED.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999100800135	19991008	00135	GL  	1999	10	8	HEEA064466       	2	19990927	G	7230	23004513	CARBON SEAL     		23051643    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					ENGINE	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122H	722  			CAC90484	760233	CAE890180S			ENGINE REMOVED DUE TO SMOKE ON SHUTDOWN.  UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING:  GROOVED SLOTS AND TA	NGS BEYOND SERVICEABLE LIMITS ON CARBON SEAL ASSY.  NEW PART INSTALLED.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999100800136	19991008	00136	GL  	1999	10	8	HEEA064467       	2	19990927	G	7230	23056634	SPUR GEAR       		23051643    	SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122H	738  			CAC90484	760233	CAE890180S			ENGINE REMOVED DUE TO SMOKE ON SHUTDOWN.  UPON INSPECTION OF COMPRESSOR PARTS NOTED THE FOLLOWING:  STEP WEAR ON SPUR GE	ARSHAFT AFT END SPLINES BEYOND SERVICEABLE LIMITS.  NEW PART INSTALLED.					1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999100800137	19991008	00137	GL  	1999	10	8	HEEA064468       	2	19990927	G	7230	23004513	CARBON SEAL     		6890550     						ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03					CAC41787		CAE270046			ENGINE REMOVED FROM TEST CELL DUE TO LOW POWER.   UPON REPAIR OF COMPRESSOR ASSY NOTED A LEAK IN CARBON SEAL ASSY DURING	 PRESSURE CHECK.  NEW PART INSTALLED.										3	U			E4CE				 
1999100800138	19991008	00138		1999	10	8	HEEA064469       	4	19990927	G	3417	214175421101	COMPUTER        			BELL  	214   	214ST       	1182106	SW  										AIR DATA	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6957Y					28139				COUNT DOWN INOPERATIVE DURING FLIGHT.						2	G	7	2 	4U				H10SW   					 
1999100800139	19991008	00139	SW  	1999	10	8	HEEA064470       	1	19990929	G	6210	407015001117	BLADE           			BELL  	407   	407         		SW  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	3133 				53114				MAIN ROTOR BLADE CRACKED IN TRIM TAB AREA.  SERIAL NUMBERS REMOVED ARE A-625, A-643, A-635, A-653.  REPLACED WITH SERIAL	 NUMBERS A-848, A-1597, A-390, A-649.  REFERENCE:  DMR NR 686521.					1	G	7	1 	3U			O	H2SW    					 
1999100800140	19991008	00140	SW  	1999	10	8	HEEA064471       	1	19990929	G	6210	407015001117	BLADE           			BELL  	407   	407         		SW  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	2728 				53159				BLADE CRACKED IN TRIM TAB AREA.  SERIAL NUMBERS REMOVED ARE A-869 AND A-879.  REPLACED WITH SERIAL NUMBERS A-664 AND A-6	06.  REFERENCE:  DMR NR 686522.					1	G	7	1 	3U			O	H2SW    					 
1999100800141	19991008	00141	SW  	1999	10	8	HEEA064477       	1	19990929	G	7712	222375077119	TRANSMITTER     			BELL  	407   	407         		SW  										TORQUE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			SW	03	721PH					53278				INSTRUMENT CHECK LIGHT TURNED ON IN-FLIGHT.  REFERENCE:  DMR NR 686462.						1	G	7	1 	3U			O	H2SW    					 
1999100800142	19991008	00142	SW  	1999	10	8	HEEA064478       	1	19990929	G	7712	222375077119	TRANSMITTER     			BELL  	407   	407         		SW  										ENGINE TORQUE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			SW	03	721PH					53278				DURING START, TRANSMITTER CAUSED GAUGE TO READ FROM ZERO TO MAX INDICATION, THEN FLUCTUATES AS LONG AS 5 MINUTES.   REFE	RENCE:  DMR NR 686463.					1	G	7	1 	3U			O	H2SW    					 
1999100800143	19991008	00143	SW  	1999	10	8	HEEA064479       	1	19990929	G	7712	222375077119	TRANSMITTER     			BELL  	407   	407         		SW  										ENGINE TORQUE	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH					53266				TORQUE INTERMITTENTLY INOPERATIVE.  REFERENCE:  DMR NR 686461.						1	G	7	1 	3U			O	H2SW    					 
1999100800144	19991008	00144	SW  	1999	10	8	HEEA064480       	1	19990930	G	6340	222375077117	TRANSMITTER     			BELL  	407   	407         		SW  										MAIN ROTOR	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	408PH					53228				TRANSMITTER HAD NO PRESSURE INDICATION.   REFERENCE:  DMR NR 686364.						1	G	7	1 	3U			O	H2SW    					 
1999100800145	19991008	00145	SW  	1999	10	8	HEEA064481       	1	19990930	G	7931	222375077113	TRANSMITTER     			BELL  	407   	407         		SW  										OIL PRESSURE	FLUCTUATES      	E			HEEA	O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			SW	03	719PH					53266				ENGINE OIL PRESSURE FLUCTUATES ON WASH.  REFERENCE:  DMR NR 686434.						1	G	7	1 	3U			O	H2SW    					 
1999100800146	19991008	00146	SW  	1999	10	8	HEEA064482       	1	19990930	G	2913	206076030111	PUMP            			BELL  	407   	407         		SW  										HYDRAULIC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				PUMP HAD SHEARED SHAFT.   REFERENCE:  DMR NR 686362.						1	G	7	1 	3U			O	H2SW    					 
1999100800147	19991008	00147	SW  	1999	10	8	HEEA064483       	1	19990930	G	6320	214040806003	PRESSURE SWITCH 			BELL  	407   	407         		SW  										M/R GEARBOX	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				PRESSURE SWITCH WILL NOT TURN ON TRANSMISSION OIL PRESSURE LIGHT.  REFERENCE:  DMR NR 686424.						1	G	7	1 	3U			O	H2SW    					 
1999100800148	19991008	00148	SW  	1999	10	8	HEEA064484       	1	19990930	G	7810	407063001101	EXHAUST STACK   			BELL  	407   	407         		SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8595X					53267				EXHAUST STACK HAD CRACK ON AFT SIDE.  REFERENCE:   DMR NR 686222.						1	G	7	1 	3U			O	H2SW    					 
1999100800149	19991008	00149	SW  	1999	10	8	HEEA064485       	1	19990930	G	7810	407063001101	EXHAUST STACK   			BELL  	407   	407         		SW  										ENGINE	CRAKED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				EXHAUST STACK CRACKED.   REFERENCE:  DMR NR 686468.						1	G	7	1 	3U			O	H2SW    					 
1999100800150	19991008	00150	SW  	1999	10	8	HEEA064486       	1	19990930	G	7810	407063001101	EXHAUST STACK   			BELL  	407   	407         		SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				EXHAUST STACK CRACKED, CENTER AFT SIDE.  REFERENCE:  DMR NR 686469.						1	G	7	1 	3U			O	H2SW    					 
1999100800151	19991008	00151	SW  	1999	10	8	HEEA064487       	1	19990930	G	7810	407063001101	EXHAUST STACK   			BELL  	407   	407         		SW  										ENGINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				EXHAUST STACK CRACKED.  REFERENCE:  DMR NR 686437.						1	G	7	1 	3U			O	H2SW    					 
1999100800152	19991008	00152	SW  	1999	10	8	HEEA064488       	1	19990930	G	3212	206050247131	COVER ASSY      			BELL  	407   	407         		SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				FLOAT COVER WORN.  REFERENCE:  DMR NR 686338.						1	G	7	1 	3U			O	H2SW    					 
1999100800153	19991008	00153	SW  	1999	10	8	HEEA064489       	1	19990930	G	3212	206050247131	COVER ASSY      			BELL  	407   	407         		SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				FLOAT COVER HAD WORN END CAP.  REFERENCE:  DMR NR 686431.						1	G	7	1 	3U			O	H2SW    					 
1999100800154	19991008	00154	SW  	1999	10	8	HEEA064490       	1	19990930	G	3212	206050247132	SNAP            			BELL  	407   	407         		SW  										FLOAT COVER	MISSING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH					53228				FLOAT COVER HAD SNAPS MISSING.   REFERENCE:  DMR NR 686390.						1	G	7	1 	3U			O	H2SW    					 
1999100800155	19991008	00155	SW  	1999	10	8	HEEA064491       	1	19990930	G	3212	212073905001	GAUGE           			BELL  	407   	407         		SW  										FLOAT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				PRESSURE GAUGE STICKING.  REFERENCE:  DMR NR 686227.						1	G	7	1 	3U			O	H2SW    					 
1999100800156	19991008	00156	SW  	1999	10	8	HEEA064492       	1	19990930	G	3212	206050247135	COVER ASSY      			BELL  	407   	407         		SW  										FLOAT	FRAYED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457PH					53147				FRONT FLAP FRAYED ON FLOAT COVER.  REFERENCE:  DMR NR 686533.						1	G	7	1 	3U			O	H2SW    					 
1999100800157	19991008	00157	SW  	1999	10	8	HEEA064493       	1	19990930	G	3212	206050247135	COVER ASSY      			BELL  	407   	407         		SW  										FLOAT	FRAYED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH					53266				END COVER FRAYED ON FLOAT COVER.  REFERENCE:  DMR NR 686358.						1	G	7	1 	3U			O	H2SW    					 
1999100800158	19991008	00158	SW  	1999	10	8	HEEA064494       	1	19990930	G	3212	206050247135	COVER ASSY      			BELL  	407   	407         		SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				END CAP WORN AND FRAYED ON FLOAT COVER.  REFERENCE:  DMR NR 686203.						1	G	7	1 	3U			O	H2SW    					 
1999100800159	19991008	00159	SW  	1999	10	8	HEEA064495       	1	19990930	G	3212	206050247135	COVER ASSY      			BELL  	407   	407         		SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				FLOAT COVER WORN.   REFERENCE:  DMR NR 686231.						1	G	7	1 	3U			O	H2SW    					 
1999100800160	19991008	00160	SW  	1999	10	8	HEEA064496       	1	19990930	G	3212	206050247135	COVER ASSY      			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				FLAPS TORN ON FLOAT COVER .  REFERENCE:  DMR NR 686409.						1	G	7	1 	3U			O	H2SW    					 
1999100800161	19991008	00161	SW  	1999	10	8	HEEA064497       	1	19991001	G	3212	212073905001	GAUGE           			BELL  	407   	407         		SW  										FLOAT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				PRESSURE GAUGE UNRELIABLE AND STICKING.  REFERENCE:  DMR NR 686296.						1	G	7	1 	3U			O	H2SW    					 
1999100800162	19991008	00162	SW  	1999	10	8	HEEA064498       	1	19991001	G	6210	407015001107	BLADE           			BELL  	407   	407         		SW  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416	3673 				53070				MAIN ROTOR BLADE CRACKED IN TRIM TAB AREA.   SERIAL NUMBERS REMOVED ARE A-145, A-442, A-330 AND A-437.  REFERENCE:  DMR 	NR 686520.  REPLACED WITH SERIAL NUMBERS A-1513, A-1519, A-645, AND A-858.					1	G	7	1 	3U			O	H2SW    					 
1999121100130	19991211	00130	GL  	1999	12	11	HEEA064646       	2	19991004	G	7250	6898764	SEAL            		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					MATING SURFACE	PITTED          	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	86CH				CAT25163	S557	CAE834061			RECEIVING INSPECTION REVEALED PITTED AND SCRATCHED SEAL FACE.  INSTALLED NEW PART.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100131	19991211	00131	GL  	1999	12	11	HEEA064647       	2	19991004	G	7250	23007202	BEARING         		6898735     						ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	SCORED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03		28   			CAT33513		CAE836370			UPON INSPECTION OF PARTS,  FOUND SCORING AND FROSTING OF NR 6 AND NR 7 BEARING ROLLERS.  SERIAL NUMBERS REMOVED ARE MP44	273 AND MP44026.  INSTALLED NEW PARTS.										3	U			E4CE				 
1999121100211	19991211	00211	SW  	1999	12	11	HEEA064649       	1	19991004	G	3212	206050247135	FASTENER        			BELL  	407   	407         		SW  										FLOAT COVER	MISSING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH					53228				FLOAT COVER HAD MISSING SNAPS.						1	G	7	1 	3U			O	H2SW    					 
1999121100212	19991211	00212	SW  	1999	12	11	HEEA064650       	1	19991004	G	3212	206050247137	FASTENER        			BELL  	407   	407         		SW  										FLOAT COVER	MISSING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH					53228				FLOAT COVER HAD MISSING SNAPS.						1	G	7	1 	3U			O	H2SW    					 
1999121100213	19991211	00213	SW  	1999	12	11	HEEA064651       	1	19991004	G	3212	206050247137	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				FLOAT COVER TORN ON THE ENDS.						1	G	7	1 	3U			O	H2SW    					 
1999121100214	19991211	00214	SW  	1999	12	11	HEEA064652       	1	19991004	G	3212	206050247138	COVER           			BELL  	407   	407         		SW  										FLOAT	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				FLOAT COVER WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100215	19991211	00215	SW  	1999	12	11	HEEA064653       	1	19991004	G	6220	407310102101	BEARING         		407010100111	BELL  	407   	407         		SW  										MAIN ROTOR HUB	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH				A203	53199				SEPARATION BETWEEN LAMINATES.  SERIAL NUMBERS REMOVED ARE LK-3563, LK-3620 AND LK-3652.  REPLACED WITH SERIAL NUMBERS LK	-4728, LK-4757 AND LK-4692.					1	G	7	1 	3U			O	H2SW    					 
1999121100216	19991211	00216	SW  	1999	12	11	HEEA064654       	1	19991004	G	6220	407310102101	BEARING         		407010100111	BELL  	407   	407         		SW  										MAIN ROTOR HUB	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH				A203	53199				BEARING HAD SEPARATION BETWEEN LAMINATES.						1	G	7	1 	3U			O	H2SW    					 
1999121100217	19991211	00217	SW  	1999	12	11	HEEA064655       	1	19991004	G	6220	407310102101	BEARING         		407010100111	BELL  	407   	407         		SW  										MAIN ROTOR HUB	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH	1832 			A220	53188				BEARING SEPARATION.  SERIAL NUMBERS REMOVED ARE LK-3751, LK-3800, LK-3811 AND LK-3746.  REPLACED WITH SERIAL NUMBERS LK-	4768, LK-4833, LK-4382 AND LK-4709.					1	G	7	1 	3U			O	H2SW    					 
1999121100218	19991211	00218	SW  	1999	12	11	HEEA064656       	1	19991004	G	6220	407010107103	SEAT            			BELL  	407   	407         		SW  										MAIN ROTOR	FLAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	1260 				53159				BLUE EPOXY COATING FLAKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100219	19991211	00219	SW  	1999	12	11	HEEA064657       	1	19991004	G	6230	406010126107	DRIVE RING      			BELL  	407   	407         		SW  										MAIN ROTOR	FLAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	2492 				53159				BLUE EPOXY COATING FLAKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100220	19991211	00220	SW  	1999	12	11	HEEA064658       	1	19991004	G	6520	406040072105	ADAPTER         			BELL  	407   	407         		SW  										T/R SPLINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH					53266				SPLINES WORN CONSIDERABLY ON THE TRANSMISSION OIL PUMP SIDE.						1	G	7	1 	3U			O	H2SW    					 
1999121100221	19991211	00221	SW  	1999	12	11	HEEA064659       	1	19991004	G	6321	406010429101	PIN             			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				WORN, PLAY IN DRIVE LINK.						1	G	7	1 	3U			O	H2SW    					 
1999121100222	19991211	00222	SW  	1999	12	11	HEEA064660       	1	19991004	G	6321	406010429101	PIN             			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				PLAY BETWEEN HUB SET AND PIN.						1	G	7	1 	3U			O	H2SW    					 
1999121100225	19991211	00225	SW  	1999	12	11	HEEA064663       	1	19991004	G	6220	407310102101	BEARING         			BELL  	407   	407         		SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH	2408 				53038				BEARING HAD SEPARATED RUBBER.  SERIAL NUMBERS REMOVED ARE LK-2808, LK-2857, LK-2823, AND LK-2570.   REPLACED WITH SERIAL	 NUMBERS LK-4872, LK-4881, LK-4862 AND LK-4829.					1	G	7	1 	3U			O	H2SW    					 
1999121100226	19991211	00226	SW  	1999	12	11	HEEA064664       	1	19991004	G	6220	407010105101	STUD            			BELL  	407   	407         		SW  										DROOP STOP	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				DROOP STOP HAD INDICATION OF CRACKS.						1	G	7	1 	3U			O	H2SW    					 
1999121100227	19991211	00227	SW  	1999	12	11	HEEA064665       	1	19991004	G	6220	407010105101	STUD            			BELL  	407   	407         		SW  										DROOP STOP	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH	2408 				53038				DROOP STOP CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100228	19991211	00228	SW  	1999	12	11	HEEA064666       	1	19991005	G	6710	407001526105	BELLCRANK       			BELL  	407   	407         		SW  										MAIN ROTOR	UNBONDED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	2160 				53114				BELLCRANK UNBONDED.						1	G	7	1 	3U			O	H2SW    					 
1999121100229	19991211	00229	SW  	1999	12	11	HEEA064667       	1	19991005	G	6710	407001526105	BELLCRANK       			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	2546 				53159				BELLCRANK LOOSE AND WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100230	19991211	00230	SW  	1999	12	11	HEEA064668       	1	19991005	G	6520	406040072105	ADAPTER         			BELL  	407   	407         		SW  										T/R SPLINE	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				SPLINE DAMAGED.						1	G	7	1 	3U			O	H2SW    					 
1999121100231	19991211	00231	SW  	1999	12	11	HEEA064669       	1	19991005	G	3230	70079H100F210	HOSE            			BELL  	407   	407         		SW  										MLG	CHAFED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				HOSE ASSY CHAFED AND KINKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100232	19991211	00232	SW  	1999	12	11	HEEA064670       	1	19991005	G	6510	406040339111	BEARING         		407040302103	BELL  	407   	407         		SW  										T/R DRIVE SHAFT	ROUGH           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416	662  			A974	53070				BEARING ROUGH.						1	G	7	1 	3U			O	H2SW    					 
1999121100233	19991211	00233	SW  	1999	12	11	HEEA064671       	1	19991005	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416	1205 				53070				BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100234	19991211	00234	SW  	1999	12	11	HEEA064672       	1	19991005	G	6230	406010428109	HUB SET         			BELL  	407   	407         		SW  										MAIN ROTOR HUB	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH	103  				53142				PIN SLOTS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100235	19991211	00235	SW  	1999	12	11	HEEA064675       	1	19991005	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH	1269 				53003				WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999121100236	19991211	00236	SW  	1999	12	11	HEEA064676       	1	19991005	G	6510	407340340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				DISC PACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100237	19991211	00237	SW  	1999	12	11	HEEA064677       	1	19991005	G	6320	406040055105	HOUSING         			BELL  	407   	407         		SW  										M/R GEARBOX	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH					53266				HOUSING ASSY CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100238	19991211	00238	SW  	1999	12	11	HEEA064678       	1	19991005	G	7120	407060111101	BIPOD MOUNT     			BELL  	407   	407         		SW  										ENGINE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	612PH					53199				MOUNT WILL NOT FIT ON AFT ENGINE MOUNT SUPPORT WITH LIP FROM BUSHING.						1	G	7	1 	3U			O	H2SW    					 
1999121100239	19991211	00239	SW  	1999	12	11	HEEA064679       	1	19991005	G	6320	206040156001	SEAL            			BELL  	407   	407         		SW  										M/R GEARBOX	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	467PH					53142				SEAL ASSY LEAKING BETWEEN CARBON RING AND MATING SURFACE.						1	G	7	1 	3U			O	H2SW    					 
1999121100240	19991211	00240	SW  	1999	12	11	HEEA064680       	1	19991005	G	6320	206040156001	SEAL            			BELL  	407   	407         		SW  										M/R GEARBOX	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	407MM					53060				SEAL LEAKING.  PART WAS SCRAPPED ON SITE.						1	G	7	1 	3U			O	H2SW    					 
1999121100241	19991211	00241	SW  	1999	12	11	HEEA064681       	1	19991005	G	6300	407340339103	BEARING         		PHIPBH40701 	BELL  	407   	407         		SW  										MAIN ROTOR	ROUGH           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM				AFS1049	53060				BEARINGS ROUGH.  SERIAL NUMBERS REMOVED ARE J98-0270 AND J98-0280.  REPLACED WITH SERIAL NUMBERS E99-0669 AND F99-1670.						1	G	7	1 	3U			O	H2SW    					 
1999121100242	19991211	00242	GL  	1999	12	11	HEEA064682       	2	19991005	G	7261	204040760109	FILTER          			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE OIL	CONTAMINATED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				METAL IN OIL.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999121100243	19991211	00243	SW  	1999	12	11	HEEA064683       	1	19991005	G	6510	206061432116	HOUSING         			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH					53209				BLOWER HOUSING CRACKED, WORKING RIVETS.						1	G	7	1 	3U			O	H2SW    					 
1999121100244	19991211	00244	SW  	1999	12	11	HEEA064684       	1	19991005	G	6420	406312100101	BEARING         		407012101111	BELL  	407   	407         		SW  										TAIL ROTOR HEAD	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	1206 			53311	53159				WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999121100245	19991211	00245	SW  	1999	12	11	HEEA064685       	1	19991006	G	6220	407001528101	PAD             			BELL  	407   	407         		SW  										M/R BELLCRANK	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	2546 				53159				BELLCRANK HAD LOOSE WEAR PAD.						1	G	7	1 	3U			O	H2SW    					 
1999121100246	19991211	00246	SW  	1999	12	11	HEEA064686       	1	19991006	G	6220	407001524105	PAD             			BELL  	407   	407         		SW  										M/R BELLCRANK	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	2546 				53159				BELLCRANK HAD LOOSE WEAR PAD.						1	G	7	1 	3U			O	H2SW    					 
1999121100247	19991211	00247	SW  	1999	12	11	HEEA064688       	1	19991006	G	2820	407076011101	LINE            			BELL  	407   	407         		SW  										FUEL SYSTEM	CHAFED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				LINE CHAFED DUE TO ID TAG.						1	G	7	1 	3U			O	H2SW    					 
1999121100248	19991211	00248	SW  	1999	12	11	HEEA064689       	1	19991006	G	2820	407076010101	LINE            			BELL  	407   	407         		SW  										FUEL SYSTEM	CHAFED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				LINE CHAFED DUE TO ID TAG.						1	G	7	1 	3U			O	H2SW    					 
1999121100249	19991211	00249	SW  	1999	12	11	HEEA064690       	1	19991006	G	6320	407040006107	TRANSMISSION    			BELL  	407   	407         		SW  										M/R GEARBOX	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH	2057 				53207				TRANSMISSION ASSY MAKING METAL.						1	G	7	1 	3U			O	H2SW    					 
1999121100250	19991211	00250	SW  	1999	12	11	HEEA064691       	1	19991007	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999121100251	19991211	00251	SW  	1999	12	11	HEEA064692       	1	19991007	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				WORN BEARINGS.  SERIAL NUMBERS REMOVED ARE NHFS-3228 AND NHFS-3200.  REPLACED WITH SERIAL NUMBERS NHFS-4376 AND NHFS-442	3.					1	G	7	1 	3U			O	H2SW    					 
1999121100252	19991211	00252	SW  	1999	12	11	HEEA064693       	1	19991007	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				WORN BEARINGS.   REPLACED WITH SERIAL NUMBERS NHFS-4302 AND NHFS-4407.						1	G	7	1 	3U			O	H2SW    					 
1999121100253	19991211	00253	SW  	1999	12	11	HEEA064694       	1	19991007	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				WORN BEARINGS.  SERIAL NUMBERS REMOVED ARE NHFS-3740 AND NHFS-3707.  REPLACED WITH SERIAL NUMBERS NHFS-4344 AND NHFS-429	0.					1	G	7	1 	3U			O	H2SW    					 
1999121100254	19991211	00254	SW  	1999	12	11	HEEA064695       	1	19991007	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH					53207				WORN BEARINGS.  SERIAL NUMBERS REMOVED ARE NHFS-3776 AND NHFS-3336.  REPLACED WITH SERIAL NUMBERS NHFS-4535 AND NHFS-443	4.					1	G	7	1 	3U			O	H2SW    					 
1999121100255	19991211	00255	SW  	1999	12	11	HEEA064696       	1	19991007	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999121100256	19991211	00256	SW  	1999	12	11	HEEA064697       	1	19991007	G	6710	065001650100	PITCH CONTROL   			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RC	530  				23037				BRAKE WILL NOT ENGAGE WHEN AUTOPILOT IS TURNED OFF, BUT WILL ENGAGE WHEN TAPPED ON.						1	G	7	2 	3U			NC	H9SW    					 
1999121100257	19991211	00257	SW  	1999	12	11	HEEA064698       	1	19991008	G	3210	70079H000Y150	HOSE            			BELL  	407   	407         		SW  										MLG	KINKED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				HOSE ASSY KINKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100258	19991211	00258	SW  	1999	12	11	HEEA064699       	1	19991008	G	2840	407362005103	SWITCH          			BELL  	407   	407         		SW  										FUEL SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH					53228				SWITCH LOW LEVEL, FUEL.						1	G	7	1 	3U			O	H2SW    					 
1999121100259	19991211	00259	GL  	1999	12	11	HEEA064700       	2	19991008	G	7270	AAB060RVP1Y1	INDICATOR       			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE BYPASS	WEAK            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				BYPASS VALVE INDICATOR BUTTON WEAK.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999121100260	19991211	00260	SW  	1999	12	11	HEEA064701       	1	19991008	G	6320	406340100101	PUMP            			BELL  	407   	407         		SW  										TRANSMISSION OIL	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				TRANSMISSION OIL PUMP HAD SPLINE DAMAGE.						1	G	7	1 	3U			O	H2SW    					 
1999121100261	19991211	00261	SW  	1999	12	11	HEEA064702       	1	19991008	G	6320	406340100101	PUMP            			BELL  	407   	407         		SW  										TRANSMISSION OIL	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	720PH					53277				TRANSMISSION OIL PUMP LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100262	19991211	00262	SW  	1999	12	11	HEEA064703       	1	19991008	G	6320	406340100101	PUMP            			BELL  	407   	407         		SW  										TRANSMISSION OIL	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH					53266				TRANSMISSION OIL PUMP SPLINES WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100263	19991211	00263	SW  	1999	12	11	HEEA064704       	1	19991008	G	2420	SM20ACD300A21	RELAY           			BELL  	407   	407         		SW  										AC GENERATOR	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH					53209				RELAY STICKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100264	19991211	00264	SW  	1999	12	11	HEEA064705       	1	19991008	G	7921	407062021101	DUCT            			BELL  	407   	407         		SW  										OIL COOLER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				DUCT FOUND CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100265	19991211	00265	SW  	1999	12	11	HEEA064706       	1	19991008	G	3300	PM212302	SWITCH          			BELL  	407   	407         		SW  										LIGHTS	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				SWITCH HAD BROKEN CONTACT.						1	G	7	1 	3U			O	H2SW    					 
1999121100266	19991211	00266	SW  	1999	12	11	HEEA064707       	1	19991008	G	6300	407010206103B	BEARING         			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH	4288 				53003				BEARINGS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100267	19991211	00267	SW  	1999	12	11	HEEA064708       	1	19991008	G	6230	406010126107	DRIVE RING      			BELL  	407   	407         		SW  										MAIN ROTOR	FLAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				BLUE EPOXY MISSING.						1	G	7	1 	3U			O	H2SW    					 
1999121100268	19991211	00268	SW  	1999	12	11	HEEA064709       	1	19991008	G	6220	407310100103	DAMPER          			BELL  	407   	407         		SW  										MAIN ROTOR	SEPARATING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH	2408 				53038				DAMPENER SEPARATING.  SERIAL NUMBERS REMOVED ARE LK-3385, LK-3349, LK-3328 AND LK-3356.  REPLACED WITH SERIAL NUMBERS LK	-7359, LK-7386, LK-7430 AND LK-7402.					1	G	7	1 	3U			O	H2SW    					 
1999121100269	19991211	00269	SW  	1999	12	11	HEEA064710       	1	19991008	G	6710	406010413117	BEARING         			BELL  	407   	407         		SW  										M/R PITCH LINK	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				PITCH LINK REMOVED, P/N 406-310-405-101, S/N RXFS-4567, TT 174:35 HOURS, DUE TO BEING WORN.  BELL WAS UNABLE TO SUPPLY T	RUNNION BEARINGS P/N 406-310-405-101, SO PHI ORDERED THE PITCH LINK ASSY P/N 406-010-413-117 INSTEAD.  PHI THEN ROBBED T	HE SERVICEABLE BEARINGS RXFS-4421 OFF THE SERVICEABLE PITCH LINK.  THE UNSERVICEABLE BEARING RXFS-4567 WAS INSTALLED ON 	THE SERVICEABLE LINK ASSY, WHICH NOW RENDERS THE LINK ASSY UNSERVICEABLE.			1	G	7	1 	3U			O	H2SW    					 
1999121100270	19991211	00270	SW  	1999	12	11	HEEA064712       	1	19991008	G	6220	407310100103	DAMPER          			BELL  	407   	407         		SW  										MAIN ROTOR	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH	1832 				53188				DAMPENER HAD RUBBER SEPARATION.  SERIAL NUMBERS REMOVED ARE LK-5791, LK-5801, LK-5793 AND LK-5826.  REPLACED WITH SERIAL	 NUMBERS LK-7331, LK-7357, LK-7324 AND LK-7326.					1	G	7	1 	3U			O	H2SW    					 
1999121100271	19991211	00271	SW  	1999	12	11	HEEA064713       	1	19991008	G	6320	412040111105	SEAL            			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										CRACKED SEAL.						1	G	7	2 	4U				H4SW    					 
1999121100272	19991211	00272	SW  	1999	12	11	HEEA064714       	1	19991011	G	3212	206050247138	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				FLOAT COVER ENDS TORN AND UNSEWED.						1	G	7	1 	3U			O	H2SW    					 
1999121100273	19991211	00273	SW  	1999	12	11	HEEA064715       	1	19991011	G	6710	406010421103	SPACER          			BELL  	407   	407         		SW  										CYCLIC	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				LINK BEARINGS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100274	19991211	00274		1999	12	11	HEEA064716       	4	19991012	G	2312	064105430	TRANSCEIVER     			BELL  	407   	407         		SW  										VHF COMM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	723PH					53283				TRANSCEIVER LOST POWER IN-FLIGHT AND BECAME VERY HOT WHEN UNIT CAME BACK ON-LINE.  PERFORMED PRELIMINARY INSPECTION AND 	FOUND UNIT DRAWING EXCESSIVE CURRENT AND NO DISPLAY.  FOUND Q507 VERY HOT.  REPLACED Q507.  CURRENT DRAW WAS LESS BUT ST	ILL HIGH.  REPLACED T501, Q505, AND Q506.  NOT REPAIRED.				1	G	7	1 	3U			O	H2SW    					 
1999121100275	19991211	00275	GL  	1999	12	11	HEEA064717       	2	19991012	G	7314	3881005	PUMP            			BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					FUEL SYSTEM	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8594X	13124				51531				FUEL PUMP HAD WORN DRIVE SPLINES.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999121100132	19991211	00132		1999	12	11	HEEA064718       	4	19991012	G	2215	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3122G	4691 				760232				ACTUATOR STICKS AND WILL NOT MOVE SOME TIMES.  INSPECTED BY ACCESSORY SHOP AND FOUND MOTOR HAS INTERMITTENT OPERATION.						1	G	7	2 	3U				H1NE    					 
1999121100571	19991211	00571		1999	12	11	HEEA064719       	4	19991012	G	3444	066304401	INDICATOR       			BOLKMS	117   	BK117B2     	5626013	EU  										COCKPIT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	136AE					7234				TWO YEAR INSPECTION DUE.  FOUND LOOSE SCREW IN UNIT.  TIGHTENED SCREW.  FOUND INTERMITTENT DH LIGHT SWITCH.  REPLACED DH	 LIGHT SWITCH.  TROUBLESHOT AND FOUND FLAG MECHANISM BROKEN.					1	G	7	2 	3U			NC	H13EU   					 
1999121100276	19991211	00276	SW  	1999	12	11	HEEA064720       	1	19991012	G	6720	214001540109	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										TAIL ROTOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				ACTUATOR ASSY WILL NOT ENGAGE IN PITCH.						2	G	7	2 	4U				H10SW   					 
1999121100277	19991211	00277	SW  	1999	12	11	HEEA064721       	1	19991012	G	6730	206076062003	CYLINDER        			BELL  	206   	206L3       	1182108	SW  										M/R SERVO	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8591X	18174				51495				STATIC LEAKING AT SERVO VALVE WITH ZERO PRESSURE AND BOOT DETERIORATED.						1	G	7	1 	3U				H2SW    					 
1999121100278	19991211	00278		1999	12	11	HEEA064722       	4	19991012	G	2312	064101900	TRANSCEIVER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	11027					45411				FREQUENCY SELECTON ERRATIC.  PERFORMED PRELIMINARY INSPECTION AND FOUND DISPLAY BAD.   REPAIRED.  UNIT ALSO HAD LOW POWE	R OUT.  REPLACED Q120, Q121, Q122.  SV ALIGNED AND ADJUSTED RECEIVER SECTION, CARRIER AND CARRIER/NOISE SQUELCH.  RECEIV	ER WILL NOT ALIGN TO SPECS.				1	G	7	1 	3U				H2SW    					 
1999121100133	19991211	00133		1999	12	11	HEEA064723       	4	19991012	G	2215	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	15460	9159 				760223				ACTUATOR'S NR 1 YAW NEEDLE STAYS RIGHT.  INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND POTENTIOMETERS ARE OUT OF CALIBR	ATION.					1	G	7	2 	3U				H1NE    					 
1999121100279	19991211	00279		1999	12	11	HEEA064724       	4	19991012	G	3457	0110005400	GPS             			BELL  	407   	407         		SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				FAILS TO ACQUIRE SIGNALS.						1	G	7	1 	3U			O	H2SW    					 
1999121100280	19991211	00280		1999	12	11	HEEA064725       	4	19991012	G	3457	0110005400	GPS             			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22425					45743				DOES NOT PICK UP SIGNALS.						1	G	7	1 	3U				H2SW    					 
1999121100281	19991211	00281		1999	12	11	HEEA064726       	4	19991012	G	3442	40016702501	RADAR UNIT      			BELL  	214   	214ST       	1182106	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				SEARCH 1 AND 2 RADAR SCREEN IS BLANK AND R/T FAULT ON SCREEN.						2	G	7	2 	4U				H10SW   					 
1999121100282	19991211	00282		1999	12	11	HEEA064727       	4	19991012	G	3452	6221270001	TRANSPONDER     			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCITONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1202T					33112				TRANSPONDER HAD WRONG FREQUENCIES SENT OUT.  PERFORMED PRELIMINARY INSPECTION AND FOUND LOW SENSITIVITY AND POWER OUT. A	DJUSTED HI/LO SENSITIVITY.  OUTPUT POWER WILL NOT ADJUST TO SPECS.					1	G	7	2 	4U				H4SW    					 
1999121100134	19991211	00134		1999	12	11	HEEA064728       	4	19991012	G	3457	8143902240B	GPS             			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4253S					760035				GPS INOPERATIVE.  WILL NOT TURN ON.  TIME SINCE REPAIR 28:30 HOURS.						1	G	7	2 	3U				H1NE    					 
1999121100283	19991211	00283	SW  	1999	12	11	HEEA064729       	1	19991012	G	7921	8543909	OIL COOLER      			BELL  	206   	206L3       	1182108	SW  										ENGINE OIL	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	31801					51074				TRANSITION DUCT WILL NOT ALIGN WITH HOLES ON COOLER MOUNTING FLANGE.  DUCT FITS TIGHT ON COOLER.   MOUNTING FLANGE ON CO	OLER MISLOCATED.					1	G	7	1 	3U				H2SW    					 
1999121100284	19991211	00284		1999	12	11	HEEA064730       	4	19991012	G	3457	0110005400	GPS             			BELL  	206   	206B3       	1181506	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	103PH					3000				WILL NOT LOCK ON.  FOUND DISPLAY LIGHT INOPERATIVE AND WILL NOT LOCK ON.						1	G	7	1 	3U				H2SW    					 
1999121100135	19991211	00135		1999	12	11	HEEA064731       	4	19991012	G	3457	8143902240B	GPS             			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4253S					760035				MESSAGE RECEIVER FAIL, BATTERY BACK UP FAIL .  FOUND UNIT DISPLAYS MESSAGE RECEIVER FAIL.						1	G	7	2 	3U				H1NE    					 
1999121100136	19991211	00136		1999	12	11	HEEA064732       	4	19991012	G	3454	6220876011	RECEIVER        			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT VOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1547D					760077				TO/FROM INDICATOR IN OBS INOPERATIVE.  PERFORMED PRELIMINARY INSPECTION AND FOUND VOR BEARINGS, LOC AND G/S CENTER OUT O	F SPECS.  ADJUST VOR BEARING AND LOC/GS CENTER.  UNIT STILL HAS A FEW VOR BEARINGS OUT OF SPECS.					1	G	7	2 	3U				H1NE    					 
1999121100572	19991211	00572	EU  	1999	12	11	HEEA064733       	1	19991012	G	6710	10541121	BELLCRANK       			BOLKMS	105   	BO105S      	5626006	EU  										FLIGHT CONTROL	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911FL					S717				T/R BELLCRANK CORRODED BEYOND LIMITS AFTER CLEAN-UP.  SCRAPPED BELLCRANK DUE TO DAMAGE BEYOND LIMITS.  REPLACED WITH SER	VICEABLE BELLCRANK.					1	G	7	2 	3U				H3EU    					 
1999121100573	19991211	00573	EU  	1999	12	11	HEEA064734       	1	19991012	G	6710	10541121	BELLCRANK       			BOLKMS	105   	BO105S      	5626006	EU  										FLIGHT CONTROL	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81992					S827				FOUND CORROSION BEYOND LIMITS ON BELLCRANK. SCRAPPED BELLCRANK AND REPLACED WITH SERVICEABLE BELLCRANK.						1	G	7	2 	3U				H3EU    					 
1999121100574	19991211	00574	EU  	1999	12	11	HEEA064735       	1	19991012	G	6510	11213152603	SHAFT           			BOLKMS	105   	BO105S      	5626006	EU  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3534T					S112				EXCESSIVE CORROSION BEYOND LIMITS ON DRIVESHAFT.  REPLACED WITH SERVICEABLE DRIVESHAFT.						1	G	7	2 	3U				H3EU    					 
1999121100575	19991211	00575	EU  	1999	12	11	HEEA064736       	1	19991012	G	6510	10531541	SHAFT           			BOLKMS	105   	BO105S      	5626006	EU  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3534T					S112				EXCESSIVE CORROSION BEYOND LIMITS ON SHAFT.  REPLACED WITH SERVICEABLE DRIVESHAFT.						1	G	7	2 	3U				H3EU    					 
1999121100576	19991211	00576	EU  	1999	12	11	HEEA064737       	1	19991012	G	6720	11788659	BEARING         			BOLKMS	117   	BK117B2     	5626013	EU  										T/R BELLCRANK	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	136AE					7234				BEARING CAME UNSTAKED AFTER ONE TEST FLIGHT.  REPLACED WITH SERVICEABLE BELLCRANK.						1	G	7	2 	3U			NC	H13EU   					 
1999121100285	19991211	00285	SW  	1999	12	11	HEEA064738       	1	19991012	G	3412	9210121	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893N					33010				WILL NOT TRANSMIT.   PERFORMED PRELIMINARY INSPECTION AND FOUND DISPLAY INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999121100577	19991211	00577		1999	12	11	HEEA064739       	4	19991012	G	2312	9210121	TRANSCEIVER     			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4034Q					2918				DOES NOT RECEIVE IN MAIN.						1	G	7	1 	3U				H9EU    					 
1999121100286	19991211	00286	SW  	1999	12	11	HEEA064740       	1	19991012	G	6730	206076062003	CYLINDER        			BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6603X					51412				SERVO LEAKING FROM FORWARD AND AFT SEALS.  REPAIRED  AND RETURNED TO SERVICE.						1	G	7	1 	3U				H2SW    					 
1999121100287	19991211	00287	SW  	1999	12	11	HEEA064741       	1	19991012	G	6720	206010361005	TUBE            			BELL  	206   	206L1       	1182107	SW  										M/R PITCH LINK	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5014Y					45219				MAIN ROTOR PITCH CHANGE LINK TUBE IS CORRODED AT LOWER END NEXT TO THREADED INSERT.  SCRAPPED AND REPLACED WITH SERVICEA	BLE TUBE ASSY.					1	G	7	1 	3U				H2SW    					 
1999121100288	19991211	00288		1999	12	11	HEEA064742       	4	19991012	G	3422	5050010902	GYRO            			BELL  	206   	206L3       	1182108	SW  										COCKPIT DG	PRECESSING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A					51611				WILL NOT HOLD HEADING. UNIT PRECESSES 3 DEGREES OUT OF TOLERANCE ON ALL HEADINGS.						1	G	7	1 	3U				H2SW    					 
1999121100289	19991211	00289		1999	12	11	HEEA064743       	4	19991012	G	3442	40005040301	DRIVE ASSY      			BELL  	214   	214ST       	1182106	SW  										WX RADAR	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				WILL NOT TILT UP.						2	G	7	2 	4U				H10SW   					 
1999121100290	19991211	00290		1999	12	11	HEEA064744       	4	19991012	G	3442	40016702513	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										RADAR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				INDICATOR HAD NO DISPLAY.						2	G	7	2 	4U				H10SW   					 
1999121100291	19991211	00291	SW  	1999	12	11	HEEA064745       	1	19991012	G	6700	212076151101	COLLECTIVE TUBE 			BELL  	412   	412         	1182202	SW  										FLIGHT CONTROL	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	3893N					33010				UPON INSTALLATION, UPPER INSERT FOUND TO BE INDEXED WRONG.						1	G	7	2 	4U				H4SW    					 
1999121100292	19991211	00292	SW  	1999	12	11	HEEA064746       	1	19991012	G	2434	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC GENERATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	142PH					33150				NO OUTPUT FROM GENERATOR.  1.5 VDC AT TEST POINTS AND CANNOT ADJUST AT ALL.						1	G	7	2 	4U				H4SW    					 
1999121100578	19991211	00578		1999	12	11	HEEA064747       	4	19991012	G	3457	0110005400	GPS             			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	81982					S818				WOULD NOT PICK UP SATELLITES						1	G	7	2 	3U				H3EU    					 
1999121100137	19991211	00137		1999	12	11	HEEA064748       	4	19991012	G	2312	4000106010	TRANSCEIVER     			SKRSKY	S76   	S76A        	8143006	NE  										COMMUNICATIONS	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911MJ					760231				ALL LED DIGITS OUT.  INTERMITTENT ONE LOWER SEGMENT OF THIRD DIGIT OUT ALL THE TIME.						1	G	7	2 	3U				H1NE    					 
1999121100138	19991211	00138	NE  	1999	12	11	HEEA064749       	1	19991013	G	3040	9000945	MOTOR           			SKRSKY	S76   	S76A        	8143006	NE  										WINDSHIELD WIPER	FAILED          	E			HEEA	K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			SW	03	31217					760229				WINDSHIELD WIPER MOTOR SMOKES AND WILL NOT OPERATE ON SLOW SPEED SETTING.						1	G	7	2 	3U				H1NE    					 
1999121100139	19991211	00139		1999	12	11	HEEA064750       	4	19991013	G	3416	066106103	INDICATOR       																	COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										RADAR ALTIMETER HAD NO SELF-TEST AND AFTER WARM-UP, UNIT QUIT TRANSMITTING.																			 
1999121100293	19991211	00293	SW  	1999	12	11	HEEA064751       	1	19991013	G	2435	23032048	GENERATOR       			BELL  	222   	222U        	1182140	SW  										STARTER/GEN	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6992					47521				STARTER/GENERATOR HAD LOW RESIDUAL VOLTAGE.  WOULD NOT COME ON-LINE UNTIL 80 PERCENT NG.						1	G	7	2 	3U				H9SW    					 
1999121100294	19991211	00294	SW  	1999	12	11	HEEA064752       	1	19991013	G	6710	206001144021	TUBE ASSY       			BELL  	206   	206L1       	1182107	SW  										CYCLIC JACKS	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	20898					45721				FOUND TUBE CORRODED AND DAMAGED BEYOND LIMITS.  REPLACED WITH SERVICEABLE TUBE ASSY.						1	G	7	1 	3U				H2SW    					 
1999121100295	19991211	00295	SW  	1999	12	11	HEEA064753       	1	19991013	G	3246	206323018	CROSSTUBE       			BELL  	206   	206L1       	1182107	SW  										SKID	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	20898					45721				FOUND AFT CROSSTUBE CORRODED BEYOND LIMITS.  REPLACED WITH SERVICEABLE TUBE ASSY.						1	G	7	1 	3U				H2SW    					 
1999121100296	19991211	00296	SW  	1999	12	11	HEEA064754       	1	19991013	G	3210	206053183103	RETAINER        			BELL  	206   	206L1       	1182107	SW  										MLG	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	20898					45721				CORRODED BEYOND LIMITS.  REPLACED WITH SERVICEABLE RETAINERS.						1	G	7	1 	3U				H2SW    					 
1999121100297	19991211	00297	SW  	1999	12	11	HEEA064755       	1	19991013	G	3201	206061613003	FITTING         			BELL  	206   	206L1       	1182107	SW  										MLG	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	20898					45721				FOUND FITTING CORRODED AND DAMAGED.  REPLACED WITH SERVICEABLE FITTING.						1	G	7	1 	3U				H2SW    					 
1999121100579	19991211	00579	EU  	1999	12	11	HEEA064756       	1	19991013	G	5302	1052180112	RING            			BOLKMS	105   	BO105S      	5626006	EU  										TAILBOOM	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3534T					S112				TAILBOOM RING ON FUSELAGE HAS A CRACK COMING FROM A RIVET HOLE.  REPLACED WITH SERVICEABLE TAILBOOM RING.						1	G	7	2 	3U				H3EU    					 
1999121100298	19991211	00298		1999	12	11	HEEA064757       	4	19991013	G	3457	0110005400	GPS             			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	979BH					51403				GPS SLOW TO COME ON AND LOSES ITSELF.						1	G	7	1 	3U				H2SW    					 
1999121100299	19991211	00299		1999	12	11	HEEA064758       	4	19991013	G	2312	063100700	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCITONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31801					51074				HF RADIO TRANSMITS AS SOON AS THE SYSTEM IS TURNED ON.						1	G	7	1 	3U				H2SW    					 
1999121100300	19991211	00300		1999	12	11	HEEA064759       	4	19991013	G	3453	066402600	LORAN           			BELL  	206   	206L3       	1182108	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	206LS					51070				LORAN SCREEN IS BLANK.  NO DISPLAY AND DATA BASE RACK CLIP BROKEN.						1	G	7	1 	3U				H2SW    					 
1999121100301	19991211	00301		1999	12	11	HEEA064760       	4	19991013	G	2310	071127401	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31801					51074				STORE BUTTON IS DEPRESSED IN CONTROL.						1	G	7	1 	3U				H2SW    					 
1999121100302	19991211	00302		1999	12	11	HEEA064761       	4	19991013	G	2310	071127401	TRANSCEIVER     			BELL  	206   	206L3       	1182108	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31821					51076				VOLUME KNOB INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999121100303	19991211	00303		1999	12	11	HEEA064762       	4	19991013	G	3457	13824120234	GPS RECEIVER    			BELL  	206   	206L3       	1182108	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	49EA					51507				RECEIVER INOPERATIVE.  SMALL INNER KNOB SKIPPING INTERMITTENTLY.						1	G	7	1 	3U				H2SW    					 
1999121100304	19991211	00304	SW  	1999	12	11	HEEA064763       	1	19991013	G	2435	200SGL132Q	STARTER         			BELL  	206   	206L1       	1182107	SW  										STARTER/GEN	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2245Y	12209				45751				STARTER/GENERATOR BURNED UP.  INSPECTED BY ACCESSORY SHOP AND FOUND COMMUTATOR AND BRUSHES BURNED AND PITTED.						1	G	7	1 	3U				H2SW    					 
1999121100305	19991211	00305	SW  	1999	12	11	HEEA064764       	1	19991013	G	6730	206076062003	CYLINDER        			BELL  	206   	206L3       	1182108	SW  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	141BH	3582 				51303				SERVO HAD EXCESSIVE INPUT FORCE AND INTERNAL LEAKAGE, LEAKING AT BOTH ENDS OF PISTON AND LEAKING AT SERVO VALVE.						1	G	7	1 	3U				H2SW    					 
1999121100306	19991211	00306	SW  	1999	12	11	HEEA064765       	1	19991013	G	2435	23032048	STARTER         			BELL  	206   	206B3       	1181506	SW  										STARTER/GEN	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2277A					3630				STARTER VIBRATED SCREWS LOOSE ON FAN SHROUD AND SHAFT NUT LOOSE TWO TIMES.   INSPECTED BY ACCESSORY SHOP AND FOUND NUT W	AS LOOSE CAUSING SHAFT TO WEAR FAN, DRIVESHAFT, AND ARMATURE SPLINES.  ALSO CAUSED CLUTCH DAMPNER HUB, PLATE AND FRICTIO	N RING TO WEAR.				1	G	7	1 	3U				H2SW    					 
1999121100307	19991211	00307		1999	12	11	HEEA064766       	4	19991013	G	3457	81439000232	GPS RECEIVER    			BELL  	206   	206L3       	1182108	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	515KA					51048				RECEIVER LOCKS UP WHEN FPL BUTTON IS PRESSED.						1	G	7	1 	3U				H2SW    					 
1999121100308	19991211	00308	SW  	1999	12	11	HEEA064767       	1	19991013	G	2435	23046020	GENERATOR       			BELL  	212   	212         	1181420	SW  										STARTER/GEN	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	27805	6516 				31106				STARTER/GENERATOR WILL NOT COME ON-LINE.  INSPECTED BY ACCESSORY SHOP AND FOUND STARTER/GENERATOR WOULD NOT COME ON-LINE	 AND SMELLED BURNT.					1	G	7	1 	4U				H4SW    					 
1999121100309	19991211	00309		1999	12	11	HEEA064768       	4	19991013	G	2200	2593996333	TARSYN 333      			BELL  	212   	212         	1181420	SW  										ADI	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	27805					31106				THE ATTITUDE FLAG ON THE ATTITUDE INDICATOR WILL NOT PULL.						1	G	7	1 	4U				H4SW    					 
1999121100310	19991211	00310		1999	12	11	HEEA064769       	4	19991013	G	2370	9806020023	CVR             			BELL  	212   	212         	1181420	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	27805	2695 				31106				SELF-TEST INOPERATIVE.						1	G	7	1 	4U				H4SW    					 
1999121100311	19991211	00311		1999	12	11	HEEA064770       	4	19991013	G	3441	066401018	RNAV            			BELL  	214   	214ST       	1182106	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				PHOTOCELL CAUSES DISPLAY TO FLICKER.  PERFORMED PRELIMINARY INSPECTION.  FOUND DISPLAY TO BE BAD, REPAIRED, ALIGNED CONV	ERTER CARD, FOUND UNIT IS NOT TRANSMITTING O.B.I. DATA TO KTS-143.   FOUND O.B.I. SYNC. LINE BAD.					2	G	7	2 	4U				H10SW   					 
1999121100312	19991211	00312	SW  	1999	12	11	HEEA064771       	1	19991013	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				WHILE PERFORMING 250 HOUR INSPECTION ON STARTER/GENERATOR FOUND TWO BRUSHES SHATTERED AND COMMUTATOR RUN OUT EXCEEDED TH	E TOTAL RUN OUT OF .0008.  CHECKS AT .0015.					2	G	7	2 	4U				H10SW   					 
1999121100313	19991211	00313		1999	12	11	HEEA064772       	4	19991013	G	2210	214074303115	AMPLIFIER ASSY  			BELL  	214   	214ST       	1182106	SW  										AUTOFLIGHT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				PITCH CHANNEL WILL NOT TRIM AFTER SYSTEM ALIGNMENT OR STAY ENGAGED.						2	G	7	2 	4U				H10SW   					 
1999121100314	19991211	00314		1999	12	11	HEEA064773       	4	19991013	G	2312	064102305	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCITONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2149S					36002				STATIC ON 123.05.  PERFORMED PRELIMINARY INSPECTION.   FOUND EXCESSIVE CORROSION ON CHASIS AND INSIDE COVERS.  CLEANED C	ORROSION.  ADJUSTED SIGNAL TO SQUELCH AND TRANSMIT POWER, ALSO ADJUSTED FREQUENCY.  NAMEPLATE IS UNREADABLE AND POWER OU	T WEAK.				1	G	7	2 	4U				H4SW    					 
1999121100315	19991211	00315		1999	12	11	HEEA064774       	4	19991013	G	3451	066106901	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT DME	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	107X					33113				INDICATOR FLASHES AND BOTH SHUT OFF WHEN EITHER NAV SYSTEMS ARE TURNED ON.  PERFORMED PRELIMINARY INSPECTION.  FOUND 5 V	OLT DECAL MISSING AND DISPLAY DIGIT ON THE FAR LEFT OF DISPLAY TO CONSTANTLY FLICKER.  REPLACED 5 VOLT DECAL, SWAPPED DI	SPLAY BOARD, IC'S 901, 902, 903, 904, 908, AND 909.  NOT REPAIRED.				1	G	7	2 	4U				H4SW    					 
1999121100316	19991211	00316	SW  	1999	12	11	HEEA064775       	1	19991013	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z	12527				33077				THE OUTBOARD ABRASION STRIP HAS NUMEROUS PIN HOLES.						1	G	7	2 	4U				H4SW    					 
1999121100317	19991211	00317	SW  	1999	12	11	HEEA064776       	1	19991013	G	6210	412015300109	BLADE           			BELL  	412   	412         	1182202	SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023	8721 				33080				EROSION SHIELD TORN ON THE INBOARD END OF THE STRIP. .						1	G	7	2 	4U				H4SW    					 
1999121100318	19991211	00318	SW  	1999	12	11	HEEA064777       	1	19991013	G	5210	AN74313	BRACKET         			BELL  	412   	412         	1182202	SW  										CREW DOOR	DAMAGED         	E			HEEA	O				OTHER                   				D			INFLIGHT SEPARATION       			NR	NOT REPORTED   	1			SW	03	2148K					36001				PILOT DOOR CAME OFF IN-FLIGHT.  AN UNEVENTFUL LANDING WAS MADE TO AN OFFSHORE PLATFORM.  MAINTENANCE FOUND HOLE IN THE B	RACKET THAT THE TENSION SPRING HOOKS TO HAD PULLED THROUGH, ALLOWING AIRCRAFT NATURAL FREQUENCIES TO WORK EMERGENCY EXIT	 PINS OUT OF THE DOOR HINGES, THUS RELEASING THE DOOR IN FLIGHT. REPLACED WITH SERVICEABLE BRACKET.				1	G	7	2 	4U				H4SW    					 
1999121100580	19991211	00580	EU  	1999	12	11	HEEA064778       	1	19991015	G	7714	614764021	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										ENGINE TACH	STICKING        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	40466					3004				NTL NEEDLE STUCK AT 300 ONE TIME.						1	G	7	1 	3U				H9EU    					 
1999121100581	19991211	00581	EU  	1999	12	11	HEEA064779       	1	19991015	G	7712	305731365	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										TORQUE	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				INDICATOR FLUCTUATES IN STEADY FLIGHT.						1	G	7	1 	3U				H9EU    					 
1999121100582	19991211	00582	EU  	1999	12	11	HEEA064780       	1	19991015	G	7722	56375600010	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	STICKIING       	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4000L					2873				INDICATOR NEEDLE STICKING ON SHUTDOWN.						1	G	7	1 	3U				H9EU    					 
1999121100583	19991211	00583	EU  	1999	12	11	HEEA064781       	1	19991015	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										T/R PITCH LINK	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				ROD, PITCH CONTROL HAD WORN BEARING.  SERIAL NUMBERS REMOVED ARE S3035 AND S2985.  REPLACED WITH SERIAL NUMBERS S3670 AN	D S3826.					1	G	7	1 	3U				H9EU    					 
1999121100319	19991211	00319	SW  	1999	12	11	HEEA064782       	1	19991015	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				STARTER DRAWING HIGH AMPERAGE.						2	G	7	2 	4U				H10SW   					 
1999121100320	19991211	00320	SW  	1999	12	11	HEEA064784       	1	19991015	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GEN	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	723PH	812  				53283				STARTER/GENERATOR FAILED 300 HOUR INSPECTION.   BRUSHES WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100321	19991211	00321	SW  	1999	12	11	HEEA064786       	1	19991015	G	7120	214060321101	MOUNT           			BELL  	214   	214ST       	1182106	SW  										ENGINE	MISMANUFACTURED 	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TUBE MOUNT ASSY MISMANUFACTURED.						2	G	7	2 	4U				H10SW   					 
1999121100140	19991211	00140	GL  	1999	12	11	HEEA064787       	2	19991015	G	7260	23038211	SEAL            		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					GEARBOX	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	133AE				CAT31355F	S800	CAE835714			ENGINE REMOVED DUE TO HIGH OIL CONSUMPTION, 5 QUARTS PER FLIGHT HOUR.  INSPECTION OF TURBINE PARTS REVEALED EXCESSIVELY 	GROOVED AND FLAKING INTERNAL SUMP SEALS.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100584	19991211	00584	EU  	1999	12	11	HEEA064788       	1	19991015	G	2435	150SG122Q	GENERATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										STARTER/GEN	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				STARTER/GENERATOR INTERMITTENT AND 500 HOUR INSPECTION.						1	G	7	1 	3U				H9EU    					 
1999121100585	19991211	00585	EU  	1999	12	11	HEEA064789       	1	19991015	G	6321	350A32050002	ROTOR           			SNIAS 	350   	AS350B2     	8680813	EU  										BRAKE ASSY	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6095S					2777				ROTOR WORN.						1	G	7	1 	3U				H9EU    					 
1999121100586	19991211	00586	EU  	1999	12	11	HEEA064790       	1	19991015	G	6321	350A32050002	ROTOR           			SNIAS 	350   	AS350B2     	8680813	EU  										BRAKE ASSY	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				DISK PAD WORN.						1	G	7	1 	3U				H9EU    					 
1999121100587	19991211	00587	EU  	1999	12	11	HEEA064791       	1	19991015	G	6420	350A33211905	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				TAIL ROTOR BEARING WORN.						1	G	7	1 	3U				H9EU    					 
1999121100588	19991211	00588	EU  	1999	12	11	HEEA064792       	1	19991015	G	2550	140277	HARNESS         			SNIAS 	350   	AS350B2     	8680813	EU  										CARGO HOOK	CORRODED        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	40466					3004				ELECTRICAL HARNESS CORRODED.  CARGO HOOK WOULD NOT ELECTRICALLY RELEASE AND BLEW FUSE.						1	G	7	1 	3U				H9EU    					 
1999121100589	19991211	00589		1999	12	11	HEEA064793       	4	19991015	G	3457	0110010600	GPS             			BOLKMS	117   	BK117B1     	5626012	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	217UC					7152				SLOW TO COME UP.						1	G	7	2 	3U				H13EU   					 
2000012100003	20000121	00003		2000	1	21	HEEA064794       	4	19991015	G	3450	066401018	RNAV            			BOLKMS	117   	BK117A4     	5626017	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911RZ					7092				LED BLINKS OUT AND LOSES MEMORY.						1	G	7	2 	3U				H13EU   					 
1999121100590	19991211	00590	EU  	1999	12	11	HEEA064795       	1	19991015	G	6500	10542321	TORSION BAR     			BOLKMS	105   	BO105S      	5626006	EU  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	81982					S818				FOUND 0.016 INCH MECHANIC DAMAGE ON TORSION BAR NEAR CENTER OF BAR.  MAXIMUM ALLOWABLE .015 INCH, AND FOUND DIAMETER AT 	END OF TUBE AT 24.83 MM.  MINIMUM ALLOWABLE DIAMETER 24.97 MM.  REPLACED WITH SERVICEABLE ASSY.					1	G	7	2 	3U				H3EU    					 
1999121100591	19991211	00591	EU  	1999	12	11	HEEA064796       	1	19991015	G	6500	1055000126	BEARING         			BOLKMS	105   	BO105S      	5626006	EU  										TAIL ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81982					S818				BEARING RING HAD CORROSION EXCEEDING .3 MM (.012 INCH).  SCRAPPED PART AND REPLACED WITH SERVICEABLE ASSY.						1	G	7	2 	3U				H3EU    					 
1999121100592	19991211	00592	EU  	1999	12	11	HEEA064797       	1	19991015	G	3201	10550301	CLAMP           			BOLKMS	105   	BO105S      	5626006	EU  										MLG	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81982					S818				CLAMP HAD RUST PITS BEYOND LIMITS.  SCRAPPED PART AND REPLACED WITH SERVICEABLE PART.						1	G	7	2 	3U				H3EU    					 
1999121100593	19991211	00593	EU  	1999	12	11	HEEA064798       	1	19991015	G	6210	10581013	BLADE           			BOLKMS	105   	BO105S      	5626006	EU  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81992	3057 				S827				THE NR 2 INBOARD ABRASION STRIP ON MAIN ROTOR BLADE HAD SEPARATION ON THE INBOARD END OF THE STRIP.						1	G	7	2 	3U				H3EU    					 
1999121100594	19991211	00594		1999	12	11	HEEA064799       	4	19991015	G	2312	40001452502	TRANSCEIVER     			BOLKMS	105   	BO105S      	5626006	EU  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	133AE					S800				NOT WORKING WHEN IN GUARD.						1	G	7	2 	3U				H3EU    					 
1999121100595	19991211	00595	EU  	1999	12	11	HEEA064800       	1	19991018	G	2911	350A75200005	ACCUMULATOR     			SNIAS 	350   	AS350B2     	8680813	EU  										HYD SYSTEM	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	4000L					2873				LEAKING ACCUMULATOR.						1	G	7	1 	3U				H9EU    					 
1999121100596	19991211	00596	EU  	1999	12	11	HEEA064801       	1	19991018	G	6730	AC67244	SERVO           			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4000L					2873				FEEDBACK IN THE CONTROLS.						1	G	7	1 	3U				H9EU    					 
1999121100322	19991211	00322	SW  	1999	12	11	HEEA064807       	1	19991019	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				STARTER BURNT AND DRAGGING.						2	G	7	2 	4U				H10SW   					 
1999121100597	19991211	00597	EU  	1999	12	11	HEEA064808       	1	19991019	G	7332	4021001	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										DUAL FUEL PRESS	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	81992					S827				NR 1 ENGINE FUEL PRESSURE READING ON NR 2 SIDE OF GAUGE.  NR 2 ENGINE FUEL PRESSURE READING ON NR 1 SIDE OF GAUGE.						1	G	7	2 	3U				H3EU    					 
1999121100598	19991211	00598	NE  	1999	12	11	HEEA064809       	2	19991019	G	7314	430137701	PUMP            			BOLKMS	117   	BK117B1     	5626012	EU  	LYC   	LTS101	LTS101750B1 	41560	NE  					FUEL SYSTEM	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	217UC					7152				FUEL PUMP HAD EXCESSIVE SEAL LEAKAGE.						1	G	7	2 	3U	3	U		H13EU   	E5NE10				 
1999121100141	19991211	00141		1999	12	11	HEEA064810       	4	19991019	G	3455	6222362001	RECEIVER        			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT ADF	WEAK            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1547D					760077				ADF RECEIVER VERY WEAK.						1	G	7	2 	3U				H1NE    					 
1999121100142	19991211	00142	NE  	1999	12	11	HEEA064811       	1	19991019	G	6210	7615009000049A	BLADE           			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	UNBONDED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	792CH	11831				760193				TOP SKIN UNBONDED APPROXIMATELY 58 INCHES SPANWISE BY 4.50 INCHES CHORDWISE.						1	G	7	2 	3U				H1NE    					 
1999121100323	19991211	00323	SW  	1999	12	11	HEEA064812       	1	19991019	G	6320	407040006107FM	TRANSMISSION    			BELL  	407   	407         		SW  										MAIN ROTOR	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH	2534 				53207				TRANSMISSION ASSY MAKING METAL.						1	G	7	1 	3U			O	H2SW    					 
1999121100324	19991211	00324	SW  	1999	12	11	HEEA064816       	1	19991019	G	7714	407375008101	INDICATOR       			BELL  	407   	407         		SW  										DUAL TACH	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				DUAL TACHOMETER HAD INTERMITTENT READINGS.						1	G	7	1 	3U			O	H2SW    					 
1999121100325	19991211	00325	SW  	1999	12	11	HEEA064817       	1	19991019	G	2841	407375006101	INDICATOR       			BELL  	407   	407         		SW  										FUEL QUANTITY	READS LOW       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				FUEL QUANTITY INDICATOR READS 140 POUNDS.  LOW, THEN 5 MINUTES LATER, JUMPS UP AND READS NORMAL.						1	G	7	1 	3U			O	H2SW    					 
1999121100326	19991211	00326	SW  	1999	12	11	HEEA064818       	1	19991019	G	6220	407010150105A	FRAHM ASSY      			BELL  	407   	407         		SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				FRAM ASSY HAD BROKEN SPRING.						1	G	7	1 	3U			O	H2SW    					 
1999121100327	19991211	00327	SW  	1999	12	11	HEEA064819       	1	19991019	G	6220	407010150105A	FRAHM ASSY      			BELL  	407   	407         		SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH					53003				FRAM ASSY HAD BROKEN SPRING.						1	G	7	1 	3U			O	H2SW    					 
1999121100328	19991211	00328	SW  	1999	12	11	HEEA064823       	1	19991019	G	7712	407375003107	INDICATOR       			BELL  	407   	407         		SW  										TORQUE	FAULTY          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				SEGMENT LIGHTS INOPERABLE.						1	G	7	1 	3U			O	H2SW    					 
1999121100143	19991211	00143		1999	12	11	HEEA064825       	4	19991019	G	2215	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	KICKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	707AE	7378 				760276				ACTUATOR KICKS IN-FLIGHT.						1	G	7	2 	3U				H1NE    					 
1999121100144	19991211	00144		1999	12	11	HEEA064826       	4	19991019	G	2215	7690001802106	ACTUATOR        			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	CHATTERS        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122G					760232				ACTUATOR KICKS AND CHATTERS.  INSPECTED BY ACCESSORY SHOP AND FOUND POTENTIOMETERS CHECKED BAD ON STRIP CHART.						1	G	7	2 	3U				H1NE    					 
1999121100145	19991211	00145		1999	12	11	HEEA064827       	4	19991019	G	2340	AA25004	AUDIO CONTROL   			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31219					760230				AUDIO CONTROL HAD WEAK AND BROKEN TRANSMIT AND RECEIVE.						1	G	7	2 	3U				H1NE    					 
1999121100329	19991211	00329	SW  	1999	12	11	HEEA064828       	1	19991019	G	7714	412075010111	CONNECTOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	BENT            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ROTOR CONNECTION BENT-CANNON PLUG CANNOT MATE AND LOCK.						1	G	7	2 	4U				H4SW    					 
1999121100330	19991211	00330		1999	12	11	HEEA064829       	4	19991019	G	3452	066106200	TRANSPONDER     			BELL  	222   	222U        	1182140	SW  										ATC	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6992					47521				ATC NOT ABLE TO PICK UP OVER 10 MILES OUT.						1	G	7	2 	3U				H9SW    					 
1999121100331	19991211	00331	SW  	1999	12	11	HEEA064832       	1	19991019	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GEN	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	1865 				53114				STARTER/GENERATOR FAILED 300 HOUR INSPECTION.  FOUND BRUSHES WERE EXCESSIVELY WORN, COMMUTATOR WAS BURNT, PITTED AND SHO	RTED TO GROUND.					1	G	7	1 	3U			O	H2SW    					 
1999121100332	19991211	00332	SW  	1999	12	11	HEEA064834       	1	19991019	G	6322	PHIPBH40701	BLOWER          			BELL  	407   	407         		SW  										OIL COOLER	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				SPLINE WORN ON SHAFT.  SCRAPPED.						1	G	7	1 	3U			O	H2SW    					 
1999121100599	19991211	00599	EU  	1999	12	11	HEEA064837       	1	19991019	G	6320	4638001004	TRANSMISSION    			BOLKMS	105   	BO105S      	5626006	EU  										MAIN ROTOR	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	818SH	7255 				S753				TRANSMISSION MAKING METAL.						1	G	7	2 	3U				H3EU    					 
1999121100333	19991211	00333	SW  	1999	12	11	HEEA064838       	1	19991019	G	3212	206373901103	SOLENOID VALVE  			BELL  	407   	407         		SW  										FLOAT	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				SOLENOID VALVE WOULD NOT SEAT.						1	G	7	1 	3U			O	H2SW    					 
1999121100334	19991211	00334	SW  	1999	12	11	HEEA064839       	1	19991019	G	2913	206076030111	PUMP            			BELL  	407   	407         		SW  										HYD SYSTEM	FAILED          	E			HEEA	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SW	03	721PH					53278				LOSS OF HYDRAULIC PRESSURE.						1	G	7	1 	3U			O	H2SW    					 
1999121100335	19991211	00335	SW  	1999	12	11	HEEA064840       	1	19991019	G	2913	206076030111	PUMP            			BELL  	407   	407         		SW  										HYD SYSTEM	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	417PH					53038				PUMP LEAKS AT SEAL DRAIN.						1	G	7	1 	3U			O	H2SW    					 
1999121100336	19991211	00336	SW  	1999	12	11	HEEA064841       	1	19991019	G	6230	406010425107	LEVER ASSY      			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH	1331 				53038				LEVER ASSY HAD WORN BUSHINGS.  SERIAL NUMBERS REMOVED ARE A-2087 AND A-2093.  REPLACED WITH SERIAL NUMBERS A-2618 AND A-	2616.					1	G	7	1 	3U			O	H2SW    					 
1999121100337	19991211	00337	SW  	1999	12	11	HEEA064842       	1	19991019	G	6300	407010206103	BEARING         			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH	2499 				53038				WORN BEARINGS.  SERIAL NUMBERS REMOVED ARE LK-0224 AND LK-0182.  REPLACED WITH SERIAL NUMBERS SR-9125 AND SR-8950.						1	G	7	1 	3U			O	H2SW    					 
1999121100338	19991211	00338	SW  	1999	12	11	HEEA064843       	1	19991019	G	6520	406040072105	SPLINE ADAPTER  			BELL  	407   	407         		SW  										TAIL ROTOR	STRIPPED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH					53278				SPLINE STRIPPED.						1	G	7	1 	3U			O	H2SW    					 
1999121100339	19991211	00339	SW  	1999	12	11	HEEA064846       	1	19991019	G	6300	407340339103	BEARING         		PHIPBH40701 	BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH				AFS1193	53114				WORN BEARINGS.  SERIAL NUMBERS REMOVED ARE H98-2271 AND H98-2327.  REPLACED WITH SERIAL NUMBERS E99-0767 AND F99-1678.						1	G	7	1 	3U			O	H2SW    					 
1999121100340	19991211	00340	SW  	1999	12	11	HEEA064847       	1	19991019	G	7120	407060111101	BIPOD MOUNT     			BELL  	407   	407         		SW  										ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				BIPOD MOUND HAD WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999121100341	19991211	00341	SW  	1999	12	11	HEEA064848       	1	19991019	G	7120	407060111101	BIPOD MOUNT     			BELL  	407   	407         		SW  										ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				BIPOD MOUNT HAD LEFT LOWER BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100342	19991211	00342	SW  	1999	12	11	HEEA064849       	1	19991019	G	7120	407060111101	BIPOD MOUNT     			BELL  	407   	407         		SW  										ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				BIPOD MOUNT HAD WORN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999121100343	19991211	00343	SW  	1999	12	11	HEEA064850       	1	19991019	G	7120	407060111101	BIPOD MOUNT     			BELL  	407   	407         		SW  										ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	723PH					53283				BIPOD MOUNT HAD WORN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999121100344	19991211	00344	SW  	1999	12	11	HEEA064851       	1	19991019	G	6320	214040806003	PRESSURE SWITCH 			BELL  	407   	407         		SW  										M/R GEARBOX	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	721PH					53278				SWITCH WILL NOT TURN ON WITH NO PRESSURE.						1	G	7	1 	3U			O	H2SW    					 
1999121100345	19991211	00345	SW  	1999	12	11	HEEA064852       	1	19991019	G	6300	407010206103	BEARING         			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH	1757 				53228				ELASTOMER CONTAMINATED AND SWOLLEN, BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100346	19991211	00346	SW  	1999	12	11	HEEA064853       	1	19991019	G	3270	206020110103	TAIL SKID ASSY  			BELL  	407   	407         		SW  										MLG	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				TAIL SKID ASSY BROKEN.						1	G	7	1 	3U			O	H2SW    					 
1999121100347	19991211	00347	SW  	1999	12	11	HEEA064854       	1	19991019	G	3270	206020110103	TAIL SKID ASSY  			BELL  	407   	407         		SW  										MLG	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				TAIL SKID ASSY BROKEN AT BOLT HOLE.						1	G	7	1 	3U			O	H2SW    					 
1999121100348	19991211	00348	SW  	1999	12	11	HEEA064855       	1	19991019	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8595X	884  				53267				AXIAL PLAY IN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999121100349	19991211	00349	SW  	1999	12	11	HEEA064856       	1	19991019	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				BEARINGS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100350	19991211	00350	SW  	1999	12	11	HEEA064857       	1	19991019	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA	999  				53016				BEARINGS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100351	19991211	00351	SW  	1999	12	11	HEEA064858       	1	19991019	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH	1772 				53198				BEARINGS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100352	19991211	00352	SW  	1999	12	11	HEEA064859       	1	19991019	G	6322	206061432121	HOUSING         			BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				BLOWER HOUSING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100353	19991211	00353	SW  	1999	12	11	HEEA064860       	1	19991020	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH	1112 				53277				UNIVERSAL BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100354	19991211	00354	SW  	1999	12	11	HEEA064861       	1	19991020	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH	1112 				53277				UNIVERSAL BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100355	19991211	00355	SW  	1999	12	11	HEEA064862       	1	19991020	G	6322	206061432121	FASTENERS       			BELL  	407   	407         		SW  										BLOWER HOUSING	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				BLOWER HOUSING HAD WORKING AND LOOSE RIVETS.						1	G	7	1 	3U			O	H2SW    					 
1999121100356	19991211	00356	SW  	1999	12	11	HEEA064863       	1	19991020	G	3212	206050247132	FASTENERS       			BELL  	407   	407         		SW  										FLOAT COVER	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				FLOAT COVER SNAP NEEDS REPLACEMENT, END CAPS FRAYED.						1	G	7	1 	3U			O	H2SW    					 
1999121100357	19991211	00357	SW  	1999	12	11	HEEA064864       	1	19991020	G	3212	206050247138	COVER           			BELL  	407   	407         		SW  										FLOAT	DETERIORATED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				FLOAT COVER HAD LEFT INSIDE COVER DETERIORATED.						1	G	7	1 	3U			O	H2SW    					 
1999121100358	19991211	00358	SW  	1999	12	11	HEEA064865       	1	19991020	G	3212	206050247138	FASTENERS       			BELL  	407   	407         		SW  										FLOAT COVER	MISSING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH					53228				FLOAT COVER HAD MISSING SNAPS.						1	G	7	1 	3U			O	H2SW    					 
1999121100359	19991211	00359	SW  	1999	12	11	HEEA064866       	1	19991020	G	6220	407310102101	BEARING         			BELL  	407   	407         		SW  										M/R HUB	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH	2492 				53059				BEARING WORN.   SERIAL NUMBERS REMOVED ARE 2965, 2994, 2988 AND 3078.  REPLACED WITH SERIAL NUMBERS 4661, 4656, 4682 AND	 4755.					1	G	7	1 	3U			O	H2SW    					 
1999121100360	19991211	00360	SW  	1999	12	11	HEEA064867       	1	19991020	G	6220	406010107105	ADAPTER         			BELL  	407   	407         		SW  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH	2492 				53059				ADAPTER CRACKED.  SERIAL NUMBERS REMOVED ARE A-2652, A-2654, A-2653, AND A-2649.   REPLACED WITH SERIAL NUMBERS A-4318, 	A-4320, A-4352, AND A-4357.					1	G	7	1 	3U			O	H2SW    					 
1999121100361	19991211	00361	SW  	1999	12	11	HEEA064868       	1	19991020	G	6220	407010105101	STUD            			BELL  	407   	407         		SW  										DROOP STOP	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH	2492 				53059				DROOP STOP STUD CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100362	19991211	00362	SW  	1999	12	11	HEEA064870       	1	19991020	G	2810	F507ST	ID PLATE        			BELL  	407   	407         		SW  										FILLER CAP	MISSING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH					53228				MISSING ID PLATE.						1	G	7	1 	3U			O	H2SW    					 
1999121100363	19991211	00363	SW  	1999	12	11	HEEA064871       	1	19991020	G	3230	70079K000Z232	LINE            			BELL  	407   	407         		SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	510PH					53209				TUBE ASSY LEAKING FROM 90 DEGREE FITTING.						1	G	7	1 	3U			O	H2SW    					 
1999121100364	19991211	00364		1999	12	11	HEEA064872       	4	19991020	G	3120	M803B205VBATT	CLOCK           			BELL  	407   	407         		SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				CLOCK CORRODED, DOES NOT KEEP ACCURATE TIME OR TEMPERATURE.						1	G	7	1 	3U			O	H2SW    					 
1999121100365	19991211	00365	SW  	1999	12	11	HEEA064873       	1	19991020	G	6230	406010126107	DRIVE RING      			BELL  	407   	407         		SW  										MAIN ROTOR	FLAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				BLUE EPOXY COATING BEING CHIPPED OFF DRIVE RING SET.						1	G	7	1 	3U			O	H2SW    					 
1999121100366	19991211	00366	SW  	1999	12	11	HEEA064874       	1	19991020	G	6320	222375077113	TRANSMITTER     			BELL  	407   	407         		SW  										OIL PRESSURE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457PH					53147				TRANSMITTER HAD HIGH OIL PRESSURE INDICATION.						1	G	7	1 	3U			O	H2SW    					 
1999121100367	19991211	00367	SW  	1999	12	11	HEEA064875       	1	19991020	G	2822	407362013101	SWITCH          			BELL  	407   	407         		SW  										ENGINE	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				PRESSURE SWITCH STUCK OPEN.						1	G	7	1 	3U			O	H2SW    					 
1999121100368	19991211	00368	SW  	1999	12	11	HEEA064876       	1	19991020	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH					53209				LINK HAD WORN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999121100369	19991211	00369	SW  	1999	12	11	HEEA064877       	1	19991020	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH					53278				LINK HAD WORN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999121100370	19991211	00370	SW  	1999	12	11	HEEA064878       	1	19991020	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				LINK HAD WORN BEARING.  SERIAL NUMBERS REMOVED ARE NHFS-2980 AND NHFS-2547.  REPLACED WITH SERIAL NUMBERS NHFS-4509 AND 	NHFS-4458.					1	G	7	1 	3U			O	H2SW    					 
1999121100371	19991211	00371	SW  	1999	12	11	HEEA064879       	1	19991020	G	6720	406312103101	LINK            			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH					53038				LINK HAD WORN BEARING.  SERIAL NUMBERS REMOVED ARE NHFS-2167 AND NHFS-2104.  REPLACED WITH SERIAL NUMBERS NHFS-4522 AND 	NHFS-4419.					1	G	7	1 	3U			O	H2SW    					 
1999121100372	19991211	00372	SW  	1999	12	11	HEEA064880       	1	19991020	G	6300	407340339103	BEARING         		PHIPBH40701 	BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH				AFS1207	53207				BEARING WORN BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999121100373	19991211	00373	SW  	1999	12	11	HEEA064881       	1	19991020	G	6300	407340339103	BEARING         		PHIPBH40701 	BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH				AFS1207	53159				BEARING WORN BEYOND LIMITS.  SERIAL NUMBERS REMOVED ARE J98-1850 AND L98-0142.						1	G	7	1 	3U			O	H2SW    					 
1999121100374	19991211	00374	SW  	1999	12	11	HEEA064882       	1	19991020	G	6321	D01631	PAD ASSY        			BELL  	407   	407         		SW  										ROTOR BRAKE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				PAD ASSEMBLY WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100375	19991211	00375	SW  	1999	12	11	HEEA064883       	1	19991020	G	3212	212073905001	GAUGE           			BELL  	407   	407         		SW  										FLOAT	CONTAMINATED    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH					53198				PRESSURE GAUGE NEEDLE STICKS AND SAND IN GAUGE.						1	G	7	1 	3U			O	H2SW    					 
1999121100376	19991211	00376	SW  	1999	12	11	HEEA064884       	1	19991020	G	6322	406040320101	SHAFT           			BELL  	407   	407         		SW  										COOLER BLOWER	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				SHAFT ASSY SPLINES WORN BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999121100377	19991211	00377	SW  	1999	12	11	HEEA064885       	1	19991020	G	6322	406040320101	SHAFT           			BELL  	407   	407         		SW  										COOLER BLOWER	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH					53207				SHAFT ASSY SPLINES WORN BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999121100378	19991211	00378	SW  	1999	12	11	HEEA064886       	1	19991020	G	3212	206373901103	SOLENOID VALVE  			BELL  	407   	407         		SW  										FLOAT	FAILED          	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	612PH					53199				SOLENOID VALVE WILL NOT HOLD FLOAT BOTTLE PRESSURE.						1	G	7	1 	3U			O	H2SW    					 
1999121100379	19991211	00379	SW  	1999	12	11	HEEA064887       	1	19991020	G	3212	206373901103	SOLENOID VALVE  			BELL  	407   	407         		SW  										FLOAT	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457PH					53147				SOLENOID VALVE STUCK OPEN.						1	G	7	1 	3U			O	H2SW    					 
1999121100380	19991211	00380		1999	12	11	HEEA064888       	4	19991020	G	3424	206070274101	INDICATOR       			BELL  	407   	407         		SW  										TURN & SLIP	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				TURN AND SLIP INDICATOR INOPERATIVE.						1	G	7	1 	3U			O	H2SW    					 
1999121100381	19991211	00381	SW  	1999	12	11	HEEA064889       	1	19991020	G	6310	406040500123	FREEWHEEL UNIT  			BELL  	407   	407         		SW  										MAIN ROTOR	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	408PH	1842 				53228				FREEWHEEL UNIT LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100382	19991211	00382	SW  	1999	12	11	HEEA064890       	1	19991020	G	6410	406312100101	BEARING         		407012101111	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH	1418 			A301	53142				WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999121100383	19991211	00383	SW  	1999	12	11	HEEA064891       	1	19991020	G	7810	407062021101	DUCT            			BELL  	407   	407         		SW  										EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				DUCT FOUND CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100384	19991211	00384	SW  	1999	12	11	HEEA064892       	1	19991021	G	6310	406040543103	NUT             		406040500123	BELL  	407   	407         		SW  										XMSN COUPLING	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	402PH	532  			A4578	53159				HEAVY LEAKING.  PART SCRAPPED.						1	G	7	1 	3U			O	H2SW    					 
1999121100385	19991211	00385	SW  	1999	12	11	HEEA064893       	1	19991021	G	6300	406340102101	CARBON SEAL     		406040500123	BELL  	407   	407         		SW  										M/R DRIVE	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	402PH	532  			A4578	53159				CARBON SEAL HAD HEAVY LEAKING.  PART SCRAPPED.						1	G	7	1 	3U			O	H2SW    					 
1999121100386	19991211	00386	SW  	1999	12	11	HEEA064894       	1	19991021	G	6310	407340106101	SLEEVE          		406040500123	BELL  	407   	407         		SW  										FREEWHEEL UNIT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	402PH	532  			A4578	53159				HEAVY LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100387	19991211	00387	SW  	1999	12	11	HEEA064895       	1	19991021	G	6310	406340102101	CARBON SEAL     		406040500123	BELL  	407   	407         		SW  										XMSN COUPLING	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	447PH	788  			A3856	53114				CARBON SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100388	19991211	00388	SW  	1999	12	11	HEEA064896       	1	19991026	G	6730	214001970111	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										M/R CONTROL	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	8045T					28101				WILL NOT ALLOW THE ACTUATOR TO MONITOR TEST; BRAKE WOULD NOT RELEASE; LOUD GRINDING NOISE DURING OPERATION WAS HEARD FRO	M INTERNAL OF THE UNIT.					2	G	7	2 	4U				H10SW   					 
1999121100600	19991211	00600	EU  	1999	12	11	HEEA064898       	1	19991026	G	6520	350A33020005	GEARBOX         			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L	3140 				2873				TAIL ROTOR GEARBOX HAD WEAR ON OUTPUT SHAFT AND CHROME PEELING.						1	G	7	1 	3U				H9EU    					 
1999121100146	19991211	00146	EU  	1999	12	11	HEEA064899       	1	19991026	G	7920	0301047170	LINE            			SNIAS 	350   	AS350B2     	8680813	EU  										ENGINE OIL SYS	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	350BZ					2653				LUBRICATION PIPE LEAKING.						1	G	7	1 	3U				H9EU    					 
1999121100601	19991211	00601	EU  	1999	12	11	HEEA064900       	1	19991026	G	6420	350A33200405	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	40466					3004				BEARING FAILED TACTILE CHECK.						1	G	7	1 	3U				H9EU    					 
1999121100602	19991211	00602	EU  	1999	12	11	HEEA064901       	1	19991026	G	7712	305731365	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										TORQUE	STICKING        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	60951					2771				TORQUE INDICATOR NEEDLE STICKS.						1	G	7	1 	3U				H9EU    					 
1999121100603	19991211	00603	EU  	1999	12	11	HEEA064902       	1	19991026	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH LINK	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z					2820				ROD, PITCH CONTROL HAD WORN BEARING.						1	G	7	1 	3U				H9EU    					 
1999121100604	19991211	00604	EU  	1999	12	11	HEEA064903       	1	19991026	G	2550	340100003	PANEL           			SNIAS 	350   	AS350B2     	8680813	EU  										BAGGAGE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6095S					2777				PANEL HAD NUMEROUS CRACKS.						1	G	7	1 	3U				H9EU    					 
1999121100605	19991211	00605	EU  	1999	12	11	HEEA064904       	1	19991027	G	2821	BFS1551	FILTER          			SNIAS 	350   	AS350B2     	8680813	EU  										FUEL SYSTEM	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				FILTER BOWL STUCK; NOT ABLE TO UNSCREW.						1	G	7	1 	3U				H9EU    					 
1999121100389	19991211	00389	SW  	1999	12	11	HEEA064905       	1	19991028	G	2435	206062200113	STARTER         			BELL  	407   	407         		SW  										STARTER/GEN	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				STARTER/GENERATOR WILL NOT TURN OVER.  INSPECTED AND REPAIRED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES WERE EXCESSIV	ELY WORN.					1	G	7	1 	3U			O	H2SW    					 
1999121100147	19991211	00147	GL  	1999	12	11	HEEA064906       	2	19991028	G	7250	23062753	NOZZLE          		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911HM	528  			CAT25227	S683	CAE830473			ENGINE REMOVED DUE TO LOW POWER.  UPON INSPECTION OF TURBINE PARTS NOTED THE FOLLOWING:  CRACKED AND MISSING COATING OUT	 OF SERVICEABLE LIMITS ON NR 1 NOZZLE VANES.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100148	19991211	00148	GL  	1999	12	11	HEEA064907       	2	19991028	G	7250	23008054	NOZZLE          		23033185    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					TURBINE	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	513EH	612  			CAT70116	45421	CAE860213			ENGINE REMOVED DUE TO MAKING METAL AND LOW POWER.  UPON INSPECTION OF TURBINE PARTS NOTED:  CRACKED 1ST STAGE NOZZLE VAN	ES BEYOND SERVICEABLE LIMITS.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999121100149	19991211	00149	GL  	1999	12	11	HEEA064908       	2	19991028	G	7250	23062753	NOZZLE          		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911PF	523  			CAT33440	S718	CAE830389			ENGINE REMOVED DUE TO BLOWING OIL OUT OF EXHAUST STACK AND SMOKING BADLY.  INSPECTION OF TURBINE PARTS REVEALED CRACKED 	VANES.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100150	19991211	00150	GL  	1999	12	11	HEEA064909       	2	19991028	G	7250	23062750	NOZZLE SHIELD   		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	DETACHED        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911PF	523  			CAT33440	S718	CAE836389			ENGINE REMOVED DUE TO BLOWING OIL OUT OF EXHAUST STACK AND SMOKING BADLY.  TEARDOWN INSPECTION REVEALED NR 1 NOZZLE SHIE	LD DOME DETACHED, NR 8 BEARING AREA EXPOSED TO EXCESSIVE HEAT CAUSING COKING AND SCAVENGE PORT BLOCKAGE FORCING OIL ACRO	SS 35-37 SEAL AND OIL QUENCHING THE WHEELS.				1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100151	19991211	00151	GL  	1999	12	11	HEEA064910       	2	19991028	G	7250	6886407	NOZZLE SHIELD   		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	DETACHED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911PF	523  			CAT33440	S718	CAE836389			ENGINE REMOVED DUE TO BLOWING OIL OUT OF EXHAUST STACK AND SMOKING BADLY.  TEARDOWN INSPECTION REVEALED NR 1 NOZZLE SHIE	LD DOME DETACHED, NR 8 BEARING AREA EXPOSED TO EXCESSIVE HEAT CAUSING COKING AND SCAVENGE PORT BLOCKAGE FORCING OIL ACRO	SS 35-37 SEAL AND OIL QUENCHING THE WHEELS.				1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100152	19991211	00152	GL  	1999	12	11	HEEA064911       	2	19991028	G	7250	6898782	NOZZLE SHIELD   		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	DETACHED        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911PF	523  			CAT33440	S718	CAE836389			ENGINE REMOVED DUE TO BLOWING OIL OUT OF EXHAUST STACK AND SMOKING BADLY.  TEARDOWN INSPECTION REVEALED NR 1 NOZZLE SHIE	LD DOME DETACHED, NR 8 BEARING AREA EXPOSED TO EXCESSIVE HEAT CAUSING COKING AND SCAVENGE PORT BLOCKAGE FORCING OIL ACRO	SS 35-37 SEAL AND OIL QUENCHING THE WHEELS.				1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100390	19991211	00390		1999	12	11	HEEA064912       	1	19991029	G	7930	407375004101	INDICATOR       																	ENG OIL TEMP	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4999					53323				ENGINE OIL TEMPERATURE INTERMITTENTLY DROPS TO ZERO FOR OIL PRESSURE.																			 
1999121100391	19991211	00391	SW  	1999	12	11	HEEA064913       	1	19991029	G	6220	407010150105A	FRAHM ASSY      			BELL  	407   	407         		SW  										MAIN ROTOR	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				FRAM ASSY HAD TWO BROKEN SPRINGS.						1	G	7	1 	3U			O	H2SW    					 
1999121100392	19991211	00392	SW  	1999	12	11	HEEA064914       	1	19991029	G	6340	407375001105	INDICATOR       			BELL  	407   	407         		SW  										MGB TACH	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				MGT INDICATOR WILL NOT INDICATE.						1	G	7	1 	3U			O	H2SW    					 
1999121100153	19991211	00153	GL  	1999	12	11	HEEA064915       	2	19991101	G	7230	23064577	SCROLL          		23063379    	BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					COMPRESSOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407JR	1105 			CAC44420	53245	CAE847267			ENGINE REMOVED DUE TO F.O.D., LOUD NOISE.  SCROLL HAS INDICATIONS IN WELDS OF TURNING VANES.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999121100154	19991211	00154	GL  	1999	12	11	HEEA064916       	2	19991101	G	7230	23064577	VANE            		23063379    	BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					COMPRESSOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416				CAC44217	53070	CAE847084			SCROLL HAD CRACKED TURNING VANE.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999121100155	19991211	00155	GL  	1999	12	11	HEEA064917       	2	19991101	G	7250	6898784	ADAPTER         		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	MISMARKED       	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	133AE				CAT35404	S800	CAE835714			NEW PART RECEIVING INSPECTION REVEALED WRONG PART NUMBER ETCHED ON PART.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100156	19991211	00156	GL  	1999	12	11	HEEA064918       	2	19991101	G	7250	23008020	TIE BOLT        		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	133AE				CAT34269	S800	CAE833901			UPON INSPECTION OF NEW NEVER INSTALLED PART FREE LENGTH OVER BP SPECS ON TIEBOLT.  INSTALLED NEW PART.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100157	19991211	00157	GL  	1999	12	11	HEEA064919       	2	19991101	G	7250	23008020	TIE BOLT        		6898735     	BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	107PH				CAT31377F	2789	CAE834648			UPON INSPECTION OF NEW NEVER INSTALLED PART FREE LENGTH OVER BP SPECS ON TIEBOLT.  INSTALLED NEW PART.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999121100158	19991211	00158	GL  	1999	12	11	HEEA064920       	2	19991101	G	7230	23004513	CARBON SEAL     		6890550     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	LEAKING         	E			HEEA	K				NONE                    				K	L		FLUID LOSS                	NO TEST                   		IN	INSP/MAINT     	1			SW	03	3520T				CAC41624	S539	CAE834884			ASSEMBLY INSPECTION REVEALED CARBON SEAL LEAKED ON PRESSURE TEST.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100159	19991211	00159	GL  	1999	12	11	HEEA064921       	2	19991101	G	7230	23004513	CARBON SEAL     		23051643    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C28B     	03013	GL  					COMPRESSOR	LEAKING         	E			HEEA	K				NONE                    				K	L		FLUID LOSS                	NO TEST                   		IN	INSP/MAINT     	1			SW	03					CAC90178					INSTALLED NEW CARBON SEAL ASSY P/N 23004513, PERFORMED PRESSURE CHECK AND ASSEMBLY LEAKED.   INSTALLED SECOND NEW CARBON	 SEAL ASSY P/N 23004513 PERFORMED LEAK CHECK AND NO LEAKS NOTED.  REPLACED CARBON SEAL ASSY.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999121100393	19991211	00393	SW  	1999	12	11	HEEA064922       	1	19991102	G	6320	406340100101	PUMP            			BELL  	407   	407         		SW  										M/R GEARBOX	STRIPPED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH	1279 				53278				SPLINES TO ADAPTER SHAFT STRIPPED.						1	G	7	1 	3U			O	H2SW    					 
1999121100394	19991211	00394	SW  	1999	12	11	HEEA064923       	1	19991102	G	6322	206061432121	HOUSING         			BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				BLOWER HOUSING CRACKED AND RIVETS WORKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100395	19991211	00395	SW  	1999	12	11	HEEA064924       	1	19991102	G	7810	407062021101	DUCT            			BELL  	407   	407         		SW  										EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				DUCT FOUND CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100396	19991211	00396	SW  	1999	12	11	HEEA064925       	1	19991102	G	7810	407062021101	DUCT            			BELL  	407   	407         		SW  										EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				DUCT FOUND CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100397	19991211	00397	SW  	1999	12	11	HEEA064926       	1	19991102	G	6300	406012129101	LINK            			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH					53278				LINK ASSEMBLY HAD WORN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999121100398	19991211	00398		1999	12	11	HEEA064927       	1	19991102	G	6320	222375077113	TRANSMITTER     																	OIL PRESSURE	FLUCTUATING     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4999					53323				ENGINE OIL PRESSURE FLUCTUATES.																			 
1999121100399	19991211	00399	SW  	1999	12	11	HEEA064928       	1	19991102	G	6310	214040814105	SLEEVE          			BELL  	407   	407         		SW  										FREEWHEEL UNIT	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				SLEEVE FOUND GROOVED.						1	G	7	1 	3U			O	H2SW    					 
1999121100400	19991211	00400	SW  	1999	12	11	HEEA064929       	1	19991102	G	2822	407362013101	SWITCH          			BELL  	407   	407         		SW  										ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				PRESSURE SWITCH NORMALLY IS CLOSED (NOT CLOSED).						1	G	7	1 	3U			O	H2SW    					 
1999121100401	19991211	00401	SW  	1999	12	11	HEEA064930       	1	19991102	G	3212	212073905001	GAUGE           			BELL  	407   	407         		SW  										FLOAT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				PRESSURE GAUGE NEEDLE STICKS.						1	G	7	1 	3U			O	H2SW    					 
1999121100402	19991211	00402		1999	12	11	HEEA064931       	1	19991102	G	6420	406312100101	BEARING         		407012101111															TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4999	775  			53324	53323				WORN BEARINGS.																			 
1999121100404	19991211	00404	SW  	1999	12	11	HEEA064933       	1	19991102	G	6320	222060084101	SWITCH          			BELL  	407   	407         		SW  										M/R GEARBOX	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				PRESSURE SWITCH WILL NOT TURN ON LIGHT.						1	G	7	1 	3U			O	H2SW    					 
1999121100405	19991211	00405	SW  	1999	12	11	HEEA064934       	1	19991102	G	7120	407060111101	BIPOD MOUNT     			BELL  	407   	407         		SW  										ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				BIPOD MOUNT HAD WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999121100406	19991211	00406	SW  	1999	12	11	HEEA064935       	1	19991102	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH	184  				53003				UNIVERSAL BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100407	19991211	00407	SW  	1999	12	11	HEEA064936       	1	19991102	G	6510	407340340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724PH					53327				CRACKED DISC IN ASSY.  NR 7 DISC PACK.						1	G	7	1 	3U			O	H2SW    					 
1999121100408	19991211	00408	SW  	1999	12	11	HEEA064937       	1	19991102	G	6520	406040072105	ADAPTER         			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				SPLINES WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100409	19991211	00409	SW  	1999	12	11	HEEA064938       	1	19991102	G	6310	406340102101	CARBON SEAL     		406040500123	BELL  	407   	407         		SW  										XMSN COUPLING	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	437PH				A3392	53072				CARBON SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100410	19991211	00410	SW  	1999	12	11	HEEA064939       	1	19991102	G	6310	406340102101	CARBON SEAL     			BELL  	407   	407         		SW  										XMSN COUPLING	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	467PH					53142				CARBON SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100411	19991211	00411	SW  	1999	12	11	HEEA064942       	1	19991102	G	6310	214040841101	SEAL            			BELL  	407   	407         		SW  										FREEWHEEL UNIT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	724PH	493  				53327				SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100606	19991211	00606	EU  	1999	12	11	HEEA064943       	1	19991102	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH LINK	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350BZ					2653				ROD, PITCH CONTROL BEARING WORN BEYOND LIMITS.						1	G	7	1 	3U				H9EU    					 
1999121100607	19991211	00607	EU  	1999	12	11	HEEA064944       	1	19991102	G	6420	350A33200405	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951	720  				2771				WORN SLIDING BEARING.						1	G	7	1 	3U				H9EU    					 
1999121100608	19991211	00608	EU  	1999	12	11	HEEA064945       	1	19991102	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										PITCH LINK	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z					2820				ROD, PITCH CONTROL BEARING WORN.						1	G	7	1 	3U				H9EU    					 
1999121100609	19991211	00609	EU  	1999	12	11	HEEA064946       	1	19991102	G	2913	350A35013004	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										HYD PUMP	ROUGH           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				PULLEY BEARING ROUGH.						1	G	7	1 	3U				H9EU    					 
1999121100412	19991211	00412		1999	12	11	HEEA064947       	4	19991102	G	3424	206070274101	INDICATOR       			BELL  	407   	407         		SW  										TURN & SLIP	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				TURN & SLIP INDICATOR 1/2 BUBBLE OFF.						1	G	7	1 	3U			O	H2SW    					 
1999121100413	19991211	00413	SW  	1999	12	11	HEEA064948       	1	19991102	G	2842	2003600000103	TRANSMITTER     			BELL  	412   	412         	1182202	SW  										FUEL QUANTITY	FAULTY          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	142PH					33150				TRANSMITTER HAD FAULTY FUEL QUANTITY READINGS.						1	G	7	2 	4U				H4SW    					 
2000012100002	20000121	00002	GL  	2000	1	21	HEEA064949       	2	19991102	G	7321	2543734	FCU             		25490925    	BELL  	230   	230         	1182149	SW  	ALLSN 	250C  	250C30G2    	03013	GL  					NR 1 ENGINE	FAILED          	E			HEEA	A				UNSCHED LANDING         				R	J		PARTIAL RPM/PWR LOSS      	WARNING INDICATION        		CR	CRUISE         	1			SW	03	236X	454  			BR56555	23015	CAE898241			AT 5,500 FEET DURING CRUISE, NR 1 ENGINE DECELERATED TO 68 PERCENT N1.  RECOVERED AT 3,300 FEET, SLIGHT OSCILLATION ON L	ANDING.  INSP OF FUEL CONTROL FOUND CATASTROPHIC DRIVE BEARING FAILURE.  SPLIT UNIT AND DISCOVERED MAJOR DAMAGE TO INTER	NAL DRIVE BODY PARTS DUE TO FAILURE OF DRIVE BEARINGS.  PARTS THAT WERE DAMAGED ARE AS FOLLOWS:  SPEED BIAS LEVER, GOVER	NOR LEVER, LAMINATED SHIMS, DRIVE SHAFT CLIP, TEFLON TUBE, SPOOL BUSHING ASSY, FLYWEIGHTS 2 EACH, FLYWEIGHT PINS 2 EACH,	 TEFLON WASHERS 4 EACH, DRIVE BEARINGS 2 EACH, AND DRIVE BODY.  LEVER BEARINGS AND ROLLER BEARINGS NEED REPLACING DUE TO	 EXCESSIVE AMOUNT OF METAL CONTAMINATION IN DRIVE BODY.	1	G	7	2 	3U	3	U	NC	H9SW    	E1GL				 
1999121100414	19991211	00414	SW  	1999	12	11	HEEA064950       	1	19991103	G	2931	209070262111	INDICATOR       			BELL  	412   	412         	1182202	SW  										HYD PRESSURE	FLUCTUATED      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z					33077				PRESSURE INDICATOR PRESSURE SIDE FLUCTUATES.						1	G	7	2 	4U				H4SW    					 
1999121100610	19991211	00610	EU  	1999	12	11	HEEA064951       	1	19991104	G	6720	350A33200405	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				SLIDER AND BEARINGS WORN.						1	G	7	1 	3U				H9EU    					 
1999121100611	19991211	00611	EU  	1999	12	11	HEEA064952       	1	19991104	G	2823	857A1641	VALVE           			SNIAS 	350   	AS350B2     	8680813	EU  										FUEL SYSTEM	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4031L					2907				VALVE STUCK.						1	G	7	1 	3U				H9EU    					 
1999121100415	19991211	00415	SW  	1999	12	11	HEEA064954       	1	19991104	G	3212	407350302101	FLOAT           			BELL  	407   	407         		SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	437PH					53072				FLOAT BAG LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100416	19991211	00416	SW  	1999	12	11	HEEA064955       	1	19991104	G	6410	406312100101	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	723PH					53283				BEARINGS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100417	19991211	00417	SW  	1999	12	11	HEEA064956       	1	19991104	G	7810	407062021101	DUCT            			BELL  	407   	407         		SW  										EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				DUCT FOUND CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100418	19991211	00418	SW  	1999	12	11	HEEA064957       	1	19991104	G	6322	206061432121	HOUSING         			BELL  	407   	407         		SW  										COOLER BLOWER	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				RIVETS PULLED AND BROKEN OUT FROM METAL ON BLOWER HOUSING.						1	G	7	1 	3U			O	H2SW    					 
1999121100419	19991211	00419	SW  	1999	12	11	HEEA064958       	1	19991104	G	7810	407063001101	STACK           			BELL  	407   	407         		SW  										EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				EXHAUST STACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100420	19991211	00420	SW  	1999	12	11	HEEA064959       	1	19991105	G	7910	206061505115	TANK            			BELL  	407   	407         		SW  										ENGINE OIL	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	405PH					53207				TANK ASSY LEAKING AT DRAIN FITTING.						1	G	7	1 	3U			O	H2SW    					 
1999121100421	19991211	00421	SW  	1999	12	11	HEEA064960       	1	19991105	G	3210	70079F045Z083	LINE            			BELL  	407   	407         		SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	437PH					53072				HOSE ASSY HAD SEEPING FROM UNDER RUBBER COATING AT 90 DEGREE FITTING.						1	G	7	1 	3U			O	H2SW    					 
1999121100422	19991211	00422	SW  	1999	12	11	HEEA064961       	1	19991105	G	2420	SM20ACD300A21	RELAY           			BELL  	407   	407         		SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457PH					53147				RELAY WILL NOT ILLUMINATE START LIGHT EVERY TIME.						1	G	7	1 	3U			O	H2SW    					 
1999121100423	19991211	00423	SW  	1999	12	11	HEEA064962       	1	19991105	G	2821	222366621103	FILTER          			BELL  	407   	407         		SW  										FUEL SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	57416					53070				FUEL FILTER LIGHT WILL NOT TEST WITH BUTTON DEPRESSED.						1	G	7	1 	3U			O	H2SW    					 
1999121100424	19991211	00424	SW  	1999	12	11	HEEA064963       	1	19991105	G	3212	206050247137	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				FLOAT COVER TORN AND TATTERED.						1	G	7	1 	3U			O	H2SW    					 
1999121100425	19991211	00425	SW  	1999	12	11	HEEA064964       	1	19991105	G	6510	407040316101	FLYWHEEL        			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				FLYWHEEL HAD WORN SPLINES.						1	G	7	1 	3U			O	H2SW    					 
1999121100426	19991211	00426	SW  	1999	12	11	HEEA064965       	1	19991105	G	3212	212073905001	GAUGE           			BELL  	407   	407         		SW  										FLOAT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				PRESSURE GAUGE WILL NOT  WORK.						1	G	7	1 	3U			O	H2SW    					 
1999121100427	19991211	00427	SW  	1999	12	11	HEEA064966       	1	19991105	G	6310	406340102101	CARBON SEAL     		406040500123	BELL  	407   	407         		SW  										M/R DRIVE	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	447PH	110  			A3856	53114				CARBON SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100428	19991211	00428	SW  	1999	12	11	HEEA064967       	1	19991105	G	6520	406040453101	SEAL            			BELL  	407   	407         		SW  										T/R GEARBOX	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	57416					53070				SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999121100429	19991211	00429	SW  	1999	12	11	HEEA064968       	1	19991105	G	5320	206032305127	CHANNEL         			BELL  	407   	407         		SW  										FUSELAGE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				CHANNEL CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100430	19991211	00430	SW  	1999	12	11	HEEA064969       	1	19991105	G	2822	407362013101	SWITCH          			BELL  	407   	407         		SW  										FUEL PRESSURE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	457PH					53147				PRESSURE SWITCH WILL NOT ILLUMINATE LIGHT WITH NO BOOST PUMP PRESSURE.						1	G	7	1 	3U			O	H2SW    					 
1999121100431	19991211	00431	SW  	1999	12	11	HEEA064970       	1	19991105	G	2822	407362013101	SWITCH          			BELL  	407   	407         		SW  										FUEL PRESSURE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724PH					53327				PRESSURE SWITCH WILL NOT TURN OFF LIGHT.						1	G	7	1 	3U			O	H2SW    					 
1999121100432	19991211	00432	SW  	1999	12	11	HEEA064971       	1	19991105	G	2420	SM20ACD300A21	RELAY           			BELL  	407   	407         		SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416					53070				RELAY CAUSES HORN TO GO OFF WITH BATTERY OFF.						1	G	7	1 	3U			O	H2SW    					 
1999121100433	19991211	00433		1999	12	11	HEEA064972       	4	19991105	G	3423	C2300L424B	GASKET          			BELL  	407   	407         		SW  										COMPASS	MISSING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH					53266				COMPASS HAD GASKET MISSING UNDER FACEPLATE.						1	G	7	1 	3U			O	H2SW    					 
1999121100612	19991211	00612	EU  	1999	12	11	HEEA064973       	1	19991105	G	7921	420800001	BLOWER          			SNIAS 	350   	AS350B2     	8680813	EU  										OIL COOLER	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350BZ					2653				BLOWER INOPERATIVE.						1	G	7	1 	3U				H9EU    					 
1999121100434	19991211	00434	GL  	1999	12	11	HEEA064974       	2	19991105	G	7320	407076503109	CONNECTOR       			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					FADEC	DAMAGED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	467PH					53142				N2 OVERSPEED TO 118.35 PERCENT, UNINITIATED ON GROUND.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999121100435	19991211	00435	GL  	1999	12	11	HEEA064975       	2	19991105	G	7320	407076503111	CONNECTOR       			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					FADEC	DAMAGED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	467PH					53142				N2 OVERSPEED TO 118.35 PERCENT, UNINITIATED ON GROUND.  SUBMITTER SUGGESTED POSSIBLE SYSTEM FAILER.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999121100436	19991211	00436	GL  	1999	12	11	HEEA064976       	2	19991105	G	7320	10648BH151	SWITCH          			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					FADEC	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	467PH					53142				N2 OVERSPEED TO 118.35 PERCENT, UNINITIATED ON GROUND.  SUBMITTER SUGGESTED POSSIBLE SYSTEM FAILER.  S						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
1999121100160	19991211	00160	GL  	1999	12	11	HEEA064981       	2	19991105	G	7230	23057142	CASE HALVE      		6890550     						ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	CHAFED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03					CAC40303		CAE836387			CASE HALVES RUBBED ON PLASTIC DURING POWER CHECK ON AIRCRAFT.  UNBONDED PLASTIC NOTED UPON INSPECTION OF COMPRESSOR PART	S.										3	U			E4CE				 
1999121100161	19991211	00161	GL  	1999	12	11	HEEA064984       	2	19991108	G	7230	23065801	HOUSING         			BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					COMPRESSOR	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										RECEIVING INSPECTION REVEALED O-RING GROOVES ON NR 1 BEARING HOUSING IMPROPERLY MACHINED IN LOCATION OF SUPERCEDING P/N 	23062751.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999121100162	19991211	00162	GL  	1999	12	11	HEEA064985       	2	19991108	G	7230	23004513	CARBON SEAL     		6890550     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					COMPRESSOR	LEAKING         	E			HEEA	K				NONE                    				K	L		FLUID LOSS                	NO TEST                   		IN	INSP/MAINT     	1			SW	03	8197X				CAC40394	S808	CAE270046			ENGINE REMOVED DUE TO METAL IN OIL.  FAILED LEAK CHECK, I/A/W 10W2 OPERATION AND MAINTENANCE MANUAL 6TH ED. REV. 3 DATED	 7-15-99 SECTION 72-30-00 PARA. 3/B/12. INSTALLED NEW REPLACEMENT NR 1 SEAL.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100163	19991211	00163	GL  	1999	12	11	HEEA064986       	2	19991108	G	7230	23004513	CARBON SEAL     		23033193    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					COMPRESSOR	LEAKING         	E			HEEA	K				NONE                    				K	L		FLUID LOSS                	NO TEST                   		IN	INSP/MAINT     	1			SW	03	41128				CAC90071	51465	CAE895589			INSTALLED NEW CARBON SEAL ASSY P/N 23004513, PRESSURE CHECKED NR 1 BEARING AREA, LEAKED. INSTALLED SECOND CARBON SEAL AS	SY AND PRESSURE CHECKED.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999121100437	19991211	00437	SW  	1999	12	11	HEEA064987       	1	19991108	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GEN	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH	1280 				53038				STARTER/GENERATOR BRUSHES WERE EXCESSIVELY WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100438	19991211	00438	SW  	1999	12	11	HEEA064988       	1	19991108	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GEN	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH	1285 				53072				STARTER/GENERATOR FAILED 300 HOUR INSPECTION.   INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES WERE EXCESSIVELY 	WORN.					1	G	7	1 	3U			O	H2SW    					 
1999121100439	19991211	00439	SW  	1999	12	11	HEEA064989       	1	19991108	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GEN	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM	1681 				53060				STARTER/GENERATOR FAILED 300 HOUR INSPECTION.   INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES WERE EXCESSIVELY 	WORN.					1	G	7	1 	3U			O	H2SW    					 
1999121100613	19991211	00613		1999	12	11	HEEA065045       	4	19991110	G	3120	B1894522282A	CLOCK           			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6095S					2777				CLOCK WILL NOT KEEP TIME.						1	G	7	1 	3U				H9EU    					 
1999121100614	19991211	00614	EU  	1999	12	11	HEEA065046       	1	19991110	G	6730	704A34240015	ACCUMULATOR     			SNIAS 	350   	AS350B2     	8680813	EU  										T/R SERVO	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	60951					2771				ACCUMULATOR LEAKS.						1	G	7	1 	3U				H9EU    					 
1999121100171	19991211	00171	EU  	1999	12	11	HEEA065047       	1	19991110	G	7170	0174078010	DRAIN VALVE     			SNIAS 	350   	AS350B2     	8680813	EU  										IGNITION	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	40466					3004				START DRAIN VALVE LEAKING.						1	G	7	1 	3U				H9EU    					 
1999121100444	19991211	00444	SW  	1999	12	11	HEEA065048       	1	19991110	G	6420	406312100101	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR HEAD	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724PH					53327				BEARING WORN BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999121100445	19991211	00445	SW  	1999	12	11	HEEA065049       	1	19991110	G	3212	206050247135	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH					53207				FLOAT COVER END CAP TORN AND FRAYED.						1	G	7	1 	3U			O	H2SW    					 
1999121100446	19991211	00446	SW  	1999	12	11	HEEA065050       	1	19991110	G	7810	206064203101	DUCT            			BELL  	407   	407         		SW  										EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH					53266				DUCT CRACKED NEAR MOUNTING BRACKET.						1	G	7	1 	3U			O	H2SW    					 
1999121100447	19991211	00447	SW  	1999	12	11	HEEA065051       	1	19991110	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH	1963 				53198				BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100448	19991211	00448	SW  	1999	12	11	HEEA065053       	1	19991110	G	6210	407015001117	BLADE           			BELL  	407   	407         		SW  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH	1828 				53142				MAIN ROTOR BLADE CRACKED FORWARD AND AFT OF THE TRIM TAB.						1	G	7	1 	3U			O	H2SW    					 
1999121100615	19991211	00615	EU  	1999	12	11	HEEA065054       	1	19991110	G	2110	5AS35034	COMPRESSOR      			SNIAS 	350   	AS350B2     	8680813	EU  										AIR DISTRIBUTION	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6095S					2777				COMPRESSOR'S HIGH SIDE PRESSURE LOW SYSTEM NOT COOLING PROPERLY.						1	G	7	1 	3U				H9EU    					 
1999121100449	19991211	00449		1999	12	11	HEEA065055       	4	19991111	G	3424	214075244001	RATE GYRO       			BELL  	212   	212         	1181420	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5736D					31135				GYRO WILL NOT DEFLECT NEEDLE.						1	G	7	1 	4U				H4SW    					 
1999121100450	19991211	00450	SW  	1999	12	11	HEEA065056       	1	19991111	G	7931	206075677103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										OIL PRESSURE	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	206FS					51506				INDICATOR READS 4 PSI HIGH.						1	G	7	1 	3U				H2SW    					 
1999121100172	19991211	00172		1999	12	11	HEEA065057       	4	19991111	G	3420	1113025	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										HSI	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911MJ					760231				VOR INVALID LIGHT STAYS ON AND VOR NEEDLE DOES NOT PAINT TO STATIONS.  GOOD I.D. TONE.						1	G	7	2 	3U				H1NE    					 
1999121100451	19991211	00451	SW  	1999	12	11	HEEA065058       	1	19991111	G	2842	2003600000101	TRANSMITTER     			BELL  	412   	412         	1182202	SW  										FUEL QUANTITY	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	142PH					33150				TRANSMITTER HAD FAULTY FUEL QUANTITY READINGS.						1	G	7	2 	4U				H4SW    					 
1999121100173	19991211	00173		1999	12	11	HEEA065059       	4	19991111	G	3421	7660002113102	VERTICAL GYRO   			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5426U					760167				VERTICAL GYRO CAUSES ATTITUDE INDICATOR TO TUMBLE.						1	G	7	2 	3U				H1NE    					 
1999121100452	19991211	00452		1999	12	11	HEEA065060       	4	19991111	G	3120	212075514001	CLOCK           			BELL  	214   	214ST       	1182106	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				CLOCK INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999121100453	19991211	00453	SW  	1999	12	11	HEEA065061       	1	19991111	G	2822	2C273	CARTRIDGE       			BELL  	412   	412         	1182202	SW  										FUEL BOOST	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893P					33012				FUEL CARTRIDGE HAD LOW PRESSURE.						1	G	7	2 	4U				H4SW    					 
1999121100454	19991211	00454		1999	12	11	HEEA065062       	4	19991111	G	3421	214175241101	GYROSCOPE       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				ADI ERRATIC IN PITCH AND ROLL AXIS.						2	G	7	2 	4U				H10SW   					 
1999121100616	19991211	00616	EU  	1999	12	11	HEEA065063       	1	19991111	G	7334	BSE206150G3	TRANSDUCER      			BOLKMS	105   	BO105S      	5626006	EU  										FUEL PRESSURE	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3071K					S859				PRESSURE TRANSDUCER NOT SENDING ANY SIGNAL.						1	G	7	2 	3U				H3EU    					 
1999121100455	19991211	00455		1999	12	11	HEEA065064       	4	19991111	G	3422	2891ESR	GYRO            			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2124Z					45646				DIRECTIONAL GYRO WILL NOT POWER UP.						1	G	7	1 	3U				H2SW    					 
1999121100617	19991211	00617	EU  	1999	12	11	HEEA065065       	1	19991111	G	6340	KDW021	WARNING BOX     			BOLKMS	105   	BO105S      	5626006	EU  										ROTOR RPM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			SW	03	3071K					S859				RPM HORN AND LIGHT ACTIVATES IN NORMAL FLIGHT.						1	G	7	2 	3U				H3EU    					 
1999121100618	19991211	00618	EU  	1999	12	11	HEEA065066       	1	19991111	G	6340	KDW021	WARNING BOX     			BOLKMS	105   	BO105S      	5626006	EU  										ROTOR RPM	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3520T					S539				NO FLASHING LIGHT.  RPM WARNING LIGHT DOES NOT COME ON.						1	G	7	2 	3U				H3EU    					 
1999121100619	19991211	00619	EU  	1999	12	11	HEEA065067       	1	19991111	G	2913	4002001	PUMP            			BOLKMS	105   	BO105S      	5626006	EU  										HYD SYSTEM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SW	03	133AE					S800				HYDRAULIC PUMP HAD HIGH PRESSURE.						1	G	7	2 	3U				H3EU    					 
1999121100620	19991211	00620	EU  	1999	12	11	HEEA065068       	1	19991111	G	2822	D107318D1	PUMP            			BOLKMS	105   	BO105S      	5626006	EU  										FUEL BOOST	MALFUNCTIONED   	E			HEEA	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SW	03	5031U	4808 				S678				FUEL PUMP HAD LOW PRESSURE.						1	G	7	2 	3U				H3EU    					 
1999121100456	19991211	00456		1999	12	11	HEEA065069       	4	19991111	G	3434	DK100	BATTERY         			BELL  	206   	206L3       	1182108	SW  										MARKER BEACON	DISCHARGED      	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	8592X					51508				BEACON HAD WEAK BATTERY.						1	G	7	1 	3U				H2SW    					 
1999121100457	19991211	00457		1999	12	11	HEEA065070       	4	19991111	G	3444	066104800	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										RADAR ALT	FLUCTUATED      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	21498					36003				ALTIMETER FLUCTUATES INTERMITTENTLY.						1	G	7	2 	4U				H4SW    					 
1999121100621	19991211	00621	EU  	1999	12	11	HEEA065071       	1	19991111	G	3340	1179203103	CONTROL UNIT    			BOLKMS	117   	BK117B1     	5626012	EU  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	191BK					7146				INSTRUMENT LIGHT WORKS INTERMITTENTLY.						1	G	7	2 	3U				H13EU   					 
1999121100458	19991211	00458		1999	12	11	HEEA065072       	4	19991111	G	3424	206070274005	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										COCKPIT	NOISY           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	92MT					51175				INDICATOR VERY NOISY.						1	G	7	1 	3U				H2SW    					 
1999121100622	19991211	00622	EU  	1999	12	11	HEEA065073       	1	19991111	G	7714	DL41239	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										ENGINE RPM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	967MB					S737				INDICATOR HANGS ON START AND FLUCTUATES.						1	G	7	2 	3U				H3EU    					 
1999121100459	19991211	00459		1999	12	11	HEEA065074       	4	19991111	G	3457	0110005400	GPS             			BELL  	206   	206L1       	1182107	SW  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22425					45743				TAKES 15 MINUTES TO START WORKING, THEN FAILS INTERMITTENTLY DURING TRIP.						1	G	7	1 	3U				H2SW    					 
1999121100623	19991211	00623	EU  	1999	12	11	HEEA065075       	1	19991111	G	2822	D107318D1	PUMP            			BOLKMS	105   	BO105S      	5626006	EU  										FUEL BOOST	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	818SH	4450 				S753				FUEL PUMP ASSY TRIPS CIRCUIT BREAKER.						1	G	7	2 	3U				H3EU    					 
1999121100624	19991211	00624	EU  	1999	12	11	HEEA065076       	1	19991111	G	2913	4002001	PUMP            			BOLKMS	105   	BO105S      	5626006	EU  										HYD SYSTEM	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3520T					S539				HYDRAULIC PUMP LEAKING.						1	G	7	2 	3U				H3EU    					 
1999121100174	19991211	00174		1999	12	11	HEEA065077       	4	19991111	G	3422	258719343	GYRO            			BEECH 	200   	200BEECH    	1152920	CE  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	30PH					BB635				GYRO INOPERATIVE.						1	L	7	2 	4T				A24CE   					 
1999121100460	19991211	00460	SW  	1999	12	11	HEEA065078       	1	19991111	G	2435	23032048	ARMATURE        			BELL  	206   	206B3       	1181506	SW  										STARTER/GEN	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2285B					3642				STARTER HAS A DEAD SPOT IN ARMATURE, WOULD NOT MOTOR ENGINE.						1	G	7	1 	3U				H2SW    					 
1999121100461	19991211	00461		1999	12	11	HEEA065079       	4	19991111	G	2210	214074303115	AMPLIFIER ASSY  			BELL  	214   	214ST       	1182106	SW  										AUTOFLIGHT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				AMPLIFIER ASSY CANNOT ADJUST R91 ON CARD II.   WILL NOT STAY WITHIN LIMITS.						2	G	7	2 	4U				H10SW   					 
1999121100462	19991211	00462		1999	12	11	HEEA065080       	4	19991111	G	2210	214074301105	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										SCAS	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59805					28141				AMPLIFIER INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999121100463	19991211	00463	SW  	1999	12	11	HEEA065081       	1	19991111	G	2400	214175153105	REGULATOR       			BELL  	214   	214ST       	1182106	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				VOLTAGE REGULATOR DROPS OFF-LINE DURING CROSS START.						2	G	7	2 	4U				H10SW   					 
1999121100464	19991211	00464		1999	12	11	HEEA065082       	4	19991111	G	3413	212070239101FM	CONNECTOR       			BELL  	214   	214ST       	1182106	SW  										VS INDICATOR	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				CANNON PLUG SOCKET BROKEN.						2	G	7	2 	4U				H10SW   					 
1999121100465	19991211	00465		1999	12	11	HEEA065083       	4	19991111	G	3460	5205160006	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	23023					33080				TO/FROM INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999121100175	19991211	00175	NE  	1999	12	11	HEEA065084       	2	19991111	G	7210	3024780	GEARBOX         			BELL  	412   	412         	1182202	SW  	PWA   	PT6T  	PT6T3B      	52045	NE  					COMBINING	OIL LOSS        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2298Z	2327 				33077				COMBINING GEARBOX HAD HIGH OIL USAGE.						1	G	7	2 	4U	4	U		H4SW    	E22EA				 
1999121100466	19991211	00466	SW  	1999	12	11	HEEA065085       	1	19991111	G	2422	ASH4501	INVERTER        			BELL  	412   	412         	1182202	SW  										AC SYSTEM	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K					33020				INVERTER INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999121100467	19991211	00467	SW  	1999	12	11	HEEA065086       	1	19991111	G	2422	ASH4501	INVERTER        			BELL  	412   	412         	1182202	SW  										DC SYSTEM	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K					33020				INVERTER HAD NO OUTPUT.						1	G	7	2 	4U				H4SW    					 
1999121100468	19991211	00468	SW  	1999	12	11	HEEA065087       	1	19991111	G	2822	205060606003	PUMP            			BELL  	412   	412         	1182202	SW  										FUEL BOOST	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893S					33022				PUMP HAD LOW PRESSURE.						1	G	7	2 	4U				H4SW    					 
1999121100469	19991211	00469	SW  	1999	12	11	HEEA065088       	1	19991111	G	6220	214010103115	SPINDLE         			BELL  	214   	214ST       	1182106	SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TANG BUSHINGS PULLING FROM TANGS AND BLUE EPOXY EXTRUDING FROM BUSHINGS.						2	G	7	2 	4U				H10SW   					 
1999121100470	19991211	00470	SW  	1999	12	11	HEEA065089       	1	19991111	G	6220	214010103115	SPINDLE         			BELL  	214   	214ST       	1182106	SW  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TANG BUSHINGS PULLING FROM TANGS AND BLUE EPOXY EXTRUDING FROM BUSHINGS.						2	G	7	2 	4U				H10SW   					 
1999121100471	19991211	00471		1999	12	11	HEEA065090       	4	19991111	G	3416	13011001	ALTIMETER       			BELL  	412   	412         	1182202	SW  										COCKPIT	INACCURATE      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2148K					36001				ALTIMETER INDICATOR HAD 100 DEGREE ERROR.						1	G	7	2 	4U				H4SW    					 
1999121100472	19991211	00472		1999	12	11	HEEA065091       	4	19991111	G	3457	13824020109	GPS             			BELL  	407   	407         		SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				GPS LOSES ITSELF.						1	G	7	1 	3U			O	H2SW    					 
1999121100176	19991211	00176		1999	12	11	HEEA065092       	4	19991111	G	3425	1113025	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										HSI	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5435V					760158				HSI INDICATOR UNABLE TO CONTROL AND WOULD NOT INDICATE PROPERLY (WRONG HEADING).						1	G	7	2 	3U				H1NE    					 
1999121100177	19991211	00177	NE  	1999	12	11	HEEA065093       	1	19991111	G	7712	7645001078106	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										DUAL TORQUE	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122G					760232				NR 1 NEEDLE STICKS ON DUAL TORQUE INDICATOR.						1	G	7	2 	3U				H1NE    					 
1999121100178	19991211	00178		1999	12	11	HEEA065094       	4	19991111	G	3421	7690001808102	RATE GYRO       			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545K					760047				GYRO WILL NOT POWER UP.						1	G	7	2 	3U				H1NE    					 
1999121100179	19991211	00179	GL  	1999	12	11	HEEA065095       	2	19991111	G	7314	3944001	FUEL PUMP       			SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					ENGINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2743E	8661 				760155				FUEL PUMP HAD WORN INTERNAL SPLINES.						1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999121100625	19991211	00625	EU  	1999	12	11	HEEA065096       	1	19991111	G	6410	11731743	BLADE           			BOLKMS	117   	BK117B2     	5626013	EU  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	136AE	1275 				7234				FOD DAMAGE ON LEADING EDGE TAIL ROTOR BLADE.						1	G	7	2 	3U			NC	H13EU   					 
1999121100473	19991211	00473		1999	12	11	HEEA065097       	4	19991111	G	3424	214075244001	GYRO            			BELL  	212   	212         	1181420	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5010F					30936				NO TURN INDICATIONS DISPLAY ON GYRO.						1	G	7	1 	4U				H4SW    					 
1999121100474	19991211	00474	SW  	1999	12	11	HEEA065098       	1	19991111	G	2841	214175257103	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										FUEL QUANTITY	ERRATIC         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				FUEL QUANTITY INDICATOR READING ERRATIC.						2	G	7	2 	4U				H10SW   					 
1999121100475	19991211	00475		1999	12	11	HEEA065099       	4	19991111	G	3421	1113034	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K					33020				RATE OF TURN NEEDLE INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999121100476	19991211	00476	SW  	1999	12	11	HEEA065100       	1	19991111	G	2437	209070264003	DUAL AMMETER    			BELL  	412   	412         	1182202	SW  										COCKPIT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K					33020				NR 1 POINTER STICKS.						1	G	7	2 	4U				H4SW    					 
1999121100477	19991211	00477	SW  	1999	12	11	HEEA065101       	1	19991111	G	7722	206375006101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	READS HIGH      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1073W					45386				TOT INDICATOR READINGS ARE HIGH.						1	G	7	1 	3U				H2SW    					 
1999121100478	19991211	00478		1999	12	11	HEEA065102       	4	19991111	G	3120	212075514001	RESET BUTTON    			BELL  	214   	214ST       	1182106	SW  										CLOCK	MISSION         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M					28102				CLOCK COUNTER RESET BUTTON MISSING.						2	G	7	2 	4U				H10SW   					 
1999121100479	19991211	00479		1999	12	11	HEEA065103       	4	19991111	G	3416	59341	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2761N					45277				ALTIMETER HAD LEAK AND ADJUSTMENT KNOB HAD EXCESSIVE NEEDLE DRAG.						1	G	7	1 	3U				H2SW    					 
1999121100480	19991211	00480		1999	12	11	HEEA065104       	4	19991111	G	3454	071121612	CONTROL UNIT    			BELL  	214   	214ST       	1182106	SW  										COCKPIT VOR	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3897N					28106				CONTROL UNIT DISPLAY INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999121100626	19991211	00626	EU  	1999	12	11	HEEA065105       	1	19991111	G	6340	10594575	TRANSMITTER     			BOLKMS	117   	BK117A3     	5626015	EU  										MAST MOMENT	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911NC					7026				TORQUE TRANSMITTER NTERMITTENTLY INOPERATIVE.						1	G	7	2 	3U				H13EU   					 
1999121100627	19991211	00627	EU  	1999	12	11	HEEA065106       	1	19991111	G	6340	117945641	INDICATOR       			BOLKMS	117   	BK117A3     	5626015	EU  										MAST MOMENT	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911NC					7026				INDICATOR INTERMITTENTLY INOPERATIVE, INDICATOR TEST AND FUNCTION.						1	G	7	2 	3U				H13EU   					 
1999121100481	19991211	00481		1999	12	11	HEEA065107       	4	19991111	G	3421	1113034	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K					33020				ATTITUDE INDICATOR TUMBLING.						1	G	7	2 	4U				H4SW    					 
1999121100482	19991211	00482	SW  	1999	12	11	HEEA065108       	1	19991111	G	7714	206075681117	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										DUAL TACH	FLUCTUATES      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				DUAL TACHOMETER INDICATOR'S N2 NEEDLE FLUCTUATES.						1	G	7	1 	3U				H2SW    					 
1999121100483	19991211	00483	SW  	1999	12	11	HEEA065109       	1	19991111	G	7714	206075681117	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										DUAL TACH	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6610Y					51419				TURBINE AND ROTOR NEEDLES SPLIT ON DUAL TACHOMETER.						1	G	7	1 	3U				H2SW    					 
1999121100484	19991211	00484		1999	12	11	HEEA065110       	4	19991111	G	3416	5934D3	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2772A					45311				ALTIMETER INDICATES 3,000-4,000 FEET.						1	G	7	1 	3U				H2SW    					 
1999121100485	19991211	00485		1999	12	11	HEEA065111       	4	19991112	G	3425	71252	GYRO            			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22347					36005				GYRO CAUSED RATE NEEDLE TO MOVE WHILE AIRCRAFT STATIC.						1	G	7	2 	4U				H4SW    					 
1999121100486	19991211	00486	SW  	1999	12	11	HEEA065112       	1	19991112	G	2822	2C271	CARTRIDGE       			BELL  	206   	206B3       	1181506	SW  										FUEL BOOST	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2272J					3620				CARTRIDGE WORKS INTERMITTENTLY.						1	G	7	1 	3U				H2SW    					 
1999121100487	19991211	00487	SW  	1999	12	11	HEEA065113       	1	19991112	G	2822	164A204	PUMP            			BELL  	206   	206B3       	1181506	SW  										FUEL BOOST	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	2270G					3610				FUEL BOOST PUMP LEAKED AT INSULATION FROM HOLE THE BOTTOM FOR POWER WIRES.						1	G	7	1 	3U				H2SW    					 
1999121100628	19991211	00628	EU  	1999	12	11	HEEA065114       	1	19991112	G	7933	TM41039	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										TRIPLE OIL TEMP	ERRATIC         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	133AE					S800				TEMPERATURE GAUGE READS ERRATIC.						1	G	7	2 	3U				H3EU    					 
1999121100629	19991211	00629	EU  	1999	12	11	HEEA065115       	1	19991112	G	2822	D107318D1	PUMP            			BOLKMS	105   	BO105S      	5626006	EU  										FUEL BOOST	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	8197X	3924 				S808				FUEL PUMP INOPERATIVE.						1	G	7	2 	3U				H3EU    					 
1999121100488	19991211	00488	SW  	1999	12	11	HEEA065116       	1	19991112	G	7722	206375006101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT TOT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1073W					45386				TOT INDICATOR READS ZERO WHEN START ATTEMPTED.						1	G	7	1 	3U				H2SW    					 
1999121100180	19991211	00180	NE  	1999	12	11	HEEA065117       	1	19991112	G	6220	7610608000050	DAMPER          			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	WEAK            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1547D					760077				MAIN ROTOR DAMPENER EXTREMELY WEAK.						1	G	7	2 	3U				H1NE    					 
1999121100181	19991211	00181		1999	12	11	HEEA065118       	4	19991112	G	2210	7611122	AMPLIFIER       			SKRSKY	S76   	S76A        	8143006	NE  										PITCH SLICE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545K					760047				NR 2 PITCH CHANNEL INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999121100182	19991211	00182		1999	12	11	HEEA065119       	4	19991112	G	3442	7009330902	WX RADAR        			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1545K					760047				PICTURE INTERMITTENT, GOES ON AND OFF.						1	G	7	2 	3U				H1NE    					 
1999121100183	19991211	00183	NE  	1999	12	11	HEEA065120       	1	19991112	G	7810	7630507003044	EJECTOR         			SKRSKY	S76   	S76A        	8143006	NE  										EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3122G					760232				EJECTOR CRACKED.						1	G	7	2 	3U				H1NE    					 
1999121100489	19991211	00489		1999	12	11	HEEA065121       	4	19991112	G	2210	214074305105	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										FBW ELEVATOR	KICKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				ELEVATOR KICKING OF-LINE.						2	G	7	2 	4U				H10SW   					 
1999121100490	19991211	00490		1999	12	11	HEEA065122       	4	19991112	G	2210	214074305105	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										FBW ELEVATOR	KICKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										ELEVATOR KICKING OFF-LINE.						2	G	7	2 	4U				H10SW   					 
1999121100491	19991211	00491		1999	12	11	HEEA065123       	4	19991112	G	3425	2593379001	COMPENSATOR     			BELL  	412   	412         	1182202	SW  										COCKPIT	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2014K					33020				COMPENSATOR CORRODED.						1	G	7	2 	4U				H4SW    					 
1999121100492	19991211	00492	SW  	1999	12	11	HEEA065124       	1	19991112	G	6330	214031617113	HELPER SPRING   			BELL  	214   	214ST       	1182106	SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M					28102				ERASER WEAR AND CRACKING ON FORWARD AND AFT SIDES.						2	G	7	2 	4U				H10SW   					 
1999121100493	19991211	00493	SW  	1999	12	11	HEEA065125       	1	19991112	G	7714	206075681105	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										DUAL TACH	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1076Y					45380				YELLOW MARKS TACHOMETER INDICATOR ARE FADING AWAY.						1	G	7	1 	3U				H2SW    					 
1999121100184	19991211	00184		1999	12	11	HEEA065126       	4	19991112	G	2210	7690001805102	SWITCH          																	AUTOFLIGHT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										SWITCH STUCK AND INOPERATIVE.																			 
1999121100494	19991211	00494	SW  	1999	12	11	HEEA065127       	1	19991112	G	5532	206020113207	SKIN            			BELL  	206   	206L1       	1182107	SW  										VERTICAL STAB	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	1073W					45386				VERTICAL FIN HAD CORROSION AND SEPARATION.						1	G	7	1 	3U				H2SW    					 
1999121100495	19991211	00495		1999	12	11	HEEA065128       	4	19991115	G	2210	214074305105	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										FBW ELEVATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				WILL NOT DRIVE THE ACTUATORS.						2	G	7	2 	4U				H10SW   					 
1999121100496	19991211	00496		1999	12	11	HEEA065129       	4	19991115	G	2210	214001970111	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										FBW ELEVATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				ACTUATOR ASSY WOULD NOT MONITOR TEST. S						2	G	7	2 	4U				H10SW   					 
1999121100497	19991211	00497		1999	12	11	HEEA065130       	4	19991115	G	2210	214001970111	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										FBW ELEVATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				BRAKE NOT RELEASING TO PERMIT OTHER ACTUATOR TO TEST.						2	G	7	2 	4U				H10SW   					 
1999121100498	19991211	00498		1999	12	11	HEEA065131       	4	19991115	G	2210	214001970111	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										FBW ELEVATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				BRAKE NOT RELEASING, WILL NOT TEST.						2	G	7	2 	4U				H10SW   					 
1999121100499	19991211	00499		1999	12	11	HEEA065132       	4	19991115	G	2210	214001970111	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										FBW ELEVATOR	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				ELEVATOR SYSTEM WILL NOT MONITOR TEST.						2	G	7	2 	4U				H10SW   					 
1999121100500	19991211	00500		1999	12	11	HEEA065133       	4	19991115	G	3421	RCA26BK7	GYRO            			BELL  	206   	206L1       	1182107	SW  										COCKPIT HORIZON	PRECESSING      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5006F					45181				HORIZONTAL GYRO PRECESSES.						1	G	7	1 	3U				H2SW    					 
1999121100630	19991211	00630	EU  	1999	12	11	HEEA065134       	1	19991115	G	7332	4021001	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										DUAL FUEL PRESS	STICKING        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3071K					S859				LEFT SIDE STICKS.						1	G	7	2 	3U				H3EU    					 
1999121100501	19991211	00501	SW  	1999	12	11	HEEA065135       	1	19991115	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONROL	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1202T					33112				CONTROL UNIT INOPERATIVE; GENERATORS KICK OFF LINE.						1	G	7	2 	4U				H4SW    					 
1999121100502	19991211	00502	SW  	1999	12	11	HEEA065136       	1	19991115	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONROL	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1202T					33112				CONTROL UNIT INOPERATIVE; GENERATORS KICK OFF-LINE.						1	G	7	2 	4U				H4SW    					 
1999121100631	19991211	00631	EU  	1999	12	11	HEEA065137       	1	19991115	G	6340	10594564	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										MAST MOMENT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	9190Y					S669				MAST MOMENT INDICATOR UNRELIABLE.						1	G	7	2 	3U				H3EU    					 
1999121100503	19991211	00503	SW  	1999	12	11	HEEA065138       	1	19991115	G	7712	206075739103	TORQUEMETER     			BELL  	206   	206L1       	1182107	SW  										COCKPIT	STICKING        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2761N					45277				TORQUEMETER STICKS THROUGHOUT SCALE.						1	G	7	1 	3U				H2SW    					 
1999121100504	19991211	00504		1999	12	11	HEEA065139       	4	19991115	G	2210	214074303115	AMPLIFIER       			BELL  	214   	214ST       	1182106	SW  										AUTOFLIGHT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3897N					28106				PITCH AND ROLL WILL NOT STAY ENGAGED.						2	G	7	2 	4U				H10SW   					 
1999121100505	19991211	00505	SW  	1999	12	11	HEEA065140       	1	19991115	G	6330	214031615106	CLEVIS ARM      			BELL  	214   	214ST       	1182106	SW  										M/R TRANSMISSION	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5748M					28102				RUBBER CRACKED, PRONOUNCED NODAL BOUNCE IN LET DOWN, AND WHEN ALLOWING AIRSPEED BELOW 120 KNOTS.						2	G	7	2 	4U				H10SW   					 
1999121100185	19991211	00185	NE  	1999	12	11	HEEA065141       	1	19991115	G	2160	7650007903102	VALVE           			SKRSKY	S76   	S76A        	8143006	NE  										BLEED S O V	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5435V					760158				BLEED  AIR SHUT-OFF VALVE WILL NOT OPEN.						1	G	7	2 	3U				H1NE    					 
1999121100186	19991211	00186	CE  	1999	12	11	HEEA065142       	1	19991115	G	7331	903800097	TRANSMITTER     			BEECH 	200   	200CBEECH   	1152926	CE  										FUEL FLOW	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	39PH					BL3				TRANSMITTER HAD INTERMITTENT FUEL FLOW READINGS.						1	L	7	2 	4T				A24CE   					 
1999121100506	19991211	00506	SW  	1999	12	11	HEEA065143       	1	19991115	G	2430	51509002R	CONTROL UNIT    			BELL  	412   	412         	1182202	SW  										DC CONTROL	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1202T					33112				CONTROL UNIT WILL NOT PARALLEL.						1	G	7	2 	4U				H4SW    					 
1999121100187	19991211	00187		1999	12	11	HEEA065144       	4	19991115	G	3424	A593002	INDICATOR       																	COCKPIT	CONTAMINATED    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										TURN & BANK INDICATOR HAD MOISTURE INSIDE OF GLASS.																			 
1999121100188	19991211	00188	NE  	1999	12	11	HEEA065145       	1	19991115	G	2420	7655009005104	GCU             			SKRSKY	S76   	S76A        	8143006	NE  										AC SYSTEM	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	1545X	1682 				760047				UNDERVOLT WILL NOT TEST.						1	G	7	2 	3U				H1NE    					 
1999121100507	19991211	00507		1999	12	11	HEEA065146       	4	19991115	G	3416	8800T	ENCODER         			BELL  	412   	412         	1182202	SW  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	293CA					33005				GPS CONSTANTLY READS EXY.  ALTIMETER IS IN ERROR.						1	G	7	2 	4U				H4SW    					 
1999121100632	19991211	00632	EU  	1999	12	11	HEEA065147       	1	19991115	G	6320	4638001004	TRANSMISSION    			BOLKMS	105   	BO105S      	5626006	EU  										MAIN ROTOR	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3520T	2671 				S539				FOUND METAL IN TRANSMISSION.						1	G	7	2 	3U				H3EU    					 
2000012100004	20000121	00004	EU  	2000	1	21	HEEA065148       	1	19991115	G	2435	23032048	BRUSHES         			BOLKMS	117   	BK117B1     	5626012	EU  										STARTER-GEN	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911TL	2746 				7198				STARTER/GENERATOR BRUSHES WORN AND INOPERATIVE.						1	G	7	2 	3U				H13EU   					 
1999121100508	19991211	00508	SW  	1999	12	11	HEEA065149       	1	19991115	G	2822	205060606003	PUMP            			BELL  	212   	212         	1181420	SW  										FUEL BOOST	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5736D					31135				PUMP INTERMITTENLY TRIPPING THE CIRCUIT BREAKER.						1	G	7	1 	4U				H4SW    					 
1999121100509	19991211	00509	SW  	1999	12	11	HEEA065150       	1	19991115	G	2422	214175104101	INVERTER        			BELL  	214   	214ST       	1182106	SW  										AC SYSTEM	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	59805					28141				INVERTER INOPERATIVE; TRIPPING CIRCUIT BREAKER.						2	G	7	2 	4U				H10SW   					 
1999121100510	19991211	00510		1999	12	11	HEEA065151       	4	19991115	G	3416	5934D3	INDICATOR       			BELL  	407   	407         		SW  										COCKPIT	INACCURATE      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	417PH					53038				ALTIMETER 140 FEET OFF.						1	G	7	1 	3U			O	H2SW    					 
1999121100511	19991211	00511	SW  	1999	12	11	HEEA065152       	1	19991115	G	2422	ASH5845	INVERTER        			BELL  	212   	212         	1181420	SW  										AC SYSTEM	MALFUNCITONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3208H					31304				INVERTER HAD OVER VOLTAGE AND EXCESSIVE VOLTAGE.						1	G	7	1 	4U				H4SW    					 
1999121100189	19991211	00189	NE  	1999	12	11	HEEA065153       	1	19991115	G	6220	7610608000047	DAMPER          			SKRSKY	S76   	S76A        	8143006	NE  										MAIN ROTOR	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2743E					760155				NO DAMPENING.						1	G	7	2 	3U				H1NE    					 
1999121100512	19991211	00512		1999	12	11	HEEA065154       	4	19991115	G	3120	811B	CLOCK           			BELL  	412   	412         	1182202	SW  										COCKPIT	INCORRECT       	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	800Y					33134				DIGITAL CLOCK KEEPS INCORRECT TIME.						1	G	7	2 	4U				H4SW    					 
1999121100513	19991211	00513	SW  	1999	12	11	HEEA065155       	1	19991115	G	2913	214076334101	PUMP            			BELL  	214   	214ST       	1182106	SW  										HYD SYSTEM	FLAKING         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5748M					28102				BRASS FLAKES IN OIL FILTER CLOGGED.						2	G	7	2 	4U				H10SW   					 
1999121100633	19991211	00633	EU  	1999	12	11	HEEA065156       	1	19991115	G	6340	KDW021A	WARNING BOX     			BOLKMS	105   	BO105S      	5626006	EU  										ENGINE RPM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				N			FALSE WARNING             			NR	NOT REPORTED   	1			SW	03	3071K					S859				LIGHT ILLUMINATES IN-FLIGHT WITHOUT HORN AT 100 PERCENT.						1	G	7	2 	3U				H3EU    					 
1999121100634	19991211	00634	EU  	1999	12	11	HEEA065157       	1	19991115	G	6410	11731743	BLADE           			BOLKMS	117   	BK117B2     	5626013	EU  										TAIL ROTOR	ERRODED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	136AE	1275 				7234				TAIL ROTOR BLADE HAD PAINT EROSION.						1	G	7	2 	3U			NC	H13EU   					 
1999121100190	19991211	00190	GL  	1999	12	11	HEEA065158       	2	19991115	G	7314	3944001	FUEL PUMP       			SKRSKY	S76   	S76A        	8143006	NE  	ALLSN 	250C  	250C30S     	03013	GL  					ENGINE	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2743E	8583 				760155				NR 2 ENGINE SLOW TO START AFTER BEING SHUT DOWN FOR AN HOUR OR MORE.						1	G	7	2 	3U	3	U		H1NE    	E1GL				 
1999121100635	19991211	00635	EU  	1999	12	11	HEEA065159       	1	19991115	G	2822	D107318D1	PUMP            			BOLKMS	105   	BO105S      	5626006	EU  										FUEL BOOST	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	5421E	5901 				S806				FUEL PUMP ASSY LEAKING AT SCREWS ON BASE PLATE.						1	G	7	2 	3U				H3EU    					 
1999121100514	19991211	00514		1999	12	11	HEEA065160       	4	19991115	G	3416	214175278101	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	READS HIGH      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2148K					36001				ALTIMETER INDICATOR READS 140 FEET HIGH.						1	G	7	2 	4U				H4SW    					 
1999121100636	19991211	00636	EU  	1999	12	11	HEEA065161       	1	19991115	G	6220	105141081	HUB             			BOLKMS	105   	BO105S      	5626006	EU  										MAIN ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	91070	6920 				S145				MAIN ROTOR HUB HAD CORROSION ON ALL FOUR PITCH HORNS.						1	G	7	2 	3U				H3EU    					 
1999121100515	19991211	00515	SW  	1999	12	11	HEEA065162       	1	19991115	G	2822	2C271	CARTRIDGE       			BELL  	206   	206L1       	1182107	SW  										FUEL BOOST	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	10814					45415				CARTRIDGE INOPERATIVE.						1	G	7	1 	3U				H2SW    					 
1999121100516	19991211	00516	SW  	1999	12	11	HEEA065163       	1	19991115	G	2822	2C271	CARTRIDGE       			BELL  	206   	206L1       	1182107	SW  										FUEL BOOST	INIOPERATIVE    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2133X					45634				CARTRIDGE TRIPS CIRCUIT BREAKER.						1	G	7	1 	3U				H2SW    					 
1999121100517	19991211	00517	SW  	1999	12	11	HEEA065164       	1	19991115	G	6220	412010190103	BEARING         			BELL  	412   	412         	1182202	SW  										M/R DAMPER	SEPARATED       	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893L	4993 				33006				DAMPER BEARING SEPARATION.						1	G	7	2 	4U				H4SW    					 
1999121100637	19991211	00637	EU  	1999	12	11	HEEA065165       	1	19991115	G	6210	10515150	BLADE           			BOLKMS	105   	BO105S      	5626006	EU  										MAIN ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721MB	5286 				S752				ROTOR BLADE ASSY HAD TIP CAP SEPARATION.						1	G	7	2 	3U				H3EU    					 
1999121100191	19991211	00191	EA  	1999	12	11	HEEA065166       	2	19991115	G	7210	3024780	GEARBOX         			BELL  	212   	212         	1181420	SW  	PWA   	PT6T  	PT6T3       	52045	EA  					COMBINING	MAKING METAL    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3208H	10133				31304				COMBINING GEARBOX MAKING METAL - GEAR TOOTH FOUND NR 2 AFT CHIP PLUG.						1	G	7	1 	4U	4	U		H4SW    	E22EA				 
1999121100638	19991211	00638	EU  	1999	12	11	HEEA065167       	1	19991115	G	3340	930500251	SEARCH LIGHT    			BOLKMS	105   	BO105S      	5626006	EU  										FUSELAGE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	133AE					S800				SEARCH LIGHT INOPERATIVE.  MOTOR IS INTERMITTENT.   GETS STUCK IN DOWN POSITION AND WILL NOT MOVE OR PARK.						1	G	7	2 	3U				H3EU    					 
1999121100192	19991211	00192	NE  	1999	12	11	HEEA065168       	1	19991115	G	7810	7630507003044	EJECTOR         			SKRSKY	S76   	S76A        	8143006	NE  										EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	706AE					760275				EJECTOR CRACKED.						1	G	7	2 	3U				H1NE    					 
1999121100639	19991211	00639	EU  	1999	12	11	HEEA065169       	1	19991115	G	2822	D105102	PUMP            			BOLKMS	105   	BO105S      	5626006	EU  										FUEL BOOST	FAILED          	E			HEEA	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SW	03	4302G					S853				FUEL PUMP ASSY HAD LOW PRESSURE AND WAS NOISY.						1	G	7	2 	3U				H3EU    					 
1999121100193	19991211	00193		1999	12	11	HEEA065170       	4	19991115	G	3416	8503S20LW5V	ALTIMETER       			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1545X					760047				ALTIMETER READ 75-100 ON GROUND 100-150 AT ALTITUDE.						1	G	7	2 	3U				H1NE    					 
1999121100518	19991211	00518		1999	12	11	HEEA065171       	4	19991115	G	3416	8503S20LW5V	INDICATOR       																	COCKPIT	READS LOW       	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03										ALTIMETER READS LOW.																			 
1999121100640	19991211	00640	EU  	1999	12	11	HEEA065172       	1	19991115	G	2822	D107318D1	PUMP            			BOLKMS	105   	BO105S      	5626006	EU  										FUEL BOOST	INOPERATIVE     	E			HEEA	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SW	03	91070					S145				FUEL PUMP INOPERATIVE.						1	G	7	2 	3U				H3EU    					 
1999121100641	19991211	00641	EU  	1999	12	11	HEEA065173       	1	19991115	G	2913	4002001	PUMP            			BOLKMS	105   	BO105S      	5626006	EU  										HYD SYSTEM	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	137AE					S851				HYDRAULIC PUMP LEAKS AROUND SHAFT.						1	G	7	2 	3U				H3EU    					 
1999121100519	19991211	00519	SW  	1999	12	11	HEEA065174       	1	19991115	G	3340	7028501	LIGHT           			BELL  	412   	412         	1182202	SW  										STROBE	INOPERATIVE     	E			HEEA	O				OTHER                   				L			NO TEST                   			NR	NOT REPORTED   	1			SW	03	1202T					33112				STROBE LIGHT NOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999121100642	19991211	00642	EU  	1999	12	11	HEEA065175       	1	19991115	G	2822	D105102	PUMP            			BOLKMS	105   	BO105S      	5626006	EU  										FUEL BOOST	NOISY           	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	131AE	13902				S787				FUEL BOOST PUMP RUNS LOUD, LOW PRESSURE.						1	G	7	2 	3U				H3EU    					 
1999121100520	19991211	00520		1999	12	11	HEEA065176       	4	19991115	G	3120	811B	CLOCK           			BELL  	412   	412         	1182202	SW  										COCKPIT	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5759N					33002				DIGITAL CLOCK INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999121100643	19991211	00643	EU  	1999	12	11	HEEA065177       	1	19991115	G	2435	23032048	STARTER         			BOLKMS	105   	BO105S      	5626006	EU  										STARTER/GEN	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911BR	7747 				S719				STARTER/GENERATOR WILL NOT MOTOR ENGINE.						1	G	7	2 	3U				H3EU    					 
1999121100521	19991211	00521	SW  	1999	12	11	HEEA065178       	1	19991115	G	6220	407010101101	YOKE            			BELL  	407   	407         		SW  										M/R HEAD	DAMAGED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	404PH	1234 				53188				DEEP SCRATCH IN WEB OF YOKE EXCEEDS ALLOWABLE LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999121100522	19991211	00522		1999	12	11	HEEA065179       	4	19991115	G	3452	066106200	TRANSPONDER     			BELL  	206   	206L3       	1182108	SW  										OSILLATOR	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6160Z					51610				TRANSCEIVER'S I.D. LIGHT STAYS ON.						1	G	7	1 	3U				H2SW    					 
1999121100194	19991211	00194	NE  	1999	12	11	HEEA065180       	1	19991115	G	6240	7645001076103	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										TRIPLE TACH	STICKING        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	15460					760223				NR 2 NEEDLE STICKS AT 40 PERCENT  WHEN DC POWER IS TURNED OFF WITH ENGINES SPOOLING DOWN.  TURNED POWER BACK ON TO NR 2,	 NEEDLE GOES TO ZERO.					1	G	7	2 	3U				H1NE    					 
1999121100523	19991211	00523	SW  	1999	12	11	HEEA065181       	1	19991115	G	7712	412075008111	INDICATOR       			BELL  	412   	412         	1182202	SW  										DUAL TORQUE	FLUCTUATING     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893S					33022				TORQUE INDICATOR FLUCTUATING.						1	G	7	2 	4U				H4SW    					 
1999121100524	19991211	00524		1999	12	11	HEEA065182       	4	19991115	G	2211	7000298901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893S					33022				AFCS ACTUATORS SLOW TO TRIM AND RE-CENTER.						1	G	7	2 	4U				H4SW    					 
1999121100644	19991211	00644	EU  	1999	12	11	HEEA065183       	1	19991115	G	6410	355A12004008	BLADE BEARING   			SNIAS 	350   	AS350B2     	8680813	EU  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L	1876 				2873				LAMINATED BEARINGS WORN, ABRASIVE STRIP PEELING, AND SPAR CRACKED.  DAMAGE TO CHINESE WEIGHT NEXT TO SPAR.						1	G	7	1 	3U				H9EU    					 
1999121100645	19991211	00645	EU  	1999	12	11	HEEA065184       	1	19991115	G	7714	56337078012	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										NG TACH	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6095S					2777				BLEED VALVE FLAG WILL NOT PULL.						1	G	7	1 	3U				H9EU    					 
1999121100195	19991211	00195	GL  	1999	12	11	HEEA065187       	2	19991116	G	7230	23004513	CARBON SEAL     		23033193    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C30P     	03013	GL  					COMPRESSOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	45RP	578  			CAC91088	45521	CAE895584			ENGINE REMOVED DUE TO TURBINE OVERHAUL.  UPON INSPECTION OF COMPRESSOR PARTS NOTED GROOVED TANG SLOTS BEYOND SERVICEABLE	 LIMITS ON CARBON SEAL ASSY. REQU					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999121100196	19991211	00196	GL  	1999	12	11	HEEA065188       	2	19991116	G	7230	23056634	GEARSHAFT       		23033193    	BELL  	206   	206L1       	1182107	SW  	ALLSN 	250C  	250C30P     	03013	GL  					SPUR ADAPTER	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	45RP	578  			CAC91088	45521	CAE895584			ENGINE REMOVED DUE TO TURBINE OVERHAUL.  UPON INSPECTION OF COMPRESSOR PARTS NOTED STEP WEAR BEYOND SERVICEABLE LIMITS O	N SPUR GEAR AFT END SPLINES.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999121100197	19991211	00197	GL  	1999	12	11	HEEA065189       	2	19991116	G	7230	23056634	GEARSHAFT       		23033193    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					SPUR ADAPTER	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6251X	555  			CAC90149	51552	CAE895594			ENGINE REMOVED DUE TO CRACKED SCROLL AND CRACKED EXHAUST COLLECTOR.   UPON INSPECTION OF COMPRESSOR PARTS NOTED EXCESSIV	E STEP WEAR ON SPUR GEAR AFT END SPLINES.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999121100198	19991211	00198	GL  	1999	12	11	HEEA065190       	2	19991116	G	7250	23062750	NOZZLE SHIELD   		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81832	833  			CAT33770	S828	CAE830763			ENGINE REMOVED DUE TO EXCESSIVE OIL CONSUMPTION (1 QUART PER MINUTE).  UPON INSPECTION OF TURBINE PARTS NOTED DOME CRACK	ED FROM 3 O'CLOCK TO 7 O'CLOCK POSITION ATTACHING BRAZEMENT CAUSING COKING OF NR 8 BEARING AREA.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100525	19991211	00525	SW  	1999	12	11	HEEA065191       	1	19991116	G	6510	206061432121	HOUSING         			BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	720PH					53277				BLOWER HOUSING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999121100526	19991211	00526	SW  	1999	12	11	HEEA065192       	1	19991116	G	2910	70079H000Y150	HOSE            			BELL  	407   	407         		SW  										HYD SYSTEM	COLLAPSED       	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	404PH					53188				HOSE ASSY COLLAPSED.						1	G	7	1 	3U			O	H2SW    					 
1999121100527	19991211	00527		1999	12	11	HEEA065193       	4	19991117	G	2211	4025008918	COMPUTER        			BELL  	412   	412         	1182202	SW  										AFCS	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3911L					33023				COMPUTER TRIPS CIRCUIT BREAKER.						1	G	7	2 	4U				H4SW    					 
1999121100528	19991211	00528	SW  	1999	12	11	HEEA065194       	1	19991117	G	2422	ASH5845	INVERTER        			BELL  	212   	212         	1181420	SW  										AC SYSTEM	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5736D					31135				INVERTER INTERMITTENTLY GOES OFF-LINE.						1	G	7	1 	4U				H4SW    					 
1999121100529	19991211	00529	SW  	1999	12	11	HEEA065195       	1	19991117	G	2422	PS3041	INVERTER        			BELL  	212   	212         	1181420	SW  										AC SYSTEM	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5736J					31140				INVERTER HAD INTERMITTENT OPERATIONS.						1	G	7	1 	4U				H4SW    					 
1999121100530	19991211	00530	SW  	1999	12	11	HEEA065196       	1	19991117	G	2844	124044	INDICATOR       			BELL  	412   	412         	1182202	SW  										FUEL PRESSURE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22347					36005				FUEL PRESSURE INDICATOR CANNOT CALIBRATE, UNIT IS NON-LINEAR THROUGH SCALE, BENCH CHECK BAD, FADED RANGE MARKINGS.						1	G	7	2 	4U				H4SW    					 
1999121100199	19991211	00199		1999	12	11	HEEA065197       	1	19991117	G	2822	91380003	PUMP            			KING A														FUEL BOOST	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	500PH					BL29				GREASE LEAKING FROM DRAIN.																			 
1999121100200	19991211	00200	NE  	1999	12	11	HEEA065198       	1	19991117	G	7930	7645001078101	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										ENGINE OIL	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	707AE					760276				INDICATOR GLASS DISTORTED.						1	G	7	2 	3U				H1NE    					 
1999121100531	19991211	00531	SW  	1999	12	11	HEEA065199       	1	19991117	G	7712	206075739103	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TORQUEMETER	DISCOLORED      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2775A					45297				TORQUEMETER INDICATOR RANGE MARKINGS DISCOLORED.						1	G	7	1 	3U				H2SW    					 
1999121100532	19991211	00532	SW  	1999	12	11	HEEA065200       	1	19991117	G	7712	206075739103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TORQUEMETER	STICKING        	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	31801					51074				TORQUEMETER INDICATOR STICKING AT 80 PERCENT TO 90 PERCENT RANGE AND GLASS IS FOGGY.						1	G	7	1 	3U				H2SW    					 
1999121100533	19991211	00533	SW  	1999	12	11	HEEA065201       	1	19991117	G	7712	206075185103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										TORQUE	FADED           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	31821					51076				TORQUE INDICATOR GLASS IS FOGGY AND RANGE MARKINGS ARE FADED.						1	G	7	1 	3U				H2SW    					 
1999121100534	19991211	00534	SW  	1999	12	11	HEEA065202       	1	19991117	G	7712	206075185101	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										TORQUE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	2251A					45755				TORQUEMETER INDICATOR GAUGE BOUNCES IN-FLIGHT.						1	G	7	1 	3U				H2SW    					 
1999121100646	19991211	00646		1999	12	11	HEEA065203       	4	19991117	G	3425	066304605	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										GLIDESCOPE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4000L					2873				GLIDESCOPE FLAG INOPERATIVE.						1	G	7	1 	3U				H9EU    					 
1999121100647	19991211	00647		1999	12	11	HEEA065204       	4	19991117	G	3425	066304605	INDICATOR       			BOLKMS	105   	BO105S      	5626006	EU  										GLIDESCOPE	INACCURATE      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911HM					S683				HSI CONTROL INDICATED 90 DEGREES OFF COURSE.						1	G	7	2 	3U				H3EU    					 
1999121100535	19991211	00535	SW  	1999	12	11	HEEA065205       	1	19991117	G	3212	206050248117	FLOAT           			BELL  	206   	206L3       	1182108	SW  										MLG	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	6610C					51425				FLOAT BAG LEAKING.						1	G	7	1 	3U				H2SW    					 
1999121100201	19991211	00201		1999	12	11	HEEA065206       	4	19991117	G	2312	064100900	TRANSCEIVER     			SKRSKY	S76   	S76A        	8143006	NE  										COCKPIT	WEAK            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	911MJ					760231				TRANSCEIVER HAD WEAK TRANSMIT.						1	G	7	2 	3U				H1NE    					 
1999121100536	19991211	00536		1999	12	11	HEEA065207       	4	19991117	G	3432	066400700	RECEIVER        			BELL  	212   	212         	1181420	SW  										GLIDESLOPE	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	1082G					31109				RECEIVER FAILED 2 YEAR INSPECTION.						1	G	7	1 	4U				H4SW    					 
1999121100537	19991211	00537		1999	12	11	HEEA065208       	4	19991117	G	2312	064102300	TRANSCEIVER     			BELL  	412   	412         	1182202	SW  										VHF COMM	FAILED          	E			HEEA	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	2149S					36002				VHF TRANSCEIVER FAILED 2 YEAR INSPECTION.						1	G	7	2 	4U				H4SW    					 
1999121100538	19991211	00538	SW  	1999	12	11	HEEA065209       	1	19991117	G	6240	209075326005	WARNING BOX     			BELL  	212   	212         	1181420	SW  										M/R RPM	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5736J					31140				ENGINE OUT LIGHTS AND HORN BLINK INTERMITTENTLY.						1	G	7	1 	4U				H4SW    					 
1999121100539	19991211	00539	EA  	1999	12	11	HEEA065210       	2	19991117	G	7322	124044	INDICATOR       			BELL  	212   	212         	1181420	SW  	PWA   	PT6T  	PT6T3       	52045	EA  					FUEL PRESSURE	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5010F					30936				FUEL PRESSURE INDICATOR INTERMITTENTLY STICKS AT ZERO.						1	G	7	1 	4U	4	U		H4SW    	E22EA				 
1999121100540	19991211	00540	EA  	1999	12	11	HEEA065211       	2	19991117	G	7322	124044	INDICATOR       			BELL  	212   	212         	1181420	SW  	PWA   	PT6T  	PT6T3       	52045	EA  					FUEL PRESSURE	ERRATIC         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5010F					30936				FUEL PRESSURE INDICATOR HAD UNRELIABLE ERRATIC READINGS.						1	G	7	1 	4U	4	U		H4SW    	E22EA				 
1999121100541	19991211	00541	GL  	1999	12	11	HEEA065212       	2	19991117	G	7322	206063633103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C20B     	03013	GL  					FUEL PRESSURE	CONTAMINATED    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6610Y					51419				FUEL QUANTITY INDICATOR HAD OIL BETWEEN THE GLASS.						1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999121100542	19991211	00542	SW  	1999	12	11	HEEA065213       	1	19991117	G	2436	206075447007	REGULATOR       			BELL  	206   	206L1       	1182107	SW  										DC SYSTEM	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	10814					45415				VOLTAGE REGULATOR NOT EXCITING FIELD.						1	G	7	1 	3U				H2SW    					 
1999121100543	19991211	00543	SW  	1999	12	11	HEEA065214       	1	19991117	G	2730	214001970107	ACTUATOR ASSY   			BELL  	214   	214ST       	1182106	SW  										ELEVATOR	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	59806					28140				ACTUATOR ASSY NOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999121100648	19991211	00648	GL  	1999	12	11	HEEA065215       	2	19991117	G	7412	49522	EXCITER         			BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					ENGINE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	137AE					S851				EXCITER INOPERATIVE.						1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999121100544	19991211	00544	SW  	1999	12	11	HEEA065216       	1	19991117	G	7931	206075677103	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										OIL PRESSURE	READS HIGH      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	54641					51184				ENGINE OIL PRESSURE READS HIGH.						1	G	7	1 	3U				H2SW    					 
1999121100545	19991211	00545		1999	12	11	HEEA065217       	4	19991117	G	2211	7000299901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AUTOPILOT	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	800Y					33134				AUTOPILOT CONTROL DOES NOT COUPLE WHEN FLIGHT DIRECTOR MODE IS SELECTED.						1	G	7	2 	4U				H4SW    					 
1999121100546	19991211	00546		1999	12	11	HEEA065218       	4	19991117	G	3420	1113025	INDICATOR       			BELL  	412   	412         	1182202	SW  										HSI	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893P					33012				HSI INDICATOR'S YELLOW NEEDLE OFF.  FLAGS WILL NOT PULL.						1	G	7	2 	4U				H4SW    					 
1999121100547	19991211	00547	SW  	1999	12	11	HEEA065219       	1	19991117	G	2437	209070264003	INDICATOR       			BELL  	212   	212         	1181420	SW  										DUAL AMMETER	READS HIGH      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5010F					30936				AMMETER READS 50 AMPS HIGHER.						1	G	7	1 	4U				H4SW    					 
1999121100548	19991211	00548	SW  	1999	12	11	HEEA065220       	1	19991117	G	7714	212070108007	INDICATOR       			BELL  	212   	212         	1181420	SW  										TRIPLE TACH	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5736J					31140				TRIPLE TACHOMETER'S NR 2 NEEDLE WILL NOT MOVE.  STAYS ON ZERO.						1	G	7	1 	4U				H4SW    					 
1999121100549	19991211	00549		1999	12	11	HEEA065221       	4	19991117	G	3421	214175241101	GYROSCOPE       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5748M					28102				ATTITUDE INDICATOR INOPERATIVE.						2	G	7	2 	4U				H10SW   					 
1999121100550	19991211	00550	SW  	1999	12	11	HEEA065222       	1	19991117	G	7720	214175248103	INDICATOR       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	STICKING        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8045T					28101				TEMPERATURE NEEDLE STICKS AT 625 DEGREES PERIODICALLY.						2	G	7	2 	4U				H10SW   					 
1999121100551	19991211	00551	SW  	1999	12	11	HEEA065223       	1	19991117	G	2840	206075186005	INDICATOR       			BELL  	206   	206L1       	1182107	SW  										COCKPIT	FADED           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2124Z					45646				DUAL INDICATOR'S MARKINGS FADED.						1	G	7	1 	3U				H2SW    					 
1999121100552	19991211	00552		1999	12	11	HEEA065224       	4	19991117	G	3421	102005901	INDICATOR       			BELL  	412   	412         	1182202	SW  										COCKPIT	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	142PH					33150				INDICATOR LIGHT INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999121100553	19991211	00553		1999	12	11	HEEA065225       	4	19991117	G	3424	214075244001	RATE GYRO       			BELL  	214   	214ST       	1182106	SW  										COCKPIT	NOISY           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6957Y					28139				GYRO MAKING LOUD NOISE.						2	G	7	2 	4U				H10SW   					 
1999121100554	19991211	00554	SW  	1999	12	11	HEEA065226       	1	19991117	G	2820	AV24B1119B	VALVE           			BELL  	212   	212         	1181420	SW  										CROSSFEED	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5010F					30936				VALVE INOPERATIVE.						1	G	7	1 	4U				H4SW    					 
1999121100555	19991211	00555	SW  	1999	12	11	HEEA065227       	1	19991117	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										FLIGHT CONTOL	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2261D					33076				MAG. BRAKE WILL NOT RELEASE ELECTRICALLY, INTERMITTENT.						1	G	7	2 	4U				H4SW    					 
1999121100556	19991211	00556	SW  	1999	12	11	HEEA065228       	1	19991117	G	7714	412075010109	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	108X					33115				NR 2 ENGINE N2 NEEDLE IS INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999121100202	19991211	00202	NE  	1999	12	11	HEEA065229       	1	19991117	G	2434	7655009006105	CONTROL UNIT    			SKRSKY	S76   	S76A        	8143006	NE  										DC SYSTEM	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	707AE					760276				GEN. NR 2 KICKS OFF LINE IN -FLIGHT.						1	G	7	2 	3U				H1NE    					 
1999121100557	19991211	00557	SW  	1999	12	11	HEEA065230       	1	19991117	G	7714	412075010111	INDICATOR       			BELL  	412   	412         	1182202	SW  										TRIPLE TACH	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893L					33006				NR 1 NEEDLE INOPERATIVE.						1	G	7	2 	4U				H4SW    					 
1999121100203	19991211	00203		1999	12	11	HEEA065231       	4	19991117	G	3421	501145301	VERTICAL GYRO   			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	KICKING         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5426U					760167				NR 1 PITCH KICKING.						1	G	7	2 	3U				H1NE    					 
1999121100204	19991211	00204		1999	12	11	HEEA065232       	4	19991117	G	3421	7660002113103	VERTICAL GYRO   			SKRSKY	S76   	S76A        	8143006	NE  										AFCS	INOPERATIVE     	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4253S					760035				VERTICAL GYRO WILL NOT COME ON-LINE.						1	G	7	2 	3U				H1NE    					 
1999121100205	19991211	00205		1999	12	11	HEEA065233       	4	19991117	G	3420	125780	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										ADI	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	5426U					760167				COPILOT'S TURN AND SLIP INDICATOR  INTERMITTENTLY INOPERATIVE.						1	G	7	2 	3U				H1NE    					 
1999121100206	19991211	00206		1999	12	11	HEEA065234       	4	19991117	G	3455	066104701	RECEIVER        			SKRSKY	S76   	S76A        	8143006	NE  										ADF	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5435V					760158				NO CONTROL HEAD BACK LIGHTING.  NO GROUND FOR LIGHTING.  PIN J NOT GROUNDED TO CASE.  TIME SINCE REPAIR 19:30 HOURS.						1	G	7	2 	3U				H1NE    					 
1999121100207	19991211	00207	NE  	1999	12	11	HEEA065235       	1	19991117	G	6240	7690001881103	AMPLIFIER       			SKRSKY	S76   	S76A        	8143006	NE  										VIB ABSORBER	INTERMITTENT    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	1545K					760047				AMPLIFLIER HAD INTERMITTENT OPERATION.						1	G	7	2 	3U				H1NE    					 
1999121100558	19991211	00558	SW  	1999	12	11	HEEA065236       	1	19991117	G	7931	206075187003	INDICATOR       			BELL  	206   	206L3       	1182108	SW  										ENGINE OIL	READS HIGH      	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	31801					51074				INDICATOR READS AT RED LINE 130 PSI.  ALL ENGINE TEMPERATURES DIRECT READING GAUGE SHOWS 120-150.						1	G	7	1 	3U				H2SW    					 
1999121100559	19991211	00559	SW  	1999	12	11	HEEA065237       	1	19991117	G	2120	212073927003	CONTROLLER      			BELL  	412   	412         	1182202	SW  										AIR DISTRIBUTION	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3893N					33010				HEATER INTERMITTENT.						1	G	7	2 	4U				H4SW    					 
1999121100649	19991211	00649	EU  	1999	12	11	HEEA065238       	1	19991117	G	6220	350A31185002	SLEEVE          			SNIAS 	350   	AS350B2     	8680813	EU  										M/R HEAD	GOUGED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6097Z	2005 				2820				GOUGE IN SLEEVE NEAR BLADE BOLT BUSHING.						1	G	7	1 	3U				H9EU    					 
1999121100208	19991211	00208		1999	12	11	HEEA065239       	4	19991117	G	3421	125780	INDICATOR       			SKRSKY	S76   	S76A        	8143006	NE  										ADI	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	5426U					760167				UNABLE TO ADJUST HORIZON ENOUGH TO BRING IT BACK LEVEL.						1	G	7	2 	3U				H1NE    					 
1999121100560	19991211	00560		1999	12	11	HEEA065240       	4	19991117	G	3420	1113025	INDICATOR       			BELL  	412   	412         	1182202	SW  										HSI	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	3893L					33006				HSI INDICATOR TRIPS CIRCUIT BREAKER.						1	G	7	2 	4U				H4SW    					 
1999121100561	19991211	00561	SW  	1999	12	11	HEEA065241       	1	19991119	G	2435	206062200123	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GEN	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH					53278				STARTER/GENERATOR BRUSHES WORN.  INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES EXCESSIVELY WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100562	19991211	00562	SW  	1999	12	11	HEEA065242       	1	19991119	G	2435	206062200113	STARTER         			BELL  	407   	407         		SW  										STARTER/GEN	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	457PH					53147				STARTER/GENERATOR WILL NOT MOTOR.  INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES EXCESSIVELY WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100209	19991211	00209	GL  	1999	12	11	HEEA065243       	2	19991119	G	7250	6853279	WHEEL           		6898735     	BELL  	206   	206B3       	1181506	SW  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE SECTION	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3181J				CAT20807F	3771				TURBINE WAS REMOVED DUE TO 1ST, 2ND, AND 3RD STAGE WHEELS CYCLED.  RECEIVING ASSEMBLY INSPECTION REVEALED EXCESSIVE RUNO	UT OF OUTER BAND AND WAS UNABLE TO BALANCE 4TH STAGE WHEEL.  INSTALLED NEW PART.					1	G	7	1 	3U	3	U		H2SW    	E4CE				 
1999121100210	19991211	00210	NE  	1999	12	11	HEEA065244       	2	19991119	G	7421	0301017420	MOUNT           			SNIAS 	350   	AS350B2     	8680813	EU  	TMECA 	ARRIEL	ARRIEL1B    	6OO30	NE  					IGNITER	CRACKED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	40466					3004				IGNITER MOUNT CRACKED.						1	G	7	1 	3U	3	U		H9EU    	E19EU				 
1999121100563	19991211	00563	SW  	1999	12	11	HEEA065247       	1	19991119	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	719PH	1000 				53266				UNIVERSAL BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100564	19991211	00564	SW  	1999	12	11	HEEA065248       	1	19991119	G	6420	407312100101	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	2778 				53159				ELASTOMERIC SEPARATION EXTRUDING ON BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999121100565	19991211	00565	SW  	1999	12	11	HEEA065249       	1	19991119	G	6210	407015001117	BLADE           			BELL  	407   	407         		SW  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	2913 				53159				MAIN ROTOR BLADE CRACKED AT TRAILING EDGE BY TRIM TAB.						1	G	7	1 	3U			O	H2SW    					 
1999121100566	19991211	00566	SW  	1999	12	11	HEEA065250       	1	19991119	G	6210	407015001117	BLADE           			BELL  	407   	407         		SW  										MAIN ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH	2913 				53159				MAIN ROTOR BLADE CRACKED AT TRAILING EDGE BY TRIM TAB.						1	G	7	1 	3U			O	H2SW    					 
1999121100567	19991211	00567	SW  	1999	12	11	HEEA065251       	1	19991119	G	6310	406040316101	SPLINES         			BELL  	407   	407         		SW  										ADAPTER	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				ADAPTER SPLINES WORN.						1	G	7	1 	3U			O	H2SW    					 
1999121100568	19991211	00568	SW  	1999	12	11	HEEA065259       	1	19991119	G	2822	1C2710	CARTRIDGE       			BELL  	407   	407         		SW  										FUEL PUMP	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	407MM					53060				FUEL PUMP QUITS RUNNING IN A SHORT TIME.						1	G	7	1 	3U			O	H2SW    					 
1999121100569	19991211	00569	SW  	1999	12	11	HEEA065260       	1	19991119	G	6720	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										M/R DRIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH	2685 				53059				UNIVERSAL BEARING HAD AXIAL PLAY.						1	G	7	1 	3U			O	H2SW    					 
1999121100570	19991211	00570	SW  	1999	12	11	HEEA065261       	1	19991119	G	7910	206061505115	VENT            			BELL  	407   	407         		SW  										OIL TANK	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	722PH					53288				TOP VENT FITTING CRACKED ON TANK ASSEMBLY.						1	G	7	1 	3U			O	H2SW    					 
1999122300234	19991223	00234	SW  	1999	12	23	HEEA065285       	1	19991123	G	6320	407040006107	TRANSMISSION    			BELL  	407   	407         		SW  										MAIN ROTOR	MAKING METAL    	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	141MA	2329 				53016				FOUND METAL IN OIL.						1	G	7	1 	3U			O	H2SW    					 
1999122300235	19991223	00235	SW  	1999	12	23	HEEA065286       	1	19991123	G	6322	PHIPBH40701	BLOWER          			BELL  	407   	407         		SW  										OIL COOLER	DAMAGED         	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	404PH					53188				UNABLE TO BALANCE OIL COOLER BLOWER.						1	G	7	1 	3U			O	H2SW    					 
1999122300236	19991223	00236	SW  	1999	12	23	HEEA065287       	1	19991123	G	6520	406040400115	GEARBOX         			BELL  	407   	407         		SW  										TAIL ROTOR	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	57416	1142 				53070				OIL LEAK FROM PITCH CHANGE OUTPUT SHAFT.						1	G	7	1 	3U			O	H2SW    					 
1999122300237	19991223	00237	SW  	1999	12	23	HEEA065288       	1	19991123	G	6230	407040011101	MAST ASSY       			BELL  	407   	407         		SW  										MAIN ROTOR	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	402PH	2625 				53159				SEAL LEAKING ON MAST ASSEMBLY.						1	G	7	1 	3U			O	H2SW    					 
1999122300238	19991223	00238	SW  	1999	12	23	HEEA065290       	1	19991123	G	6300	406340102101	CARBON SEAL     		406040500123	BELL  	407   	407         		SW  										M/R DRIVE	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	409PH	1203 			A4361	53059				CARBON SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
1999122300239	19991223	00239	SW  	1999	12	23	HEEA065291       	1	19991123	G	6300	406340102101	CARBON SEAL     		406040500123	BELL  	407   	407         		SW  										M/R DRIVE	LEAKING         	E			HEEA	O				OTHER                   				K			FLUID LOSS                			NR	NOT REPORTED   	1			SW	03	405PH				A4294	53207				CARBON SEAL LEAKING AND WEAR SLEEVE ON OUTPUT ADAPTER IS WORN.						1	G	7	1 	3U			O	H2SW    					 
1999122300240	19991223	00240	SW  	1999	12	23	HEEA065293       	1	19991124	G	6420	407310203101	MOUNT           			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH	1985 				53188				CRACKS IN ELASTOMER ARE BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999122300241	19991223	00241	SW  	1999	12	23	HEEA065294       	1	19991124	G	6420	407310203101	MOUNT           			BELL  	407   	407         		SW  										TAIL ROTOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH	1985 				53188				CRACKS IN ELASTOMER ARE BEYOND LIMITS.						1	G	7	1 	3U			O	H2SW    					 
1999122300244	19991223	00244		1999	12	23	HEEA065297       	4	19991129	G	2211	4033089901	COMPUTER        			BELL  	412   	412         	1182202	SW  										AUTO FLIGHT	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	800Y					33134				FLIGHT DIRECTOR DECOUPLES WHEN IAS IS SELECTED.						1	G	7	2 	4U				H4SW    					 
1999122300245	19991223	00245	SW  	1999	12	23	HEEA065298       	1	19991129	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	2149S					36002				ACTUATOR WOULD NOT RETRACT.  TIME SINCE REPAIR 357:05 HOURS.						1	G	7	2 	4U				H4SW    					 
1999122300246	19991223	00246	SW  	1999	12	23	HEEA065299       	1	19991129	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	7128R					36007				ACTUATOR WOULD NOT RETRACT.  TIME SINCE REPAIR 158:40 HOURS.						1	G	7	2 	4U				H4SW    					 
1999122300247	19991223	00247	SW  	1999	12	23	HEEA065300       	1	19991129	G	5260	212075418105	ACTUATOR        			BELL  	412   	412         	1182202	SW  										STEP	SLOW            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	22608					33075				ACTUATOR MOVES VERY SLOW.  TIME SINCE REPAIR 117:05 HOURS.						1	G	7	2 	4U				H4SW    					 
1999122300227	19991223	00227	GL  	1999	12	23	HEEA065301       	2	19991130	G	7250	23062753	NOZZLE          		6898735     	BOLKMS	105   	BO105S      	5626006	EU  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	81832	833  			CAT33770	S828	CAE830763			ENGINE REMOVED DUE TO EXCESSIVE OIL CONSUMPTION (1 QUART PER MINUTE).  UPON INSPECTION OF TURBINE PARTS NOTED VANES CRAC	KED AND ERODED MAR-M COATING.					1	G	7	2 	3U	3	U		H3EU    	E4CE				 
1999122300228	19991223	00228	GL  	1999	12	23	HEEA065302       	2	19991130	G	7260		COLLECTOR       		23053349    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41128	5715 			CAG95691	51465	CAE895576			CRACKED EXHAUST COLLECTOR.  REMOVED IN COMPLIANCE WITH CEBA72-3217 R-2.  SERIAL NUMBERS REMOVED ARE MP03890 AND MP03914.	  REPLACED WITH SERIAL NUMBERS JJ02242 AND JJ02236.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999122300229	19991223	00229	GL  	1999	12	23	HEEA065303       	2	19991130	G	7260		COLLECTOR       		23053349    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	41128	5715 			CAG95691	51465	CAE895576			CRACKED EXHAUST COLLECTOR.  REMOVED IN COMPLIANCE WITH CEBA72-3217 R-2.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999122300230	19991223	00230	GL  	1999	12	23	HEEA065304       	2	19991130	G	7260	23031219	BEARING         		23053349    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					NR 2 & 3	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	32041	9018 			CAG90649	51539	CAE890166			ENGINE HAS WHINE RELATED TO N1 SPEED.  BEARINGS REMOVED IN COMPLIANCE WITH CEBA72-3217 R-2.   SERIAL NUMBERS REMOVED ARE	 MP01700 AND MP01418.  REPLACED WITH SERIAL NUMBERS JJ02197 AND JJ02207.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999122300231	19991223	00231	GL  	1999	12	23	HEEA065305       	2	19991130	G	7260	230312681	BEARING         		23053349    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					NR 3 & 4	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	32041	9018 			CAG90649	51539	CAE890166			ENGINE HAS WHINE RELATED TO N1 SPEED.  BEARINGS REMOVED IN COMPLIANCE WITH CEBA72-3217 R-2.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999122300232	19991223	00232	GL  	1999	12	23	HEEA065306       	2	19991130	G	7260	23031219	BEARING         		23035178    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					NR 3 & 4	CLOGGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A	6515 			CAG95496	51611	CAE895491			ENGINE REMOVED DUE TO 6 AND 7 BEARING SUMP CLOGGED.   BEARINGS REMOVED IN COMPLIANCE WITH CEBA72-3217 R-2.   SERIAL NUMB	ERS REMOVED ARE MP00520 AND MP01232.  REPLACED WITH SERIAL NUMBERS JJ02374 AND JJ02192.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999122300233	19991223	00233	GL  	1999	12	23	HEEA065307       	2	19991130	G	7260	230312681	BEARING         		23035178    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					NR 3 & 4	CLOGGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6161A	6515 			CAG95496	51611	CAE895491			ENGINE REMOVED DUE TO 6 AND 7 BEARING SUMP CLOGGED.  BEARINGS REMOVED IN COMPLIANCE WITH CEBA72-3217 R-2.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
1999122300248	19991223	00248	SW  	1999	12	23	HEEA065310       	1	19991130	G	8011	214060056103	STARTER         			BELL  	214   	214ST       	1182106	SW  										ENGINE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	6957Y	573  				28139				WHEN STARTING OFF BATTERY KICKS OFF AT 10 PERCENT.						2	G	7	2 	4U				H10SW   					 
1999122300249	19991223	00249	SW  	1999	12	23	HEEA065312       	1	19991130	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GEN	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407PH	1568 				53003				FAILED 300-HOUR INSPECTION.  BRUSHES HAD EXCESSIVE WEAR.						1	G	7	1 	3U			O	H2SW    					 
1999122300250	19991223	00250	SW  	1999	12	23	HEEA065316       	1	19991203	G	6510	406040320101	SHAFT           			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				SPLINES WORN BEYOND LIMITS ON SHAFT ASSEMBLY.						1	G	7	1 	3U			O	H2SW    					 
1999122300251	19991223	00251	SW  	1999	12	23	HEEA065319       	1	19991207	G	6420	407312100101	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM	2484 				53060				ELASTOMER SEPARATED AND EXTRUDING.						1	G	7	1 	3U			O	H2SW    					 
1999122300252	19991223	00252	SW  	1999	12	23	HEEA065320       	1	19991207	G	6300	407340339103	BEARING         		PHIPBH40701 	BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH				AFS1399	53277				BEARING WORN AND ROUGH.  SERIAL NUMBERS REMOVED ARE E99-0669 AND E99-1670.						1	G	7	1 	3U			O	H2SW    					 
1999122300253	19991223	00253	SW  	1999	12	23	HEEA065321       	1	19991207	G	6322	406040320101	SHAFT           			BELL  	407   	407         		SW  										COOLER BLOWER	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				SPLINES WORN BEYOND LIMITS ON SHAFT ASSEMBLY.						1	G	7	1 	3U			O	H2SW    					 
1999122300254	19991223	00254	SW  	1999	12	23	HEEA065322       	1	19991207	G	6410	406312100101	BEARING         		407012101111	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM				53057	53060				WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999122300255	19991223	00255	SW  	1999	12	23	HEEA065323       	1	19991207	G	6410	406312100101	BEARING         		407012101105	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH	1861 			53187	53207				WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999122300256	19991223	00256	SW  	1999	12	23	HEEA065325       	1	19991208	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				UNIVERSAL HAD WORN BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999122300257	19991223	00257	SW  	1999	12	23	HEEA065326       	1	19991208	G	6420	407310203101	MOUNT           			BELL  	407   	407         		SW  										TAIL ROTOR	DEBONDED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				MOUNT RUBBER DEBONDED, OIL FOULED.						1	G	7	1 	3U			O	H2SW    					 
1999122300258	19991223	00258	SW  	1999	12	23	HEEA065327       	1	19991208	G	6420	407310203101	MOUNT           			BELL  	407   	407         		SW  										TAIL ROTOR	DEBONDED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	467PH					53142				MOUNT RUBBER DEBONDED, OIL FOULED.						1	G	7	1 	3U			O	H2SW    					 
1999122300259	19991223	00259	SW  	1999	12	23	HEEA065328       	1	19991208	G	6420	407310203101	MOUNT           			BELL  	407   	407         		SW  										TAIL ROTOR	DELAMINATED     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				BEARING DELAMINATED.						1	G	7	1 	3U			O	H2SW    					 
1999122300260	19991223	00260	SW  	1999	12	23	HEEA065329       	1	19991208	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	LOOSE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				UNIVERSAL HAD AXIAL PLAY.						1	G	7	1 	3U			O	H2SW    					 
1999122300261	19991223	00261	SW  	1999	12	23	HEEA065330       	1	19991208	G	7714	407375008101	INDICATOR       			BELL  	407   	407         		SW  										DUAL TACH	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				DUAL TACHOMETER DID NOT TEST.						1	G	7	1 	3U			O	H2SW    					 
1999122300262	19991223	00262	SW  	1999	12	23	HEEA065331       	1	19991208	G	6510	206061432121	HOUSING         			BELL  	407   	407         		SW  										COOLER BLOWER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				BLOWER HOUSING CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999122300263	19991223	00263	SW  	1999	12	23	HEEA065332       	1	19991208	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	417PH	2630 				53038				UNIVERSAL HAD BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999122300264	19991223	00264	SW  	1999	12	23	HEEA065333       	1	19991208	G	6710	406312103101	LINK            			BELL  	407   	407         		SW  										COLLECTIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	510PH					53209				WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999122300265	19991223	00265	SW  	1999	12	23	HEEA065334       	1	19991208	G	7714	407375002103	INDICATOR       			BELL  	407   	407         		SW  										ENGINE NG	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				NG INDICATOR INTERMITTENTLY GOES BLANK.						1	G	7	1 	3U			O	H2SW    					 
1999122300266	19991223	00266	SW  	1999	12	23	HEEA065335       	1	19991208	G	7714	407375002103	INDICATOR       			BELL  	407   	407         		SW  										ENGINE NG	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	437PH					53072				NG INDICATOR SELF-TEST INTERMITTENTLY.						1	G	7	1 	3U			O	H2SW    					 
1999122300267	19991223	00267	SW  	1999	12	23	HEEA065336       	1	19991208	G	7931	407375004101	INDICATOR       			BELL  	407   	407         		SW  										ENG OIL PRESS	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4999					53323				ENGINE OIL TEMPERATURE PRESSURE GOES FULL TO ZERO CONSTANTLY.						1	G	7	1 	3U			O	H2SW    					 
1999122300268	19991223	00268	SW  	1999	12	23	HEEA065337       	1	19991208	G	3246	206053184121	SKID TUBE       			BELL  	407   	407         		SW  										MLG	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH					53228				SKID TUBE ASSY, AFT END WORN.						1	G	7	1 	3U			O	H2SW    					 
1999122300269	19991223	00269	SW  	1999	12	23	HEEA065338       	1	19991208	G	3246	206053184121	SKID TUBE       			BELL  	407   	407         		SW  										MLG	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	408PH					53228				SKID TUBE ASSY, AFT END WORN.						1	G	7	1 	3U			O	H2SW    					 
1999122300270	19991223	00270	SW  	1999	12	23	HEEA065343       	1	19991208	G	6420	407310203101	MOUNT           			BELL  	407   	407         		SW  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				MOUNT RUBBER TORN.						1	G	7	1 	3U			O	H2SW    					 
1999122300271	19991223	00271	SW  	1999	12	23	HEEA065344       	1	19991208	G	6420	407310203101	MOUNT           			BELL  	407   	407         		SW  										TAIL ROTOR	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				MOUNT RUBBER TORN.						1	G	7	1 	3U			O	H2SW    					 
1999122300272	19991223	00272	SW  	1999	12	23	HEEA065348       	1	19991208	G	7933	407375004101	INDICATOR       			BELL  	407   	407         		SW  										ENG OIL TEMP	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4999					53323				NO ENGINE OIL INDICATION ON START-UP.						1	G	7	1 	3U			O	H2SW    					 
1999122300273	19991223	00273	SW  	1999	12	23	HEEA065349       	1	19991208	G	2420	SM20ACD300A21	RELAY           			BELL  	407   	407         		SW  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	402PH					53159				INTERMITTENT NO START LIGHT AND NO IGNITER ON START.						1	G	7	1 	3U			O	H2SW    					 
1999122300274	19991223	00274		1999	12	23	HEEA065350       	4	19991209	G	3421	5040045902	INDICATOR       			BELL  	407   	407         		SW  										COCKPIT ATTITUDE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	141MA					53016				ATT INDICATOR TILTS GRADUALLY MORE AND MORE.						1	G	7	1 	3U			O	H2SW    					 
1999122300275	19991223	00275	SW  	1999	12	23	HEEA065351       	1	19991209	G	5210	206031324001	HINGE           			BELL  	407   	407         		SW  										CREW DOOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8595X					53267				HINGE CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999122300276	19991223	00276	SW  	1999	12	23	HEEA065352       	1	19991209	G	5210	206031323001	HINGE           			BELL  	407   	407         		SW  										CREW DOOR	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8595X					53267				HINGE CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999122300277	19991223	00277	SW  	1999	12	23	HEEA065353       	1	19991209	G	3210	70079H000Y150	HOSE            			BELL  	407   	407         		SW  										MLG	KINKED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH					53198				HOSE ASSY KINKED.						1	G	7	1 	3U			O	H2SW    					 
1999122300278	19991223	00278	SW  	1999	12	23	HEEA065354       	1	19991209	G	3340	A490A	POWER SUPPLY    			BELL  	407   	407         		SW  										STROBE	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH					53198				POWER SUPPLY, INTERMITTENT OPERATION.						1	G	7	1 	3U			O	H2SW    					 
1999122300279	19991223	00279	SW  	1999	12	23	HEEA065355       	1	19991209	G	6420	407310203101	MOUNT           			BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	406PH					53198				MOUNT WORN.  SERIAL NUMBERS REMOVED ARE LK-0799, LK-0855, LK-0817 AND LK-0860.  REPLACED WITH SERIAL NUMB NR 68244501, L	P-1869; DMR NR 68244503, LP-1859; DMR NR 68244500.					1	G	7	1 	3U			O	H2SW    					 
1999122300280	19991223	00280	SW  	1999	12	23	HEEA065356       	1	19991209	G	3340	A490ATSDF1428	POWER SUPPLY    			BELL  	407   	407         		SW  										STROBE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	723PH					53283				POWER SUPPLY INOPERATIVE.						1	G	7	1 	3U			O	H2SW    					 
1999122300281	19991223	00281	SW  	1999	12	23	HEEA065357       	1	19991209	G	6510	407340340101	DISC PACK       			BELL  	407   	407         		SW  										T/R DRIVE	CRAKED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	723PH					53283				DISC PACK CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999122300282	19991223	00282	SW  	1999	12	23	HEEA065358       	1	19991209	G	2822	407362013101	SWITCH          			BELL  	407   	407         		SW  										ENGINE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH					53207				PRESSURE SWITCH NOT EXTINGUISHING CAUTION LIGHT.						1	G	7	1 	3U			O	H2SW    					 
1999122300283	19991223	00283	SW  	1999	12	23	HEEA065359       	1	19991209	G	2822	407362013101	SWITCH          			BELL  	407   	407         		SW  										ENGINE	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	405PH					53207				PRESSURE SWITCH NOT FUNCTIONING.						1	G	7	1 	3U			O	H2SW    					 
1999122300284	19991223	00284	SW  	1999	12	23	HEEA065361       	1	19991209	G	2912	206076035103	FILTER          			BELL  	407   	407         		SW  										HYDRAULIC SYS	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				BYPASS BUTTON KEEPS TRIPPING.						1	G	7	1 	3U			O	H2SW    					 
1999122300285	19991223	00285	SW  	1999	12	23	HEEA065362       	1	19991209	G	6300	407010206103	BEARING         			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH	3362 				53114				BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999122300286	19991223	00286	SW  	1999	12	23	HEEA065363       	1	19991209	G	3340	A490A	POWER SUPPLY    			BELL  	407   	407         		SW  										STROBE	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				STROBE LIGHT INTERMITTENT.						1	G	7	1 	3U			O	H2SW    					 
1999122300287	19991223	00287	SW  	1999	12	23	HEEA065364       	1	19991209	G	7810	407062021101	DUCT            			BELL  	407   	407         		SW  										EXHAUST	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				DUCT CRACKED.						1	G	7	1 	3U			O	H2SW    					 
1999122300288	19991223	00288	SW  	1999	12	23	HEEA065365       	1	19991209	G	6420	407312100101	BEARING         			BELL  	407   	407         		SW  										TAIL ROTOR	SEPARATING      	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH					53114				RUBBER EXTRUDING AND SEPARATING ON BEARING.						1	G	7	1 	3U			O	H2SW    					 
1999122300289	19991223	00289	SW  	1999	12	23	HEEA065366       	1	19991209	G	6420	406312100101	BEARING         		407012101111	BELL  	407   	407         		SW  										TAIL ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	447PH				53207	53114				WORN BEARINGS.						1	G	7	1 	3U			O	H2SW    					 
1999122300290	19991223	00290	SW  	1999	12	23	HEEA065367       	1	19991209	G	6300	206362002103	CAP SEAL        			BELL  	407   	407         		SW  										M/R DRIVE	LEAKING         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724PH					53327				CAP AND ADAPTER LEAKS.						1	G	7	1 	3U			O	H2SW    					 
1999122300291	19991223	00291	SW  	1999	12	23	HEEA065368       	1	19991209	G	6520	406040072105	ADAPTER         			BELL  	407   	407         		SW  										T/R SPLINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				OIL PUMP SPLINES WORN.						1	G	7	1 	3U			O	H2SW    					 
1999122300292	19991223	00292	SW  	1999	12	23	HEEA065370       	1	19991209	G	6710	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										COLLECTIVE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	57416	1288 				53070				UNIVERSAL HAD BEARING WORN.						1	G	7	1 	3U			O	H2SW    					 
1999122300293	19991223	00293	SW  	1999	12	23	HEEA065371       	1	19991209	G	3340	MS2774318	RELAY           			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724PH					53327				RELAY WILL NOT DISENGAGE ALL THE TIME.						1	G	7	1 	3U			O	H2SW    					 
1999122300294	19991223	00294	SW  	1999	12	23	HEEA065372       	1	19991209	G	6320	214040036107	INPUT QUIL      			BELL  	214   	214ST       	1182106	SW  										GEARBOX	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										MISMANUFACTURED.  PLATING WORN THROUGH TO PARENT METAL AND CAN BE FELT WITH .020 INCH PROBE.						2	G	7	2 	4U				H10SW   					 
1999122300295	19991223	00295	SW  	1999	12	23	HEEA065373       	1	19991209	G	5320	206023100121A	SUPPORT         			BELL  	206   	206L1       	1182107	SW  										FUSELAGE	MISMARKED       	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										MISIDENTIFIED.  PART TAGGED FOR LEFT SUPPORT, BUT IS ACTUALLY RIGHT SUPPORT.						1	G	7	1 	3U				H2SW    					 
1999122300296	19991223	00296	SW  	1999	12	23	HEEA065374       	1	19991209	G	6320	204040725003	ROLLER SET      			BELL  	412   	412         	1182202	SW  										TRANSMISSION	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										MISMANUFACTURED.  ROLLER NOT STAMPED ON TOP SIDE.						1	G	7	2 	4U				H4SW    					 
1999122300297	19991223	00297	SW  	1999	12	23	HEEA065375       	1	19991209	G	6300	406340102101	CARBON SEAL     			BELL  	407   	407         		SW  										M/R DRIVE	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03										CARBON SEAL LEAKING.  REPLACED WITH SERVICEABLE SEAL.						1	G	7	1 	3U			O	H2SW    					 
1999122300298	19991223	00298	SW  	1999	12	23	HEEA065376       	1	19991209	G	6240	222375077119	TRANSMITTER     			BELL  	407   	407         		SW  										TORQUE	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	724PH					53327				TORQUE TRANSMITTER CAUSED ERRONEOUS READINGS.						1	G	7	1 	3U			O	H2SW    					 
1999122300300	19991223	00300	EU  	1999	12	23	HEEA065380       	1	19991209	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										T/R PITCH LINK	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951					2771				ROD, PITCH CONTROL HAD WORN BEARING.  SERIAL NUMBERS REMOVED ARE S3388 AND S3424.  REPLACED WITH SERIAL NUMBERS S3634 AN	D S4043.					1	G	7	1 	3U				H9EU    					 
1999122300301	19991223	00301	EU  	1999	12	23	HEEA065381       	1	19991209	G	7921	420800001	FAN             			SNIAS 	350   	AS350B2     	8680813	EU  										OIL COOLER	BROKE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6095S					2777				FAN BLADE BROKEN.						1	G	7	1 	3U				H9EU    					 
1999122300302	19991223	00302		1999	12	23	HEEA065384       	4	19991209	G	3120	B1894522282A	CLOCK           			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	SLOW            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4036H					2919				CLOCK LOSES TIME.						1	G	7	1 	3U				H9EU    					 
1999122300303	19991223	00303	EU  	1999	12	23	HEEA065385       	1	19991210	G	3000	350A89000007	MOTOR           			SNIAS 	350   	AS350B2     	8680813	EU  										WINDSHIELD WIPER	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6095S					2777				WINDSHIELD MOTOR BLOWS FUSES.						1	G	7	1 	3U				H9EU    					 
1999122300304	19991223	00304	EU  	1999	12	23	HEEA065387       	1	19991210	G	2435	150SG122Q	GENERATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										STARTER/GEN	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4036H	967  				2919				STATIC THROUGH HEADSETS AND INTERMITTENTLY INOPERATIVE.						1	G	7	1 	3U				H9EU    					 
1999122300305	19991223	00305	EU  	1999	12	23	HEEA065389       	1	19991210	G	2510	504305401	INERTIA REEL    			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	BROKE           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	40466					3004				CABLE BROKEN.						1	G	7	1 	3U				H9EU    					 
1999122300299	19991223	00299	SW  	1999	12	23	HEEA065393       	1	19991210	G	6320	206040156101	SEAL            			BELL  	206   	206L1       	1182107	SW  										GEARBOX	CORRODED        	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03										CORROSION ON SEAL.						1	G	7	1 	3U				H2SW    					 
1999122300306	19991223	00306	EU  	1999	12	23	HEEA065394       	1	19991210	G	7931	DK042	TRANSMITTER     			BOLKMS	105   	BO105S      	5626006	EU  										ENG OIL PRESS	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	86CH					S557				TRANSMITTER INOPERABLE.						1	G	7	2 	3U				H3EU    					 
1999122300307	19991223	00307	EU  	1999	12	23	HEEA065395       	1	19991210	G	7931	DK042	TRANSMITTER     			BOLKMS	105   	BO105S      	5626006	EU  										ENG OIL PRESS	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TRANSMITTER INOPERABLE.						1	G	7	2 	3U				H3EU    					 
1999122300308	19991223	00308	EU  	1999	12	23	HEEA065396       	1	19991210	G	7931	DK042	TRANSMITTER     			BOLKMS	105   	BO105S      	5626006	EU  										ENG OIL PRESS	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TRANSMITTER INOPERABLE.						1	G	7	2 	3U				H3EU    					 
1999122300309	19991223	00309	EU  	1999	12	23	HEEA065397       	1	19991210	G	7931	DK042	TRANSMITTER     			BOLKMS	105   	BO105S      	5626006	EU  										ENG OIL PRESS	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TRANSMITTER INOPERABLE.						1	G	7	2 	3U				H3EU    					 
1999122300310	19991223	00310	EU  	1999	12	23	HEEA065398       	1	19991210	G	7931	DK042	TRANSMITTER     			BOLKMS	105   	BO105S      	5626006	EU  										ENG OIL PRESS	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										TRANSMITTER INOPERABLE.						1	G	7	2 	3U				H3EU    					 
1999122300311	19991223	00311	EU  	1999	12	23	HEEA065399       	1	19991210	G	2800	DK042	TRANSMITTER     			BOLKMS	105   	BO105S      	5626006	EU  										ENG OIL PRESS	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	86CH					S557				TRANSMITTER INOPERABLE.						1	G	7	2 	3U				H3EU    					 
2000010800126	20000108	00126	GL  	2000	1	8	HEEA065430       	2	19991214	G	7510	23007827	VALVE           		23063354    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C47B     		GL  					ANTI-ICE SYSTEM	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	823  			CAT44432	51042	CAE847293			VALVE ASSEMBLY REMOVED DUE TO INOPERATIVE.  STUCK CLOSED.  INSPECTION DETERMINED BURNT COIL P/N V105-22.						1	G	7	1 	3U	3	U		H2SW    	E1GL				 
2000010800130	20000108	00130	SW  	2000	1	8	HEEA065434       	1	19991216	G	5320	214031401297S	SUPPORT         			BELL  	214   	214ST       	1182106	SW  										FUSELAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										SUPPORT MISMANUFACTURED.  PART .6250 INCH TOO SHORT.						2	G	7	2 	4U				H10SW   					 
2000010800127	20000108	00127	GL  	2000	1	8	HEEA065435       	2	19991216	G	7230	23008030	TIE BOLT        		23035128    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					COMPRESSOR	BENT            	E			HEEA	K				NONE                    				B			SMOKE/FUMES/ODORS/SPARKS  			IN	INSP/MAINT     	1			SW	03	979BH				CAT90407	51403	CAE895174			ENGINE REMOVED DUE TO EXCESSIVE SMOKING.  UPON ATTEMPT TO BALANCE NOTED TIE BOLT BENT AND UNABLE TO BALANCE DUE TO CHAMF	ER INSIDE NR 2 WHEEL SHAFT MISMACHINED.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
2000010800128	20000108	00128	GL  	2000	1	8	HEEA065436       	2	19991216	G	7230	23032280	WHEEL           		23035128    	BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C30P     	03013	GL  					2ND STAGE	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	979BH				CAT90407	51403	CAE895174			ENGINE REMOVED DUE TO EXCESSIVE SMOKING.  UPON ATTEMPT TO BALANCE NOTED TIE BOLT BENT AND UNABLE TO BALANCE DUE TO CHAMF	ER INSIDE #2 NR 2 WHEEL SHAFT MISMACHINED.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
2000022300002	20000223	00002	GL  	2000	2	23	HEEA065437       	2	19991216	G	7250	23062753	NOZZLE          		6898735     	BOLKMS	105   	BO105CB*    		SW  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RS	901  			CAT40380	S670	CAE831864			ENGINE REMOVED DUE TO LOW POWER.  UPON INSPECTION OF TURBINE PARTS NOTED A 1 PIECE OF NOZZLE SHIELD DOME BROKEN OUT AND 	LODGED AGAINST NR 1 NOZZLE VANES.					1	G	7	2 	4U	3	U		H3EU    	E4CE				 
2000022300003	20000223	00003	GL  	2000	2	23	HEEA065438       	2	19991216	G	7250	6886407	BLADE           		6898735     	BOLKMS	105   	BO105CB*    		SW  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	DAMAGED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RS	632  			CAT40380	S670	CAE831864			ENGINE REMOVED DUE TO LOW POWER.  UPON INSPECTION OF TURBINE PARTS NOTED NR 1 WHEEL BLADES DAMAGED DUE TO FAILED NR 1 NO	ZZLE SHIELD DOME.					1	G	7	2 	4U	3	U		H3EU    	E4CE				 
2000022300004	20000223	00004	GL  	2000	2	23	HEEA065439       	2	19991216	G	7250	23062750	NOZZLE SHIELD   		6898735     	BOLKMS	105   	BO105CB*    		SW  	ALLSN 	250C  	250C20B     	03013	GL  					TURBINE	BROKEN          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	911RS	632  			CAT40380	S670	CAE831864			ENGINE REMOVED DUE TO LOW POWER.  UPON INSPECTION OF TURBINE PARTS NOTED A 1 PIECE OF DOME BROKEN OUT OF NR 1 NOZZLE SHI	ELD AND LODGED AGAINST NR 1 NOZZLE VANES.					1	G	7	2 	4U	3	U		H3EU    	E4CE				 
2000010800131	20000108	00131	SW  	2000	1	8	HEEA065441       	1	19991217	G	6300	406010417101	BEARING         			BELL  	407   	407         		SW  										MAIN  ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8595X	1163 				53267				PLAY IN BEARING - AXIAL AND RADIAL.  SERIAL NUMBERS REMOVED ARE A-1925 AND A-1930.						1	G	7	1 	3U			O	H2SW    					 
2000022400001	20000224	00001	SW  	2000	2	24	HEEA065442       	1	19991217	G	6520	406040072105	ADAPTER         			BELL  	407   	407         		SW  										T/R SPLINE	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	4999	919  				53323				ADAPTER HAD WORN SPLINES.						1	G	7	1 	3U			O	H2SW    					 
2000010800132	20000108	00132	SW  	2000	1	8	HEEA065443       	1	19991217	G	2822	407362013101	SWITCH          			BELL  	407   	407         		SW  										ENGINE	STUCK           	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	490PH	33   				53378				PRESSURE SWITCH STICKS IN OPEN POSITION.						1	G	7	1 	3U			O	H2SW    					 
2000010800133	20000108	00133	SW  	2000	1	8	HEEA065444       	1	19991217	G	3212	206050247138	COVER           			BELL  	407   	407         		SW  										FLOAT	TORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	404PH					53188				FLOAT COVER ASSEMBLY TORN.						1	G	7	1 	3U			O	H2SW    					 
2000010800134	20000108	00134	SW  	2000	1	8	HEEA065445       	1	19991217	G	6320	406340100101	PUMP            			BELL  	407   	407         		SW  										TRANSMISSION	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				SPLINES WORN ON OIL PUMP.						1	G	7	1 	3U			O	H2SW    					 
2000022400002	20000224	00002	SW  	2000	2	24	HEEA065446       	1	19991217	G	3320	A490ATSDF1428	POWER SUPPLY    			BELL  	407   	407         		SW  										COCKPIT	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	721PH					53278				POWER SUPPLY INOPERATIVE.						1	G	7	1 	3U			O	H2SW    					 
2000010800135	20000108	00135	SW  	2000	1	8	HEEA065447       	1	19991217	G	7714	407375002103	INDICATOR       			BELL  	407   	407         		SW  										COCKPIT	INTERMITTENT    	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	409PH					53059				DIGITAL READ-OUT DOES NOT WORK AT TIMES ON NG INDICATOR.						1	G	7	1 	3U			O	H2SW    					 
2000010800136	20000108	00136	SW  	2000	1	8	HEEA065448       	1	19991217	G	2822	407362013101	PRESSURE SWITCH 			BELL  	407   	407         		SW  										ENGINE	INOPERATIVE     	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				PRESSURE SWITCH INOPERATIVE.						1	G	7	1 	3U			O	H2SW    					 
2000022400003	20000224	00003	SW  	2000	2	24	HEEA065449       	1	19991217	G	6320	206040156001	SEAL            			BELL  	407   	407         		SW  										M/R GEARBOX	SCRATCHED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	407MM					53060				SCRATCHED ALONG LONG SEAL AREA.						1	G	7	1 	3U			O	H2SW    					 
2000010800137	20000108	00137	SW  	2000	1	8	HEEA065450       	1	19991217	G	2822	407362005105	SWITCH          			BELL  	407   	407         		SW  										ENGINE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SW	03	612PH					53199				LOW LEVEL LIGHT CAME ON WITH FUEL ON BOARD.						1	G	7	1 	3U			O	H2SW    					 
2000010800138	20000108	00138	SW  	2000	1	8	HEEA065451       	1	19991217	G	6520	406040453101	SEAL            			BELL  	407   	407         		SW  										T/R GEARBOX	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	467PH					53142				SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
2000010800139	20000108	00139	SW  	2000	1	8	HEEA065452       	1	19991217	G	6520	406040453101	SEAL            			BELL  	407   	407         		SW  										T/R GEARBOX	LEAKING         	E			HEEA	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	8595X					53267				SEAL LEAKING.  PART SCRAPPED IN HOUSE.						1	G	7	1 	3U			O	H2SW    					 
2000010800140	20000108	00140	SW  	2000	1	8	HEEA065453       	1	19991217	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	8595X	282  				53267				UNIVERSAL HAD EXCESSIVE PLAY.						1	G	7	1 	3U			O	H2SW    					 
2000010800141	20000108	00141	SW  	2000	1	8	HEEA065455       	1	19991217	G	6220	407310100103	DAMPER          			BELL  	407   	407         		SW  										MAIN ROTOR	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				REMOVED HEAD DUE TO GRIP RETIREMENT.  AT INSPECTION OF ASSY  FOUND CORROSION IN SHEAR BEARING BORE BEYOND LIMITS.  REQUE	STED DAMPERS TO BE SENT TO BELL FOR EVALUATION.  SERIAL NUMBERS REMOVED ARE LK5540, LK5603, LK5654, AND LK5473.  REPLACE	MENT PART SERIAL NUMBERS ARE LK7355, LK7111, LK7255, AND LK7093.				1	G	7	1 	3U			O	H2SW    					 
2000010800142	20000108	00142	SW  	2000	1	8	HEEA065456       	1	19991217	G	6220	407010103101	HORN            			BELL  	407   	407         		SW  										M/R HUB	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				REMOVED HEAD DUE TO GRIP RETIREMENT.  AT INSPECTION OF ASSY  FOUND PAD UNBONDED ON TWO EACH PITCH HORNS.  CLEANED AND FO	UND CORROSION BEYOND LIMITS.  REMAINING TWO EACH FOUND UNBONDED AND REQUESTED TO BE SENT TO BELL FOR EVALUATION.  SERIAL	 NUMBERS REMOVED ARE A-933 AND A-936.  REPLACEMENT PART SERIAL NUMBERS ARE A-1856 AND A-1780.				1	G	7	1 	3U			O	H2SW    					 
2000010800143	20000108	00143	SW  	2000	1	8	HEEA065457       	1	19991217	G	6220	407010103101	HORN            			BELL  	407   	407         		SW  										M/R HUB	CORRODED        	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	612PH					53199				REMOVED HEAD DUE TO GRIP RETIREMENT.  AT INSPECTION OF ASSY  FOUND PAD UNBONDED ON TWO EACH PITCH HORNS.  CLEANED AND FO	UND CORROSION BEYOND LIMITS.  REMAINING TWO EACH FOUND UNBONDED AND REQUESTED TO BE SENT TO BELL FOR EVALUATION.  SERIAL	 NUMBERS REMOVED ARE A-946 AND A-934.   REPLACEMENT PART SERIAL NUMBERS ARE A-1834 AND A-1852.				1	G	7	1 	3U			O	H2SW    					 
2000010800159	20000108	00159		2000	1	8	HEEA065458       	4	19991217	G	3421	5040032902	INDICATOR       			SNIAS 	350   	AS350B2     	8680813	EU  										COCKPIT	FAILED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350BZ					2653				ATTITUDE INDICATOR DOES NOT CAGE PROPERLY.						1	G	7	1 	3U				H9EU    					 
2000010800160	20000108	00160	EU  	2000	1	8	HEEA065459       	1	19991217	G	2913	350A35013004	PULLEY          			SNIAS 	350   	AS350B2     	8680813	EU  										HYD PUMP	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350BZ					2653				HYDRAULIC PUMP D HAD WORN BEARING.						1	G	7	1 	3U				H9EU    					 
2000010800161	20000108	00161	EU  	2000	1	8	HEEA065460       	1	19991217	G	6720	350A33214501	ROD             			SNIAS 	350   	AS350B2     	8680813	EU  										T/R PITCH LINK	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6095S					2777				ROD, PITCH CONTROL WORN.						1	G	7	1 	3U				H9EU    					 
2000010800162	20000108	00162	EU  	2000	1	8	HEEA065461       	1	19991217	G	6220	704A33633109	BEARING         			SNIAS 	350   	AS350B2     	8680813	EU  										SPHERICAL	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951	1411 				2771				BEARING SEPARATION.						1	G	7	1 	3U				H9EU    					 
2000010800163	20000108	00163	EU  	2000	1	8	HEEA065462       	1	19991217	G	6220	704A3363310951	STOP            			SNIAS 	350   	AS350B2     	8680813	EU  										SPHERICAL	SEPARATED       	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	60951	1411 				2771				SEPARATION.  SERIAL NUMBERS REMOVED ARE 12839 AND 13244.  REPLACED WITH SERIAL NUMBERS 0920 AND 0926.						1	G	7	1 	3U				H9EU    					 
2000010800164	20000108	00164	EU  	2000	1	8	HEEA065463       	1	19991217	G	2820	J26108	HOSE            			SNIAS 	350   	AS350B2     	8680813	EU  										FUEL SYSTEM	WORN            	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	6100R					2862				HOSE WORN.						1	G	7	1 	3U				H9EU    					 
2000010800144	20000108	00144	SW  	2000	1	8	HEEA065464       	1	19991217	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										M/R CONTROL	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	7128R					36007				WILL NOT RELEASE IN ATT MODE.						1	G	7	2 	4U				H4SW    					 
2000010800145	20000108	00145	SW  	2000	1	8	HEEA065465       	1	19991217	G	6710	214001347005	ACTUATOR        			BELL  	412   	412         	1182202	SW  										M/R CONTROL	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	7128R					36007				AFTER HEATING UP, UNIT WILL STICK INTERMITTENTLY WHEN RELEASED.						1	G	7	2 	4U				H4SW    					 
2000010800165	20000108	00165	EU  	2000	1	8	HEEA065466       	1	19991217	G	6730	AC67244	SERVO           			SNIAS 	350   	AS350B2     	8680813	EU  										MAIN ROTOR	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4000L					2873				FEEDBACK FELT DURING LEFT CYCLIC INPUT.						1	G	7	1 	3U				H9EU    					 
2000010800166	20000108	00166	EU  	2000	1	8	HEEA065467       	1	19991217	G	6330	350A38101832	CROSSBEAM       			SNIAS 	350   	AS350B2     	8680813	EU  										TRANSMISSION	GOUGED          	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	350BZ	4160 				2653				CROSS BEAM GOUGED AT BOTTOM EDGE CORNER.						1	G	7	1 	3U				H9EU    					 
2000010800146	20000108	00146	SW  	2000	1	8	HEEA065468       	1	19991217	G	2840	407362005103	SWITCH          			BELL  	407   	407         		SW  										FUEL SYSTEM	FAILED          	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	723PH					53283				FUEL LOW  LIGHT WILL NOT GO OUT.						1	G	7	1 	3U			O	H2SW    					 
2000010800147	20000108	00147	SW  	2000	1	8	HEEA065469       	1	19991217	G	2822	407362013101	PRESSURE SWITCH 			BELL  	407   	407         		SW  										ENGINE	MALFUNCTIONED   	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	723PH					53283				RIGHT TRANSFER LIGHT WILL NOT COME ON.						1	G	7	1 	3U			O	H2SW    					 
2000010800148	20000108	00148	SW  	2000	1	8	HEEA065470       	1	19991220	G	6300	406010426101	LINK ASSEMBLY   			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	407MM	1794 				53060				LINK ASSEMBLY WORN.						1	G	7	1 	3U			O	H2SW    					 
2000010800149	20000108	00149	SW  	2000	1	8	HEEA065471       	1	19991220	G	6300	406010426101	LINK ASSEMBLY   			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	407MM	1794 				53060				LINK ASSEMBLY WORN.						1	G	7	1 	3U			O	H2SW    					 
2000010800150	20000108	00150	SW  	2000	1	8	HEEA065472       	1	19991220	G	6300	406010425107	LEVER ASSEMBLY  			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	407MM	1794 				53060				LEVER ASSEMBLY WORN.						1	G	7	1 	3U			O	H2SW    					 
2000010800151	20000108	00151	SW  	2000	1	8	HEEA065473       	1	19991220	G	6300	406010425107	LEVER ASSEMBLY  			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	407MM	1794 				53060				LEVER ASSEMBLY WORN.						1	G	7	1 	3U			O	H2SW    					 
2000010800152	20000108	00152	SW  	2000	1	8	HEEA065474       	1	19991220	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	447PH	1182 				53114				UNIVERSAL WORN.						1	G	7	1 	3U			O	H2SW    					 
2000010800153	20000108	00153	SW  	2000	1	8	HEEA065475       	1	19991220	G	6300	406310405101	UNIVERSAL       			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	404PH	2059 				53188				UNIVERSAL WORN AND ROUGH.						1	G	7	1 	3U			O	H2SW    					 
2000010800129	20000108	00129	GL  	2000	1	8	HEEA065476       	2	19991220	G	7320	23069551	HMU             			BELL  	206   	206L3       	1182108	SW  	ALLSN 	250C  	250C47B     		GL  					ENGINE	FAILED          	E			HEEA	O				OTHER                   				J			WARNING INDICATION        			NR	NOT REPORTED   	1			SW	03	3193E	817  				51042	CAE847293			RESTART FAULT AND DEGRADE LIGHTS ILLUMINATED.  ENGINE RPM HAD TO BE REDUCED FROM 100 PERCENT TO CUT OFF IN MANUAL MODE (	WOULD NOT RESPOND IN AUTO) DAILY OVERSPEED CHECK WOULD NOT WORK.  (REMOVED FROM AIRCRAFT) INSTALLED SERVICEABLE HMU.					1	G	7	1 	3U	3	U		H2SW    	E1GL				 
2000010800154	20000108	00154	SW  	2000	1	8	HEEA065477       	1	19991220	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GEN	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	4999	869  				53323				STARTER/GENERATOR FAILED 300 HOUR INSPECTION.    BRUSHES WERE EXCESSIVELY WORN AND COMMUTATOR WAS PITTED.						1	G	7	1 	3U			O	H2SW    					 
2000010800155	20000108	00155	SW  	2000	1	8	HEEA065478       	1	19991220	G	2435	206062200123	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GEN	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	510PH	2562 				53209				STARTER/GENERATOR FAILED 300 HOUR INSPECTION.   BRUSHES WERE EXCESSIVELY WORN.						1	G	7	1 	3U			O	H2SW    					 
2000010800156	20000108	00156	SW  	2000	1	8	HEEA065479       	1	19991220	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GEN	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	402PH	2562 				53159				STARTER/GENERATOR FAILED 300 HOUR INSPECTION.   BRUSHES WERE EXCESSIVELY WORN.						1	G	7	1 	3U			O	H2SW    					 
2000010800157	20000108	00157	SW  	2000	1	8	HEEA065480       	1	19991220	G	2435	206062200113	BRUSHES         			BELL  	407   	407         		SW  										STARTER/GEN	WORN            	E			HEEA	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	447PH					53114				STARTER/GENERATOR BRUSHES WERE EXCESSIVELY WORN.						1	G	7	1 	3U			O	H2SW    					 
2000010800158	20000108	00158	SW  	2000	1	8	HEEA065483       	1	19991220	G	5320	407030734101	PANEL           			BELL  	407   	407         		SW  										OIL COOLER	CRACKED         	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	720PH					53277				REPAIRED CRACKED OIL COOLER DECK ON FUSELAGE.						1	G	7	1 	3U			O	H2SW    					 
2000012200398	20000122	00398		2000	1	22	HEEA065584       	4	19991230	G	2210	214074104101	SENSOR DUALRATE 			BELL  	214   	214ST       	1182106	SW  										SCAS SYSTEM	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										SCAS YAW KICKS OFF IN TURBULENCE.  PART IS BAD FROM STOCK.  WAS INSTALLED FOR TROUBLESHOOTING AND CAUSED A DIFFERENT PRO	BLEM.  TIME SINCE REPAIR 0:00.					2	G	7	2 	4U				H10SW   					 
2000012200399	20000122	00399	SW  	2000	1	22	HEEA065585       	1	19991230	G	6710	214001540117	ACTUATOR        			BELL  	214   	214ST       	1182106	SW  										SCAS	MALFUNCTIONED   	E			HEEA	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										SCAS YAW KICKS OFF AFTER ENGAGED.  SUSPECT LOCKED SOLENOID.  TIME SINCE REPAIR 0:00.						2	G	7	2 	4U				H10SW   					 
2000012200400	20000122	00400	SW  	2000	1	22	HEEA065586       	1	19991230	G	6320	206040525007	HOUSING         			BELL  	206   	206L3       	1182108	SW  										M/R GEARBOX	MISMANUFACTURED 	E			HEEA	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03										HOUSING ASSY MISMANUFACTURED.  FILTER AREA NOT FINISHED, FILTER ELEMENT AREA CANNOT BE INSTALLED.						1	G	7	1 	3U				H2SW    					 
1999111900066	19991119	00066	NE  	1999	11	19	HEED064523       	1	19990405	G	6320		FASTENER        			SKRSKY	S76   	S76C        	8143008	NE  										M/R GEARBOX	MISSING         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	272  				760493				ON DAILY INSPECTION, FOUND (1 EACH) HI-LOCK PIN AND COLLAR MISSING FROM TRANSMISSION SUPPORT BEAM.   REPLACED HI-LOCK PI	N AND COLLAR.					1	G	7	2 	3U			NC	H1NE    					 
1999111900105	19991119	00105	SW  	1999	11	19	HEED064526       	1	19990427	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	19   				53276				LAMP BURNED OUT.  ORDERED REPLACEMENT.						1	G	7	1 	3U			O	H2SW    					 
1999111900106	19991119	00106	SW  	1999	11	19	HEED064527       	1	19990427	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E					53276				LAMP BURNED OUT.  ORDERED REPLACEMENT.						1	G	7	1 	3U			O	H2SW    					 
1999111900107	19991119	00107	SW  	1999	11	19	HEED064528       	1	19990427	G	3340	A469B	STROBE          			BELL  	407   	407         		SW  										FUSELAGE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	88   				53276				FLASH TUBE ON STROBE LIGHT BURNED OUT.  ORDERED REPLACEMENT.						1	G	7	1 	3U			O	H2SW    					 
1999111900108	19991119	00108	SW  	1999	11	19	HEED064530       	1	19990427	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E					53276				LAMP BURNED OUT, ORDERED REPLACEMENT.						1	G	7	1 	3U			O	H2SW    					 
1999111900109	19991119	00109	SW  	1999	11	19	HEED064531       	1	19990427	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	16   				53276				LAMP BURNED OUT.  ORDERED REPLACEMENT.						1	G	7	1 	3U			O	H2SW    					 
1999111900110	19991119	00110	SW  	1999	11	19	HEED064532       	1	19990427	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E					53276				LAMP BURNED OUT.  ORDERED REPLACEMENT.						1	G	7	1 	3U			O	H2SW    					 
1999111900111	19991119	00111	SW  	1999	11	19	HEED064534       	1	19990427	G	7921	406360500100	OIL COOLER      			BELL  	407   	407         		SW  										ENGINE OIL	LEAKING         	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3193E	223  				53276				OIL COOLER LEAKING FROM BASE.  ORDERED REPLACEMENT.						1	G	7	1 	3U			O	H2SW    					 
1999111900112	19991119	00112	SW  	1999	11	19	HEED064536       	1	19990427	G	6330	230030535103	BEARING         			BELL  	407   	407         		SW  										M/R TRANSMISSION	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	929  				53276				ROD END HAS WORN BEARING.  ORDERED REPLACEMENT.						1	G	7	1 	3U			O	H2SW    					 
1999111900113	19991119	00113	SW  	1999	11	19	HEED064537       	1	19990427	G	6520	222340059101	CHIP DETECTOR   			BELL  	230   	230         	1182149	SW  										T/R GEARBOX	LOOSE           	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	3886 				23015				CHIP DETECTOR HAS PLUG LOOSE IN HOUSING AND BODY VALVE WILL NOT SEAT.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900114	19991119	00114	SW  	1999	11	19	HEED064538       	1	19990427	G	7600	222060790101	BEARING         			BELL  	230   	230         	1182149	SW  										BELLCRANK	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	3823 				23015				BELLCRANK HAS WORN BEARINGS.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900115	19991119	00115	SW  	1999	11	19	HEED064539       	1	19990427	G	2520	222320823123	RESTRAINT       			BELL  	230   	230         	1182149	SW  										CABIN SEAT	FRAYED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	3881 				23015				RESTRAINT HAS FRAYED SHOULDER HARNESS.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900116	19991119	00116	SW  	1999	11	19	HEED064542       	1	19990427	G	3340	900601	LIGHT           			BELL  	230   	230         	1182149	SW  										SEARCH LIGHT	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	28   				23015				MOTOR LOCKED UP.  REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900117	19991119	00117	GL  	1999	11	19	HEED064543       	2	19990427	G	7260	23053968	SEAL            			BELL  	230   	230         	1182149	SW  	ALLSN 	250C  	250C30G2    	03013	GL  					GEARBOX	LEAKING         	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	236X					23015				MAG SEAL LEAKS.  ORDERED REPLACEMENT.						1	G	7	2 	3U	3	U	NC	H9SW    	E1GL				 
1999111900118	19991119	00118	SW  	1999	11	19	HEED064544       	1	19990427	G	6320	780531	SEAL            			BELL  	230   	230         	1182149	SW  										TRANSMISSION	LEAKING         	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	236X					23015				SEAL LEAKS.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900119	19991119	00119	GL  	1999	11	19	HEED064545       	2	19990427	G	7260	23053968	SEAL            			BELL  	230   	230         	1182149	SW  	ALLSN 	250C  	250C30G2    	03013	GL  					GEARBOX	LEAKING         	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	236X					23015				MAG SEAL LEAKS.  ORDERED REPLACEMENT.						1	G	7	2 	3U	3	U	NC	H9SW    	E1GL				 
1999111900120	19991119	00120	SW  	1999	11	19	HEED064546       	1	19990429	G	6330	222010548105	BEARING LINER   			BELL  	230   	230         	1182149	SW  										XMSN MOUNT	BROKEN          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	809  				23015				LINER BROKEN.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900121	19991119	00121	SW  	1999	11	19	HEED064547       	1	19990429	G	6330	222010545101	BEARING LINER   			BELL  	230   	230         	1182149	SW  										TRANSMISSION	CHAFED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	407  				23015				LINER CHAFED.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900122	19991119	00122	SW  	1999	11	19	HEED064548       	1	19990429	G	6220	222310503103	BEARING         			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	SEPARATED       	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	723  				23015				BEARING PAD SEPERATED.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900123	19991119	00123	SW  	1999	11	19	HEED064549       	1	19990429	G	6220	222310504101	BEARING PAD     			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	SEPARATED       	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	3524 				23015				BEARING PAD SEPARATED.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900124	19991119	00124	SW  	1999	11	19	HEED064550       	1	19990429	G	7714	222375022111	INDICATOR       			BELL  	230   	230         	1182149	SW  										ENGINE NG	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4081 				23015				INDICATOR WILL NOT HOLD STARTER ON.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900067	19991119	00067	NE  	1999	11	19	HEED064553       	1	19990616	G	3340	3012543	STROBE          			SKRSKY	S76   	S76C        	8143008	NE  										FUSELAGE	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X					760493				ANTI-COLLISION LIGHT HAS SLOW FLASH RATE.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900068	19991119	00068	NE  	1999	11	19	HEED064554       	1	19990616	G	7714	7645001096101	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										N1	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	292  				760493				N1 INDICATOR'S LED LIGHTS WILL NOT DIM.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900069	19991119	00069	NE  	1999	11	19	HEED064555       	1	19990616	G	7714	7645001096101	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										N1	MALFUNCTIONED   	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	478X	131  				760493				GAUGE GOES TO ZERO IN-FLIGHT, HAPPENED TWICE ON 1-1/2 HOUR FLIGHT.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900070	19991119	00070	NE  	1999	11	19	HEED064556       	1	19990616	G	7714	7645001096101	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										N1	FAILED          	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	478X					760493				N1 INDICATOR FAILED OFFSHORE.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900071	19991119	00071	NE  	1999	11	19	HEED064557       	1	19990616	G	7714	7645001096101	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										N1	INTERMITTENT    	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	5    				760493				GAUGE INDICATED ERR 3 INTERMITTENTLY.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900072	19991119	00072	NE  	1999	11	19	HEED064558       	1	19990616	G	7714	7645001096101	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										N1	FAILED          	E			HEED	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	478X	420  				760493				N1 INDICATOR WILL NOT SELF-TEST WITHOUT RESETTING 3 OR 4 TIMES.   ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900125	19991119	00125	SW  	1999	11	19	HEED064560       	1	19990625	G	6220	222031613103	LIFT LINK       			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	2381 				23015				LIFT LINK ASSEMBLY'S ELASTOMETRIC BEARING WORN.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900126	19991119	00126	SW  	1999	11	19	HEED064562       	1	19990625	G	3246	222336010111	WHEEL           			BELL  	230   	230         	1182149	SW  										MLG	DAMAGED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	3959 				23015				BRAKE KEYS BROKEN.  ORDERED REPLACEMENT						1	G	7	2 	3U			NC	H9SW    					 
1999111900127	19991119	00127	SW  	1999	11	19	HEED064563       	1	19990625	G	6720	230312001101	LINK            			BELL  	230   	230         	1182149	SW  										TAIL ROTOR	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	365  				23015				TAIL ROTOR LINKS HAD WORN BEARINGS.   ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900128	19991119	00128	SW  	1999	11	19	HEED064564       	1	19990625	G	3340	900601	LIGHT           			BELL  	230   	230         	1182149	SW  										SEARCH LIGHT	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X					23015				MOTOR FROZEN.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900129	19991119	00129	SW  	1999	11	19	HEED064566       	1	19990625	G	1100	222075185103	SIGN            			BELL  	230   	230         	1182149	SW  										CABIN	BROKEN          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4009 				23015				FACE PLATE BROKEN.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900130	19991119	00130	SW  	1999	11	19	HEED064567       	1	19990625	G	7332	7G1056	SWITCH          			BELL  	230   	230         	1182149	SW  										FUEL SYSTEM	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4019 				23015				PRESSURE SWITCH FAILED.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900131	19991119	00131	SW  	1999	11	19	HEED064568       	1	19990625	G	6300	222366652003	FITTING         			BELL  	230   	230         	1182149	SW  										M/R DRIVE	CORRODED        	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	401  				23015				FITTING CORRODED ON THREADS WHERE HOSE ATTACHED.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900132	19991119	00132	SW  	1999	11	19	HEED064569       	1	19990625	G	2821	70079H100F210	HOSE            			BELL  	230   	230         	1182149	SW  										FUEL FILTER	CORRODED        	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	401  				23015				FITTING CORRODED ON THREADS WHERE HOSE ATTACHED TO FUEL FILTER.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900133	19991119	00133	SW  	1999	11	19	HEED064570       	1	19990625	G	3340	4596	LAMP            			BELL  	230   	230         	1182149	SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	63   				23015				LAMP BURNED OUT.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900134	19991119	00134	SW  	1999	11	19	HEED064571       	1	19990625	G	3340	4596	LAMP            			BELL  	230   	230         	1182149	SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	20   				23015				LAMP BURNED OUT.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900135	19991119	00135	SW  	1999	11	19	HEED064573       	1	19990625	G	5210	407064806102	DOOR            			BELL  	230   	230         	1182149	SW  										FUSELAGE	MISMARKED       	E			HEED	K				NONE                    				W			INADEQUATE Q C            			IN	INSP/MAINT     	1			SW	03	236X	361  				23015				DOOR ASSY RETURNED.  REASON, MISMARKED.  DOOR IS A -102 RIGHT WITH -101A LEFT NUMBER STAMPED ON IT.  ORDERED REPLACEMENT	.					1	G	7	2 	3U			NC	H9SW    					 
1999111900136	19991119	00136	SW  	1999	11	19	HEED064576       	1	19990625	G	3340	A469B	STROBE          			BELL  	230   	230         	1182149	SW  										FUSELAGE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	78   				23015				STROBE LIGHT HAD BROKEN WIRE.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900073	19991119	00073	NE  	1999	11	19	HEED064577       	1	19990625	G	7714	7645001096101	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										N1	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	1    				760493				N1 INDICATOR WENT TO ERR 2.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900074	19991119	00074	NE  	1999	11	19	HEED064578       	1	19990625	G	2400	6032745	POWER SUPPLY    			SKRSKY	S76   	S76C        	8143008	NE  										28V SUPPLY	INOPERATIVE     	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	354  				760493				POWER SUPPLY INOPERATIVE.  ORDERED REPLACEMENT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900075	19991119	00075	NE  	1999	11	19	HEED064579       	1	19990625	G	6520	7635805112042	HOUSING         			SKRSKY	S76   	S76C        	8143008	NE  										T/R GEARBOX	CORRODED        	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	478X	234  				760493				TAIL ROTOR GEARBOX S/N: A239-00202 REMOVED FROM AIRCRAFT DUE TO  LEAKING.  FOUND OUTPUT HOUSING (ABOVE) QUADRANT ATTACHM	ENT BOLT HOLE AREA CORRODED.   REPLACED WITH NEW OUTPUT HOUSING.					1	G	7	2 	3U			NC	H1NE    					 
1999111900137	19991119	00137	SW  	1999	11	19	HEED064580       	1	19990625	G	6400	222012713001	IDLER           			BELL  	230   	230         	1182149	SW  										TAIL ROTOR	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4162 				23015				IDLER ASSEMBLY HAD WORN BEARINGS.   REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900138	19991119	00138	SW  	1999	11	19	HEED064581       	1	19990625	G	6400	222031308115	SHIELD          			BELL  	230   	230         	1182149	SW  										TAIL ROTOR	CRACKED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4162 				23015				SHIELD CRACKED.  REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900139	19991119	00139	SW  	1999	11	19	HEED064582       	1	19990625	G	6400	222012714001	BEARING         			BELL  	230   	230         	1182149	SW  										TAIL ROTOR	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4162 				23015				TAIL ROTOR'S INNER RACE WORN.  REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900140	19991119	00140	SW  	1999	11	19	HEED064583       	1	19990625	G	7110	230361801101	SPRING          			BELL  	230   	230         	1182149	SW  										LATCH	BROKEN          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4189 				23015				LATCH HAD BROKEN SPRING.  REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900141	19991119	00141	SW  	1999	11	19	HEED064584       	1	19990625	G	2910	222080060001	CYLINDER        			BELL  	230   	230         	1182149	SW  										HYDRAULIC SYS	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X					23015				BYPASSING FLUID, RESERVOIR OVERFILLS.  REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900142	19991119	00142	SW  	1999	11	19	HEED064585       	1	19990625	G	3340	930500251	RING            			BELL  	230   	230         	1182149	SW  										SEARCH LIGHT	BROKEN          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	1732 				23015				SEARCH LIGHT'S RETAINING RING INSERT BROKEN.  REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
1999111900076	19991119	00076	NE  	1999	11	19	HEED064586       	1	19990922	G	6410	7610105501042	BLADE           			SKRSKY	S76   	S76C        	8143008	NE  										TAIL ROTOR	ERODED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	563  				760493				EROSION OF PROTECTIVE RUBBER COATING ON LEADING EDGES OF TAIL ROTOR BLADE.  REPLACED BLADE.						1	G	7	2 	3U			NC	H1NE    					 
1999111900077	19991119	00077	NE  	1999	11	19	HEED064587       	1	19990922	G	6410	7610105501042	BLADE           			SKRSKY	S76   	S76C        	8143008	NE  										TAIL ROTOR	ERODED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	563  				760493				EROSION OF PROTECTIVE RUBBER COATING ON LEADING EDGES OF TAIL ROTOR BLADE.  REPLACED BLADE.						1	G	7	2 	3U			NC	H1NE    					 
1999111900078	19991119	00078	GL  	1999	11	19	HEED064588       	2	19991105	G	7200	1S1	ENGINE          		1S1         	SKRSKY	S76   	S76C        	8143008	NE  	ALLSN 	250C  	250C30S     	03013	GL  					ENGINE BAY	MAKING METAL    	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	276X	2352 			15529	760405				ENGINE ASSEMBLY MAKING METAL.  REPLACED WITH ANOTHER ENGINE.						1	G	7	2 	3U	3	U	NC	H1NE    	E1GL				 
1999111900079	19991119	00079	GL  	1999	11	19	HEED064590       	2	19991108	G	7200	1S1	ENGINE          		1S1         	SKRSKY	S76   	S76C        	8143008	NE  	ALLSN 	250C  	250C30S     	03013	GL  					ENGINE BAY	MAKING METAL    	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H	2966 			15537	760406				METAL FOUND IN REAR MAG PLUG.  REPLACED WITH ANOTHER ENGINE.						1	G	7	2 	3U	3	U	NC	H1NE    	E1GL				 
1999111900143	19991119	00143	SW  	1999	11	19	HEED064594       	1	19991108	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	543  				53276				LUMP BURNED OUT.  SCRAPPED.  ORDERED REPLACEMENT PARTS.						1	G	7	1 	3U			O	H2SW    					 
1999111900144	19991119	00144	SW  	1999	11	19	HEED064596       	1	19991108	G	2821	222366621103	FUEL FILTER     			BELL  	407   	407         		SW  										FUEL SYSTEM	CORRODED        	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	455  				53276				FUEL FILTER ASSEMBLY HAD CORROSION ON BYPASS INDICATOR SWITCH CONNECTOR.  ORDERED REPLACEMENT PARTS.						1	G	7	1 	3U			O	H2SW    					 
1999111900145	19991119	00145	SW  	1999	11	19	HEED064597       	1	19991108	G	2435	206062200113	STARTER/GEN     			BELL  	407   	407         		SW  										ENGINE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	519  				53276				STARTER/GENERATOR WILL NOT ENGAGE OR TURN FOR START.						1	G	7	1 	3U			O	H2SW    					 
1999111900146	19991119	00146	SW  	1999	11	19	HEED064598       	1	19991108	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	26   				53276				LAMP BURNED OUT.  REPLACED PART.						1	G	7	1 	3U			O	H2SW    					 
1999111900147	19991119	00147	SW  	1999	11	19	HEED064599       	1	19991108	G	3340	A469B	STROBE          			BELL  	407   	407         		SW  										FUSELAGE	FAILDED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	30   				53276				STROBE LIGHT BURNED OUT, SCRAPPED.  REPLACED PART.						1	G	7	1 	3U			O	H2SW    					 
1999111900148	19991119	00148	SW  	1999	11	19	HEED064600       	1	19991108	G	3212	8226003	FUSIBLE PLUG    			BELL  	407   	407         		SW  										FLOAT	LEAKING         	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3193E	509  				53276				PLUG LEAKING, REPLACED PART.						1	G	7	1 	3U			O	H2SW    					 
1999111900149	19991119	00149	SW  	1999	11	19	HEED064601       	1	19991108	G	3340	A469B	STROBE          			BELL  	407   	407         		SW  										FUSELAGE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	71   				53276				STROBE LIGHT BURNED OUT.  REPLACED PART.						1	G	7	1 	3U			O	H2SW    					 
1999111900150	19991119	00150	SW  	1999	11	19	HEED064603       	1	19991108	G	6510	222344606101	BEARING         			BELL  	230   	230         	1182149	SW  										T/R DRIVE	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4497 				23015				BEARING WORN AND HIGH VIBRATION NR 2 POSITION.   REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999111900151	19991119	00151	SW  	1999	11	19	HEED064604       	1	19991108	G	6510	222344606101	BEARING         			BELL  	230   	230         	1182149	SW  										T/R DRIVE	DAMAGED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4497 				23015				BEARING SUSPECTED AS CAUSING VIBRATION.  REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999111900152	19991119	00152	SW  	1999	11	19	HEED064605       	1	19991108	G	6330	222331618105	ISOLATION MOUNT 			BELL  	230   	230         	1182149	SW  										M/R GEARBOX	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	1213 				23015				ISOLATION MOUNT HAD WORN BEARING.  REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999111900153	19991119	00153	SW  	1999	11	19	HEED064606       	1	19991108	G	5210	1008402	LATCH ASSY      			BELL  	230   	230         	1182149	SW  										PILOT DOOR	DAMAGED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4273 				23015				RIGHT LATCH ASSEMBLY DIFFICULT TO OPEN.  REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999111900154	19991119	00154	SW  	1999	11	19	HEED064607       	1	19991108	G	6330	222331618105	ISOLATION MOUNT 			BELL  	230   	230         	1182149	SW  										M/R GEARBOX	DAMAGED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	1110 				23015				ISOLATION MOUNT SUSPECT VIBRATION/EXCESSIVE.  REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999111900155	19991119	00155	SW  	1999	11	19	HEED064608       	1	19991108	G	6330	230030535101	ROD END         			BELL  	230   	230         	1182149	SW  										M/R TRANSMISSON	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X					23015				ROD END HAD WORN BEARING.   REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999121000028	19991210	00028	GL  	1999	12	10	HEED064609       	2	19991108	G	7250	34219	LINING CARRIER  			BELL  	230   	230         	1182149	SW  	ALLSN 	250C  	250C20      	03013	GL  					ENGINE	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X					23015				LINING CARRIER WORN.  REPLACED PART.						1	G	7	2 	3U	3	U	NC	H9SW    	E4CE				 
1999111900156	19991119	00156	SW  	1999	11	19	HEED064610       	1	19991108	G	6730	222382001105	ACTUATOR ASSY   			BELL  	230   	230         	1182149	SW  										PILOT VALVE	LEAKING         	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	236X	2953 				23015				ACTUATOR ROD SEAL LEAKING.  REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999111900157	19991119	00157	SW  	1999	11	19	HEED064611       	1	19991108	G	5250	1008406	LATCH ASSY      			BELL  	230   	230         	1182149	SW  										LAV DOOR	STICKING        	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4253 				23015				LATCH ASSEMBLY STICKING AND JAMMING.  REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999111900158	19991119	00158		1999	11	19	HEED064612       	4	19991108	G	3414	222375036103	SWITCH          			BELL  	230   	230         	1182149	SW  										AIRSPEED	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4459 				23015				AIRSPEED SWITCH ALLOWS GEAR WARNING HORN.   REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999111900159	19991119	00159	SW  	1999	11	19	HEED064613       	1	19991108	G	2910	230065535101	LINE            			BELL  	230   	230         	1182149	SW  										HYDRAULIC SYS	DAMAGED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4470 				23015				FLARE MISSING.  REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999111900160	19991119	00160	SW  	1999	11	19	HEED064614       	1	19991108	G	6730	222382001105	ACTUATOR ASSY   			BELL  	230   	230         	1182149	SW  										PILOT VALVE	LEAKING         	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	236X	3246 				23015				ACTUATOR ASSEMBLY LEAKING.  REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999111900161	19991119	00161	SW  	1999	11	19	HEED064615       	1	19991108	G	6720	230312001101	LINK            			BELL  	230   	230         	1182149	SW  										TAIL ROTOR	DAMAGED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X					23015				TAIL ROTOR LINK BEARINGS WORN.  REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999111900162	19991119	00162	SW  	1999	11	19	HEED064616       	1	19991108	G	6210	222015600111	BLADE           			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	CRACKED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4194 				23015				MAIN ROTOR BLADE CRACKED LEADING EDGE AND LOWER SKIN.   REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999111900080	19991119	00080	NE  	1999	11	19	HEED064619       	1	19991108	G	6240	7645001076112	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										TRIPLE TACH	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	770  				760493				INSTALLED IN AIRCRAFT ROTOR NEEDLE ADVANCED ABOVE NR 1, 32 ENGINE NEEDLES, ENGINE NEEDLES WOULD NOT MARRY WITH ROTOR NEE	DLE, ROTOR NEEDLE 107 PERCENT, NR 1 ENGINE 70 PERCENT.  THROTTLES IN FLY POSITION.  SPLIT STAYED THE SAME START TO SHUT 	DOWN.   REPLACED PART.				1	G	7	2 	3U			NC	H1NE    					 
1999111900081	19991119	00081		1999	11	19	HEED064620       	4	19991108	G	3416	066304400	ALTIMETER       			SKRSKY	S76   	S76C        	8143008	NE  										COCKPIT	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	770  				760493				INDICATOR OFF FLAG WILL NOT PULL WHEN INDICATOR POWERED UP, BUT INDICATOR WORKED OTHERWISE.  REPLACED PART.						1	G	7	2 	3U			NC	H1NE    					 
1999111900082	19991119	00082		1999	11	19	HEED064621       	4	19991108	G	2210	7690001825103	AMPLIFIER       			SKRSKY	S76   	S76C        	8143008	NE  										PITCH ACTUATOR	ERRATIC         	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	478X	728  				760493				PILOT REPORTED ERRATIC PITCH BIAS ACTUATOR MOVEMENT.  REPLACED PART.						1	G	7	2 	3U			NC	H1NE    					 
1999111900083	19991119	00083	GL  	1999	11	19	HEED064622       	2	19991108	G	7220	7630207028062	SCREEN          			SKRSKY	S76   	S76C        	8143008	NE  	ALLSN 	250C  	250C30S     	03013	GL  					ENGINE INTAKE	BROKEN          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	694  				760493				INTAKE SCREEN HAD BROKEN WIRE.  REPLACED PART.						1	G	7	2 	3U	3	U	NC	H1NE    	E1GL				 
1999111900084	19991119	00084	NE  	1999	11	19	HEED064623       	1	19991108	G	7714	H190110	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										N1	FAILED          	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	478X	5    				760493				N1 INDICATOR NEEDLE STOPS MOVING IN-FLIGHT.  CAN GET IT BACK IN OPERATIONAL BY DISCONNECTING ALL POWER THEN RECONNECTING	 POWER, BUT INDICATOR CONTINUES TO MALFUNCTION, REPLACED PART.					1	G	7	2 	3U			NC	H1NE    					 
1999111900085	19991119	00085		1999	11	19	HEED064624       	4	19991108	G	2210	7040002200108	SERVO           			SKRSKY	S76   	S76C        	8143008	NE  										PITCH BIAS LINER	INTERMITTENT    	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	784  				760493				PITCH BIAS ACTUATOR , PBA, IMTERMITTENTLY CAUSES AIRCRAFT TO PITCH UP OR DOWN DURING CRUISE FLIGHT.  REPLACED PART.						1	G	7	2 	3U			NC	H1NE    					 
1999111900086	19991119	00086		1999	11	19	HEED064625       	4	19991108	G	3120	W33751010ET20L	CLOCK           			SKRSKY	S76   	S76C        	8143008	NE  										COCKPIT	SLOW            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	752  				760493				CLOCK LOOSES 10 MINUTES EVERY DAY.  REPLACED PART.						1	G	7	2 	3U			NC	H1NE    					 
1999111900087	19991119	00087	NE  	1999	11	19	HEED064626       	1	19991108	G	7714	7645001096101	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										N1	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	330  				760493				THE DIGITAL NUMBERS THAT WERE LIT UP, WERE BRIGHTER THAN THE OTHER N1 INDICATOR, IT WOULD PULL THE BRIGTHNESS OF ANY OTH	ER INDICATOR IT WAS PAIRED WITH DOWN TO ALMOST NO INDICATION, WHEN LIGHT CONTROL SET TO MINIMUM AND WHEN SET AT MAXIMUM,	 IT WAS ALWAYS BRIGHTER THAN THE OTHER.  REPLACED PART.				1	G	7	2 	3U			NC	H1NE    					 
1999111900088	19991119	00088	NE  	1999	11	19	HEED064627       	1	19991108	G	7714	H190110	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										N1	FLUCTUATING     	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	478X	21   				760493				N1 INDICATOR AFTER APPROXIMATELY 1 TO 1-1/2 HOURS OF OPERATION, INDICATOR NEEDLE STARTED FLUCTUATING FROM OPERATING RANG	E TO ZERO AND BACK AGAIN.  ALL TESTS AND WARNING LIGHTS WOULD BLINK OFF AND ON AND DIGITS WOULD READ 8888.  SUBMITTER ST	ATED THE CONNECTOR WAS TIGHT AND HAD NO PROBLEMS LIKE THIS WITH ANY INDICATOR BEFORE OR AFTER.  REPLACED PART.				1	G	7	2 	3U			NC	H1NE    					 
1999111900089	19991119	00089	NE  	1999	11	19	HEED064628       	1	19991108	G	6240	7645001076112	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										TRIPLE TACH	STICKING        	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X					760493				NR 1 AND NR 2 NEEDLES STICK AT 20 PERCENT ON TRIPLE TACHOMETER.  REPLACED PART.						1	G	7	2 	3U			NC	H1NE    					 
1999111900090	19991119	00090	NE  	1999	11	19	HEED064629       	1	19991108	G	7933	7645001078126	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										ENG OIL TEMP	FLUCTUATES      	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				ENGINE OIL TEMPERATURE'S PRESSURE NEEDLE FLUCTUATES VERY RAPIDLY (BLURRY), THEN DROPS BELOW ZERO PRESSURE.  REPLACED PAR	T.					1	G	7	2 	3U			NC	H1NE    					 
1999111900091	19991119	00091	NE  	1999	11	19	HEED064630       	1	19991108	G	6240	7690001802106	ACTUATOR        			SKRSKY	S76   	S76C        	8143008	NE  										AFCS	STICKING        	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X	2704 				760436				AFCS ACTUATOR STICKING, CAUSED FEEDBACK IN CONTROLS.  REPLACED PART.						1	G	7	2 	3U			NC	H1NE    					 
1999111900092	19991119	00092	NE  	1999	11	19	HEED064631       	1	19991108	G	6230	SB52001	BEARING         			SKRSKY	S76   	S76C        	8143008	NE  										SWASHPLATE	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				SCISSOR BEARING WORN.  REPLACED PART.						1	G	7	2 	3U			NC	H1NE    					 
1999111900093	19991119	00093		1999	11	19	HEED064632       	4	19991108	G	3420	1418523211	AHRS            			SKRSKY	S76   	S76C        	8143008	NE  										COCKPIT	FAILED          	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	476X	1350 				760436				ATTITUDE FLAG FAILED TO PULL OUT OF SIGHT AND AHRS CAUTION LIGHT WILL NOT EXTINGUISH.  REPLACED PART.						1	G	7	2 	3U			NC	H1NE    					 
1999111900094	19991119	00094	NE  	1999	11	19	HEED064633       	1	19991108	G	3212	062001420200	TRANSCEIVER     			SKRSKY	S76   	S76C        	8143008	NE  										COCKPIT	MALFUNCTIONED   	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	476X	293  				760436				RECEIVES CLEARLY ON 158 FREQUENCY. BUT TRANSMISSION IS GARBLED.  REPLACED PART.						1	G	7	2 	3U			NC	H1NE    					 
1999111900095	19991119	00095	NE  	1999	11	19	HEED064634       	1	19991108	G	6320	0292105230	PUMP            			SKRSKY	S76   	S76C        	8143008	NE  	TMECA 	ARRIEL	ARRIEL1S1   	60030	NE  					GEARBOX	FAILED          	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	476X	276  				760436	15529TEC			LOW OIL PRESSURE AND CHECK VALVE ALLOWS THE OIL TANK TO DRAIN BACK INTO THE GEARBOX AFTER SHUTDOWN .  REPLACED PART.						1	G	7	2 	3U	3	U	NC	H1NE    	E19EU				 
1999111900096	19991119	00096	NE  	1999	11	19	HEED064635       	1	19991108	G	7714	9580115900	SENSOR          			SKRSKY	S76   	S76C        	8143008	NE  	TMECA 	ARRIEL	ARRIEL1S1   	60030	NE  					OVERSPEED	FAILED          	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	476X	386  				760436	15529TEC			N2 OVERSPEED LIGHT FAILS TO EXTINGUISH.  REPLACED PART.						1	G	7	2 	3U	3	U	NC	H1NE    	E19EU				 
1999111900097	19991119	00097		1999	11	19	HEED064637       	4	19991108	G	3444	066104800	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										COCKPIT	READS HIGH      	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X	3162 				760436				INDICATORS HIGH.  REPLACED PART.						1	G	7	2 	3U			NC	H1NE    					 
1999111900098	19991119	00098	NE  	1999	11	19	HEED064638       	1	19991108	G	6220	7610608050043	RESERVIOR       			SKRSKY	S76   	S76C        	8143008	NE  										MAIN ROTOR HEAD	DIRTY           	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				RESERVOIR STAINED AND DIRTY.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900099	19991119	00099	NE  	1999	11	19	HEED064639       	1	19991108	G	7933	7645001078126	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										ENG OIL TEMP	FLUCTUATES      	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				ENGINE OIL TEMPERATURE NEEDLE FLUCTUATED RAPIDLY (BLUFFY) FOR A FEW SECONDS, 3-5 TIMES PER MINUTE.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900100	19991119	00100		1999	11	19	HEED064640       	4	19991108	G	2213	775330200	CONTROLLER      			SKRSKY	S76   	S76C        	8143008	NE  										AFCS	MALFUNCTIONED   	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	89H					760406				RDA DATA UNIT WOULD NOT UPDATE.  INDICATED LOW BATTERY. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900101	19991119	00101	NE  	1999	11	19	HEED064641       	1	19991108	G	2160	7650007903102	VALVE           			SKRSKY	S76   	S76C        	8143008	NE  										AIR SHUTOFF	MALFUNCTONED    	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				SHUT-OFF VALVE WOULD NOT CLOSE COMPLETELY.   REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900102	19991119	00102		1999	11	19	HEED064642       	4	19991108	G	3457	8144002241B	GPS             			SKRSKY	S76   	S76C        	8143008	NE  										COCKPIT	FAILED          	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	89H					760406				EVERY LIGHT FLASHED, UNIT WENT OFF CAME BACK ON WITH NO MEMORY.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
1999111900103	19991119	00103	GL  	1999	11	19	HEED064643       	2	19991108	G	7322	0164348490	FCU             			SKRSKY	S76   	S76C        	8143008	NE  	ALLSN 	250C  	250C30S     	03013	GL  					ENGINE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	278X	1559 				760440				UNABLE TO CONTROL START LIGHT OFF TEMPERATURES.   REPLACED FCU.						1	G	7	2 	3U	3	U	NC	H1NE    	E1GL				 
1999111900104	19991119	00104	NE  	1999	11	19	HEED064644       	1	19991108	G	2120	2515	GASPER          			SKRSKY	S76   	S76C        	8143008	NE  										CABIN	BROKEN          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				VALVE GATE GUIDE AND GUIDE SPRING MISSING.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
1999121100440	19991211	00440	SW  	1999	12	11	HEED064995       	1	19991108	G	3340	4596	BULB            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	3193E	545  				53276				LAMP BURNT, SCRAPPED.						1	G	7	1 	3U			O	H2SW    					 
1999121100441	19991211	00441	SW  	1999	12	11	HEED065008       	1	19991108	G	6310	230030535101	BEARING         			BELL  	230   	230         	1182149	SW  										M/R TRANSMISSION	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X					23015				ROD END HAD WORN BEARING.  REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999121100442	19991211	00442	SW  	1999	12	11	HEED065009       	1	19991108	G	3242	34219	CARRIER         			BELL  	230   	230         	1182149	SW  										BRAKE	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X					23015				CARRIER LINING WORN.   REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999121100443	19991211	00443	SW  	1999	12	11	HEED065015       	1	19991108	G	6720	230312001101	LINK            			BELL  	230   	230         	1182149	SW  										TAIL ROTOR	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X					23015				TAIL ROTOR LINK HAD WORN BEARINGS.  REPLACED PART.						1	G	7	2 	3U			NC	H9SW    					 
1999121100164	19991211	00164	NE  	1999	12	11	HEED065031       	1	19991108	G	6230	SB52001	BEARING         			SKRSKY	S76   	S76C        	8143008	NE  										SWASHPLATE	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				BEARING WORN.  REPLACED PART.						1	G	7	2 	3U			NC	H1NE    					 
1999121100165	19991211	00165		1999	12	11	HEED065036       	4	19991108	G	3416	066303100	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										COCKPIT	READS HIGH      	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				INDICATORS HIGH, REPLACED PART.						1	G	7	2 	3U			NC	H1NE    					 
1999121100166	19991211	00166	NE  	1999	12	11	HEED065039       	1	19991108	G	7933	7645001078126	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										ENGINE OIL TEMP	FLUCTUATING     	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				TEMPERATURE NEEDLE FLUCTUATES RAPIDLY (BLUFFY) FOR A FEW SECOND 3-5 TIMES PER MINUTE R.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
1999121100167	19991211	00167		1999	12	11	HEED065040       	4	19991108	G	2213	775330200	CONTROLLER      			SKRSKY	S76   	S76C        	8143008	NE  										AFCS	FAILED          	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	89H					760406				WOULD NOT UPDATE/INDICATED LOW BATTERY.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
1999121100168	19991211	00168	NE  	1999	12	11	HEED065041       	1	19991108	G	2160	7650007903102	VALVE           			SKRSKY	S76   	S76C        	8143008	NE  										BLEED S O V	FAILED          	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	89H					760406				BLEED AIR VALVE WILL NOT CLOSE COMPLETELY.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
1999121100169	19991211	00169		1999	12	11	HEED065042       	4	19991108	G	3457	8144002241B	GPS             			SKRSKY	S76   	S76C        	8143008	NE  										COCKPIT	FAILED          	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	89H					760406				EVERY LIGHT FLASHED, UNIT WENT OFF CAME BACK ON WITH NO MEMORY.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
1999121100170	19991211	00170	NE  	1999	12	11	HEED065044       	1	19991108	G	2120	2515	GASPER          			SKRSKY	S76   	S76C        	8143008	NE  										CABIN	DAMAGED         	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	476X					760436				VALVE GATE GUIDE AND GUIDE SPRING MISSING.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200596	20000212	00596	NE  	2000	2	12	HEED065697       	2	19991214	G	7421	9550166670	IGNITER         			SKRSKY	S76   	S76C        	8143008	NE  	TMECA 	ARRIEL	ARRIEL1S1   	60030	NE  					IGNITION SYS	CRACKED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406	15537			IGNITER HAS CRACKED AND ERODED INSULATOR .						1	G	7	2 	3U	3	U	NC	H1NE    	E19EU				 
2000021200597	20000212	00597	NE  	2000	2	12	HEED065698       	1	19991214	G	7330	7645001078103	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										COCKPIT	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	533  				760493				NR 2 NEEDLE WENT TO ZERO ON FUEL QUANTITY CONTROL.						1	G	7	2 	3U			NC	H1NE    					 
2000021200598	20000212	00598	NE  	2000	2	12	HEED065699       	1	19991214	G	7921	9560156750	BLOWER          			SKRSKY	S76   	S76C        	8143008	NE  										OIL COOLER	LEAKING         	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	476X					760436				OIL COOLER BLOWER IS LEAKING.						1	G	7	2 	3U			NC	H1NE    					 
2000021200599	20000212	00599	NE  	2000	2	12	HEED065700       	1	19991214	G	3246	50075551	WHEEL           			SKRSKY	S76   	S76C        	8143008	NE  										NLG	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				NOSE WHEEL WORN BEYOND LIMITS.						1	G	7	2 	3U			NC	H1NE    					 
2000021200600	20000212	00600	NE  	2000	2	12	HEED065701       	1	19991214	G	7722	9550158500	THERMOCOUPLE    			SKRSKY	S76   	S76C        	8143008	NE  										ENGINE	FAILED          	E			HEED	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03	89H					760406				THERMOCOUPLE DOES NOT MEET MINIMUM RESISTANCE VALUE OF 5.5 OHMS PLUS OR MINUS 1.5 OHMS.						1	G	7	2 	3U			NC	H1NE    					 
2000021200601	20000212	00601	NE  	2000	2	12	HEED065702       	1	19991214	G	2910	0401272610	TUBE            			SKRSKY	S76   	S76C        	8143008	NE  										HYD SYSTEM	CRACKED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				THE TUBE CRACKS AT THE SMALL WELDS SECURING AN ADEL CLAMP TO THE TUBE.						1	G	7	2 	3U			NC	H1NE    					 
2000021200602	20000212	00602		2000	2	12	HEED065703       	4	19991214	G	3425	1113025	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										HSI	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				HSI INDICATOR CANNOT CHANGE COURSE WITH KNOB.						1	G	7	2 	3U			NC	H1NE    					 
2000021200603	20000212	00603	NE  	2000	2	12	HEED065706       	2	19991214	G	7421	9550166670	IGNITER         			SKRSKY	S76   	S76C        	8143008	NE  	TMECA 	ARRIEL	ARRIEL1S1   	60030	NE  					ENGINE	CRACKED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406	15535TEC			IGNITER - TIP EROSION ON S/N 3830 AND INSULATOR CRACKED ON S/N 3769.						1	G	7	2 	3U	3	U	NC	H1NE    	E19EU				 
2000021200661	20000212	00661		2000	2	12	HEED065707       	4	19991214	G	3422	206075606107	GYRO            			BELL  	407   	407         		SW  										COCKPIT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	579  				53276				FLAG DOES NOT RETRACT ON DIRECTIONAL GYRO.						1	G	7	1 	3U			O	H2SW    					 
2000021200662	20000212	00662	SW  	2000	2	12	HEED065708       	1	19991214	G	6310	204040760109	FILTER          			BELL  	407   	407         		SW  	ALLSN 	250C  	250C47B     		GL  					TRANSMISSION	DAMAGED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	292  				53276	CAE847293			TRANSMISSION OIL FILTER ELEMENT, O-RINGS P/N M832481-024.						1	G	7	1 	3U	3	U	O	H2SW    	E1GL				 
2000021200663	20000212	00663	SW  	2000	2	12	HEED065709       	1	19991214	G	6300	406012129101	LINK ASSY       			BELL  	407   	407         		SW  										MAIN ROTOR	WORN            	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3193E	566  				53276				BEARING WORN AND LEAKING GREASE.						1	G	7	1 	3U			O	H2SW    					 
2000021200664	20000212	00664	SW  	2000	2	12	HEED065710       	1	19991214	G	6520	406040453101	SEAL            			BELL  	407   	407         		SW  										T/R GEARBOX	LEAKING         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	599  				53276				SEAL LEAKING AT TAIL ROTOR GEARBOX.						1	G	7	1 	3U			O	H2SW    					 
2000021200665	20000212	00665	SW  	2000	2	12	HEED065711       	1	19991214	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	55   				53276				LAMP BURNED OUT.						1	G	7	1 	3U			O	H2SW    					 
2000021200666	20000212	00666	SW  	2000	2	12	HEED065713       	1	19991214	G	6300	406340102101	CARBON SEAL     			BELL  	407   	407         		SW  										M/R DRIVE	LEAKING         	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3193E	455  				53276				FORWARD FRONT SEAL LEAKING.						1	G	7	1 	3U			O	H2SW    					 
2000021200667	20000212	00667	SW  	2000	2	12	HEED065714       	1	19991214	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	43   				53276				LAMP BURNT.						1	G	7	1 	3U			O	H2SW    					 
2000021200668	20000212	00668	SW  	2000	2	12	HEED065715       	1	19991214	G	3340	A469B	STROBE          			BELL  	407   	407         		SW  										FUSELAGE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	151  				53276				STROBE LIGHT BURNT.						1	G	7	1 	3U			O	H2SW    					 
2000021200669	20000212	00669	SW  	2000	2	12	HEED065716       	1	19991214	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	46   				53276				LAMP BURNT.						1	G	7	1 	3U			O	H2SW    					 
2000021200670	20000212	00670	SW  	2000	2	12	HEED065717       	1	19991214	G	6520	222312753103	BEARING         			BELL  	230   	230         	1182149	SW  										T/R GEARBOX	CRACKED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X					23015				BEARING CRACKED.						1	G	7	2 	3U			NC	H9SW    					 
2000021200671	20000212	00671	SW  	2000	2	12	HEED065718       	1	19991214	G	3244	028630	TIRE            			BELL  	230   	230         	1182149	SW  										LT MLG	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	615  				23015				TIRE HAS WORN TREAD, LEFT HAND.						1	G	7	2 	3U			NC	H9SW    					 
2000021200672	20000212	00672	SW  	2000	2	12	HEED065720       	1	19991214	G	2430	200SGL1009	BRUSH           			BELL  	230   	230         	1182149	SW  										GENERATOR	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	500  				23015				GENERATOR HAD WORN BRUSHES.						1	G	7	2 	3U			NC	H9SW    					 
2000021200673	20000212	00673	SW  	2000	2	12	HEED065723       	1	19991214	G	3244	50056TT	TIRE            			BELL  	230   	230         	1182149	SW  										MLG	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	1106 				23015				TIRE HAS WORN TREAD.						1	G	7	2 	3U			NC	H9SW    					 
2000021200674	20000212	00674	SW  	2000	2	12	HEED065724       	1	19991214	G	6220	222310503101	PAD BEARING     			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	SEPARATED       	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	968  				23015				ELASTOMERIC SEPARATION ON AFT PAD.						1	G	7	2 	3U			NC	H9SW    					 
2000021200675	20000212	00675	SW  	2000	2	12	HEED065725       	1	19991214	G	6400	222012711107	LINK ASSY       			BELL  	230   	230         	1182149	SW  										T/R COUNTERWT	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	510  				23015				LINK ASSY HAS WORN BEARINGS.						1	G	7	2 	3U			NC	H9SW    					 
2000021200676	20000212	00676		2000	2	12	HEED065726       	4	19991214	G	3425	066308100	HSI             			BELL  	230   	230         	1182149	SW  										COCKPIT	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4255 				23015				CDI SHOWS NO DEVIATION.						1	G	7	2 	3U			NC	H9SW    					 
2000021200677	20000212	00677	SW  	2000	2	12	HEED065731       	1	19991215	G	6400	222001736005	BELLCRANK ASSY  			BELL  	230   	230         	1182149	SW  										T/R CONTROL	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	1342 				23015				BELLCRANK ASSY HAS WORN BEARING.  REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
2000021200678	20000212	00678	SW  	2000	2	12	HEED065732       	1	19991215	G	3244	028630	TIRE            			BELL  	230   	230         	1182149	SW  										RT MLG	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	788  				23015				RIGHT TIRE HAS WORN TREAD.  REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
2000021200679	20000212	00679	SW  	2000	2	12	HEED065733       	1	19991215	G	8011	SM20ACD300A21	RELAY           			BELL  	407   	407         		SW  										STARTER	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	658  				53276				STARTER LIGHT INTERMITTENTLY WILL NOT COME ON DURING START SEQUENCE.  REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200680	20000212	00680	SW  	2000	2	12	HEED065734       	1	19991215	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	55   				53276				LAMP BURNT OUT.  REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200681	20000212	00681	NE  	2000	2	12	HEED065736       	1	19991215	G	3246	50075542	WHEEL           			SKRSKY	S76   	S76C        	8143008	NE  										MLG	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X	145  				760436				WHEEL ASSY WORN.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200682	20000212	00682	NE  	2000	2	12	HEED065737       	2	19991215	G	7421	955016670	IGNITER         			SKRSKY	S76   	S76C        	8143008	NE  	TMECA 	ARRIEL	ARRIEL1S1   	60030	NE  					ENGINE	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				IGNITER HAS WORN TIP.  REPLACED UNIT.						1	G	7	2 	3U	3	U	NC	H1NE    	E19EU				 
2000021200683	20000212	00683		2000	2	12	HEED065738       	4	19991215	G	2220	7040002200108	ACTUATOR        			SKRSKY	S76   	S76C        	8143008	NE  										PBA LINEAR	INTERMITTENT    	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	276X	962  				760405				ACTUATOR WORKS INTERMITTENLY AND STICKS.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200684	20000212	00684	NE  	2000	2	12	HEED065739       	1	19991215	G	2824	7630707901102	VALVE ASSY      			SKRSKY	S76   	S76C        	8143008	NE  										FUEL SYSTEM	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X	669  				760436				VALVE ASSY WILL NOT ALLOW PRIME TO OPERATE.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200604	20000212	00604		2000	2	12	HEED065740       	4	19991215	G	3457	MRAC50S	CONNECTOR       			SKRSKY	S76   	S76C        	8143008	NE  										GPS	CRACKED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H	119  				760406				TRIMBLE GPS T-BAR RELAY CONNECTOR IS CRACKED.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200605	20000212	00605	NE  	2000	2	12	HEED065744       	1	19991216	G	3212	7625101102102	FLOAT BAG       			SKRSKY	S76   	S76C        	8143008	NE  										MLG	DAMAGED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X	1768 				760436				DURING 12 MONTH INSPECTION, FOUND 2 SMALL PIN HOLES WHICH CAUSED BAG TO LEAK. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200606	20000212	00606	NE  	2000	2	12	HEED065745       	1	19991216	G	3212	7625101102105	ELBOW           			SKRSKY	S76   	S76C        	8143008	NE  										FLOATBAG	DETERIORATED    	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				BOTH INFLATION ELBOWS RUBBER REINFORCEMENT RINGS ARE DETERIORATED.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200607	20000212	00607		2000	2	12	HEED065746       	4	19991216	G	3416	5035P2P25	ENCODER         			SKRSKY	S76   	S76C        	8143008	NE  										COCKPIT	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	611  				760493				ENCODING ALT. SENDS 020 ERROR CODE TO SKYWATCH IND DURING FLIGHT INTERMITTENTLY.   SKY WATCH SYSTEM CYCLES OFF AND ON, 0	20 ERROR IS BAROMETRIC ALTITUDE INPUT. REPLACED UNIT.					1	G	7	2 	3U			NC	H1NE    					 
2000021200608	20000212	00608		2000	2	12	HEED065747       	4	19991216	G	2215	7690001802106	ACTUATOR        			SKRSKY	S76   	S76C        	8143008	NE  										AFCS	CHATTERED       	E			HEED	O				OTHER                   				O			OTHER                     			NR	NOT REPORTED   	1			SW	03	89H	406  				760406				NR 1 ROLL CHANNEL CHATTERS WHEN ENGAGED.  ACTUATOR ATTEMPTS UNCOMMANDED EXTEND AND RETRACT OPERATIONS.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200609	20000212	00609	NE  	2000	2	12	HEED065748       	1	19991216	G	3340	7655002005102	SEARCH LIGHT    			SKRSKY	S76   	S76C        	8143008	NE  										FUSELAGE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				SEARCH LIGHT ASSY WILL NOT PIVOT TO THE STOW POSITION.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200610	20000212	00610	NE  	2000	2	12	HEED065749       	1	19991216	G	6210	7610208500045	SPINDLE         			SKRSKY	S76   	S76C        	8143008	NE  										M/R BLADE	DELAMINATED     	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H	3434 				760406				RED SPINDLE MAIN ROTOR BLADE RETENTION (PIVOT) BEARING HAS ELASTOMERIC DELAMINATION.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200611	20000212	00611	NE  	2000	2	12	HEED065750       	1	19991216	G	6310	7636104008103	COUPLING        			SKRSKY	S76   	S76C        	8143008	NE  										NR 2 ENGINE	CORRODED        	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				NR 2 ENGINE MAIN DRIVE SHAFT FORWARD COUPLING HAS SURFACE CORROSION PITTING BETWEEN DISC SEGMENTS.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200612	20000212	00612	NE  	2000	2	12	HEED065751       	1	19991216	G	3340	6032745	LIGHT           			SKRSKY	S76   	S76C        	8143008	NE  										ANTI-COLLISION	INOPERATIVE     	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				UNIT HAS NO POWER OUTPUT TO ILLUMINATE THE ANTI-COLLISION LIGHT LAMP.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200613	20000212	00613		2000	2	12	HEED065752       	4	19991216	G	2215	7690001802106	ACTUATOR        			SKRSKY	S76   	S76C        	8143008	NE  										AFCS	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				NR 1  YAW AFCS ACTUATOR WILL NOT EXTEND.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200614	20000212	00614	NE  	2000	2	12	HEED065753       	1	19991216	G	3246	50075551	WHEEL           			SKRSKY	S76   	S76C        	8143008	NE  										NLG	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				NOSE WHEEL WORN BEYOND LIMITS.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200685	20000212	00685	SW  	2000	2	12	HEED065754       	1	19991216	G	6220	222310504101	BEARING PAD     			BELL  	230   	230         	1182149	SW  										MAIN ROTOR	SEPARATED       	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X					23015				BEARING PAD SEPARATED.  REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
2000021200686	20000212	00686	SW  	2000	2	12	HEED065756       	1	19991216	G	2510	222320823123	RESTRAINT       			BELL  	230   	230         	1182149	SW  										COCKPIT	FRAYED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4527 				23015				SHOULDER HARNESS FRAYED.  REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
2000021200687	20000212	00687	SW  	2000	2	12	HEED065757       	1	19991217	G	6420	222012738001	LOCK RING       			BELL  	230   	230         	1182149	SW  										TAIL ROTOR	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4348 				23015				LOCK RING WORN. REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
2000021200688	20000212	00688	SW  	2000	2	12	HEED065762       	1	19991217	G	6410	222012702119	BEARING         			BELL  	230   	230         	1182149	SW  										T/R BLADE	CRACKED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	1485 				23015				CRACKED T/R FEATHER BEARING AND PLAY IN TRUNNION BEARING. REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
2000021200689	20000212	00689	SW  	2000	2	12	HEED065763       	1	19991217	G	6720	230312001101	LINK            			BELL  	230   	230         	1182149	SW  										TAIL ROTOR	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X					23015				WORN BEARINGS. REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
2000021200690	20000212	00690	SW  	2000	2	12	HEED065764       	1	19991217	G	3212	212073905001	GAUGE           			BELL  	407   	407         		SW  										FLOAT PRESSURE	STICKING        	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	865  				53276				NEEDLE STICKS RUSTY INSIDE. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200615	20000212	00615	SW  	2000	2	12	HEED065765       	1	19991217	G	7920	6871937	TUBE            			BELL  	407   	407         		SW  										ENGINE OIL	LEAKING         	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3193E	442  				53276				TUBE WEEPS OIL AROUND LARGER B-NUT. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200691	20000212	00691	SW  	2000	2	12	HEED065766       	1	19991217	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	78   				53276				LAMP BURNT OUT.  REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200692	20000212	00692	SW  	2000	2	12	HEED065767       	1	19991217	G	7700	407375016103	SIGNAL COND     			BELL  	407   	407         		SW  										ENGINE	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	645  				53276				LOW LEVEL LIGHT STAYS ON. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200693	20000212	00693		2000	2	12	HEED065769       	4	19991217	G	2312	064105430	TRANSCEIVER     			BELL  	407   	407         		SW  										COCKPIT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	596  				53276				TRANSCEIVER DOES NOT RECEIVE ON FREQ. 129.10. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200694	20000212	00694	NE  	2000	2	12	HEED065770       	2	19991217	G	7323	6854424	SHAFT SEAL      			BELL  	407   	407         		SW  	TMECA 	ARRIEL	ARRIEL1S1   	60030	NE  					ENGINE	LEAKING         	E			HEED	K				NONE                    				K			FLUID LOSS                			IN	INSP/MAINT     	1			SW	03	3193E	507  				53276				SHAFT SEAL LEAKING. REPLACED UNIT.						1	G	7	1 	3U	3	U	O	H2SW    	E19EU				 
2000021200695	20000212	00695	SW  	2000	2	12	HEED065771       	1	19991217	G	5320	900094	STEP            			BELL  	407   	407         		SW  										FUSELAGE	CORRODED        	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	590  				53276				RUST/PAINT PEELING. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200696	20000212	00696	SW  	2000	2	12	HEED065773       	1	19991217	G	3000	96487	SOLNOID         			BELL  	407   	407         		SW  										ANTI-ICE SYSTEM	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	477  				53276				ANTI-ICE INDICATOR. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200616	20000212	00616		2000	2	12	HEED065774       	4	19991217	G	2215	7690001802106	ACTUATOR        			SKRSKY	S76   	S76C        	8143008	NE  										AFCS	KICKING         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	946  				760493				ACTUATOR KICKS. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200617	20000212	00617		2000	2	12	HEED065775       	4	19991217	G	2215	7690001802106	ACTUATOR        			SKRSKY	S76   	S76C        	8143008	NE  										AFCS	KICKING         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	961  				760493				ACTUATOR KICKS. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200618	20000212	00618	NE  	2000	2	12	HEED065776       	1	19991217	G	7331	12281301	FLOW METER      			SKRSKY	S76   	S76C        	8143008	NE  										FUEL FLOW	READS HIGH      	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				FLOW METER GIVES HIGH READING. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200619	20000212	00619		2000	2	12	HEED065777       	4	19991217	G	2215	7690001802106	ACTUATOR        			SKRSKY	S76   	S76C        	8143008	NE  										AFCS	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				ACTUATOR WILL NOT EXTEND, TRIPS CIRCUIT BREAKER. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200620	20000212	00620		2000	2	12	HEED065778       	4	19991217	G	2210	7611113	AMPLIFIER       			SKRSKY	S76   	S76C        	8143008	NE  										YAW SLICE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				AMPLIFIER TRIPS CIRCUIT BROKEN. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200621	20000212	00621	NE  	2000	2	12	HEED065779       	1	19991217	G	7714	764500195101	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										N1	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	934  				760493				DIGITAL LIGHTS. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200622	20000212	00622	NE  	2000	2	12	HEED065780       	1	19991217	G	3246	50075542	WHEEL           			SKRSKY	S76   	S76C        	8143008	NE  										MLG	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X	341  				760436				WHEEL WORN.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200623	20000212	00623	NE  	2000	2	12	HEED065782       	1	19991217	G	6510	FN100	FAN             			SKRSKY	S76   	S76C        	8143008	NE  										TAIL ROTOR	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	278X					760440				FAN WILL NOT RUN . REMOVED FROM STOCK WILL NOT TURN. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200624	20000212	00624	NE  	2000	2	12	HEED065783       	1	19991217	G	2550	PHISK76205	CARGO NET       			SKRSKY	S76   	S76C        	8143008	NE  										CARGO BAY	FRAYED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				CARGO NET HAD FRAYED WEBBING. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200697	20000212	00697	SW  	2000	2	12	HEED065785       	1	19991217	G	6510	S7052EC1	BLOWER          			BELL  	407   	407         	1182206	SW  										TAIL ROTOR	SHORTED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	817  				53276				BLOWER HAD INTERNAL SHORT. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200698	20000212	00698	SW  	2000	2	12	HEED065786       	1	19991217	G	3212	212073905001	GAUGE           			BELL  	407   	407         		SW  										FLOAT PRESSURE	STICKING        	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	865  				53276				GAUGE NEEDLE STICKS-RUSTY INSIDE. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200699	20000212	00699		2000	2	12	HEED065787       	2	19991217	G	7510	23007827	VALVE           			BELL  	407   	407         		SW  										ANTI-ICE SYSTEM	STUCK           	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	821  				53276				SOLENIOD STUCK IN CLOSED POSITION.  REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200700	20000212	00700	SW  	2000	2	12	HEED065789       	1	19991217	G	5210	407070620137	SKIN            			BELL  	407   	407         		SW  										CREW DOOR	CRACKED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	706  				53276				SKIN CRACKED ON CREW DOOR. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200701	20000212	00701	SW  	2000	2	12	HEED065790       	1	19991217	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	87   				53276				LAMP BURNT OUT. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200702	20000212	00702	SW  	2000	2	12	HEED065791       	1	19991217	G	2822	407362013101	SWITCH          			BELL  	407   	407         		SW  										FUEL PRESSURE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	719  				53276				MUST CYCLE BOOST PUMP SWITCH SEVERAL TIMES TO GET CAUTION LIGHT WHEN BOOST PUMP (RIGHT) IS TURNED OFF. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200703	20000212	00703	SW  	2000	2	12	HEED065792       	1	19991217	G	7700	407375016103	SIGNAL COND     			BELL  	407   	407         		SW  										ENGINE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	761  				53276				LOW LEVEL LIGHT WILL NOT TURN OFF. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200704	20000212	00704	SW  	2000	2	12	HEED065793       	1	19991217	G	7110	407064806141	SCREEN          			BELL  	407   	407         		SW  										ENGINE COWL	CRACKED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	644  				53276				SCREEN CRACKED. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200625	20000212	00625	NE  	2000	2	12	HEED065794       	1	19991217	G	5210	7620710009226	PANEL           			SKRSKY	S76   	S76C        	8143008	NE  										PAX DOOR	CRACKED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X					760493				COVER PANEL FOR RIGHT HAND PASSENGER'S DOOR VENT CONTROL CRACKS AND MOUNT HOLES AND CORNER BROKEN OFF. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200626	20000212	00626	NE  	2000	2	12	HEED065795       	2	19991217	G	7421	9550164470	IGNITER         			SKRSKY	S76   	S76C        	8143008	NE  	TMECA 	ARRIEL	ARRIEL1S1   	60030	NE  					ENGINE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X	514  				760436				IGNITER WILL NOT OPERATE. REPLACED UNIT.						1	G	7	2 	3U	3	U	NC	H1NE    	E19EU				 
2000021200627	20000212	00627		2000	2	12	HEED065796       	4	19991217	G	3425	1418523200	AHARS UNIT      			SKRSKY	S76   	S76C        	8143008	NE  										E/E BAY	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				ATTITUDE INDICATOR RT AND ATT. FLAGS WILL NOT PULL RMI FLAG WILL NOT PULL. GREEN NEEDLE WILL NOT POINT TO THE GPS WAYPOI	NT HEADING SELECTED.  GPS GIVES HEADING DATA INVALID MESSAGE. REPLACED UNIT.					1	G	7	2 	3U			NC	H1NE    					 
2000021200628	20000212	00628	NE  	2000	2	12	HEED065797       	1	19991217	G	3246	50075551	WHEEL           			SKRSKY	S76   	S76C        	8143008	NE  										NLG	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X					760493				WHEEL WORN. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200705	20000212	00705	SW  	2000	2	12	HEED065798       	1	19991217	G	2622	112111997	FIRE EXTINGUISH 			BELL  	230   	230         	1182149	SW  										CABIN	DISCHARGED      	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	236X	4527 				23015				FIRE EXTINGUISHER GAUGE INDICATES LOW CHARGE.  REPLACED UNIT.						1	G	7	2 	3U			NC	H9SW    					 
2000021200706	20000212	00706		2000	2	12	HEED065800       	4	19991217	G	3421	5040045904	GYRO            			BELL  	407   	407         		SW  										COCKPIT	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	644  				53276				GYRO WILL NOT CAGE. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200707	20000212	00707	SW  	2000	2	12	HEED065801       	1	19991217	G	3340	4596	LAMP            			BELL  	407   	407         		SW  										LANDING LIGHT	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	65   				53276				LAMP BURNED OUT. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200629	20000212	00629		2000	2	12	HEED065802       	4	19991220	G	3416	80510800001	ENCODER         																	COCKPIT	FAILED          	E			HEED	K				NONE                    				L			NO TEST                   			IN	INSP/MAINT     	1			SW	03		13   								ENCODER BAD FROM STOCK. WHEN INSTALLED IN AIRCRAFT N476X, UNIT WENT THROUGH THE CALIBRATION MODE OK BUT FAILED THE TEST 	MODE WITH AN ERROR CONFIGURATION OF NR 30. WHEN INSTALLED, AIRCRAFT N89H, THE CALIBRATION MODE CHECKED OK, BUT THE TEST 	MODE SHOWED ERROR CONFIGURATION NR 18 AND NR 30. REPLACED UNIT.																	 
2000021200630	20000212	00630		2000	2	12	HEED065803       	4	19991221	G	2210	7611113	AMPLIFIER       			SKRSKY	S76   	S76C        	8143008	NE  										YAW SLICE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				AMPLIFIER TRIPS CIRCUIT BREAKER. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200631	20000212	00631		2000	2	12	HEED065804       	1	19991221	G	2160	7650007903102	VALVE           																	BLEED SOV	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03										VALVE REMOVED FROM STOCK BAD. REPLACED UNIT.																			 
2000021200632	20000212	00632		2000	2	12	HEED065805       	4	19991221	G	2215	7690001802106	ACTUATOR        			SKRSKY	S76   	S76C        	8143008	NE  										AFCS	INOPERATIVE     	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X	496  				760436				ACTUATOR WILL NOT EXTEND, INOPERATIVE, TRIPS CIRCUIT BREAKER. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200633	20000212	00633	NE  	2000	2	12	HEED065806       	1	19991221	G	7331	12281301	FLOW METER      			SKRSKY	S76   	S76C        	8143008	NE  										FUEL FLOW	READS HIGH      	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				GIVES HIGH READINGS. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200634	20000212	00634		2000	2	12	HEED065807       	4	19991221	G	3457	8144002241B	GPS             			SKRSKY	S76   	S76C        	8143008	NE  										COCKPIT	INACCURATE      	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X	550  				760436				TRIMBLE HEADING READS 20 DEGREES OFF FROM BOTH HIS CDI NEEDLES HEADINGS. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200635	20000212	00635	NE  	2000	2	12	HEED065808       	1	19991221	G	2510	5042364012251	SEAT BELT       			SKRSKY	S76   	S76C        	8143008	NE  										COCKPIT	FRAYED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				WEBBING (STRAPS) SWOLLEN AND FRAYED ON EDGES, DIRTY AND NOT TSO TAGS. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200636	20000212	00636		2000	2	12	HEED065809       	4	19991221	G	2300	VFS1090	ANTENNA         			SKRSKY	S76   	S76C        	8143008	NE  										FUSELAGE	CRACKED         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				LEADING EDGE IS CRACKED. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200637	20000212	00637	NE  	2000	2	12	HEED065810       	2	19991221	G	7421	9550164470	IGNITER         			SKRSKY	S76   	S76C        	8143008	NE  	TMECA 	ARRIEL	ARRIEL1S1   	60030	NE  					ENGINE	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				IGNITER WILLNOT OPERATE. REPLACED UNIT.						1	G	7	2 	3U	3	U	NC	H1NE    	E19EU				 
2000021200638	20000212	00638	NE  	2000	2	12	HEED065811       	1	19991221	G	6510	JBS20241	BLADE           			SKRSKY	S76   	S76C        	8143008	NE  										BLOWER FAN	BROKEN          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				BLADE BROKEN OFF.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200639	20000212	00639	NE  	2000	2	12	HEED065812       	2	19991221	G	7412	9580113800	H.E. GENERATOR  			SKRSKY	S76   	S76C        	8143008	NE  	TMECA 	ARRIEL	ARRIEL1S1   	60030	NE  					ENGINE IGNITER	INOPERATIVE     	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	276X					760405				H.E. UNIT INOPERATIVE. REPLACED UNIT.						1	G	7	2 	3U	3	U	NC	H1NE    	E19EU				 
2000021200640	20000212	00640		2000	2	12	HEED065813       	4	19991221	G	2215	7690001802106	ACTUATOR        			SKRSKY	S76   	S76C        	8143008	NE  										AFCS	INOPERATIVE     	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	162  				760493				ACTUATOR INOPERATIVE. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200641	20000212	00641	NE  	2000	2	12	HEED065815       	1	19991221	G	7931	7645001078119	TRANSMITTER     			SKRSKY	S76   	S76C        	8143008	NE  										OIL PRESSURE	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	476X					760436				OIL PRESSURE NEEDLE FLUCTUATES 10 PSI DURING FLIGHT.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200642	20000212	00642	NE  	2000	2	12	HEED065816       	1	19991221	G	7714	04011277660	INDICATOR       			SKRSKY	S76   	S76C        	8143008	NE  										N1	READS HIGH      	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				T2 PORTION MAKES THE N1 GAUGE READ .6 HIGH DURING TEST.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200643	20000212	00643	NE  	2000	2	12	HEED065817       	1	19991222	G	6210	7615009043054	TIP CAP         			SKRSKY	S76   	S76C        	8143008	NE  										M/R BLADE	DISBONDED       	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				RETENTION DOUBLER STRIPS UNBONDED. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200644	20000212	00644	NE  	2000	2	12	HEED065818       	1	19991222	G	6210	7615009043054	TIP CAP         			SKRSKY	S76   	S76C        	8143008	NE  										M/R BLADE	DISBONDED       	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				RETENTION DOUBLER STRIPS UNBONDED. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200708	20000212	00708		2000	2	12	HEED065819       	2	19991222	G	7510	23007827	VALVE ASSY      			BELL  	407   	407         		SW  										ANTI-ICE SYSTEM	STICKING        	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	3193E	877  				53276				STICKING CAUSES LIGHT TO REMAIN ILLUMINATED. REPLACED UNIT.						1	G	7	1 	3U			O	H2SW    					 
2000021200645	20000212	00645	NE  	2000	2	12	HEED065824       	1	19991222	G	3240	50075551	LINING          			SKRSKY	S76   	S76C        	8143008	NE  										MLG BRAKE	WORN            	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X					760493				WORN BRAKE LINNING.  REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200646	20000212	00646	NE  	2000	2	12	HEED065825       	1	19991222	G	6730	7826002	SERVO           			SKRSKY	S76   	S76C        	8143008	NE  										TAIL ROTOR	LEAKING         	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	478X	885  				760493				SERVO LEAKING. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200647	20000212	00647	NE  	2000	2	12	HEED065826       	2	19991222	G	7200	1S1	ENGINE          			SKRSKY	S76   	S76C        	8143008	NE  	TMECA 	ARRIEL	ARRIEL1S1   	60030	NE  					TURBINE SECTION	CHAFED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H	337  				760406				TURBINE SECTION RUBBING EXCESSIVELY INSIDE. REPLACED UNIT.						1	G	7	2 	3U	3	U	NC	H1NE    	E19EU				 
2000021200648	20000212	00648		2000	2	12	HEED065828       	4	19991222	G	3454	066107800	RECEIVER        			SKRSKY	S76   	S76C        	8143008	NE  										VHF NAV	FAILED          	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H	611  				760406				RECEIVER WILL NOT POWER UP, FIND STATION OR GIVE HEADING INFORMATION. REPLACED UNIT.						1	G	7	2 	3U			NC	H1NE    					 
2000021200649	20000212	00649		2000	2	12	HEED065829       	4	19991222	G	3425	1418523200	AHARS UNIT      			SKRSKY	S76   	S76C        	8143008	NE  										E/E BAY	MALFUNCTIONED   	E			HEED	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			SW	03	89H					760406				AHRS CAUTION LIGHT REMAINS ILLUMINATED, ATT AND RT FLAGS FAIL TO PULL AND GPS HEADING INFORMATION INVALID APPEARS AFTER 	25 - 30 MINUTES.  REPLACED UNIT.					1	G	7	2 	3U			NC	H1NE    					 
1999102900777	19991029	00777		1999	10	29	LS1R99101        	4	19991007	G	3416	AT3000	ENCODER         			BELL  	206   	206B        	1181511	SW  										COCKPIT	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	9907K				19528	2040				ENCODER WILL NOT CORRELATE WITH ALTIMETER.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U				H2SW    					 
1999102900782	19991029	00782	WP  	1999	10	29	LS1R99102        	1	19990710	G	3610	369H8407	LINE            			HUGHES	369   	369D        	4470706	WP  										HEATER	CRACKED         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	500DC					290456D				NOTICED BLACK SOOT ON CUSTOMER BLEED LINE TO HEATER.  FOUND AIR LEAKING OUT BRAID LINE AREA.  REMOVED AND REPLACED.  FOU	ND MATERIAL CRACKS ON FLEX PART OF LINE.  (X)					1	G	7	1 	3U				H3WE    					 
1999102900778	19991029	00778	SW  	1999	10	29	LS1R99103        	1	19991007	G	6310	206040117003	COUPLING        		206040015103	BELL  	206   	206B        	1181511	SW  										DRIVESHAFT	GOUGED          	B		A	LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	9907K				A17419	2040				FORWARD COUPLING ON MAIN DRIVESHAFT WAS LEAKING GREASE.  UPON TEAR-DOWN INSPECTION, THE SPRING WAS FOUND BROKEN INTO MAN	Y PIECES.  THE SPRING WAS MOVING AROUND IN THE COUPLING WHICH CAUSED GOUGES ON THE CAP AND GEAR.  REPLACED CAP GEAR AND 	SPRING.  RETURNED TO SERVICE.  (X)				1	G	7	1 	3U				H2SW    					 
1999102900784	19991029	00784	WP  	1999	10	29	LS1R99104        	1	19991007	G	2841	369D29630521	INDICATOR       			HUGHES	369   	369D        	4470706	WP  										FUEL QUANTITY	ERRATIC         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	5211R				151	1161D				ENGINE OIL TEMPERATURE ERRATIC.  SOMETIMES HIGH AND SOMETIMES LOW.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U				H3WE    					 
1999102900779	19991029	00779	SW  	1999	10	29	LS1R99105        	1	19991007	G	6240	2060702657	INDICATOR       			BELL  	206   	206B        	1181511	SW  										DUAL TACHOMETER	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	90322				11390	1736				POWER TURBINE INDICATOR NOT READING PROPERLY.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U				H2SW    					 
1999102900785	19991029	00785	SW  	1999	10	29	LS1R99106        	1	19991007	G	7722	12444412	INDICATOR       			BELL  	206   	206B        	1181511	SW  										COCKPIT TOT	ERRATIC         	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	206BX				78K0593C	2872				TOT INDICATOR HAD INTERMITTENT AND ERRATIC NEEDLE MOVEMENT.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U				H2SW    					 
1999102900783	19991029	00783	WP  	1999	10	29	LS1R99107        	1	19991007	G	7330	369H81443	SWITCH          			HUGHES	369   	369D        	4470706	WP  	ALLSN 	250C  	250C20B     	03013	GL  					FUEL BYPASS	FAILED          	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	5211R					1161D	CAE834135			FUEL BYPASS CHECK.  DID NOT MAKE CONTACT UNDER PRESSURE.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U	3	U		H3WE    	E4CE				 
1999102900781	19991029	00781	WP  	1999	10	29	LS1R99108        	1	19991007	G	7933	369D29630521	INDICATOR       			HUGHES	369   	369D        	4470706	WP  										OIL TEMPERATURE	INTERMITTENT    	B			LS1R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			EA	13	5027P				414	611002D				ENGINE OIL TEMPERATURE INDICATOR INTERMITTENTLY JUMPS.  REMOVED AND REPLACED.  (X)						1	G	7	1 	3U				H3WE    					 
2003020500031	20030205	00031	CE  	2003	2	5	MEA200303        	1	19990118	G	5610		WINDSHIELD      			BEECH 	B300  	B300        	1159232	CE  	PWA   	PT6   	PT6A60A     	52043	NE  	HARTZL	HCB4M	HCB4MP3     	GL  	COCKPIT	FAILED          	C				C				ABORTED TAKEOFF         				O			OTHER                     			TO	TAKEOFF        	1			GL	23	593MA	1974 	1974 			FL68				A/C ON TAKEOFF ROLL AT ABOUT 60 KNOTS COPILOTS WINDSHIELD DEVELOPED LARGE CRACK THROUGH THE INNER PANE OF GLASS. TAKEOFF	 WAS ABORTED AND RETURNED TO THE HANGAR. WEATHER AT TIME WAS MID TEENS AND SNOW.					2	L	7	2 	4T	4	T	RT	A24CE   	E4EA	6	C	P56GL	 
1999042300001	19990423	00001	WP  	1999	4	23	NZBL061023       	1	19990316	G	6210	369D21100517	BLADE           			HUGHES	369   	369D        	4470706	WP  										MAIN ROTOR	DELAMINATED     	H			NZBL	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	513SB	784  				1120				THIS MAIN ROTOR BLADE WAS REMOVED FOR DELAMINATED ABRASION STRIP REPLACEMENT AT 396.7 HOURS TT.  SUBSEQUENT FAILURES ON 	THIS SET HAVE CAUSED REJECTION OF THE FULL SET OF BLADES.					1	G	7	1 	3U				H3WE    					 
1999042300002	19990423	00002	WP  	1999	4	23	NZBL061024       	1	19990316	G	6210	369D21100517	BLADE           			HUGHES	369   	369D        	4470706	WP  										MAIN ROTOR	DELAMINATED     	H			NZBL	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	513SB	782  				1120				THIS MAIN ROTOR BLADE WAS REMOVED FOR THE REPLACEMENT OF A DELAMINATED ABRASION STRIP AT 569.4 HOURS TT.  SUBSEQUENT FAI	LURES ON THIS SET HAVE CAUSED REJECTION OF THE FULL SET OF BLADES.					1	G	7	1 	3U				H3WE    					 
1999042300003	19990423	00003	WP  	1999	4	23	NZBL061025       	1	19990316	G	6210	369D21100517	BLADE           			HUGHES	369   	369D        	4470706	WP  										MAIN ROTOR	DELAMINATED     	H			NZBL	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	513SB	847  				1120				THIS MAIN ROTOR BLADE WAS REMOVED FOR DELAMINATED ABRASION STRIP REPLACEMENT AT 664.1 HOURS TT.  THE BLADE WAS NEXT REMO	VED AT 846.9 HOURS TT FOLLOWING ANOTHER ABRASION STRIP DELAMINATION.					1	G	7	1 	3U				H3WE    					 
1999042300004	19990423	00004	WP  	1999	4	23	NZBL061026       	1	19990316	G	6210	369D21100517	BLADE           			HUGHES	369   	369D        	4470706	WP  										MAIN ROTOR	DELAMINATED     	H			NZBL	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	513SB	784  				1120				THIS MAIN ROTOR BLADE WAS REMOVED FOR DELAMINATED ABRASION STRIP REPLACEMENT AT 396.7 HOURS TT.  SUBSEQUENT ABRASION STR	IP DELAMINATIONS ON THIS SET OF BLADES HAVE CAUSED REJECTION OF THE SET.					1	G	7	1 	3U				H3WE    					 
1999042300005	19990423	00005	WP  	1999	4	23	NZBL061027       	1	19990316	G	6210	369D21100517	BLADE           			HUGHES	369   	369D        	4470706	WP  										MAIN ROTOR	DELAMINATED     	H			NZBL	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			AL	05	513SB	877  				1120				THIS MAIN ROTOR BLADE WAS REMOVED FOR DELAMINATED ABRASION STRIP REPLACEMENT AT 664.1 HOURS TT.  SUBSEQUENT DELAMINATION	 ON THIS SET OF BLADES HAVE CAUSED REJECTION OF THE SET.					1	G	7	1 	3U				H3WE    					 
1999031200424	19990312	00424	NE  	1999	3	12	SI3R99003        	2	19990202	G	7210	5074T51G10	WASHER          		GC49        	SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					GEARBOX	BROKEN          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		1034 			IHI00631		GEE785762			DURING DISASSEMBLY, FOUND RIGHT FORWARD IDLER TAB WASHER BROKEN.  BROKEN DAMPER RINGS ALSO.  HSS SO NR 230417 SO.  CUST:	  MESABA A/L.  (X)					2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999031200423	19990312	00423	NE  	1999	3	12	SI3R99004        	2	19990202	G	7210	5074T51G10	WASHER          		GC49        	SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					GEARBOX	BROKEN          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		1545 			IHI00623		GEE785756			DURING DISASSEMBLY, FOUND RIGHT FORWARD IDLER TAB WASHER BROKEN.  BROKEN DAMPER RINGS ALSO.  NOTE:  THE RT AFT, LT AND R	T FWD BEARINGS ALL HAVE MISMATCHED SERIAL NUMBERS ON THE INNER AND OUTER RACES.  HSS SO NR 230418 SO.  CUST:  MESABA A/L	.  (X)				2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999040900319	19990409	00319	NE  	1999	4	9	SI3R99008        	2	19990322	G	7210	7757652	BEARING         		5074T51G10  	SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					GEARBOX	FAILED          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		3542 			TBC00416					DURING DISASSEMBLY OF GEARBOX, SLIDER BLOCK BEARING CAGE AND RIGHT IDLER FORWARD TAB WASHER WERE FOUND BROKEN.  HSS SO N	R 249856 SO.  CUST:  MESABA A/L.  (X)					2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999043000137	19990430	00137	NE  	1999	4	30	SI3R99009        	2	19990301	G	7210	77576752	BEARING         		5074T51G10  	SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					GEARBOX	FAILED          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		1891 			TBC00499		GEE785757			DURING DISASSEMBLY OF GEARBOX, SLIDER BLOCK BEARING AND RIGHT IDLER FORWARD TAB WASHER WERE FOUND BROKEN WHICH CAUSED DA	MAGE TO BULKHEAD.  HSS SO NR 251975 SO.  CUST:  MESABA A/L.  (X)					2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999043000136	19990430	00136	NE  	1999	4	30	SI3R99011        	2	19990301	G	7210	7895781	WASHER          		5074T51G10  	SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					GEARCASE	BROKEN          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		14790			IHI00034		GEE785328			DURING DISASSEMBLY OF GEARCASE, RIGHT IDLER FORWARD TAB WASHER WAS FOUND BROKEN.  OIL PUMP HOUSING HAS SOME DAMAGE.  HSS	 SO NR 251671 SO.  CUST:  SIMMONS A/L.  (X)					2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999100800433	19991008	00433	NE  	1999	10	8	SI3R99019        	2	19990830	G	7260	77577531	HOUSING         	HAMSTD      	6044T35P10  	SAAB  	SF340 	SF340A      	7850100	EU  	GE    	CT7TP 	CT79B       	30030	NE  					GEARBOX	DAMAGED         	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		13584			242		GEE785592			UPON DISASSEMBLY OF GEARBOX, THE FOLLOWING WAS OBSERVED:  ON AFT SIDE OF BULKHEAD AT THE RT IDLER GEAR OPENING, THERE IS	 A 360 DEGREE GROOVE, .078 INCH DEEP BY .200 INCH WIDE, (PN 775775-31, SET NR 242).  RT IDLER FORWARD TAB WASHER (PN 789	578-1) BROKEN.  BEARINGS REJECTED FOR NICKS/PITS TO ROLLER AND RACE SURFACES.  HSS SO NR 325699 SO.  CUST:  KENDELL.  RE	F:  OPER CNTRL NR 99ZZZX3833 THROUGH 99ZZZX3839.   (X)			2	L	7	2 	4T	4	T	RT	A52EU   	E8NE				 
1999102200800	19991022	00800	NE  	1999	10	22	SI3R99020        	2	19991006	G	7210	775652	BEARING         		5074T51G10  	SAAB  	SF340 	340B        	7860101	EU  	GE    	CT7TP 	CT79B       	30030	NE  					GEARBOX	FAILED          	B			SI3R	K				NONE                    				O			OTHER                     			IN	INSP/MAINT     	1			NE	03		13692			IH100150		GEE785272			DURING DISASSEMBLY, THE FOLLOWING DAMAGE WAS NOTED:  BROKEN BEARING CAGE (P/N 775765-2) S/N:  TBC 00044.  HSS SO NR 3281	25 SO CUST:  SIMMONS A/L.  (X)					2	L	7	2 	4T	4	T	RT	A52EU   	E8NE